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ENG-12-000107/31/980109/25/988SERVICING - INTRODUCTION OF ADDITIONAL ALTERNATIVE ENGINE OIL LUBRICANT EXXON 219712-00-00V2500-A1,-A5,-D5
ENG-12-000207/23/998SERVICING - INTRODUCTION OF ADDITIONAL ALTERNATIVE ENGINE LUBRICANT TURBO NYCOIL 60012-00-00V2500-A1,-A5,-D5
ENG-12-000310/01/008SERVICING - INTRODUCTION OF ADDITIONAL ALTERNATIVE ENGINE OIL LUBRICANT MOBIL JET 29112-00-00V2500-A1,-A5,-D5
ENG-12-000410/15/018SERVICING - INTRODUCTION OF ADDITIONAL ALTERNATIVE ENGINE OIL LUBRICANTS - AEROSHELL TURBINE OIL 500, 555, 560 AND CASTROLAERO 500012-00-00V2500-A5,-D5
NAC-24-000103/10/956NACELLE - POWERPLANT - ELECTRICAL POWER - SUPPORT BRACKET, IDG POWER CABLE - REWORK OF24-00-00V2500-A1
ENG-24-000210/11/917ENGINE - HYDRAULICS - PROVIDE A NEW IDG OIL COOLER WITHOUT AN OIL INLET THERMOCOUPLE PORT24-00-00V2500-A1
NAC-24-000306/15/966NACELLE - ELECTRICAL POWER - IDG CABLE BRACKET, MODIFICATION OF24-00-00V2500-A1
ENG-24-000403/16/946ENGINE - ELECTRICAL POWER - IDG OIL COOLING TUBES - MODIFIED SUPPORT BRACKET FOR CLIP POINT 107224-21-49V2500-A1,-A5
ENG-24-000502/10/956ENGINE - ELECTRICAL POWER - PROVIDE A NEW IDG OIL COOLER OIL INLET CONNECTOR SUPPORT BRACKET24-21-49V2500-A1
NAC-24-000603/03/950105/15/953NACELLE - ELECTRICAL POWER - POWER FEEDER HARNESSES, VARIABLE SPEED CONSTANT FREQUENCY (VSCF) - SHIELDING OF24-00-00V2500-D5
NAC-24-000705/15/956NACELLE - ELECTRICAL POWER - TERMINAL LUGS, VSCF POWER FEEDER HARNESSES - REPLACEMENT OF24-00-00V2500-D5
NAC-24-000805/15/953NACELLE - ELECTRICAL POWER - COVER ASSEMBLY, VSCF POWER FEEDER HARNESS - REPLACEMENT OF24-00-00V2500-D5
NAC-24-001001/02/980103/20/976NACELLE - ELECTRICAL POWER - POWER FEEDER HARNESS, VARIABLE SPEED CONSTANT FREQUENCY (VSCF) GENERATOR - GROUND TERMINAL ATTACH BOLT, AND POWER FEEDER HARNESS SUPPORT CLAMPS - REPLACEMENT OF24-00-00V2500-D5
NAC-24-001212/18/950209/20/964NACELLE - ELECTRICAL POWER - VARIABLE SPEED CONSTANT FREQUENCY (VSCF) GENERATOR, REPLACEMENT OF24-00-00V2500-D5
NAC-24-001403/14/035NACELLE - POWER PLANT - IDG COOLING TUBES - "O" RING SEALS - REPLACEMENT OF24-00-00V2500-A1,-A5
NAC-24-001603/16/990211/30/004NACELLE - ELECTRICAL POWER - CONTROL HARNESS, VARIABLE SPEED CONSTANT FREQUENCY (VSCF) GENERATOR - CLIPPING POINT BRACKET - MODIFICATION OF24-00-00V2500-D5
NAC-24-001702/07/034MODIFICATION SERVICE BULLETIN - NACELLE - POWERPLANT - REPLACE AND INCREASE TORQUE OF QAD ATTACHMENT SCREWS24-21-44V2500-D5
ENG-24-001909/24/040208/12/058ELECTRICAL POWER - VARIABLE SPEED CONSTANT FREQUENCY GENERATOR OIL COOLER - INTRODUCTION OF REVISED VARIABLE SPEED CONSTANT FREQUENCY (VSCF) GENERATOR COOLING TUBES24-21-47V2500-D5
NAC-24-002004/14/050210/29/076NACELLE - POWERPLANT - ENGINE BUILD UNIT (EBU) - REPLACEMENT OF THE IDG EARTH STUD BRACKET24-21-43V2500-A1,-A5
NAC-24-002103/08/217ELECTRICAL POWER - QUICK-ATTACH - DETACH (QAD) ADAPTER KIT - INTRODUCTION OF A NEW QAD ADAPTER KIT WITH NEO ENGINE MARKINGS24-21-41V2500-A1,-A5
NAC-26-000209/14/047NACELLE - POWERPLANT - FIRE PROTECTION - OVERHEAT DETECTOR - REPLACEMENT OF26-00-00V2500-A1
NAC-26-000404/08/944NACELLE - POWERPLANT - FIRE PROTECTION - CORE ZONE FIRE DETECTOR - CLIPPING POINT - DELETION OF26-00-00V2500-A1,-A5
NAC-26-000510/27/950204/09/037NACELLE - FIRE PROTECTION - FIRE DETECTOR ASSEMBLY - REPLACEMENT OF26-12-15V2500-A1,-A5
NAC-26-000602/15/953NACELLE - FIRE PROTECTION - CORE FIRE DETECTION ELEMENT, LEFT HAND AND RIGHT HAND - REPLACEMENT OF26-00-00V2500-D5
NAC-26-000702/15/953NACELLE - FIRE PROTECTION - CORE FIRE DETECTOR RAIL SUPPORT CLAMP, RIGHT HAND - ADDITION OF26-00-00V2500-D5
NAC-26-000807/15/954NACELLE - FIRE PROTECTION - FIRE DETECTOR ASSEMBLIES AND SUPPORT BRACKETS, ACCESSORY AND CORE - REPLACEMENT OF26-00-00V2500-D5
NAC-26-000910/15/950405/11/996NACELLE - FIRE PROTECTION - HARNESS ASSEMBLY, OVERHEAT SENSOR - REPLACEMENT OF26-00-00V2500-D5
NAC-26-001103/21/970303/31/984NACELLE - EXHAUST - SUPPORT BRACKETS OVERHEAT DETECTOR THRUST REVERSER26-00-00V2500-D5
NAC-26-001210/02/970109/03/994NACELLE - EXHAUST - BRACKET, INBOARD BIFURCATION OVERHEAT DETECTOR - MODIFICATION OF26-00-00V2500-D5
NAC-26-001301/10/006NACELLE - POWERPLANT - REPLACEMENT OF FIRE DETECTOR CLAMPS26-00-00V2500-A1,-A5
NAC-26-001410/30/020112/09/023NACELLE - POWER PLANT - FIRE PROTECTION - CORE ZONE FIRE DETECTOR - INSPECTION AND REPLACEMENT OF FIRE DETECTOR CLAMPS26-00-00V2500-A1,-A5
NAC-29-000105/31/900105/31/903NACELLE - POWERPLANT - HYDRAULICS - HYDRAULIC HOSE TO LOW PRESSURE SWITCH - REPLACEMENTOF29-00-00V2500-A1
NAC-29-000209/20/960102/10/978NACELLE - HYDRAULICS - HYDRAULIC FILTER MOUNTING RAFT - IDENTIFICATION PLATE - INSTALLATION OF29-11-00V2500-A1
NAC-29-026212/06/006NACELLE - HYDRAULIC POWER - LOW PRESSURE (LP) HYDRAULIC SWITCH - INSTALLATION OF ANCHOR TABS AND LOCKING WIRE29-00-00V2500-A1,-A5
NAC-29-026307/18/010508/07/036NACELLE - HYDRAULIC POWER - LOW PRESSURE (LP) HYDRAULIC SWITCH INSTALLATION OF NEW FLEXIBLE HOSE ASSEMBLY AND SUPPORT BRACKET29-00-00V2500-A1,-A5
NAC-29-026602/17/170103/23/208NACELLE - HYDRAULIC SYSTEM - REPLACEMENT OF UNION ON THE ENGINE DRIVEN PUMP (EDP) SUCTION LINE OUTLET29-11-49V2500-A5
NAC-29-026710/11/183NON-MODIFICATION SERVICE BULLETIN - NACELLE - HYDRAULIC SYSTEM - REPLACEMENT OF SUSPECT PACKING ON THE ENGINE DRIVEN HYDRAULIC PUMP PRESSURE SWITCH29-11-17V2500-A5
NAC-30-000112/15/950105/05/974NACELLE - ICE AND RAIN PROTECTION - ANTI-ICE REGULATOR VALVE - REPLACEMENT OF30-00-00V2500-D5
NAC-30-000207/01/970108/15/974NACELLE - ICE AND RAIN PROTECTION - ANTI-ICE REGULATOR VALVE - REPLACEMENT OF30-00-00V2500-D5
NAC-36-000108/06/960208/06/964NACELLE - POWERPLANT - TUBES, PRESSURE INDICATING - SERVO TUBE - REPLACEMENT OF36-00-00V2500-A1
NAC-36-000206/16/970210/30/976NACELLE - PNEUMATIC - SUPPORT BRACKETS, SENSE LINES, ENVIRONMENTAL CONTROL SYSTEM - REPLACEMENT OF36-00-00V2500-D5
NAC-36-000303/12/980201/26/994NACELLE - PNEUMATIC - ENVIRONMENTAL CONTROL SYSTEM - CHECK VALVE- INTERMEDIATE PRESSURE - REPLACEMENT OF36-11-00V2500-D5
NAC-36-000404/25/024MODIFICATION SERVICE BULLETIN - NACELLE - POWERPLANT - ECS SENSE LINE SUPPORT BRACKET - MODIFICATION OF36-00-00V2500-D5
NAC-36-000509/29/984NACELLE - PNEUMATIC - FLANGE, FAN AIR VALVE SUPPORT - REPLACEMENT OF36-00-00V2500-D5
NAC-36-000606/12/980102/04/005NACELLE - POWERPLANT - TUBES, PRESSURE INDICATING - TUBE CLIPS - REPLACEMENT OF36-00-00V2500-A1,-A5
ENG-36-000711/05/014NACELLE - POWERPLANT - TUBES, PRESSURE INDICATING - INSTALLATION OF A NEW IMPROVED ECS SENSE LINE TUBE36-00-00V2500-A5
NAC-36-000908/29/194NON-MODIFICATION SERVICE BULLETIN - PNEUMATIC - BLEED AIR - TO APPLY CORRECT TORQUE VALUE TO IMPROPERLY TORQUED BLEED AIR AND STARTER DUCT COUPLINGS36-11-41V2500-A5
ENG-70-000107/13/908INFORMATION - TO ANNOUNCE THE INCORPORATION OF A STIFFENED LP TURBINE CASE BRACKET ASSEMBLY79-00-00V2500-A1
ENG-70-000201/18/917GENERAL INFORMATION - PROVIDE AN INTERMEDIATE STRUCTURE THAT ELIMINATES FLIGHT TEST INSTRUMENTATION PROVISIONS72-32-00V2500-A1
ENG-70-000310/20/897INFORMATION - ANNOUNCEMENT OF A WEIGHT REDUCED LP TURBINE CASE ASSEMBLY72-50-00V2500-A1
ENG-70-000403/02/907ENGINE - PROVIDE AN ALTERNATE FAN SPEED PROBE ELECTRICAL HARNESS ASSEMBLY WITH ALTERNATE BRACKET ATTACHING BOLTS72-32-00V2500-A1
ENG-70-000507/28/897INFORMATION - ANNOUNCEMENT OF A NEW PRESSURE OIL TUBE THAT ELIMINATES UNUSED EEC FAN HARNESS CLIPPING LUGS79-00-00V2500-A1
ENG-70-000606/16/897INFORMATION - ANNOUNCEMENT OF A NEW PART NUMBER CUSHION LOOP CLAMP FOR THE EGT HARNESS77-00-00V2500-A1
ENG-70-000710/20/897INFORMATION - ANNOUNCEMENT OF STANDARDIZED LENGTH THIRD STAGE TURBINE VANE STRIP SEALS72-50-00V2500-A1
ENG-70-000802/15/91See SBINFORMATION - ANNOUNCEMENT OF A NEW STAGE 1 TURBINE HUB METERING PLUG72-45-00V2500-A1
ENG-70-000907/28/897INFORMATION - INTRODUCE A REVISED LP COMPRESSOR HYDRAULIC SEAL LOCK PLATE72-32-00V2500-A1
ENG-70-001007/28/897INFORMATION - INTRODUCE A REVISED NO. 3 BEARING RETAINING NUT CUP WASHER72-32-00V2500-A1
ENG-70-001107/28/897INFORMATION - TO ANNOUNCE THE PART NUMBER REVISION OF THE FUEL PUMP ATTACHING PARTS73-12-41V2500-A1
ENG-70-001209/08/897INFORMATION - TO ANNOUNCE VARIOUS EXTERNAL TUBE PART NUMBERS WITH REVISED END FITTINGS79-21-49V2500-A1
ENG-70-001305/08/927INFORMATION - INTRODUCTION OF A WEIGHT REDUCED STAGE 2.5 STATOR ASSEMBLY72-32-76V2500-A1
ENG-70-001406/16/89See SBINFORMATION - ANNOUNCEMENT OF A NEW PART NUMBER STAGE 1 HPT AIRSEAL (OUTER)72-45-00V2500-A1
ENG-70-001508/09/917INFORMATION - ANNOUNCEMENT OF GASKET OPTIONS FOR THE TURBINE CASE AND VANE ASSEMBLY72-45-00V2500-A1
ENG-70-001604/20/93See SBINFORMATION - TO ANNOUNCE AN ALTERNATE STAGE 10 TO HPT AIR VALVE75-00-00V2500-A1
ENG-70-001707/28/898INFORMATION - PROVIDE ALTERNATE SCREWS ATTACHING THE FAN CASE LINER PANELS AND THE PANEL RUBBER SEALS TO THE FAN CASE72-32-00V2500-A1
ENG-70-001808/01/89See SBINFORMATION - TO ANNOUNCE THE AVAILABILITY OF PARTS TO PERMIT THE REPAIR OF FUEL TUBE ASSEMBLIES73-11-49V2500-A1
ENG-70-001912/08/89See SBINFORMATION - PROVIDE ALTERNATE IGNITOR MOUNT BRACKETS AND ATTACHING HARDWARE72-41-00V2500-A1
ENG-70-002007/28/897INFORMATION - INTRODUCE A REVISED ANGLE GEARBOX BRACKET72-60-00V2500-A1
ENG-70-002111/10/897INFORMATION - TO ANNOUNCE THE INCORPORATION OF A REVISED MATERIAL IGNITION EXCITER AIRSEAL WASHER74-00-00V2500-A1
ENG-70-002212/08/897INFORMATION - COMMONIZATION OF WASHERS USED AT TUBE OR HARNESS CLIPPING71-00-00V2500-A1
ENG-70-002302/02/907INFORMATION - ANNOUNCEMENT OF FUEL TUBE ASSEMBLIES WITH SILVER PLATED NUTS73-00-00V2500-A1
ENG-70-002412/15/897INFORMATION - TO ANNOUNCE NEW STAGES 4 and 5 COMPRESSOR BLADES WITH REVISED SEALING PROVISIONS72-41-15V2500-A1
ENG-70-002508/18/897INFORMATION - LP COMPRESSOR - TO ANNOUNCE A FAN BLADE WITH IMPROVED BONDING FEATURES72-31-00V2500-A1
ENG-70-002611/10/897INFORMATION - TO ANNOUNCE THE AVAILABILITY OF A REVISED IGNITION EXCITER MOUNT SUPPORT BRACKET74-00-00V2500-A1
ENG-70-002710/01/938GENERAL INFORMATION - TO ANNOUNCE AN ALTERNATE VENDOR SOURCE FOR FUEL AND OIL TEMPERATURE THERMOCOUPLES73-35-15V2500-A1
ENG-70-002801/06/927INFORMATION - ANNOUNCEMENT OF A NEW NO. 2 AND 3 BEARING OIL DISTRIBUTOR ASSEMBLY WITH ANODIZED COATING72-32-00V2500-A1
ENG-70-002909/15/897INFORMATION - TO ANNOUNCE NEW PART NUMBER SLAVE AND MASTER BSBVA MOUNT BRACKET ASSEMBLIES75-00-00V2500-A1
ENG-70-003009/28/907INFORMATION - TO ANNOUNCE MATERIAL CHANGE ON LP TURBINE ACC SYSTEM75-24-49V2500-A1
ENG-70-003109/15/89See SBINFORMATION - TO ANNOUNCE BUSH HELICOIL INSERT PART NUMBERS24-00-00V2500-A1
ENG-70-003207/06/900206/17/048ENGINE - INFORMATION - TO ANNOUNCE THE AVAILABILITY OF SPARE PARTS FOR LP TURBINE HONEYCOMB SEAL REPAIRS72-50-00V2500-A1,-A5,-D5
ENG-70-003302/16/907INFORMATION - TO ANNOUNCE A REDESIGNED IGNITOR MOUNT BRACKET74-00-00V2500-A1
ENG-70-003409/15/89See SBINFORMATION - CATALOG SEQUENCE NUMBER CHANGE AT CP564471-00-00V2500-A1
ENG-70-003509/15/897INFORMATION - TO ANNOUNCE A NEW HPC STAGE 10 SOLENOID VALVE MOUNT BRACKET ASSEMBLY TO IMPROVE VALVE RETENTION75-00-00V2500-A1
NAC-70-003612/16/947INFORMATION - NACELLE - NEW AIR INTAKE COWL WITH IMPROVED COVER RIVET RETENTION71-11-00V2500-A1
ENG-70-003705/29/917INFORMATION - TO ANNOUNCE THE AVAILABILITY OF A NEW BLOCK TERMINAL ASSEMBLY73-00-00V2500-A1
ENG-70-003811/03/897INFORMATION - TO ANNOUNCE COMMON PART NUMBER TURBINE NOZZLE GROUP FEATHER SEALS72-44-00V2500-A1
ENG-70-003908/09/91See SBINFORMATION - TO ANNOUNCE VARIOUS ALTERATIONS IN PARTS SPAREABILITY CODES72-00-00V2500-A1
ENG-70-004010/11/91See SBINFORMATION - TO ANNOUNCE A CATALOG SEQUENCE NUMBER RELOCATION FOR AN OIL TANK SUPPORT BRACKET79-00-00V2500-A1
ENG-70-004112/07/90See SBINFORMATION - TO ANNOUNCE THE AVAILABILITY OF FORGED RATHER THAN CAST FUEL NOZZLE AND SUPPORT ASSEMBLIES73-00-00V2500-A1
ENG-70-004212/08/89See SBINFORMATION - ADD A REVISED PART NUMBER IDENTIFICATION TO THE EXISTING P2/T2 SENSOR73-00-00V2500-A1
ENG-70-004310/05/907INFORMATION - TO ANNOUNCE THE AVAILABILITY OF NEW STAGE 3 LP TURBINE VANE ASSEMBLIES72-50-00V2500-A1
ENG-70-004402/23/907INFORMATION - TO ANNOUNCE A NO. 5 BEARING OIL SCAVENGE TUBE ASSEMBLY WITH REVISED HALF SLEEVES79-00-00V2500-A1
ENG-70-004502/09/907INFORMATION - TO ANNOUNCE A NO. 5 BEARING OIL SCAVENGE TUBE ASSEMBLY WITH REVISED SLEEVES79-00-00V2500-A1
ENG-70-004611/10/897INFORMATION - TO ANNOUNCE A NEW PART NUMBER FOR THE LOCKWIRE USED TO SECURE THE FUEL AND OIL DRAIN PLUGS ON THE FUEL COOLED IDG OIL COOLER24-00-00V2500-A1
ENG-70-004702/09/90See SBINFORMATION - TO ANNOUNCE THE PART NUMBER REVISION OF VARIOUS SELF LOCKING NUT ASSEMBLIES71-00-00V2500-A1
ENG-70-004803/22/917INFORMATION - TO ANNOUNCE THE NO. 1 BEARING SUPPORT ASSEMBLY MADE OF TITANIUM72-32-00V2500-A1
ENG-70-004911/10/897INFORMATION - PROVIDE A REPLACEMENT BSBVA MASTER AND SLAVE GUIDE ASSEMBLY75-00-00V2500-A1
ENG-70-005005/03/917INFORMATION - AIR - TO ANNOUNCE A NEW HPT/LPT ACC AIR VALVE ASSEMBLY WITH STRENGTHENED CAMBOX75-00-00V2500-A1
ENG-70-005106/30/938INFORMATION - TO ANNOUNCE AN ALTERNATE SOURCE FOR THE NO. 5 BEARING72-50-00V2500-A1
ENG-70-005210/30/920204/13/057STANDARD PRACTICES - ENGINE INFORMATION - HP COMPRESSOR - PROVIDE AN ALTERNATE SOURCE FOR VARIABLE STATOR VANE SPINDLE BUSHINGS72-41-31V2500-A1
ENG-70-005302/16/907INFORMATION - TO ANNOUNCE THE CHANGE OF A BOLT PART NUMBER AND A NUT PART NUMBER TO IAE STANDARD PART NUMBERS75-00-00V2500-A1
ENG-70-005406/21/917INFORMATION - MAIN GEARBOX ASSEMBLY - TO ANNOUNCE A NEW OIL SCAVENGE TUBE ASSEMBLY WITH ARECONTOURED COLLAR79-22-48V2500-A1
ENG-70-005511/02/907INFORMATION - TO ANNOUNCE THE INTRODUCTION OF A NEW FUEL TUBE ATTACHING BOLT73-00-00V2500-A1
ENG-70-005611/30/907INFORMATION - FUEL AND CONTROL - TO ANNOUNCE A HINGED HEATSHIELD CONFIGURATION FOR THE (EEC) ELECTRONIC ENGINE CONTROL73-00-00V2500-A1
ENG-70-005706/15/900207/07/947INFORMATION - MAIN GEARBOX ASSEMBLY - TO ANNOUNCE AN ADDITIONAL SOURCE FOR REPLACEMENT CARBON SEALS AND MATING RINGS72-60-00V2500-A1
ENG-70-005802/23/908INFORMATION - LP COMPRESSOR - TO ANNOUNCE A DUAL SOURCE FOR THE NO. 2 BEARING72-32-00V2500-A1
ENG-70-005911/30/908INFORMATION - LP COMPRESSOR - TO ANNOUNCE A DUAL SOURCE FOR THE NO. 1 BEARING72-32-00V2500-A1
ENG-70-006005/18/908INFORMATION - TO ANNOUNCE THE SUPPLY AVAILABILITY OF NEW BOLTS ATTACHED TO THE FCOC79-00-00V2500-A1
ENG-70-006109/06/917INFORMATION - INTRODUCE LONGER BOLTS AT CLIPPING POINTS CP0876 AND CP087777-00-00V2500-A1
ENG-70-006204/12/918INFORMATION - LP TURBINE - INTRODUCE AN LP TURBINE SHAFT WITH TRIM BALANCING PROVISIONS72-50-00V2500-A1
ENG-70-006303/09/907INFORMATION - TO ANNOUNCE A NEW ELECTRICAL CONNECTOR COOLING SHIELD BRACKET73-00-00V2500-A1
ENG-70-006402/29/920105/22/987INFORMATION - HP COMPRESSOR - PROVIDE MATCHED PAIRS OF COMPRESSOR BLADE LOCKING BOLTS AND JACKSCREWS72-41-00V2500-A1
ENG-70-006507/13/907INFORMATION - TO ANNOUNCE A PART NUMBER CHANGE TO ELECTRICAL HARNESS CLAMP DETAILS72-32-00V2500-A1
ENG-70-006605/08/928INFORMATION - TO ANNOUNCE THE AVAILABILITY OF FAN CASE REPAIR PARTS72-32-00V2500-A1
ENG-70-006812/19/917INFORMATION - HP COMPRESSOR - TO ANNOUNCE REVISED QUANTITIES OF STAGE 3 COMPRESSOR BLADE RETAINING PLATES72-41-00V2500-A1
ENG-70-006906/15/907INFORMATION - TO ANNOUNCE THE AVAILABILITY OF A NEW FUEL TUBE ASSEMBLY WITH REVISED CLIPPING PROVISIONS73-00-00V2500-A1
ENG-70-007001/25/967INFORMATION - TO ANNOUNCE A NEW FAN DISK ASSEMBLY WITH A REVISED RADIUS IN THE SLOT AREA72-31-00V2500-A1
ENG-70-007104/20/907INFORMATION - MAIN GEARBOX ASSEMBLY - PROVIDE A NEW LAYSHAFT EXTENSION GEAR WITH A REDUCEDGEAR OUTER DIAMETER72-60-00V2500-A1
ENG-70-007205/10/917INFORMATION - LOW PRESSURE TURBINE - TO ANNOUNCE A WEIGHT REDUCED DIFFUSER INNER SUPPORT ASSEMBLY AND STAGE 3 TURBINE AIR SEAL RING72-50-00V2500-A1
NAC-70-007312/09/927INFORMATION - NACELLE - NEW AIR INTAKE COWL DESIGNED TO ELIMINATE INTO WIND STEPS71-11-00V2500-A1
ENG-70-007502/10/92See SBINFORMATION - TO ANNOUNCE VARIOUS ALTERATIONS OF PARTS SPAREABILITY CODES71-00-00V2500-A1
NAC-70-007605/24/917INFORMATION - ANNOUNCEMENT OF NEW THERMAL ANTI-ICING DUCT30-00-00V2500-A1
ENG-70-007705/04/907INFORMATION - PROVIDE A NEW FAN CASE ASSEMBLY WITH REVISED FRONT FLANGE AREA ANTI-ICE IMPACT LINING MATERIAL72-32-00V2500-A1
ENG-70-007805/10/917INFORMATION - LP TURBINE - INTRODUCE DIFFUSER OUTER SEGMENT ASSEMBLIES WITH REDUCED GAPS72-50-00V2500-A1
ENG-70-007901/28/910106/07/058INFORMATION - TO ANNOUNCE THE AVAILABILITY OF VARIOUS REPAIR PARTS FOR MAIN GEARBOX72-60-00V2500-A1
ENG-70-008011/22/91See SBINFORMATION - TO ANNOUNCE THE AVAILABILITY OF EXPENDABLE PARTS REQUIRED TO PERMIT LINEREPLACEMENT OF THE FUEL DISTRIBUTION VALVE AND THE BOX AND HARNESS ASSEMBLY73-00-00V2500-A1
ENG-70-008109/06/96See SBINFORMATION - TO ANNOUNCE VARIOUS CHANGES IN PARTS SPAREABILITY STATUS72-00-00V2500-A1
ENG-70-008211/03/91See SBINFORMATION - TO ANNOUNCE AN ALTERATION IN PARTS SPAREABILITY CODING74-00-00V2500-A1
ENG-70-008307/26/917ENGINE - TO ANNOUNCE THE NEW PART NUMBER ALLOCATIONS FOR THE HEAT SHRINKABLE TUBES OF THE EEC HARNESS-CORE, EEC LINK HARNESS-CORE, AND EGT HARNESS71-00-00V2500-A1
ENG-70-008412/09/927INFORMATION - ENGINE - PROVIDE A NEW GENERAL SERVICES HARNESS.71-00-00V2500-A1
ENG-70-008610/26/908INFORMATION - TO PROVIDE COMBUSTION CHAMBER LINER SEGMENTS FOR REPAIR72-42-00V2500-A1
ENG-70-008711/02/907INFORMATION - TO ANNOUNCE VARIOUS THICKNESS LPT SHAFT ADJUSTING WASHERS72-00-00V2500-A1
ENG-70-008807/13/907INFORMATION - TO ANNOUNCE VARIOUS MINOR CHANGES TO CORE HARNESS PARTS71-00-00V2500-A1
ENG-70-008907/13/907INFORMATION - TO ANNOUNCE REVISED LENGTH EXCITER COOLING HOSES75-00-00V2500-A1
NAC-70-009005/29/917INFORMATION - THRUST REVERSER - TO ANNOUNCE THE AVAILABILITY OF VARIOUS REPAIR PARTS78-00-00V2500-A1
ENG-70-009107/06/907INFORMATION - TO ANNOUNCE THE AVAILABILITY OF OVERSIZE RING SEALS TO PERMIT THE REPAIR OFVARIOUS CARBON SEAL RING HOLDERS72-32-00V2500-A1
ENG-70-009208/20/937INFORMATION - TO ANNOUNCE NEW HP COMPRESOR VARIABLE STATOR VANES, STAGES 3,4, AND 5 MADE OF IMPROVED CORROSION RESISTANT, MATERIAL72-41-00V2500-A1
ENG-70-009309/06/91See SBINFORMATION - AIR - TO ANNOUNCE THE AVAILABILITY OF A REPAIR PART FOR THE HPC STAGE 7 BLEED VALVE DUCT AND SEAL ASSEMBLY72-32-52V2500-A1
ENG-70-009508/03/907INFORMATION - MAIN GEARBOX ASSEMBLY - TO ANNOUNCE AN ADDITIONAL SOURCE FOR MAIN GEARBOX BEARINGS72-60-00V2500-A1
ENG-70-009607/06/908INFORMATION - LP COMPRESSOR - PROVIDE AN OPTION NUMBER FOR THE NO. 1 BEARING FACE SEAL ASSEMBLY72-32-00V2500-A1
NAC-70-009705/31/937INFORMATION - ANNOUNCEMENT OF NEW CABLES WITH REVISED BACKSHELLS71-11-00V2500-A1
NAC-70-009805/31/937INFORMATION -ANNOUNCEMENT OF NEW FIRE DETECTION SYSTEM "B" HARNESS, EBU CORE SERVICES HARNESS, INTERPHONE JACK CABLE, AND P2/T2 CABLE ASSEMBLIES71-00-00V2500-A1
ENG-70-009904/15/93See SBINFORMATION - TO ANNOUNCE THE AVAILABILITY OF VARIOUS PARTS TO PERMIT ACCESSORY COMPONENTREPLACEMENT73-00-00V2500-A1
ENG-70-010108/09/917INFORMATION - ENGINE - PROVIDE A STRENGTHENED FUEL SYSTEM AIR TUBE MOUNT BRACKET ASSEMBLY71-00-00V2500-A1
ENG-70-010211/03/91See SBINFORMATION - TO ANNOUNCE CHANGES IN VARIOUS SPAREABILITY CODES72-41-00V2500-A1
ENG-70-010410/05/920103/05/998INFORMATION - AIR SYSTEM - INTRODUCE SPARE PARTS USED IN LPT-ACC REPAIRS75-00-00V2500-A1,-A5,-D5
ENG-70-010503/22/918INFORMATION - TO ANNOUNCE VARIOUS CHANGES IN PARTS SPAREABILITY CODES72-50-00V2500-A1
ENG-70-010609/13/918INFORMATION - TO ANNOUNCE THE AVAILABILITY OF STRENGTHENED FAN CASE REAR LINER PANEL ASSEMBLIES72-32-00V2500-A1
ENG-70-010710/05/927INFORMATION - TO ANNOUNCE NEW STAGES 6 AND 7 TURBINE VANE ASSEMBLIES72-50-00V2500-A1
ENG-70-010812/07/907INFORMATION - TO ANNOUNCE REINFORCED RACEWAYS71-00-00V2500-A1
ENG-70-010911/30/907INFORMATION - TO ANNOUNCE NEW FUEL TUBE-TO-FUEL DIVERTER VALVE ATTACHING BOLTS73-00-00V2500-A1
ENG-70-011012/14/907INFORMATION - MAIN GEARBOX ASSEMBLY - TO ANNOUNCE A NEW DEOILER CASING ASSEMBLY72-60-00V2500-A1
ENG-70-011103/08/917INFORMATION - MAIN GEARBOX ASSEMBLY - TO ANNOUNCE NEW FUEL PUMP GEAR AND IDLER GEAR SHROUDS TO PERMIT IMPROVED LUBRICATION72-60-00V2500-A1
ENG-70-011203/08/917INFORMATION - MAIN GEARBOX ASSEMBLY - TO ANNOUNCE A NEW MAIN GEARBOX CASING ASSEMBLY72-60-00V2500-A1
ENG-70-011301/18/917INFORMATION - AIR - TO ANNOUNCE A NEW HPT/LPT ACC VALVE ACTUATOR75-00-00V2500-A1
ENG-70-011406/07/917INFORMATION - LP COMPRESSOR - TO ANNOUNCE A NEW NO. 1 BEARING OIL SUPPLY TUBE ASSEMBLY72-32-00V2500-A1
ENG-70-011509/15/930304/07/038INFORMATION - ENGINE - PROVIDE ADDITIONAL OPTIONS FOR THE NO. 1 AND NO. 4 FACE SEAL ASSEMBLIES72-00-00V2500-A1,-A5,-D5
NAC-70-011603/15/910103/15/917INFORMATION - NACELLE - TO ANNOUNCE NEW THRUST REVERSER HINGE BOLTS WITHOUT LOCKING FEATURES78-32-00V2500-A1
NAC-70-011702/15/917INFORMATION - POWERPLANT - TO ANNOUNCE NEW FRONT MOUNT ATTACHMENT BOLTS WITH AN UNNECESSARY LOCKING PROVISION ELIMINATED71-00-00V2500-A1
ENG-70-011808/09/917INFORMATION - FUEL AND CONTROL - INTRODUCE A NEW FUEL DIVERTER AND RETURN VALVE WITH IMPROVED SEALING FEATURES73-00-00V2500-A1
NAC-70-011903/15/910103/15/917INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF VARIOUS NACELLE IDENTIFICATION DECALS FOR THRUST REVERSER AND COMMON NOZZLE78-11-00V2500-A1
ENG-70-012005/31/918INFORMATION - LP COMPRESSOR - TO ANNOUNCE A SECOND SOURCE FOR TOWERSHAFT BEARINGS72-32-00V2500-A1
ENG-70-012105/15/937INFORMATION - PROVIDE NEW NO. 4 BEARING SCAVENGE TUBE ATTACHING SCREWS72-42-00V2500-A1
ENG-70-012205/31/917CANCELLATION OF INFORMATION BULLETIN V2500-ENG-70-0122 (OIL - TO ANNOUNCE THE AVAILABILITY OF A COATED FUEL COOLED OIL COOLER THREADED INSERT)79-00-00V2500-A1
ENG-70-012410/29/927INFORMATION - MAIN GEARBOX ASSEMBLY - TO ANNOUNCE SPAREABLE MAIN GEARBOX SEAL ASSEMBLIES72-60-00V2500-A1
ENG-70-012510/05/92See SBINFORMATION - ENGINE - TO ANNOUNCE CHANGES IN VARIOUS SPAREABILITY CODES79-00-00V2500-A1
ENG-70-012603/30/947INFORMATION - ENGINE - PROVIDE A NEW ACC SUPPORT ASSEMBLY FOR PARTS COMMONALITY75-00-00V2500-A1,-A5
ENG-70-012708/12/947INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF A NEW ANNULUSFILLER ASSEMBLY WITH A REVISED PROFILE72-31-00V2500-A5,-D5
ENG-70-012910/12/947INFORMATION - ENGINE - INTRODUCE IMPROVED VARIABLE STATOR RIGGING PIN BRACKETS72-41-00V2500-A5,-D5
NAC-70-013011/12/920111/12/927INFORMATION - ANNOUNCEMENT OF NEW FAN CASE FIRE DETECTOR26-00-00V2500-A1
NAC-70-013105/24/917INFORMATION - ANNOUNCEMENT OF NEW EBU CABIN AIR DUCT36-11-00V2500-A1
NAC-70-013205/24/917INFORMATION - ANNOUNCEMENT OF NEW EBU UPPER STARTER AIR DUCT ASSEMBLY80-13-49V2500-A1
NAC-70-013305/24/917NACELLE - ANNOUNCEMENT OF NEW FAN CASE STRUT ANCHORAGE BRACKETS71-00-00V2500-A1
NAC-70-013405/24/917INFORMATION - ANNOUNCEMENT OF NEW FAN COWL ASSEMBLY AND VARIOUS DETAILS71-11-00V2500-A1
NAC-70-013505/24/917INFORMATION - ANNOUNCEMENT OF NEW EBU NACELLE P2/T2 CABLE ASSEMBLIES71-11-00V2500-A1
ENG-70-013602/08/937INFORMATION - ANNOUNCEMENT OF NEW GENERAL SERVICES AND EEC AND IGNITION HARNESSES71-00-00V2500-A1
NAC-70-013703/15/910103/15/917INFORMATION - THRUST REVERSER - TO ANNOUNCE REDIMENSIONED FORWARD CROSS-OVER BEAM78-00-00V2500-A1
NAC-70-013812/16/940212/16/947INFORMATION - NACELLE - THRUST REVERSER - REINTRODUCE THE ORIGINAL DESIGN OF THE ENGINERADIAL BUMPER71-00-00V2500-A1
NAC-70-014010/04/917INFORMATION - EBU - TO ANNOUNCE OIL TANK REMOTE FILL PROVISION - STRAIGHT CONNECTOR71-00-00V2500-A1
NAC-70-014205/24/917INFORMATION - ANNOUNCEMENT OF NEW EBU CABIN AIR BLEED AND DRAIN TUBE ASSEMBLIES71-71-00V2500-A1
ENG-70-014312/16/947INFORMATION - ANNOUNCEMENT OF NEW EBU OIL SYSTEM, IDG COOLING SYSTEM, AND FUEL DRAIN SYSTEM TUBE ASSEMBLIES24-00-00V2500-A1
ENG-70-014405/29/917INFORMATION - ANNOUNCEMENT OF NEW EBU CABIN AIR SERVO PIPE BRACKET AND ENGINE CORE EARTHBRACKET72-41-00V2500-A1
ENG-70-014505/29/917INFORMATION - ANNOUNCEMENT OF NEW BLOCK TERMINAL ASSEMBLY73-00-00V2500-A1
ENG-70-014605/29/917INFORMATION - ANNOUNCEMENT OF NEW EBU FUEL SYSTEM MOUNTING BRACKET ASSEMBLY73-00-00V2500-A1
NAC-70-014705/24/917INFORMATION - ANNOUNCEMENT OF NEW FAN COWL ASSEMBLY71-13-00V2500-A1
NAC-70-014805/24/917INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF VARIOUS NACELLE IDENTIFICATION DECALS FOR INLET COWL AND FAN COWL DOORS71-11-00V2500-A1
NAC-70-015012/09/92See SBINFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF VARIOUS INLET COWL REPAIR PARTS71-11-00V2500-A1
NAC-70-015103/14/91See SBINFORMATION - NACELLE - TO ANNOUNCE THE ATA CHAPTER RELOCATION OF THE NACELLE TEMPERATURE SENSOR75-00-00V2500-A1
ENG-70-015209/24/938INFORMATION - ENGINE - INTRODUCE THE AVAILABILITY OF SHIMS TO ASSIST IN PROPER INSTALLATION OF THE ELECTRONIC ENGINE CONTROL (EEC)73-22-34V2500-A1,-A5
ENG-70-015308/04/937INFORMATION - MAIN GEARBOX ASSEMBLY - PROVIDE OVERSIZE RINGS AND SHIMS AT VARIOUS GEARBOX LOCATIONS AND A CHANGE OF AN ITEM CATALOG SEQUENCE NUMBER72-60-00V2500-A1
ENG-70-015404/10/920211/08/937INFORMATION - HP TURBINE ROTOR AND STATOR ASSEMBLY - INTRODUCE REVISED MATERIAL STAGE 2 TURBINE BLADE ASSEMBLIES72-45-00V2500-A1
ENG-70-015509/06/917INFORMATION - ENGINE - TO ANNOUNCE AN ALTERNATIVE SOURCE FOR A FUEL TUBE RETAINING RING73-00-00V2500-A1
ENG-70-015609/30/937INFORMATION - ELECTRICAL HARNESS - PROVIDE AN ALTERNATIVE SOURCE FOR ELECTRICAL HARNESSCONNECTORS71-00-00V2500-A1
ENG-70-015701/14/947INFORMATION - ELECTRICAL HARNESSES - COMMONISATION OF RAYCHEM SLEEVING PART NUMBERS71-00-00V2500-A1
ENG-70-015801/14/947INFORMATION - ENGINE - INTRODUCE VARIOUS REVISED MATERIAL EXTERNAL BRACKETS71-00-00V2500-A1
ENG-70-015907/05/91See SBINFORMATION - PROVIDE A NO. 3 BEARING OPTION AND HALF SIZE CLASSES FOR THE STAGE 1 VANE CLUSTER ASSEMBLY AND THE STAGE 2 RING SEGMENT AND VANE CLUSTER ASSEMBLY72-32-00V2500-A1
ENG-70-016008/09/918INFORMATION - LP COMPRESSOR - TO ANNOUNCE A NEW FAN FRAME ASSEMBLY72-32-00V2500-A1
ENG-70-016105/20/927INFORMATION - TO ANNOUNCE VARIOUS ACC SPHERICAL JOINT PARTS SPAREABILITY75-00-00V2500-A1
ENG-70-016209/10/93See SBINFORMATION - ENGINE - TURBINE EXHAUST CASE ASSEMBLY - PROVIDE A CORRECT SELF-LOCKING NUT PART NUMBER72-50-00V2500-A1
ENG-70-016310/27/997INFORMATION - ENGINE - LP COMPRESSOR - PROVIDE NEW FIRE- SHIELDS72-32-00V2500-A1
NAC-70-016412/09/927INFORMATION - ANNOUNCEMENT OF A NEW LOOP CLAMP AT CLIPPING POINT CP089177-32-00V2500-A1
ENG-70-016509/06/967INFORMATION - ENGINE - HP COMPRESSOR - TO ANNOUNCE AN ALTERNATE SOURCE FOR STAGE 6 VARIABLE STATOR VANE BUSHINGS72-41-00V2500-A1
ENG-70-016602/24/927INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE A PART NUMBER CHANGE TO THE ROD END ASSEMBLY REPAIR PARTS72-32-00V2500-A1
NAC-70-016710/12/927INFORMATION - ANNOUNCEMENT OF REVISED TRANSLATING SLEEVE TRIM78-11-00V2500-A1
ENG-70-016802/24/920102/25/007INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF AN INLET CONEREPAIR DETAIL72-38-00V2500-A1
ENG-70-016908/04/937INFORMATION - ENGINE - MAIN GEARBOX ASSEMBLY - INTRODUCE A NEW ANGLE GEARBOX OIL DUCT72-60-00V2500-A1
ENG-70-017212/15/917INFORMATION - ENGINE - LP COMPRESSOR - NEW HYDRAULIC SEAL ASSEMBLY72-32-00V2500-A1
NAC-70-017312/09/910101/12/007NACELLE - THRUST REVERSER - TO ANNOUNCE THE AVAILABILITY OF A MACHINED BLOCKER DOOR WITH REVISED RIB CONFIGURATION78-32-00V2500-A1
NAC-70-017512/09/920111/11/007INFORMATION - ANNOUNCEMENT OF NEW BLEED AIR SYSTEM CONNECTING ROD ASSEMBLIES36-11-49V2500-A1
NAC-70-017612/09/927INFORMATION - NACELLE - ANNOUNCEMENT OF THE AVAILABILITY OF SERVICE REPAIR PARTS FOR THE OIL FILLER ACCESS DOOR HINGE OF THE LH FAN COWL DOOR71-13-00V2500-A1
NAC-70-017712/09/920102/13/027INFORMATION - ANNOUNCEMENT OF THE ADDITION OF REVISED BLOCKER DOOR HINGE FITTINGS78-32-00V2500-A1
ENG-70-018007/30/927INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE A GEARSHAFT BEARING HOUSING ASSEMBLY WITH REVISED COATING72-32-00V2500-A1
NAC-70-018112/09/927INFORMATION - TO ANNOUNCE THE AVAILABILITY OF VARIOUS REPAIR PARTS FOR FAN COWL DOOR AND IGNITION HARNESS71-13-00V2500-A1
ENG-70-018207/03/957INFORMATION - ENGINE - TURBINE NOZZLE ASSEMBLY - NEW STAGE 1 HPT DUCT SEGMENT RETAINING BOLTS72-44-00V2500-A1
ENG-70-018310/05/928INFORMATION - ACC MANIFOLD - TO ANNOUNCE THE AVAILABILITY OF ACC MANIFOLD CLAMP RETAINING RIVETS75-00-00V2500-A1
ENG-70-018403/30/940107/19/997INFORMATION - ENGINE - LP TURBINE - NEW STAGE 3 SHROUD SEGMENT SEAL ASSEMBLY72-50-00V2500-A1,-A5,-D5
NAC-70-018503/30/94See SBINFORMATION - ANNOUNCEMENT OF NEW NO. 4 HINGE BOLT AND WASHER ATTACHMENT78-32-00V2500-A1
ENG-70-018610/05/920103/05/998INFORMATION - ENGINE - LP TURBINE - PROVIDE ACC CONNECTOR REPAIR PARTS75-00-00V2500-A1,-A5,-D5
NAC-70-018710/20/927INFORMATION - ANNOUNCEMENT OF NEW EBU CABIN AIR SYSTEM CONNECTING ROD36-00-00V2500-A1
ENG-70-018801/15/977INFORMATION - ENGINE - TO ANNOUNCE NEW STAGE 1 TURBINE VANE ASSEMBLIES72-44-00V2500-A1
ENG-70-018905/31/937INFORMATION - MAIN GEARBOX ASSEMBLY - TO ANNOUNCE A NEW MAIN GEARBOX CASING ASSEMBLY72-60-00V2500-A1
NAC-70-019012/09/927INFORMATION - ANNOUNCEMENT OF NEW FAN COWL DOOR LATCH ANTI- SWIVEL PLATE71-13-00V2500-A1
ENG-70-019104/29/938INFORMATION - ENGINE INDICATING - PROVIDE AN ALTERNATE SOURCE FOR THE EGT THERMOCOUPLE77-21-15V2500-A1
ENG-70-019204/17/928INFORMATION - TO ANNOUNCE THE AVAILABILITY OF PARTS TO PERMIT REPAIR OF HP COMPRESSOR STAGE 4 AND 5 ROTOR BLADES72-41-00V2500-A1
ENG-70-019302/01/938INFORMATION - OIL - TO ANNOUNCE THE INTRODUCTION OF NEW FUEL COOLED OIL COOLER WITH ADDITIONAL CRIMP79-00-00V2500-A1
ENG-70-019407/30/927INFORMATION - ENGINE - PROVIDE REPLACEMENT FAN CASE LINER PANEL ASSEMBLIES72-32-00V2500-A1
ENG-70-019609/25/928INFORMATION - ENGINE - PROVIDE REVISED IDENTIFICATION FOR FUEL DISTRIBUTION VALVE PACKINGS73-00-00V2500-A1
ENG-70-019709/14/93See SBINFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF VARIOUS GEARBOX REPAIR PARTS72-60-00V2500-A1
ENG-70-019808/17/928INFORMATION - ENGINE - LP COMPRESSOR - PROVIDE REPAIR DETAILS FOR THE WEIGHT-REDUCED FAN CASE ASSEMBLY72-32-00V2500-A1
ENG-70-020007/31/927INFORMATION - ENGINE - DIFFUSER AND COMBUSTION GROUP - PROVIDE A NEW NO. 4 BEARING COOLING DUCT ASSEMBLY72-42-00V2500-A1
ENG-70-020109/30/927INFORMATION - ENGINE - LP COMPRESSOR - STAGES 1.5 AND 2.0 STATOR ASSEMBLIES WITH REVISED MOLDING MATERIAL72-32-00V2500-A1
ENG-70-020204/15/93See SBINFORMATION - LP COMPRESSOR - TO ANNOUNCE VARIOUS REVISIONS TO ATA NUMBER ASSIGNMENTS72-32-00V2500-A1
ENG-70-020401/04/94See SBINFORMATION - ENGINE - PROVIDE REPAIR PARTS FOR REPAIR OF THE TURBINE EXHAUST CASE GROUND HANDLINGIMOUNT BUSHINGS72-50-00V2500-A1
ENG-70-020607/11/94See SBINFORMATION - ENGINE - MAIN GEARBOX ASSEMBLY - PROVIDE AN ALTERNATE SOURCE FOR THE OIL DISTRIBUTOR ASSEMBLY79-00-00V2500-A1
ENG-70-020710/05/927INFORMATION - ENGINE - PROVIDE A NEW STAGE 4 LP TURBINE AIR SEAL ASSEMBLY72-50-00V2500-A1
ENG-70-020802/01/948INFORMATION - ENGINE - LP COMPRESSOR - INTRODUCE PARTS FOR VARIOUS FAN CASE REPAIRS72-32-00V2500-A5,-D5
ENG-70-020909/30/927INFORMATION - ENGINE - PROVIDE A NEW ENGINE IDENTIFICATION PLATE WITH REVISED LABELLING AREAS72-32-00V2500-A1
ENG-70-021105/12/937INFORMATION - ENGINE - HP COMPRESSOR - PROVIDE A NEW HPC STATIC AIR SEAL ASSEMBLY THATELIMINATES UNNECESSARY BYPASS HOLES72-32-00V2500-A1
ENG-70-021301/14/94See SBINFORMATION - ENGINE - HP COMPRESSOR - PROVIDE REPAIR PARTS FOR THE STAGE 8 COMPRESSOR CASE ASSEMBLY BORESCOPE PORT72-41-00V2500-A1
NAC-70-021403/31/937INFORMATION - ANNOUNCEMENT OF A NEW QUICK RELEASE VERSION OF CABLE CLAMP24-00-00V2500-A1
ENG-70-021601/31/948INFORMATION - ENGINE - HP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF REPAIR PARTS FOR THE STAGE 10 COMPRESSOR CASE ASSEMBLY72-41-00V2500-A1
NAC-70-021712/09/927INFORMATION - NACELLE - HYDRAULICS - TO ANNOUNCE THE AVAILABILITY OF INCREASED LENGTH FLEXIBLE HOSES29-11-00V2500-A1
ENG-70-021806/16/930308/21/097INFORMATION - ENGINE - LP TURBINE - TO ANNOUNCE NEW STAGE 3 TURBINE VANES WITH REVISED COMPOUND RADIUS AT INNER PLATFORM TRAILING EDGE72-50-22V2500-A1
ENG-70-021912/22/977ENGINE - LP TURBINE - TO ANNOUNCE NEW STAGE 4 TURBINE VANES WITH REVISED COMPOUND RADIUS AT INNER PLATFORM TRAILING EDGE72-50-00V2500-A1
ENG-70-022011/08/93See SBINFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF REPAIR PARTS TO SUPPORT VARIOUS REPAIR SCHEMES72-00-00V2500-A1
ENG-70-022108/27/938INFORMATION - TO ANNOUNCE THE AVAILABILITY OF PARTS TO PERMIT THE REPAIR OF HP COMPRESSOR SEAL RING CARRIER ASSEMBLIES72-32-23V2500-A1
ENG-70-022209/06/96See SBINFORMATION - ENGINE - HP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF SPARE PARTS TO SUPPORT VARIOUS REPAIR SCHEMES72-00-00V2500-A1,-A5,-D5
NAC-70-022301/07/947INFORMATION - THRUST REVERSER - TO ANNOUNCE THE AVAILABILITY OF BLOCKER DOORS WITH IMPROVED TRAILING EDGE CLEARANCES78-32-00V2500-A1
NAC-70-022507/16/010109/13/017INFORMATION - NACELLE - TO INTRODUCE NEW PIN RETAINER AND SPACER - LOWER TRACK INSTALLATION78-30-00V2500-A1,-A5
NAC-70-022612/09/92See SBINFORMATION - ANNOUNCEMENT OF SPAREABLE EBU PARTS30-21-00V2500-A1
ENG-70-022805/27/937INFORMATION - ENGINE - TO ANNOUNCE A NEW ANGLE GEARBOX LINK PIN THAT PROVIDES IMPROVED MAINTAINABILITY72-00-60V2500-A1
ENG-70-022901/09/957INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE A REVISED QUANTITY OF NO. 3 BEARING SHIMS72-32-10V2500-A1
ENG-70-023006/16/930302/17/067INFORMATION - ENGINE - LP TURBINE - TO ANNOUNCE NEW STAGES 4,5,6, AND 7 TURBINE VANES WITH REDUCED INNER AIR SEAL CLEARANCES72-50-22V2500-A1,-A5,-D5
ENG-70-023208/30/968INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A STEEL BUSHING TO SUPPORT REPAIR OF THE FAN CASE ASSEMBLY72-32-85V2500-A1
ENG-70-023312/27/937INFORMATION - ENGINE - LP COMPRESSOR - PROVIDE A NEW STAGE 1.5 COMPRESSOR BLADE ASSEMBLYWITH A REVISED PLATFORM72-32-82V2500-A1
ENG-70-023506/30/948INFORMATION - ENGINE - HP COMPRESSOR - PROVIDE REPLACEMENT SHANK NUTS FOR THE STAGES 8 AND 11 CASE ASSEMBLIES72-41-21V2500-A1
ENG-70-023602/09/947INFORMATION - ENGINE - PROVIDE NEW THERMOCOUPLE STUD NUTS FOR THE EEC CORE HARNESS ASSEMBLY71-52-00V2500-A1
NAC-70-023807/17/017INFORMATION-NACELLE-TO INTODUCE A NEW SEAL CARRIER HALF and SHIM-CNA78-11-11V2500-D5
NAC-70-023905/31/930104/03/097INFORMATION - NACELLE - PROVIDE A REVISED SOURCE FOR FORWARD ENGINE MOUNT BOLT71-21-12V2500-A1
ENG-70-024011/18/938INFORMATION - ENGINE - LP COMPRESSOR - PROVIDE ADDITIONAL CLASSES OF HPC ROTOR ADJUSTING WASHERS72-32-26V2500-A1
ENG-70-024105/27/93See SBINFORMATION - ENGINE - FUEL AND CONTROL - TO ANNOUNCE THE AVAILABILITY OF REPAIR PARTS FOR THE P4.9 PRESSURE CONTROL MANIFOLD ASSEMBLY73-22-51V2500-A1
ENG-70-024204/15/930107/14/007INFORMATION - ENGINE - OIL - PROVIDE A NEW NO. 4 BEARING PRESSURE TRANSDUCER WITH REVISED OUTPUT CHARACTERISTICS79-33-16V2500-A1
ENG-70-024303/30/947INFORMATION - ENGINE - PROVIDE A NEW ACC MANIFOLD MOUNTING BRACKET RIVET75-24-49V2500-A1,-A5,-D5
ENG-70-024403/27/950103/21/977ENGINE - INFORMATION - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF A NEW FAN FRAME ASSEMBLY72-32-00V2500-D5
ENG-70-024502/25/947INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A NEW TURBINE EXHAUST CASE ASSEMBLY72-50-00V2500-A5
ENG-70-024603/30/947INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF NEW HIGH TEMPERATURE RESISTANT ACC MANIFOLD SEALING RINGS75-24-49V2500-A1,-A5,-D5
ENG-70-024705/26/947INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF NEW P2.5CM TUBE ASSEMBLIES72-32-00V2500-A1,-A5,-D5
ENG-70-024806/30/930312/15/057INFORMATION - ENGINE - LP TURBINE ROTOR AND STATOR ASSEMBLY - INTRODUCE NEW STAGES 3 AND 4 TURBINE VANE ASSEMBLIES72-50-00V2500-A5,-D5
ENG-70-025006/01/938INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF IGNITION LEADS WITH IMPROVED INSULATION74-21-00V2500-A1,-A5
ENG-70-025107/10/947INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A REVISED MATERIAL THRUST MOUNTBRACKET ASSEMBLY71-21-11V2500-A5
ENG-70-025207/30/947INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF A NEW LPC INLET GUIDE VANE ASSEMBLY72-32-00V2500-A1
ENG-70-025306/15/937INFORMATION - ENGINE - DIFFUSER AND COMBUSTION SECTION - PROVIDE NEW INNER AND OUTER COMBUSTION CHAMBERS WITH INCREASED HARDFACE THICKNESS AND RELOCATED COOLING HOLES72-00-00V2500-A1
ENG-70-025508/20/938INFORMATION - ENGINE - DIFFUSER AND COMBUSTION SECTION PERMIT THE USE OF ADDITIONAL COMBUSTION CHAMBER CLAMP SPACERS72-40-00V2500-A1,-A5,-D5
ENG-70-025609/07/937INFORMATION - ENGINE - HP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF AN ALTERNATE STAGE 10 COMPRESSOR SEALING RING72-41-00V2500-A1
ENG-70-025701/25/967INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A NEW WASHER FOR USE AT THE FAN EXIT GUIDE VANE INNER PLATFORM72-32-00V2500-A5,-D5
ENG-70-025810/14/947INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF A SILVER-PLATED LPC STATOR SELF-LOCKING NUT72-32-00V2500-A5,-D5
ENG-70-026010/20/937INFORMATION - ENGINE - PROVIDE AN IGNITION COOLING BOX WITH IMPROVED CLEARANCE TOLERANCES74-11-00V2500-A1,-A5,-D5
ENG-70-026105/26/947INFORMATION - ENGINE - INTRODUCE A REINFORCED NF HARNESS SUPPORT BRACKET72-32-17V2500-A1,-A5,-D5
ENG-70-026205/26/947INFORMATION - ENGINE - LP COMPRESSOR - INTRODUCE A NEW BLEED VALVE RING VESPEL GUIDE RIVET72-32-00V2500-A5,-D5
ENG-70-026301/20/95See SBINFORMATION - ENGINE - FAN CASE ASSEMBLY - TO ANNOUNCE THE AVAILABILITY OF FAN CASE REPAIR PARTS72-38-00V2500-A1
ENG-70-026409/12/958INFORMATION - ENGINE - LP COMPRESSOR - PROVIDE ADDITIONAL FLANGED SLEEVE BEARINGS TO ENSURE PROPER ASSEMBLY OF THE 2.5 BLEED VALVE MECHANISM72-32-00V2500-A5,-D5
NAC-70-026511/29/930103/22/947INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW COMMON NOZZLE ASSEMBLY71-00-00V2500-A1
ENG-70-026603/22/977INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF A ONE PIECE CAST FAN FRAME ASSEMBLY72-32-00V2500-A1,-A5
ENG-70-026709/24/93See SBINFORMATION - ENGINE - LP TURBINE - PROVIDE ALTERNATE SOURCES FOR THE NO. 5 BEARING, THE NO. 5 BEARING FACE SEAL, AND THE EGT THERMOCOUPLE72-50-00V2500-A1
ENG-70-026801/14/94See SBINFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF VARIOUS AIR TUBE REPAIR PARTS36-11-47V2500-A1
ENG-70-026903/11/94See SBINFORMATION - ENGINE - PROVIDE REPAIR PARTS FOR VARIOUS HP COMPRESSOR REPAIRS72-41-00V2500-A1
ENG-70-027008/20/937INFORMATION - ELECTRICAL HARNESSES - INTRODUCTION OF NEW LACING AND ALTERNATIVE TAPE71-52-00V2500-A1,-A5
NAC-70-027001/07/94See SBINFORMATION - NACELLE - THRUST REVERSER - TO ANNOUNCE THE DELETION OF SEVERAL PARTS INCORRECTLY LISTED AS SPAREABLE ITEMS78-30-15V2500-A1
ENG-70-027106/20/947INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A NEW HARNESS CLIP AT CLIPPING POINT CP569371-52-00V2500-A1
NAC-70-027110/07/947NACELLE - ELECTRICAL POWER - TO ANNOUNCE THE AVAILABILITY OF REPAIR PARTS FOR IDG CABLE REPLACEMENT24-21-00V2500-A1
ENG-70-027207/07/957INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF REVISED MATERIAL LP COMPRESSOR BLEED ACTUATOR MOUNTING BRACKETS75-31-00V2500-A1,-A5
NAC-70-027206/15/968NACELLE - INLET - PROVIDE REPAIR PARTS FOR VARIOUS INLET AND FAN COWL REPAIRS71-11-00V2500-A1,-A5
ENG-70-027310/01/937INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF A BIFURCATIONPANEL BOX COVER ASSEMBLY WITH IMPROVED INSTALLATION FEATURES72-38-00V2500-A1,-D5
NAC-70-027301/07/947INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF VARIOUS PARTS TO SUPPORT COMMON NOZZLE ASSEMBLY REPAIRS78-11-00V2500-A1
ENG-70-027408/08/05See SBINFORMATION - AIR - TURBINE COOLING AIR TUBES MATERIAL CHANGE79-21-42V2500-A1,-A5
ENG-70-027510/14/947INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF A NEW FAN FRAME DRAIN PIPE72-32-00V2500-A1,-A5
ENG-70-027610/20/937INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A NEW IGNITOR PLUG FEATURING REVISED GLASS SEAL MATERIAL74-21-00V2500-A1,-A5,-D5
ENG-70-027706/30/05See SBINFORMATION - INTRODUCTION OF ALTERNATIVE SPAREABLE PART NUMBERS FOR BULK STOCK ITEMS71-52-00V2500-A1,-A5,-D5
ENG-70-027802/25/948INFORMATION - ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - TO ANNOUNCE THE SPAREABILITY OF A STAGE 2 HPT TURBINE RETAINING PLATE72-45-00V2500-A1
ENG-70-027912/15/937INFORMATION - ENGINE - TURBINE EXHAUST CASE ASSEMBLY - TO ANNOUNCE THE CORRECT SPAREABLE THERMAL BLANKET72-50-00V2500-A1
ENG-70-028006/24/947INFORMATION - ENGINE - INTRODUCE A LONGER BOLT AT CLIPPING POINT CP605775-31-00V2500-A5
ENG-70-028112/19/947INFORMATION - ENGINE - AIR - TO ANNOUNCE A NEW HPT/LPT ACC VALVE ACTUATOR ASSEMBLY WITH IMPROVED PIN RETENTION FEATURES75-24-52V2500-A1,-A5
ENG-70-028207/20/940107/10/017INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF VARIOUS REVISED MATERIAL FRONT COMPRESSOR PARTS72-32-00V2500-A1,-A5,-D5
ENG-70-028301/27/957INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF A REVISED MATERIAL FAN EXIT COOLING AIR PRESSURE BOSS72-32-00V2500-A1,-A5,-D5
ENG-70-028406/30/940106/29/017INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A NEW TERMINAL FOR THE NF HARNESS ASSEMBLY72-32-00V2500-A1,-A5,-D5
ENG-70-028607/03/95See SBINFORMATION - ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - TO ANNOUNCE THE AVAILABILITY OF A NEW STAGE 2 HPT VANE COVER72-45-24V2500-A1
ENG-70-028706/20/947INFORMATION - ENGINE - HP COMPRESSOR - TO ANNOUNCE THE DELETION OF ALTERNATE STEEL-BACKED VIGV AND VSV SPINDLE BUSHINGS72-41-31V2500-A5,-D5
ENG-70-028806/30/947INFORMATION - ENGINE - PROVIDE ALTERNATE VENDOR PART NUMBER IDENTIFICATION FOR VARIOUS HARNESS CONNECTORS AND PINS71-51-41V2500-A1,-A5
NAC-70-028901/28/947INFORMATION - NACELLE - REPLACE EXISTING HARNESS CONNECTORS WITH ESC10 TYPE CONNECTORS71-11-00V2500-A1
ENG-70-029001/28/940106/11/037INFORMATION - NACELLE - REPLACE EXISTING HARNESS CONNECTORS WITH ESC10 TYPE CONNECTORS71-51-00V2500-A1,-A5
ENG-70-029107/20/947INFORMATION - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF A FAN CASE ASSEMBLY WITH AREDESIGNED FLANGE TO ACCOMMODATE BRACKET INSTALLATION72-32-00V2500-D5
ENG-70-029201/20/957INFORMATION - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF A COMMON OIL FEED ADAPTOR72-32-00V2500-A1
ENG-70-029309/10/930104/05/008INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A NEW LIGHTER WEIGHT INLET CONE WITH SPIRAL MARKINGS72-38-00V2500-A1
ENG-70-029406/25/947INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A NEW CLIP AT CLIPPING POINT CP575874-21-00V2500-A5
ENG-70-029505/24/967INFORMATION - ENGINE - PROVIDE REDUCED LENGTH RIVETS FOR THE TURBINE CASE COOLING MANIFOLDSUPPORT RIVET72-00-50V2500-A1,-A5,-D5
NAC-70-029601/07/947INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF INCREASED LENGTH TRANSLATING SLEEVE HYDRAULIC HOSES78-32-00V2500-A1
ENG-70-029710/20/937INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A NEW BIFURCATION BOX THAT INCORPORATES A STRENGHENED SEAL RETAINER72-38-00V2500-D5
ENG-70-030002/25/947INFORMATION - ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - INTRODUCE NEW FIRST STAGE HPT DUCT SEGMENTS WITH REVISED COATED AREAS.72-45-00V2500-A5,-D5
ENG-70-030210/07/947INFORMATION - ENGINE - PROVIDE NEW LONGER FAN CASE TO RAFT ATTACHING BOLTS71-51-00V2500-A1
ENG-70-030510/14/947INFORMATION - ENGINE - OIL - TO ANNOUNCE THE AVAILABILITY OF A NEW NO. 5 BEARING OIL TUBE ASSEMBLY79-22-00V2500-D5
ENG-70-030610/14/947INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A NEW LOOP CLAMP AT CLIPPING POINT CP254471-51-00V2500-D5
ENG-70-030712/03/937INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A NEW FAN BLADE ASSEMBLY THAT ELIMINATES UNNECESSARY MANUFACTURING FEATURES72-31-00V2500-A1
ENG-70-030810/22/938INFORMATION - ENGINE - FUEL AND CONTROL - TO ANNOUNCE THE AVAILABILITY OF A FUEL DIVERTER AND RETURN VALVE WITH CHROME PLATING ON THE PISTON ROD73-13-42V2500-A1,-A5,-D5
ENG-70-031103/11/947INFORMATION - ENGINE - HP COMPRESSOR - HPC BLADES STAGES 9, 10, 11, AND 12 QUANTITIES AMENDED72-41-15V2500-A1
NAC-70-031309/01/987INFORMATION - NACELLE - FAN COWL - TO INTRODUCE NEW FAN COWL LATCHES WITH IMPROVED AEROSMOOTHNESS FEATURES71-13-00V2500-A1
ENG-70-031406/20/947INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF EEC SENSE LINES THAT FEATURE PROTECTIVE SLEEVING73-22-49V2500-A5
ENG-70-031509/15/950110/19/997INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A NEW BRACKET AT CLIPPING POINT CP120071-00-00V2500-A5
ENG-70-031611/15/937INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A CORE COWL PANEL THAT ELIMINATES CADMIUM PLATED ATTACHING HARDWARE71-12-11V2500-D5
ENG-70-031706/20/947INFORMATION - ENGINE - REPLACE VARIOUS STANDARD PART NUMBER BOLTS WITH IAE PART NUMBER BOLTS71-00-00V2500-A5,-D5
ENG-70-031806/06/977INFORMATION - ANNOUNCEMENT OF TRANSFER OF ATA CHAPTER /FIG ITEM NUMBER OF CLIPPING BRACKET AND ATTACHING BOLTS72-50-00V2500-D5
ENG-70-031904/15/94See SBINFORMATION - ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - TO ANNOUNCE THE AVAILABILITY OF AN OPTIONAL GASKET FOR USE IN THE TURBINE CASE AND VANE ASSEMBLY72-45-00V2500-A1,-A5,-D5
ENG-70-032001/25/957INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A PART NUMBER ADJUSTING RING USED FOR OTHER MODELS72-00-50V2500-A1
ENG-70-032105/04/978INFORMATION - ENGINE - MAIN GEARBOX ASSEMBLY - TO ANNOUNCE THE AVAILABILITY OF REPAIR PARTS TO SUPPORT VARIOUS GEARBOX REPAIRS72-60-00V2500-A1
ENG-70-032209/06/968INFORMATION - ENGINE - HP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF PARTS TO SUPPORT REPAIR OF THE STAGE 3 VARIABLE VANE ACTUATING RING ASSEMBLY72-41-34V2500-A1
ENG-70-032303/30/957INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF A NEW LPC INLET GUIDE VANE ASSEMBLY WITH REVISED MOLDING MATERIAL72-32-00V2500-A5,-D5
ENG-70-032406/30/947INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF ALTERNATE CABLES FOR THE EEC FAN CASE HARNESS AND THE DOUBLE IGNITION SUPPLY HARNESS71-51-00V2500-A1,-A5
ENG-70-032506/30/947INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE NEW FAN SPEED AND TRIM BALANCE PROBESWITH REVISED SURFACE TREATMENT TO IMPROVE DURABILITY72-32-18V2500-A1,-A5,-D5
ENG-70-032701/20/957INFORMATION - ENGINE - PROVIDE A NEW NO. 1 BEARING OIL SUPPLY TUBE BRACKET ASSEMBLY DESIGNED TO ENSURE PROPER TUBE INSTALLATION72-32-00V2500-A1,-A5,-D5
NAC-70-032810/07/947NACELLE - INTRODUCE A NEW P2T2 FLEXIBLE HOSE ASSEMBLY TO EASE INSTALLATION PROCEDURE73-22-48V2500-A1,-A5
ENG-70-033111/15/967INFORMATION - ENGINE - HP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF A NEW STAGE 10 HPC REAR INNER TO OUTER CASE SEALING RING ASSEMBLY72-41-00V2500-A1,-A5,-D5
ENG-70-033206/21/967INFORMATION - ENGINE - TO INTRODUCE REDUCED SIZE CLIPS AT CLIPPING POINTS CP0302 AND CP0305.73-00-00V2500-A1,-A5
NAC-70-033310/07/947INFORMATION - NACELLE - THRUST REVERSER - TO INTRODUCE A NEW C-DUCT OPENING ACTUATOR HOSE CLAMP78-00-00V2500-A1,-A5
ENG-70-033402/17/978INFORMATION - ENGINE - TO ANNOUNCE AN ALTERNATE SOURCE FOR FUEL AND OIL TEMPERATURE THERMOCOUPLES24-21-00V2500-A5,-D5
ENG-70-033507/11/958INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A COMMON FUEL COOLED IDG OIL COOLER BETWEEN V2500-Al AND V2500-AS ENGINE MODELS24-21-00V2500-A1
ENG-70-033602/15/958INFORMATION - PROVIDE A NEW ELECTRONIC ENGINE CONTROL WITH SCN12B/N SOFTWARE AND FEATURING HARDWARE COMMON TO THE A573-22-34V2500-A1
ENG-70-033707/04/947INFORMATION - ENGINE - MAIN GEARBOX ASSEMBLY - TO ANNOUNCE THE AVAILABILITY OF A NEW ANGLE GEARBOX RADIAL GEAR SUPPORT ASSEMBLY72-60-00V2500-D5
ENG-70-033806/10/027INFORMATION - AIR - ACTIVE CLEARANCE CONTROL (ACC) INTRODUCTION OF FLIGHT TEST INSTRUMENTATION ACC FOR PRODUCTION ENGINES75-24-49V2500-A1,-A5,-D5
NAC-70-034306/30/957INFORMATION -NACELLE - HYDRAULICS - TO ANNOUNCE THE AVAILABILITY OF AN ALTERNATE HYDRAULIC PUMP ASSEMBLY29-11-51V2500-A5
NAC-70-034410/07/948INFORMATION - NACELLE - AIR INTAKE COWL - TO ANNOUNCE THE AVAILABILITY OF REPAIR PARTS FOR THE REPLACEMENT OF THE AFT BULKHEAD HEATSHIELD71-11-11V2500-A1
ENG-70-034706/23/940105/18/057INFORMATION - ENGINE - MAIN GEARBOX ASSEMBLY - TO ANNOUNCE THE AVAILABILITY OF NEW OIL SCAVENGE TUBE ASSEMBLIES79-22-48V2500-A5
ENG-70-034803/25/947INFORMATION - ENGINE - MAIN GEAR130X ASSEMBLY - TO ANNOUNCE THE AVAILABILITY OF A NEW MAIN OIL SCAVENGE PUMP SUCTION TUBE COLLAR79-21-00V2500-A1
ENG-70-035103/28/947INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF A NEW BIFURCATION BOX COVER ASSEMBLY THAT ALLOWS IMPROVED ACCESS TO THE THRUST REVERSER HINGE BEAM BRACKET ATTACHING PARTS72-38-27V2500-D5
ENG-70-035201/24/970201/24/977INFORMATION - ENGINE - TURBINE EXHAUST - TO ANNOUNCE THE AVAILABILITY OF NEW NO. 5 BEARING SCAVENGE AND PRESSURE TUBE ASSEMBLIES MADE OF REVISED MATERIAL AND WITH AN IMPROVED BRAZE MATERIAL72-50-53V2500-A1,-A5,-D5
ENG-70-035309/25/98See SBINFORMATION - ENGINE - HP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF VARIOUS PARTSTO SUPPORT HIGH COMPRESSOR REPAIRS72-41-00V2500-A1,-A5,-D5
NAC-70-035409/25/010101/28/027INFORMATION - NACELLE - TO INTRODUCE NEW BRACKETS - TRACK FAIRING INSTL.78-32-23V2500-D5
ENG-70-035512/15/95See SBINFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF REPAIR PARTS TO SUPPORT THE REPAIR OF FAN BLADE ASSEMBLIES72-31-11V2500-A1
NAC-70-035708/28/978INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF REPAIR PARTS FOR THE REPAIR OF THE LEFT AND RIGHT HAND FAN COWL DOOR OUTLET GRILLES71-00-00V2500-A1
ENG-70-035909/25/98See SBINFORMATION - ENGINE - HP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF PARTS TO PERMIT VARIOUS HP COMPRESSOR REPAIRS72-41-00V2500-A5,-D5
NAC-70-036203/22/027INFORMATION - NACELLE - TO INTRODUCE AN OPTIONAL EMM I.D.G. AND QAD ADAPTER KIT24-21-00V2500-A1,-A5
ENG-70-036305/01/957INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF AN LPC BLEED VALVE SCREEN WITH IMPROVED DURABILITY FEATURES72-32-00V2500-A5,-D5
ENG-70-036409/04/98See SBINFORMATION - ANNOUNCEMENT OF REPAIR PARTS TO SUPPORT REPAIR OF FUEL SYSTEM AIR TUBES70-00-00V2500-A1
ENG-70-036507/04/947INFORMATION - ENGINE - MAIN GEARBOX ASSEMBLY - TO ANNOUNCE THE AVAILABILITY OF AN OIL SCAVENGE PUMP DRIVE GEAR FEATURING A WIDER TOOTH FACE79-22-00V2500-A1,-A5
ENG-70-036710/12/940306/16/007INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF NEW FAN CASE EEC AND CORE IGNITION SUPPLY HARNESSES WITH REPLACEMENT BACKSHELLS, CABLE, AND BUSHES71-51-00V2500-A1,-A5
ENG-70-036809/06/960110/01/997INFORMATION - ENGINE - HP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF A NEW HPC REAR OUTER CASE ASSEMBLY THAT PROVIDES PARTS COMMONALITY BETWEEN THE V2500-Al AND V2500-A5 ENGINE MODELS72-41-00V2500-A1,-A5
NAC-70-036903/22/027INFORMATION - NACELLE - TO INTRODUCE A NEW ALIGNMENT PIN - LOWER TRACK INSTL.78-30-00V2500-A1,-A5
ENG-70-037003/10/977INFORMATION - POWERPLANT - TO ANNOUNCE THE AVAILABILITY OF A NEW GENERAL SERVICES HARNESS FEATURING A NEW BACKSHELL AT THE ANTI-ICE VALVE CONNECTOR LOCATION71-51-00V2500-A1
NAC-70-037003/10/977STANDARD PRACTICES - ENGINE - INFORMATION - POWERPLANT - TO ANNOUNCE THE AVAILABILITY OF A NEW GENERAL SERVICES HARNESS FEATURING A NEW BACKSHELL AT THE ANTI-ICE VALVE CONNECTOR LOCATION - CATEGORY CODE 7 - MOD.ENG-70-037071-51-43V2500-A1
ENG-70-037410/12/947INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A CORE EEC HARNESS WITH ALUMINUM BACKSHELLS AND STEEL COUPLINGS71-52-00V2500-A1,-A5
ENG-70-037502/15/957INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A NEW GEARBOX OIL SCAVENGE TUBE ASSEMBLY79-22-00V2500-A1,-A5
ENG-70-037609/22/978CANCELLATION OF ENGINE SERVICE BULLETIN V2500 ENG-70-0376 (INFORMATION - ENGINE - AIR SYSTEM - TO ANNOUNCE THE AVAILABILITY OF REPAIR PARTS USED TO SUPPORT THE REPAIR OF THE AIR COOLING DUCT)75-24-49V2500-A1,-A5,-D5
ENG-70-037709/22/957INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF NEW FAN EXIT GUIDE VANES WITH OUTER PLATFORMS OF REDUCED WEIGHT MATERIAL72-32-00V2500-A5,-D5
ENG-70-037809/06/967INFORMATION - ENGINE - HP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF A NEW VARIABLE STATOR VANE SYSTEM CRANK SHAFT72-41-00V2500-A1
ENG-70-037911/23/937INFORMATION - ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - TO ANNOUNCE THE AVAILABILITY OF A NEW FIRST STAGE TURBINE BLADE WITH IMPROVED DURABILITY FEATURES72-45-00V2500-A5,-D5
ENG-70-038006/16/957INFORMATION - ENGINE - OIL - TO ANNOUNCE THE AVAILABILITY OF A NEW NO. 4 SCAVENGE VALVE79-23-00V2500-A5,-D5
ENG-70-038103/28/967INFORMATION - ENGINE - LP COMPRESSOR - INTRODUCE A NEW WEIGHT REDUCED REAR FAIRING ASSEMBLY72-32-86V2500-A5,-D5
ENG-70-038201/27/957INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF A NEW 2.5 BLEED ARM LOCKNUT72-32-00V2500-A1
ENG-70-038301/20/957INFORMATION - ENGINE - LP COMPRESSOR - INTRODUCE A NEW 2.5 BLEED RING SUPPORT THAT ELIMINATES AN UNNECESSARY COATING MATERIAL72-32-00V2500-A5,-D5
ENG-70-038507/05/950110/01/01See SBINFORMATION - ENGINE - DIFFUSER AND COMBUSTION SECTION - TO ANNOUNCE THE AVAILABILITY OF ADDITIONAL CLASSES OF DIFFUSER CASE FUEL NOZZLE BOSS INSERTS72-42-00V2500-A1,-A5,-D5
ENG-70-038610/21/947INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF A NEW ANNULUSFILLER ASSEMBLY72-31-11V2500-A1
ENG-70-038701/25/957INFORMATION - ENGINE - LP TURBINE ROTOR AND STATOR ASSEMBLY - TO ANNOUNCE THE AVAILABITY OF A NEW LP TURBINE SHAFT SEAL ASSEMBLY72-50-00V2500-A1
ENG-70-038808/15/957INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF A NEW ANNULUSFILLER WITH REVISED RUBBER SEAL72-31-11V2500-A5,-D5
ENG-70-039007/15/957INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF NEW MATERIAL ADJUSTING WASHERS72-32-26V2500-A1,-A5,-D5
ENG-70-039112/13/968INFORMATION - ENGINE - STARTING - TO ANNOUNCE THE AVAILABILITY OF A STARTER WITH AN OIL SIGHT GLASS FEATURE80-13-41V2500-D5
ENG-70-039209/06/967INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF IAE IDENTIFIED BOLTS AND SCREWS75-00-00V2500-A1,-A5,-D5
ENG-70-039306/21/967INFORMATION - ENGINE - POWERPLANT - TO ANNOUNCE THE AVAILABILITY OF A NEW FIRE DETECTION HARNESS71-52-42V2500-A1
ENG-70-039409/25/98See SBINFORMATION - ENGINE - HP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF REPAIR PARTS TO SUPPORT REPAIR OF THE STAGE 6 VARIABLE VANES ACTUATING RING ASSEMBLY72-41-00V2500-A1
ENG-70-039507/24/988INFORMATION - STARTING - TO ANNOUNCE THE INTRODUCTION OF A NEW PNEUMATIC STARTER WITH ANOIL PRESSURE FILL FACILITY80-13-00V2500-A1,-A5
ENG-70-039808/15/957INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF A NEW NO. 4 BEARING SCAVENGE TUBE ASSEMBLY72-32-00V2500-D5
ENG-70-039908/25/958INFORMATION - ENGINE - INTRODUCE AN ALTERNATE SOURCE FOR THE MAIN OIL FILTER ELEMENT79-00-00V2500-A1,-A5,-D5
NAC-70-040208/13/967INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW THRUST REVERSER MOUNT BRACKET AND ATTACHING HARDWARE78-33-00V2500-D5
NAC-70-040405/02/950110/20/957INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF AN IMPROVED THERMAL ANTI ICE DUCT ASSEMBLY30-00-00V2500-D5
NAC-70-040508/13/957INFORMATION - NACELLE - TO ANNOUNCE THE DELETION OF UNUSED SHIMS IN THE NACELLE SUPPORT SYSTEM71-14-00V2500-D5
NAC-70-040601/23/037INFORMATION - NACELLE - TO INTRODUCE AN ALTERNATIVE FORWARD ENGINE MOUNT BOLT WITHOUT A DRILLED HEAD71-21-00V2500-A1,-A5
NAC-70-040708/13/967INFORMATION - NACELLE - TO ANNOUNCE A PART NUMBER CORRECTION TO A FIREWALL ASSEMBLY AND A RIGHT HAND INDICATOR71-00-00V2500-D5
NAC-70-040805/02/950107/15/967INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW VSCF CABLE SUPPORT BRACKET WASHER24-21-00V2500-D5
NAC-70-040908/13/967INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF NEW ATTACHING HARDWARE FOR THE VSCF MOUNTING BRACKET24-00-00V2500-D5
NAC-70-041012/03/960102/05/977INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF NEW WIRE HARNESS ASSEMBLIES FOR THE UPPER C-DUCT MODIFICATION78-30-00V2500-D5
ENG-70-041709/25/980103/12/99See SBINFORMATION - ENGINE - HP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF REPAIR PARTS FOR STAGES 4 AND 5 ACTUATING RING CONNECTORS72-41-00V2500-A5,-D5
ENG-70-041806/15/958INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE AN ALTERNATE SOURCE FOR THE NO. 2 BEARING72-32-52V2500-A5,-D5
ENG-70-041907/11/957INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF NEW LP COMPRESSOR REAR CASE FLANGE PLATE WASHERS72-32-00V2500-A5,-D5
NAC-70-042212/02/967INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF AN ALTERNATE ACAC (AFT) DUCT ASSEMBLY75-22-00V2500-D5
NAC-70-042304/20/957INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF PARTS TO SUPPORT THE REPAIR OF THE TAI RING71-11-11V2500-A1
NAC-70-042403/17/960112/04/987INFORMATION - NACELLE - COMMON NOZZLE ASSEMBLY - TO ANNOUNCE THE INTRODUCTION OF A NON-VECTORED COMMON NOZZLE ASSEMBLY78-11-00V2500-A1,-A5
NAC-70-042602/20/967INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW INLET COWL TA] BULKHEAD FITTING COUPLING NUT71-11-00V2500-D5
ENG-70-042701/29/960303/12/987INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABITY OF A NEW BIFURCATION PANEL SEAL ASSEMBLY72-38-00V2500-D5
ENG-70-042810/15/950110/16/067STANDARD PRACTICES - ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - TO ANNOUNCE THE AVAILABILITY OF NEW STAGE 2 HP TURBINE VANES72-45-24V2500-A5,-D5
ENG-70-042907/15/967INFORMATION - ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - TO ANNOUNCE THE AVAILABILITY OF A NEW STAGE 1 HP TURBINE ROTOR BLADE72-45-00V2500-A1
ENG-70-043107/05/957INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A SPARE FUEL NOZZLE BAFFLE TO PERMIT REPAIR OF THE FUEL NOZZLE AND SUPPORT ASSEMBLY73-13-00V2500-A1,-A5,-D5
ENG-70-043201/30/97See SBINFORMATION - ENGINE - DIFFUSER AND COMBUSTION - TO ANNOUNCE THE AVAILABILITY OF A REPLACEMENT NO. 4 BEARING COOLING TUBE HEATSHIELD72-42-00V2500-A1,-A5,-D5
ENG-70-043309/22/958INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF AN ALTERNATE FAN CASE NUT PLATE ATTACHING RIVET72-32-00V2500-A1,-A5,-D5
ENG-70-043407/24/988INFORMATION - ENGINE - AIR - TO ANNOUNCE THE AVAILABILITY OF PARTS FOR REPAIR OF THE ACC VALVE STATOR ROD ASSEMBLY75-24-00V2500-A1,-A5,-D5
ENG-70-043501/01/967INFORMATION - ENGINE - MAIN GEARBOX ASSEMBLY - TO ANNOUNCE THE AVAILABILITY OF A NEW DEOILER IMPELLOR ASSEMBLY72-60-00V2500-A1,-A5,-D5
ENG-70-043606/16/958INFORMATION - ENGINE - FUEL - TO ANNOUNCE THE AVAILABILITY OF AN ALTERNATE FUEL FILTER ELEMENT73-12-42V2500-A1,-A5,-D5
ENG-70-043707/05/95See SBINFORMATION - ENGINE - DIFFUSER CASE ASSEMBLY - TO ANNOUNCE THE AVAILABILITY OF REPLACEMENT SEALING SLEEVES FOR THE REPAIR OF DIFFUSER CASE SEALING SLEEVES72-42-11V2500-A1,-A5,-D5
NAC-70-043902/15/968INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF NEW ANTI-ICE, CABIN AIR, AND STARTER SYSTEM DUCT LINK BEARINGS30-00-00V2500-A1,-A5
ENG-70-044209/13/967INFORMATION - ENGINE - SCAVENGE OIL TUBES - INTRODUCTION OF NEW OIL TUBE ASSEMBLY WITH IMPROVED NUT RESTRAINING FEATURES79-22-00V2500-A1,-A5
NAC-70-044407/17/957INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A SHORTER AFT THRUST STRUT BOLT71-00-00V2500-D5
ENG-70-044501/30/967INFORMATION - ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - TO ANNOUNCE THE AVAILABILITY OF NEW STAGE 2 TURBINE VANES WITH IMPROVED AIRFOIL COATING72-45-24V2500-A1
ENG-70-044709/25/95See SBINFORMATION - ENGINE - MAIN GEARBOX ASSEMBLY - PROVIDE A SECOND SOURCE FOR THE SPHERICAL BEARINGS ON THE MAIN GEARBOX LINKS70-00-60V2500-A1,-A5,-D5
ENG-70-044811/13/98See SBINFORMATION - ENGINE - MAIN GEARBOX ASSEMBLY - TO ANNOUNCE THE AVAILABILITY OF VARIOUS CLASSES FOR THE OIL SCAVENGE PUMP DRIVEN GEARS79-22-41V2500-A1,-A5,-D5
ENG-70-044909/25/95See SBINFORMATION - ENGINE - MAIN GEARBOX ASSEMBLY - PROVIDE A SECOND SOURCE FOR ROLLER BEARINGS70-60-00V2500-D5
ENG-70-045009/26/967INFORMATION - ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - TO ANNOUNCE THE AVAILABILITY OF A NEW TURBINE CASE AND VANE ASSEMBLY72-45-00V2500-A1
ENG-70-045108/25/957INFORMATION - AIR - TO ANNOUNCE THE AVAILABILITY OF NEW ACAC INLETIOUTLET DUCT75-22-41V2500-D5
ENG-70-045208/15/950110/01/987INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF NEW PANEL LINERS WITH REVISED BUSHES72-32-00V2500-A1,-A5,-D5
ENG-70-045303/10/977INFORMATION - ENGINE - TO ANNOUNCE NEW HARNESS BRACKET AND HARNESS SUPPORT RACEWAY BOLTSAND TO ALTER THE QUANTITY OF A FUEL TUBE WASHER71-51-00V2500-A5
ENG-70-045411/13/98See SBINFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A REPAIR PART TO SUPPORT THE REPAIR OF THE MAIN OIL PUMP ASSEMBLY79-21-41V2500-A1
NAC-70-045511/26/967INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW VSCF CONTROL HARNESS ASSEMBLY24-21-00V2500-D5
ENG-70-045612/20/968INFORMATION - ENGINE - TO ANNOUNCE THE DELETION OF AN ELECTRONIC ENGINE CONTROL SUPPORT NUT OPTION SOURCE73-22-00V2500-D5
ENG-70-046009/20/957INFORMATION - LP COMPRESSOR - TO ANNOUNCE THE CATALOG SEQUENCE NUMBER CHANGE TO THESEALING RING OF THE PTO SHAFT SEALTUBE72-32-00V2500-A1,-A5,-D5
NAC-70-046108/23/957INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF IMPROVED UPPER STRUT ON FAN COWL HOLD OPEN RODS71-13-00V2500-D5
NAC-70-046209/15/957INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW BRACKET ASSEMBLY FOR FAN FIRE DETECTION SYSTEM26-00-00V2500-D5
NAC-70-046302/15/967INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF NEW FITTING ASSEMBLIES FOR THE UPPER AND LOWER C-DUCT71-14-00V2500-D5
ENG-70-046512/04/957INFORMATION - ENGINE - MAIN GEARBOX ASSEMBLY - TO PROVIDE INFORMATION ON AN EARLIER STANDARD OF MAIN OIL SCAVENGE PUMP ASSEMBLY THAT WAS FITTED ON DELIVERED ENGINES79-22-00V2500-D5
ENG-70-046610/25/95See SBENGINE - MAIN GEARBOX ASSEMBLY - PROVIDE A SECOND SOURCE FOR CARBON SEALS72-60-00V2500-D5
NAC-70-046812/20/950504/06/007INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF NEW CABIN AIR SENSE LINES WITH SILVER PLATED NUTS36-00-00V2500-A1,-A5
NAC-70-046903/20/967INFORMATION - NACELLE - ICE AND RAIN PROTECTION - TO ANNOUNCE THE AVAILABILITY OF A NEW ANTI-ICE REGULATOR VALVE30-00-00V2500-D5
ENG-70-047012/15/957INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A NEW 2.5 BLEED VALVE RING72-32-00V2500-A5,-D5
NAC-70-047211/26/967INFORMATION - NACELLE - ELCTRICAL POWER, HYDRAULIC POWER - TO ANNOUNCE THE AVAILABILITY OF NEW WEIGHT-REDUCED FAN CASE BRACKETS24-21-00V2500-D5
NAC-70-047407/02/977INFORMATION - NACELLE - PNEUMATIC - TO ANNOUNCE THE AVAILABILITY OF A NEW FAN AIRVALVE SUPPORT FLANGE AND A NEW ELBOW DUCT ASSEMBLY36-00-00V2500-D5
NAC-70-047611/30/957INFOMATION - NACELLE - PNEUMATIC - TO ANNOUNCE THE AVAILABILITY OF A NEW PRESSURE INDICATING TUBE ASSEMBLY36-21-49V2500-A5
ENG-70-047703/08/967INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF THE NEW FAN CASE LINER PANEL ASSEMBLIES WITH IMPROVED IMPACT STRENGTH72-32-87V2500-A1
ENG-70-047808/23/967INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A NEW FIRST STAGE HPT OUTER AIRSEAL GASKET72-45-00V2500-A5,-D5
ENG-70-047909/20/968INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A NEW FUEL MANIFOLD BRACKET NUTPLATE72-40-00V2500-D5
ENG-70-048009/26/967INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A NEW TURBINE EXHAUST CASE ASSEMBLY72-50-00V2500-A1,-A5
ENG-70-048212/12/97See SBINFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAIL ABILITY OF REPAIR PARTS TO SUPPORT THE REPAIR OF FAN FRAME ASSEMBLIES72-32-00V2500-D5
ENG-70-048312/27/96See SBINFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE CHANGES IN SPAREABILITY CODES72-32-41V2500-A1,-A5,-D5
ENG-70-048412/16/960304/03/098INFORMATION - ENGINE - TO INTRODUCE A NEW INLET CONE ASSEMBLY72-38-00V2500-A1,-A5,-D5
ENG-70-048602/10/977TO ANNOUNCE NEW ATTACHING BOLTS FOR FANCASE BRACKET71-52-00V2500-A5
ENG-70-048709/16/960104/07/097INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A NEW CORE SERVICE AND FIRE DETECTION HARNESS71-52-00V2500-A5
ENG-70-048812/20/967INFORMATION - ENGINE - TO INTRODUCE A NEW LP TURBINE SHAFT72-50-00V2500-A5,-D5
ENG-70-048901/09/978INFORMATION - ENGINE - TO INTRODUCE AN ALTERNATIVE ANCHOR NUT FOR THE FAN FRAME72-32-00V2500-A1,-A5,-D5
ENG-70-049001/10/978INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF AN ALTERNATIVE FRONT MOUNT TUBE ASSEMBLY71-21-11V2500-A1,-A5
ENG-70-049101/09/977INFORMATION - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF A NEW LPC BLEED LINK WITH IMPROVED SPHERICAL BEARING STAKING72-32-71V2500-A1
ENG-70-049212/20/967INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE NEW REPAIR ONLY PART FOR THE FAN CASE ASSEMBLY72-32-85V2500-A1,-A5,-D5
ENG-70-049301/09/977INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A NEW SELF PLUGGED BLIND RIVET72-32-85V2500-D5
ENG-70-049404/21/977INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF A NEW BIFURCATION BOX AND COVER72-38-00V2500-D5
NAC-70-049511/04/967INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW THRUST REVERSER LATCH ACCESS DOOR78-32-00V2500-D5
NAC-70-049611/04/967INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF NEW POWER PLANT FANCOWL SUPPORT BRACKETS71-00-00V2500-D5
NAC-70-049711/04/967INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF IMPROVED FAN COWL DAMPERS71-13-00V2500-D5
NAC-70-049911/04/967INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW FAN COWL DOOR HOLD OPEN ROD STRUT71-13-00V2500-D5
ENG-70-050008/11/987INFORMATION - ENGINE - TO ANNOUNCE A TRANSFER OF CORE ENGINE FAIRING PANELS FROM PARTS OF SPARABLE ENGINE TO PARTS OF DEMOUNTABLE POWER PLANT70-00-00V2500-D5
ENG-70-050103/07/97See SBINFORMATION - ENGINE - TURBINE EXHAUST CASE ASSEMBLY - TO ANNOUNCE THE AVAILABILITY OF OVERSIZE BUSHINGS FOR THE TURBINE EXHAUST CASE MOUNT AND GROUND HANDLING LUGS72-50-53V2500-A1,-A5
ENG-70-050202/14/977INFORMATION - ENGINE - HP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF A NEW STAGE 10 HPC REAR INNER TO OUTER CASE SEALING RING ASSEMBLY72-41-21V2500-A1,-A5,-D5
ENG-70-050301/10/977INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A NEW OIL JET ASSEMBLY72-32-00V2500-A1,-A5,-D5
ENG-70-050401/27/977INFORMATION - ENGINE - LP TURBINE ROTOR AND STATOR ASSEMBLY - INTRODUCE NEW SEAL STRIPS AT THE LP TURBINE DIFFUSER SEGMENTS72-50-00V2500-A1,-A5,-D5
ENG-70-050502/21/977INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A NEW INLET CONE ATTACHING BOLT72-38-11V2500-A1,-A5,-D5
NAC-70-050702/11/977INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF NEW DOOR ASSEMBLIES ON THE FAN COWL71-13-00V2500-D5
NAC-70-050802/14/977INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW BRACKET AT THE C-DUCT NO.1 LATCH POSITION78-32-00V2500-D5
NAC-70-050902/14/977INFORMATION - TO ANNOUNCE THE AVAILABILITY OF AN ALTERNATIVE BEARING ASSEMBLY FOR THE NO. 4 HINGE BEAM ASSEMBLY71-11-00V2500-D5
NAC-70-051002/11/977INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW FAN COWL DOOR HOLD OPEN ROD STRUT71-13-00V2500-D5
ENG-70-051112/12/97See SBINFORMATION - ENGINE LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF REPAIR PART TO SUPPORT THE REPAIR OF REAR FAIRING ASSEMBLIES72-32-86V2500-A1
ENG-70-051201/30/977INFORMATION - ENGINE - LP TURBINE ROTOR AND STATOR ASSEMBLY - INTRODUCTION OF LP TURBINE VANE STAGE 4 CAST CLUSTER72-50-00V2500-A1,-A5,-D5
ENG-70-051301/30/977INFORMATION - ENGINE - LP TURBINE ROTOR AND STATOR ASSEMBLY - INTRODUCTION OF LPTURBINE VANE STAGE 3 CAST CLUSTER72-50-22V2500-A1,-A5,-D5
ENG-70-051401/30/970103/03/977INFORMATION - ENGINE - LP TURBINE ROTOR AND STATOR ASSEMBLY - RE-INTRODUCTION OF LP TURBINE VANE STAGE 4 BRAZED CLUSTER72-50-00V2500-A1,-A5,-D5
NAC-70-051502/27/977INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF NEW COMMON NOZZLE ASSEMBLY SEAL ASSEMBLIES AND REPAIR PARTS78-11-00V2500-A1
NAC-70-051602/14/977INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW "Y" DUCT ASSEMBLY36-00-00V2500-D5
NAC-70-051702/11/977INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW THRUST REVERSER HOLD OPENROD78-32-00V2500-D5
NAC-70-051805/16/977INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW THRUST REVERSER ACTUATOR FAIRING78-00-00V2500-D5
ENG-70-051909/22/970107/19/997INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A NEW LP TURBINE CASE MADE OUT OF ONE FORGING PIECE72-50-00V2500-A1,-A5,-D5
ENG-70-052002/14/970209/23/037INFORMATION - ENGINE - LP TURBINE - TO ANNOUNCE THE AVAILABILITY OF AN IMPROVED STAGE 3, 5 AND 7 TURBINE DISK AND STAGE 4 AND 5 TURBINE AIR SEAL INTO V2500 D5 ENGINE FOR COMMONALITY72-50-00V2500-D5
ENG-70-052102/14/977INFORMATION - ENGINE - LP TURBINE - TO ANNOUNCE THE AVAILABILITY OF AN IMPROVED TURBINE DISK STG 7 IN D5 ENGINE FOR COMMONALITY72-50-00V2500-D5
ENG-70-052204/30/970709/03/107INFORMATION - ENGINE - LP TURBINE - TO ANNOUNCE THE AVAILABILITY OF IMPROVED STAGE 3, 5, 7 TURBINE DISKS AND AIRSEALS STAGE 4 AND 572-50-00V2500-A1,-A5
ENG-70-052311/25/977INFORMATION - ENGINE - LP TURBINE ROTOR AND STATOR ASSEMBLY - RE-INTRODUCTION OF LP TURBINE VANE STAGE 4 CAST CLUSTER72-50-00V2500-A1,-A5,-D5
ENG-70-052403/10/008INFORMATION - AIR - TO ANNOUNCE THE AVAILABILITY OF AN A1 TITANIUM DUCT ASSY; COOLING FOR LIMITED USAGE IN V2500 A5/D5 APPLICATIONS75-24-00V2500-A5,-D5
ENG-70-052508/31/980201/22/047INFORMATION - LP TURBINE ROTOR AND STATOR ASSEMBLY - TO ANNOUNCE THE AVAILABILITY OF A NEW DIFFUSOR OUTER SEGMENT72-50-00V2500-A5,-D5
ENG-70-052604/04/977INFORMATION - ANNOUNCEMENT OF TRANSFER OF ATA CHAPTER/FIGURE ITEM NUMBER OF MAGNETIC CHIP DETECTORS79-22-45V2500-D5
NAC-70-052702/26/970105/06/977INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW THRUST REVERSER NO. 1 LATCH OPEN INDICATOR ASSEMBLY78-00-00V2500-D5
NAC-70-052802/26/977INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW VSCF GENERATOR POWER FEEDER HARNESS24-00-00V2500-D5
ENG-70-053503/07/97See SBINFORMATION - ENGINE - TURBINE EXHAUST CASE ASSEMBLY - TO ANNOUNCE THE AVAILABILITY OF OVERSIZE BUSHINGS FOR THE TURBINE EXHAUST CASE MOUNT AND GROUND HANDLING LUGS72-50-53V2500-D5
ENG-70-053604/18/970212/08/047INFORMATION-ANNOUNCEMENT OF ALTERNATIVE SPACERS71-00-00V2500-A5,-D5
NAC-70-053705/19/977INFORMATION - NACELLE - INTERPHONE HARNESS - INTRODUCTION OF NEW CLIPPING POINT BOLTS23-44-41V2500-A5
ENG-70-053805/19/977INFORMATION - ENGINE - HYDRAULIC SYSTEM - TO ANNOUNCE THE AVAILABILITY OF A SPAREABLE " O" RING SEAL AND HYDRAULIC UNIONS ,29-11-49V2500-A1,-A5
NAC-70-053905/02/977INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW ANCHORAGE BRACKET FOR THE FAN COWL STRUTS71-13-00V2500-A1,-A5
NAC-70-054007/14/977INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF NEW COMMON NOZZLE ASSEMBLIES (CNA) AND VARIOUS FASTENERS ON THE CNA78-11-00V2500-A1
NAC-70-054105/15/980202/06/987INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW EXHAUST PLUG ASSEMBLY78-32-00V2500-A1
NAC-70-054302/17/987INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW THRUST REVERSER AUXILIARY LATCH ASSEMBLY73-00-00V2500-D5
NAC-70-054407/23/977NOSE COWL P2T2 PIPE ASSEMBLY CLIP REPLACEMENT73-00-00V2500-D5
NAC-70-054507/02/977INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A COMMON NOZZLE ASSEMBLY (CNA) WITH A REINFORCED PEN NIB FAIRING78-11-00V2500-D5
NAC-70-054609/23/970104/14/987INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF U-PLEX SEALS FOR THE ENGINE BUILD-UP UNIT (EBU)30-00-00V2500-D5
NAC-70-055110/03/977INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW VSCF GENERATOR24-00-00V2500-D5
NAC-70-055210/06/977INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW 7TH STAGE ELBOW DUCT ASSEMBLY36-00-00V2500-D5
NAC-70-055310/13/977INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF AN ALTERNATE BOLT FOR THE FORWARD ENGINE MOUNT ASSEMBLY71-00-00V2500-A1,-A5
NAC-70-055510/24/977INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW DEFLECTOR ASSEMBLY26-00-00V2500-D5
NAC-70-055610/27/970103/16/987INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF NEW BUSHING PART NUMBERS30-00-00V2500-D5
NAC-70-055711/10/977INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF NEW INNER CORE COWL BLANKING PANELS71-00-00V2500-D5
ENG-70-055805/22/97See SBINFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF REPAIR PARTS TO SUPPORT THE REPAIR OF FAN FRAME ASSEMBLIES72-32-00V2500-A1
ENG-70-055912/01/977INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A NEW INNER CORE COWL PANEL71-12-11V2500-D5
ENG-70-056011/14/97See SBINFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE SPAREABILITY OF A BUSHINGS FOR THE LP COMPRESSOR STAGE 1.5, 2.0 AND 2.5 DISK ASSEMBLY72-32-81V2500-A1,-A5,-D5
ENG-70-056111/07/978INFORMATION - ANNOUNCEMENTOF ALTERNATIVE ALUMINIUM BACKSHELLS71-00-00V2500-D5
ENG-70-056211/07/977INFORMATION - ANNOUNCEMENT OF REVISED WASHER CONFIGURATION TO INCREASE THE CLEARANCE ON THE BEND RADIUS OF THE HARNESS SUPPORT BRACKET OF THE VSCF GENERATOR75-32-51V2500-D5
ENG-70-056307/14/987INFORMATION - AIR - TO ANNOUNCE THE AVAILABILITY OF NEW ACTIVE CLEARANCE CONTROL (ACC) SUPPORTS AND CLAMPS IN X10 MATERIAL75-24-00V2500-A1,-A5,-D5
ENG-70-056410/27/978INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE NEW REPAIR ONLY PART FOR BIFURCATION BOX AND COVER72-38-27V2500-D5
ENG-70-056507/30/97See SBINFORMATION - ENGINE - TURBINE EXHAUST CASE ASSEMBLY - PROVIDE BUSHINGS AND BOLTS TOREPLACE THE PARTS PREVIOUSLY AVAILABLE FROM THE ORIGINAL MANUFACTURER OF THE TURBINE EXHAUST CASE ASSEMBLY72-50-00V2500-A1
ENG-70-056610/31/977INFORMATION - ANNOUNCEMENT OF ALTERNATIVE VEE-CLAMPS75-22-00V2500-D5
ENG-70-056711/07/977INFORMATION - ANNOUNCEMENT OF ALTERNATIVE FLEXIBLE TUBE ASSEMBLIES24-00-00V2500-A1,-A5,-D5
ENG-70-056810/10/977INFORMATION - INTRODUCTION OF ALTERNATIVE TITANIUM BRACKETS71-00-00V2500-A1,-A5
ENG-70-056907/11/970305/25/057INFORMATION - AIR - TO ANNOUNCE THE AVAILABILITY OF NEW ACTIVE CLEARANCE CONTROL (ACC) A] R DUCT IN X10 MATERIAL75-24-49V2500-A1,-A5,-D5
ENG-70-057008/25/97See SBINFORMATION - ENGINE- OUTER COMBUSTION CHAMBER ASSEMBLY - TO ANNOUNCE THE AVAILABILITY OF THE LATEST COMBUSTION CHAMBER LINER SEGMENTS72-42-61V2500-A1
ENG-70-057110/10/977INFORMATION - ANNOUNCEMENT OF AVAILABILITY OF ALTERNATIVE AIR MOISTURE TRAPS73-22-49V2500-A1,-A5
ENG-70-057210/31/977INFORMATION - ANNOUNCEMENT OF AVAILABILITY OF ALTERNATIVE ELECTRICAL INSULATION TAPES71-51-41V2500-A1,-A5
ENG-70-057311/21/970203/05/997INFORMATION - INTRODUCTION OF ALTERNATIVE TCA PIPE BRACKETS73-13-00V2500-A1,-A5
ENG-70-057412/19/970103/05/997INFORMATION - INTRODUCTION OF ALTERNATIVE ACC AND ACAC MOUNT BRACKETS72-00-00V2500-A1,-A5
ENG-70-057510/17/977INFORMATION - INTRODUCTION OF ALTERNATIVE ACC MOUNT BRACKETS AND CONTROL LINKS72-40-00V2500-D5
ENG-70-057609/15/97See SBPROVIDE NEW CUBIC BORON NITRIDE (CBN) TIP HPT BLADES72-45-00V2500-A1
ENG-70-057712/16/977INFORMATION - ENGINE - LP COMPRESSOR - INTRODUCTION OF NEW REAR FAIRING ASSEMBLY72-32-00V2500-A5,-D5
ENG-70-057808/06/997INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF REPAIR PART TO SUPPORT THE REPAIR OF FAN EXIT GUIDE FRAME.72-32-00V2500-A1,-A5,-D5
ENG-70-057912/19/97See SBINFORMATION - DELETION OF DUPLICATE PARTS INSTALLED IN THE VSCF GENERATOR BY THE VENDOR24-21-25V2500-D5
ENG-70-058001/30/987INFORMATION - ENGINE - MAIN GEARBOX ASSEMBLY TO IMPROVE A MICROCASTING OIL DISTRIBTORON D5 MODEL79-21-00V2500-D5
ENG-70-058112/19/97See SBINFORMATION - ENGINE - MAIN GEARBOX ASSEMBLY SIGHT GLASS SECOND SOURCE (SHAW AEROSUPPLIER)79-41-11V2500-A1,-A5,-D5
ENG-70-058201/30/98See SBINFORMATION - ENGINE - MAIN GEARBOX ASSEMBLY - CORRECTION OF PARTS CATALOG72-60-00V2500-A5,-D5
ENG-70-058303/18/987INFORMATION - ENGINE - LP TURBINE ROTOR AND STATOR ASSEMBLY - TO ANNOUNCE AVAILABILITY OFNEW STAGE 5 AND 7 BLADES72-50-32V2500-A1,-A5,-D5
ENG-70-058407/24/984INFORMATION - DELETION OF REDUNDANT SUPPORT BRACKETS FROM THE COMBUSTION OUTER CASE72-40-00V2500-D5
ENG-70-058512/19/976INFORMATION - ENGINE - MAIN GEARBOX ASSEMBLY - GEAR ASSEMBLY DRIVE - PMA INFORMATION72-60-33V2500-A1,-A5,-D5
NAC-70-059401/23/987INFORMATION - NACELLE - TO ANNOUNCE TRANSFER OF THE ATTACHING PARTS FOR THE INNERCORE COWL PANELS FROM PARTS OF THE SPAREABLE ENGINE TO PARTS OF THE BUILD-UP UNIT71-00-00V2500-D5
NAC-70-059502/05/987INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW APRON ASSY71-00-00V2500-D5
NAC-70-059602/09/987INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW APRON ASSY71-00-00V2500-D5
NAC-70-059702/11/987INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW FANCASE BRACKET ASSY71-00-00V2500-D5
NAC-70-059802/18/987INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW SEAL ASSY71-00-00V2500-D5
NAC-70-059902/23/987INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW FAN CASE BRACKET ASSY. SHIMMING.71-00-00V2500-D5
NAC-70-060002/24/987INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW PEEL SHIM TO ELIMINATE ANUNDESIREABLE GAP BETWEEN THE PIN AND LATCH HOUSING ON THE THRUST REVERSER71-00-00V2500-D5
ENG-70-060112/19/977INFORMATION - ENGINE - LP COMPRESSOR - COMMON USE OF REPAIR ONLY PART FOR FAN CASE ATTRITION LINING72-32-85V2500-A1
ENG-70-060201/30/987INFORMATION - ENGINE - MAIN GEARBOX ASSEMBLY - PROVIDE THE MICROCASTING PMA SUPPORT72-60-33V2500-D5
ENG-70-060301/30/987INFORMATION - ENGINE - MAIN GEARBOX ASSEMBLY - IDENTIFICATION MARKINGS ON OIL SCAVENGE PUMP79-22-41V2500-A1,-A5,-D5
ENG-70-060401/09/98See SBINFORMATION - TO ANNOUNCE ALTERNATIVE P2 LINE and IGNITION BOX COOLING HOSES73-00-00V2500-A1,-A5
ENG-70-060510/19/980101/08/007INFORMATION - ENGINE - TO DELETE THE TRIM BALANCE SLOT OF THE LP TURBINE SHAFT72-50-00V2500-A5,-D5
ENG-70-060603/13/98See SBINFORMATION - ENGINE - MAIN GEARBOX ASSEMBLY - GEAR ASSY DRIVE PMA FOR SPARES72-60-33V2500-A1,-A5,-D5
NAC-70-060702/27/987INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW FAN COWL ACCESS DOOR ASSEMBLIES71-00-00V2500-D5
NAC-70-060803/10/980103/18/987INFORMATION - NACELLE - TO INTRODUCE PART NUMBERS NECESSARY TO REPAIR DAMAGED BIFURCATIONFAIRINGS ON THE CNA. REPAIR SCHEME VRS264171-11-11V2500-D5
NAC-70-060903/11/987INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW TAI INLET AND P2T2 PROBE ACCESS PANELS71-11-01V2500-D5
NAC-70-061009/29/987INFORMATION - NACELLE - TO ANNOUNCE THE CHANGE OF NUTPLATE PART NUMBERS IN THE SUPPORT ASSY CAN INNER ANNULUS (A1) AND THE SUPPORT ASSY CONE (A5)78-11-00V2500-A1,-A5
NAC-70-061107/22/987TO ANNOUNCE THE AVAILABILITY OF A NEW LH AND RH UPPER C-DUCT T/R HARNESS AND OVERHEAT SENSOR CHANNEL B HARNESS71-00-00V2500-D5
NAC-70-061408/12/987INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF HEATSHIELDS FOR THE PRESSURE REGULATING VALVE AND THE HIGH PRESSURE BLEED VALVE71-00-00V2500-A5
NAC-70-061509/04/987INFORMATION - NACELLE - TO REINTRODUCE THE ATTACHING HARDWARE UNIONS USED ON THE VSCF GENERATOR24-21-25V2500-D5
NAC-70-061609/21/987INFORMATION - NACELLE - TO ANNOUNCE THE REPLACEMENT OF HOUSING ASSY - SUPPORT FOR THE ACAC DUCT ASSY75-00-00V2500-A1,-A5
NAC-70-061910/20/980112/15/997INFORMATION - NACELLE - TO ANNOUNCE A CORRECTION TO THE IP BLEED VALVE PART NUMBER36-00-00V2500-A1,-A5
NAC-70-062010/20/987INFORMATION - NACELLE - TO ANNOUNCE THE CHANGE TO THE HIGH PRESSURE BLEED VALVE (HPBV) PART NUMBERS36-00-00V2500-A5
NAC-70-062103/24/980107/09/987INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF NEW FAN COWL DOORS AND ACCESS PANELS71-00-00V2500-A1
ENG-70-062206/30/027ENGINE - LP COMPRESSOR - ANNOUNCEMENT OF THE ENGINE IDENTIFICATION PLATE WITH NEW IAE LOGO72-32-00V2500-A1,-A5,-D5
ENG-70-062308/15/077INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A FAIRLEAD BRACKET PACKING PIECE29-11-49V2500-A5
NAC-70-062503/10/997INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF NEW PART NUMBERS FOR THE P2T2 BONDING LEADS71-00-00V2500-A1
NAC-70-062604/08/997INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW STANDARD OF V2500-Al INLET COWL AND SPAREABLE DETAILS71-00-00V2500-A1
NAC-70-062709/13/99See SBINFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF ALTERNATIVE CLAMPS FOR THE GENERAL SERVICES HARNESS AND IGNITION SUPPLY HARNESS71-00-00V2500-A1,-A5
ENG-70-062809/26/007INFORMATION - ENGINE - TO ANNOUNCE CHANGES TO THE MAGNETIC CHIP DETECTOR PARTS CALLED UP IN THE IPC71-00-00V2500-A1,-A5
ENG-70-063009/13/99See SBINFORMATION - ENGINE - HYDRAULIC POWER AND FUEL TUBES - TO ANNOUNCE THE AVAILABILITY OF ALTERNATIVE UNIONS29-00-00V2500-A1,-A5
ENG-70-063112/18/980306/30/107INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF A NEW RUBBER SEAL OF LPC BLEED DUCT ASSEMBLY72-32-00V2500-A5,-D5
ENG-70-063210/01/98See SBINFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF REPAIR PARTS TO SUPPORT THE REPAIR OF FAN FRAME ASSEMBLIES72-32-00V2500-D5
ENG-70-063307/09/997INFORMATION - ENGINE - LP TURBINE ROTOR AND STARTER ASSEMBLY - TO ANNOUNCE THE RELEASE OF V2500 A5/D5 INNER AIR SEALS STAGE 5 AND 6 FOR V2500 A1 SPARES72-50-00V2500-A1
ENG-70-063407/14/980107/01/998INFORMATION - ENGINE - LP TURBINE ROTOR AND STATOR ASSEMBLY - TO ANNOUNCE THE AVAILABILITY OF A NEW INNER TRANSITION DUCT WITHOUT SHEET METAL SEAL RIM72-50-00V2500-A1,-A5,-D5
ENG-70-063605/08/980108/07/987INFORMATION - ENGINE - MAIN GEARBOX ASSEMBLY - DELETION OF THE PULLER PINS72-60-00V2500-A1,-A5,-D5
ENG-70-063709/18/98See SBINFORMATION - ANNOUNCEMENT OF ALTERNATIVE LACING TIES, CLIP DATUMS AND SUPPORT BUSHES71-51-00V2500-D5
ENG-70-063806/26/980203/15/04See SBINFORMATION - INTRODUCTION OF ALTERNATIVE SPAREABLE PART NUMBERS FOR BULK STOCK ITEMS71-51-00V2500-A1,-A5,-D5
ENG-70-063908/24/99See SBINFORMATION - ANNOUNCEMENT OF MINOR CHANGES TO THE ENGINE ILLUSTRATED PARTS CATALOG71-51-00V2500-D5
ENG-70-064001/29/997INFORMATION - ENGINE - LP TURBINE ROTOR AND STATOR ASSEMBLY - TO ANNOUNCE THE AVAILABILITY OF NEW TURBINE VANES STAGE 6 AND 772-50-00V2500-A1,-A5,-D5
ENG-70-064106/26/98See SBINFORMATION - ANNOUNCEMENT OF STANDARD PARTS TO EQUIVALENT IAE PART NUMBERS24-00-00V2500-D5
ENG-70-064209/04/980103/19/997INFORMATION - ANNOUNCEMENT OF ALTERNATIVE HARNESS LACING TIES, CLIP DATUMS AND SUPPORTBUSHES71-51-00V2500-A1,-A5
ENG-70-064307/17/98See SBINFORMATION - MAIN GEARBOX ASSEMBLY - TO ANNOUNCE THE INTRODUCTION OF A GEARBOX LINK-PIN COMMON TO A1 ENGINES72-00-00V2500-A5
ENG-70-064405/31/997INFORMATION - ENGINE - LP TURBINE ROTOR AND STATOR ASSEMBLY - TO ANNOUNCE THE AVAILABILITY OF A NEW LP TURBINE DISK STAGE 4,6 AND 7 FOR Al ENGINE MODEL APPLICATION72-50-00V2500-A1
ENG-70-064509/18/98See SBINFORMATION - ANNOUNCEMENT OF PARTS FOR REPAIR OF HP COMPRESSOR STAGE-7, STAGE 9 AND STAGE 10 HEATSHIELD ASSEMBLIES72-41-00V2500-A1,-A5,-D5
NAC-70-064905/10/00See SBINFORMATION - NACELLE - ADDITION OF SPAREABLE DETAILS - FOR THE FORWARD ENGINE MOUNT ASSEMBLY71-21-12V2500-A1,-A5
NAC-70-065105/10/007INFORMATION - NACELLE - ANNOUNCEMENT OF A NEW ACAC EXHAUST DUCT SEAL75-22-48V2500-A1,-A5
NAC-70-065901/27/997INFORMATION - NACELLE - ANNOUNCEMENT OF NEW ECS CHECK VALVE36-11-10V2500-D5
ENG-70-066308/24/01See SBINFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF ALTERNATIVE ELECTRICAL CONNECTORS FOR THE GENERAL SERVICES HARNESS71-00-00V2500-A1,-A5
NAC-70-066408/18/997NACELLE - TO ANNOUNCE THE AVAILABILITY OF NEW CONNECTORS AND BACKSHELLS FOR THE ACCESSORY ZONE FIRE DETECTORS71-00-00V2500-A1,-A5
NAC-70-066807/31/00See SBINFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW RAFT ASSEMBLY71-00-00V2500-A5
NAC-70-066901/20/007INFORMATION -NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW DRAINS COLLECTOR PLATE ASSEMBLY71-00-00V2500-A5
ENG-70-067005/18/047INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF ALTERNATIVE SEALS FOR THE ANTI-ICE DUCT, PNEUMATIC-BLEED AIR DUCT AND STARTER DUCT.30-00-00V2500-A1,-A5
NAC-70-067102/19/027INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW GEARBOX BREATHER MAST71-00-00V2500-A1,-A5
NAC-70-067904/06/097INFORMATION - NACELLE - ANNOUNCEMENT OF THE AVAILABLILITY OF THE NEW LOCKING ACTUATOR PROXIMITY SWITCH ASSEMBLY78-30-00V2500-A5,-D5
NAC-70-068209/02/997INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF NEW 45 DEGREE BACKSHELLS USED ON THE UPPER AND LOWER C-DUCT ELECTRICAL HARNESSES78-33-12V2500-D5
NAC-70-068808/08/017INFORMATION - NACELLE - ANNOUNCEMENT OF A NEW TRACK LINERS - UPPER TRACK INSTALLATION.78-30-00V2500-A1,-A5
NAC-70-069004/13/017INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF NEW FANCASE BRACKET ASSEMBLIES71-00-24V2500-D5
NAC-70-069201/24/017INFORMATION - NACELLE - ANNOUNCEMENT OF NEW TRACK LINERS78-32-23V2500-D5
NAC-70-069301/24/010104/12/017INFORMATION - NACELLE - ANNOUNCEMENT OF NEW HOLD OPEN ROD PIN78-35-13V2500-D5
NAC-70-069402/14/027CANCELLATION OF INFORMATION - NACELLE - TO INTRODUCE ALTERNATE EQUIVALENT PARTS78-31-17V2500-D5
NAC-70-069501/24/017INFORMATION - NACELLE - ANNOUNCEMENT OF A NEW SHOULDERED BUSH - FAN COWL71-13-03V2500-D5
NAC-70-069611/11/007INFORMATION - NACELLE - ANNOUNCEMENT OF A NEW BEARING LINK36-11-49V2500-A1,-A5
NAC-70-069701/24/017INFORMATION - NACELLE - ANNOUCEMENT OF A NEW HINGE BODY AND PIN - BLOW-OUT DOOR, FAN COWL71-13-00V2500-D5
ENG-70-070108/28/98See SBINFORMATION - INTRODUCTION OF ALTERNATIVE RIGGING PIN BRACKETS FOR THE HP COMPRESSOR VIGV/VSV"S72-41-34V2500-A5,-D5
ENG-70-070210/24/01See SBENGINE- RESTRUCTURE THE FRONT AND REAR NUMBER FOUR BEARING SEAL ASSEMBLIES AND DETAILS72-00-00V2500-A1,-A5,-D5
NAC-70-070311/16/988INFORMATION - NACELLE - NEW REPAIR ONLY PARTS FOR INNER CORE COWL PANEL71-12-00V2500-D5
ENG-70-070408/31/98See SBINFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF REPAIR PARTS TO SUPPORT THE REPAIR OF BOOSTER STAGE BLEED VALVE AND ACTUATING MECHANISM72-32-00V2500-A1
ENG-70-070507/01/990102/11/008INFORMATION ENGINE - LP TURBINE ROTOR AND STARTER ASSEMBLY - TO ANNOUNCE THE AVAILABILITY OF NEW LP TURBINE DISK 3 AND 7 WITH ROUND STRESS RELIEF HOLES72-50-00V2500-A1,-A5,-D5
ENG-70-070607/02/990203/21/027INFORMATION - INTRODUCTION OF THE ALTERNATIVE FAN FRAME ASSEMBLY73-32-00V2500-A1,-A5
ENG-70-070704/15/990112/05/057INFORMATION - ENGINE - LP TURBINE ROTOR AND STATOR ASSEMBLY - TO ANNOUNCE THE AVAILABILITY OF A NEW INNER AIR SEAL STAGE 772-50-33V2500-A1,-A5,-D5
ENG-70-070812/04/98See SBINFORMATION - INTRODUCTION OF ALTERNATIVE HP COMPRESSOR STAGE 4 AND 5 CONTROL ROD CONNECTORS72-41-34V2500-A1,-A5,-D5
ENG-70-070912/04/98See SBINFORMATION - ANNOUNCEMENT OF PARTS FOR THE REPAIR OF THE HP COMPRESSOR CASE ASSEMBLY72-41-00V2500-A1,-A5,-D5
ENG-70-071012/04/98See SBINFORMATION - ENGINE - MAIN GEARBOX ASSEMBLY - INTRODUCTION OF AN ALTERNATIVE BOLT79-21-00V2500-D5
ENG-70-071205/08/997ENGINE - LP COMPRESSOR - TO ANNOUNCE AVAILABILITY OF A NEW FAN DISK WITH HEAVY SHANK NUTFOR BALANCING72-31-00V2500-A1,-A5,-D5
ENG-70-071301/25/998INFORMATION - ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - TO ANNOUNCE THE AVAILABILITY OF THE NO.4 BEARING COOLING DUCTSPACER72-43-40V2500-A1,-A5,-D5
ENG-70-071405/27/990110/04/99See SBINFORMATION - ANNOUNCEMENT OF ALTERNATIVE SUPER POLISHED HP COMPRESSOR BLADES AND VANES72-41-00V2500-A5,-D5
ENG-70-071503/05/997INFORMATION - ENGINE - MAIN GEARBOX ASSEMBLY - NEW SUPPLIER FOR THE WIRE ROPE CUP OF THE OIL TANK79-11-00V2500-A1,-A5,-D5
ENG-70-071604/10/99See SBINFORMATION - TO ANNOUNCE THE TRANSFER OF THE MANUFACTURE OF THE HP/LP FUEL PUMP FROM TEIJIN SEIKI COMPANY LIMITED TO SUNDSTRAND AEROSPACE73-12-41V2500-A5,-D5
ENG-70-071805/27/990101/31/007INFORMATION - ENGINE - MAIN GEARBOX ASSEMBLY - INTRODUCTION OF REDESIGNED TRANSPORTATION COVERS72-60-00V2500-A1,-A5
ENG-70-071903/31/00See SBINFORMATION - LP TURBINE - TO ANNOUNCE AVAILABILITY OF AN ADDITIONAL ADJUSTMENTS RING WITH DIFFERENT THICKNESS72-00-00V2500-A1,-A5,-D5
ENG-70-072101/12/00See SBINFORMATION TO TRANSFER THE ATA FIGURE LOCATION OF ELECTRICAL INSULATION TAPE FOR THE EEC FAN HARNESS ASSEMBLY72-51-00V2500-A1,-A5
ENG-70-072209/10/99See SBINFORMATION - ENGINE - ANNOUNCEMENT OF PARTS FOR REPAIR OF HP COMPRESSOR INNER SHROUD RING ASSEMBLIES, REPAIR OF STAGE 6 VARIABLE STATOR VANE BUSH LOCATION AND VANE REPLACEMENT OF STAGE 12 VANE (S)72-41-00V2500-A1,-A5,-D5
ENG-70-072403/15/00See SBINFORMATION - ENGINE - ANNOUNCEMENT OF PARTS FOR REPAIR OF RIGID STAINLESS STEEL, TUBE ASSEMBLIES70-35-00V2500-A1,-A5,-D5
ENG-70-072502/13/00See SBINFORMATION - INTRODUCTION OF THE OVERSIZED BUSHES FOR REPAIR OF THE VALVE72-32-00V2500-A5,-D5
ENG-70-072610/15/997INFORMATION - ANNOUNCEMENT OF HP COMPRESSOR BLADES AND VANES WITHOUT SUPER POLISHED FINISH72-41-00V2500-A5,-D5
ENG-70-072702/19/027INFORMATION - ENGINE - HYDRAULIC POWER, OIL AND FUEL TUBES - TO ANNOUNCE THE AVAILABILITY OF ALTERNATIVE UNIONS29-00-00V2500-A5
NAC-70-072810/05/01See SBINFORMATION-NACELLE - INTEGRATED DRIVE GENERATOR-TO ELECTRICAL POWER, ANNONCE THE AVAILABILITY OF NEW COUPLINGS FOR THE EMM IDG OIL PIPES24-00-00V2500-A5
NAC-70-073004/15/020205/01/037INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF NEW WIRING HARNESS ASSEMBLIES FITTED WITH MORE DURABLE TERMINAL LUGS.71-00-00V2500-A5
ENG-70-073206/13/02See SBTO ANNOUNCE THE AVAILABILITY OF ALTERNATIVE BOLTS FOR THE POWERPLANT, FUEL SYSTEM TUBES73-11-47V2500-A5
NAC-70-073403/23/050103/23/057INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF NEW RACEWAYS FAN HARNESS SUPPORT BRACKETS71-51-50V2500-A1,-A5
NAC-70-073601/28/030104/03/037INFORMATION - NACELLE - TO ANNOUNCE THE AVAILIBILTY OF A NEW IDG HARNESS WITH A NEW IMPROVED PYLON CONNECTOR24-21-43V2500-A5
NAC-70-073706/13/057INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW HINGE ASSEMBLY FOR THE L/H OIL FILLER ACCESS DOOR71-13-00V2500-A1,-A5
NAC-70-073809/28/057INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF NEW WIRING HARNESS ASSEMBLIES FITTED WITH MORE DURABLE TERMINAL LUGS71-00-00V2500-A5
NAC-70-073907/31/037INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF NEW FAN COWL DOOR LATCHES WITH REDUCED PAINTED AREA71-13-13V2500-A1,-A5
ENG-70-074007/01/037INFORMATION - ANNOUNCEMENT OF A NEW PROFORM CABIN AIR Y INTERSECTION DUCT36-11-49V2500-A1,-A5
ENG-70-074205/11/047INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A SHORTER CLAMP STACK BOLT AT THE GENERAL SERVICES PYLON INTERFACE HARNESS LIMB77-32-43V2500-A1,-A5
ENG-70-074303/24/057INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF SPAREABLE BOLTS AT THE HYDRAULIC DRAIN FILTER AND BRACKET ASSEMBLIES29-11-43V2500-A1,-A5
NAC-70-074410/10/067INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF ALTERNATE ROD END BEARINGS FOR THE THERMAL ANTI-ICE, CABIN AIR AND STARTER SYSTEM DUCTS30-21-49V2500-A1,-A5
NAC-70-074509/28/057INFORMATION - NACELLE - TO INTRODUCE STANDARD ESC10 ELECTRICAL CONNECTOR PART NUMBERS71-00-00V2500-A1,-A5
ENG-70-074611/20/077INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF ALTERNATIVE CLAMPS AND ASSOCIATED SPARE PARTS71-00-00V2500-A5
NAC-70-074703/07/070110/11/078INFORMATION - NACELLE - TO ANNOUNCE CHANGES TO THE DECALS ON THE INLET COWL AND THE FAN COWL DOORS71-11-00V2500-A1,-A5
ENG-70-074904/23/077INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF TWO NEW HALF LOCATING PLATES WHICH ARE USED TO SECURE THE TAI INTER-BULKHEAD SYSTEM TO THE REAR BULKHEAD71-11-11V2500-A1,-A5
NAC-70-075006/04/078INFORMATION - NACELLE - TO ANNOUNCE THE INTRODUCTION OF ALTERNATIVE DECALS FOR THE INLET COWL AND THE FAN COWL DOORS71-11-00V2500-A1,-A5
NAC-70-075101/04/077INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW IMPROVED OIL FILL ACCESS DOOR ON THE LEFT FAN COWL DOOR71-13-00V2500-A1,-A5
NAC-70-076012/15/997INFORMATION-NACELLE-TO ANNOUNCE THE AVAILABILITY OF A NEW IP BLEED CHECK VALVE36-00-00V2500-A1,-A5
NAC-70-076112/20/997INFORMATION - NACELLE - THRUST REVERSER - TO ANNOUNCE THE AVAILABILITY OF NEW BIFURCATION LATCH SHIMS AND SPACERS78-32-13V2500-D5
NAC-70-076310/25/000104/13/017INFORMATION - NACELLE - TO INTRODUCE THE A5 COMMON NOZZLE ASSEMBLY (CNA) AS AN ALTERNATIVE FOR THE A1 CNA.36-00-00V2500-A1
NAC-70-076603/08/017NACELLE - ANNOUNCEMENT OF NEW SPARES78-32-16V2500-D5
NAC-70-076703/30/017INFORMATION - NACELLE - ANNOUNCEMENT OF ALTERNATIVE COMMON NOZZLE ASSEMBLY (C.N.A)78-11-11V2500-D5
NAC-70-077106/20/017INFORMATION - NACELLE- ANNOUNCEMENT OF A NEW SEAL ASSY. - PLUG, UPPER TRACK78-32-46V2500-A1,-A5
NAC-70-077206/20/017INFORMATION - NACELLE- ANNOUNCEMENT OF A NEW SEAL BLOCK ASSY. - PRESSURE SEAL INSTL.78-30-00V2500-A1,-A5
NAC-70-077305/03/017INFORMATION - NACELLE - ANNOUNCEMENT OF A NEW BULKHEAD FITTING ASSEMBLY71-11-11V2500-D5
NAC-70-077806/21/017INFORMATION - NACELLE - ANNOUNCEMENT OF A NEW ACC DUCT AND SEAL ASSY. - INLET78-30-00V2500-A1,-A5
NAC-70-077906/08/057INFORMATION - NACELLE - THRUST REVERSER - ANNOUNCEMENT OF NEW HEAT SHIELD AT THE 7A BLEED PORT78-30-00V2500-A1,-A5
ENG-70-078102/22/008INFORMATION - ENGINE - PROVIDE A SALEABLE FAIRING FOR THE REPAIR OF FUEL NOZZLE AND SUPPORT ASSEMBLIES73-00-00V2500-A1,-A5,-D5
ENG-70-078306/09/000107/31/017INFORMATION - ENGINE - TURBINE EXHAUST CASE GROUP - TO ANNOUNCE THE AVAILABILITY OF A NEW TURBINE EXHAUST CASE ASSEMBLY72-50-00V2500-A1,-A5
ENG-70-078411/30/017ENGINE - OIL PART NUMBER CORRECTION79-22-43V2500-A1,-A5,-D5
ENG-70-078505/05/00See SBGENERAL INFORMATION BULLETIN - TO ANNOUNCE THE AVAILABILITY OF REPAIR PARTS FOR THE SCAVENGE OIL FILTER HOUSING ASSEMBLY79-22-43V2500-A1,-A5,-D5
ENG-70-078606/09/007INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF STRIP SEAL FOR NEW REPAIR PART72-32-00V2500-A1,-A5,-D5
ENG-70-078710/05/007ENGINE - INLET CONE - INTRODUCTION OF A THICKENED INLET CONE FAIRING WITH REVISED PROFILE72-38-00V2500-A1,-A5,-D5
ENG-70-078803/29/007INFORMATION-ENGINE-LP COMPRESSOR-INTRODUCTION OF AN INTERMEDIATE STRUCTURE FRONT FAIRING ASSEMBLY WITH REVISED MATERIAL72-32-00V2500-A1
ENG-70-078903/31/000202/21/067INFORMATION - ENGINE - LP TURBINE ROTOR AND STATOR ASSEMBLY - TO ANNOUNCE THE AVAILABILITY OF AN ALTERNATE TURBINE DISK STAGE 572-50-31V2500-A1
ENG-70-079206/09/00See SBINFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF VARIOUS REPAIR PARTS72-32-00V2500-A1,-A5,-D5
NAC-70-079207/08/030107/11/038INFORMATION - NACELLE - ANNOUNCEMENT OF NEW FWD OUTER DUCT FAIRING78-11-11V2500-A5
ENG-70-079407/23/017INFORMATION - ENGINE ANNOUNCEMENT OF PARTS FOR REPAIR OF FAN EXIT VANES72-32-00V2500-A5,-D5
NAC-70-079408/06/037INFORMATION - NACELLE - ANNOUNCEMENT OF NEW TORQUE RING FAIRING ASSEMBLY78-30-00V2500-A5
ENG-70-079501/18/02See SBINFORMATION - ANNOUNCEMENT OF THE RE-ITEMISATION OF PARTS AT INCORRECT ATA LOCATIONS71-71-49V2500-D5
ENG-70-079609/06/00See SBINFORMATION - ENGINE - DIFFUSER CASE ASSEMBLY - TO ANNOUNCE THE AVAILABILITY OF A SPARE FUEL NOZZLE CLASSIFIED SPACER TO PERMIT REPAIR OF THE FUEL NOZZLE AND SUPPORT ASSEMBLY.73-13-00V2500-A5,-D5
ENG-70-079709/06/008INFORMATION - ENGINE - TRANSFER VARIOUS BRACKETS TO MORE APPROPRIATE CHAPTERS72-50-00V2500-A1,-A5
ENG-70-079801/30/020106/06/05See SBINFORMATION - ANNOUNCEMENT OF PARTS FOR REPAIR OF HP COMPRESSOR REAR STATIC SEAL BY REPLACEMENT OF WORN AND/OR DAMAGED BALANCE TUBES72-42-50V2500-A1,-A5,-D5
ENG-70-079910/13/00See SBGENERAL INFORMATION BULLETIN - TO ANNOUNCE THE AVAILABILITY OF REPAIR PART FOR THE BIFURCATION BOX ASSEMBLY72-38-27V2500-D5
ENG-70-080002/22/02See SBINFORMATION - ANNOUNCEMENT OF PARTS FOR REPAIR OF HP COMPRESSOR VIGV, STAGE 3, STAGE 4 AND STAGE 5 VARIABLE VANE ACTUATING RING ASSEMBLIES BY REPLACEMENT OF BUSHES AND LOOSE FITTINGS72-41-34V2500-A5,-D5
ENG-70-080104/13/017ENGINE - INFORMATION - PROVIDE NEW FRONT AND REAR NO.4 BEARING FACE SEALS72-00-00V2500-A1,-A5,-D5
ENG-70-080212/11/008ENGINE - PROVIDE SPAREABLE HIGH PRESSURE TURBINE (HPT) DUCT SEGMENT COVER72-45-00V2500-A1,-A5,-D5
ENG-70-080302/12/02See SBINFORMATION - TO ANNOUNCE TRANSFER OF OIL SCAVENGE TEMPERATURE THERMOMETER FROM LEWIS ENGINEERING TO BF GOODRICH AEROSPACE (ROSEMOUNT AEROSPACE INC)79-32-16V2500-D5
ENG-70-080511/29/020201/19/097INFORMATION - ENGINE - LP TURBINE INTRODUCTION OF CAST TO SIZE BLADES STAGE 3, 4 AND 672-50-32V2500-A1,-A5,-D5
ENG-70-080601/22/02See SBINFORMATION - AIR COOLING - IGNITION COOLING LEADS INTRODUCTION OF ALTERNATIVE TOROIDAL SEAL RINGS75-27-49V2500-A1,-A5
ENG-70-080710/22/018GIB TO ANNOUNCE THE NEW REPAIR ONLY PART FOR FAN CASE ASSEMBLY72-32-85V2500-A1
ENG-70-080802/21/047INFORMATION - ENGINE - LP COMPRESSOR - INTRODUCTION OF A NEW ANNULUS FILLER WITH REDESIGNED SOURCE MATERIAL72-31-11V2500-A1
ENG-70-080909/20/017ENGINE - PROVIDE NEW COMBUSTOR GANG CHANNEL NUT ASSEMBLY72-44-00V2500-A1,-A5,-D5
ENG-70-081001/13/060101/11/088INFORMATION - ENGINE - LP TURBINE - RELEASE OF SALEABLE DETAIL PARTS TO REPLACE LP TURBINE HONEYCOMB SEALS72-50-22V2500-A1,-A5,-D5
ENG-70-081110/03/01See SBINFORMATION - POWERPLANT - ANNOUNCEMENT OF REPAIR PARTS FORWARD MOUNT SUPPORT71-21-00V2500-A1
ENG-70-081305/14/02See SBINFORMATION - ANNOUNCEMENT OF INTRODUCTION OF SAFETY CABLE AS A PREFERRED METHOD TO LOCKWIRE71-51-41V2500-A1,-A5,-D5
ENG-70-081403/29/027GENERAL INFORMATION BULLETIN - TO ANNOUNCE THE RELEASE OF OVERSIZE RIVET FOR THE TURBINE EXHAUST CASE THERMAL BLANKET72-50-00V2500-A1
ENG-70-081609/20/028INFORMATION - ENGINE - LP TURBINE - TO USE PRE V10198 ENGINE PARTS IN A5 33K ENGINES72-50-22V2500-A5
ENG-70-081709/20/028INFORMATION - ENGINE - LP TURBINE - TO USE PRE V10198 ENGINE PARTS IN A5 33K ENGINES72-50-23V2500-A5
ENG-70-081809/20/028INFORMATION - ENGINE - LP TURBINE - TO USE PRE V10198 ENGINE PARTS IN A5 33K ENGINES72-24-49V2500-A5
ENG-70-081909/20/028INFORMATION - ENGINE - LP TURBINE - TO USE PRE V10198 ENGINE PARTS IN A5 33K ENGINES72-50-10V2500-A5
ENG-70-082007/15/028INFORMATION - ENGINE - PROVIDE NEW SECOND STAGE HPT BLADES72-45-00V2500-D5
ENG-70-082105/04/040102/17/067INFORMATION - ENGINE - CORRECTION OF INTERCHANGE CONTROL NO. OF SELF LOCKING CLINCH NUTS (ST1578)72-50-00V2500-A1,-A5,-D5
ENG-70-082210/15/020205/01/037INFORMATION - ENGINE - PROVIDE OVERSIZED PISTON SEAL RING FOR NO. 3 BEARING HOUSING72-32-00V2500-A1,-A5,-D5
ENG-70-082310/15/020206/15/037INFORMATION - ENGINE - PROVIDE IDENTIFICATION FOR CAST TO SIZE DUCT SEGMENTS72-45-00V2500-A1,-A5,-D5
ENG-70-082410/03/027ENGINE - LP - COMPRESSOR - INTRODUCTION OF VALVE RING WITH SOLID RIVET72-32-00V2500-A5,-D5
ENG-70-082504/13/03See SBINFORMATION - LP TURBINE - TO ANNOUNCE AVAILABILITY OF ADDITIONAL ADJUSTING RINGS WITH DIFFERENT THICKNESS72-00-00V2500-A1,-A5
ENG-70-082601/31/038INFORMATION - ENGINE - REIDENTIFY COVER PLATE FOR BLADE OUTER AIR SEAL72-45-00V2500-A1,-A5,-D5
ENG-70-082707/20/030103/23/047ENGINE - LP COMPRESSOR - TO ANNOUNCE THE PART NUMBER CHANGES ABOUT THE NO.3 ROTOR CENTRE DETAILS72-32-00V2500-A1,-A5,-D5
ENG-70-082907/07/037INFORMATION - ENGINE - PROVIDE A NEW NO.4 BEARING COMPARTMENT GASKET AND LOCK72-42-00V2500-D5
ENG-70-083008/01/030201/30/047INFORMATION - ENGINE - REMOVE ONE OF THE SOURCES FOR THE NO. 3 BEARING72-32-24V2500-A5,-D5
ENG-70-083109/01/03See SBINFORMATION - ENGINE - PROVIDE ADDITIONAL DIMENSIONS FOR CLASSES 4, 5, AND 6 OF THE DIFFUSER CASE BUSHING INSERT72-42-00V2500-A5,-D5
ENG-70-083202/11/050107/07/088INFORMATION - ELECTRONIC ENGINE CONTROL (EEC) - FLAME SHIELD REMOVAL73-22-00V2500-A1,-A5
ENG-70-083301/22/040412/15/057INFORMATION - ENGINE - INTRODUCTION OF LP TURBINE VANE STAGE 4 WITH CAST TO SIZE LINER LOCATION SLOT72-50-22V2500-A1,-A5,-D5
ENG-70-083504/06/040104/16/04See SBINFORMATION - FUEL SYSTEM AIR TUBES - INTRODUCTION OF ALTERNATIVE FLEXIBLE TUBE ASSEMBLIES SOURCED FROM MEGGITT AEROSPACE73-22-49V2500-A1,-A5
NAC-70-083807/22/057INFORMATION - NACELLE - INTRODUCTION OF UPPER TRACK INSTALLATION AND FAIRING INSTALLATION AND HINGE FITTING ASSY UPPER TRACKS78-30-00V2500-A1,-A5
NAC-70-084304/28/087INFORMATION - COMMON NOZZLE ASSEMBLY - ANNOUNCEMENT OF NEW LOWER STRUT ASSY78-11-11V2500-A5
NAC-70-084904/30/047INFORMATION - NACELLE - TO PROVIDE PARTS PROGRESSION COVERAGE FOR NEW QUICK ENGINE CHANGE (QEC) KIT PART NUMBERS71-00-02V2500-A5
ENG-70-085705/28/040207/25/067INFORMATION - ENGINE - PROVIDE IMPROVED PREFORMED PACKINGS72-32-00V2500-A1,-A5,-D5
ENG-70-085802/27/047INFORMATION - ENGINE - LP COMPRESSOR - TO USE SPECIFIC ENGINE PARTS IN V2533-A5 ENGINES72-32-00V2500-A5
ENG-70-085904/22/047ENGINE - LP COMPRESSOR - TO ANNOUNCE THE MOUNTING BRACKETS AND THE NF TERMINAL BLOCK WITH REVISED MATERIAL72-32-00V2500-A1,-A5,-D5
NAC-70-086701/09/077INFORMATION - NACELLE - ANNOUNCEMENT OF AN ALTERNATE COUPLING24-21-51V2500-A1,-A5
NAC-70-087203/14/087INFORMATION - NACELLE - ANNOUNCE THE AVAILABILITY OF A NEW IP CHECK VALVE36-11-41V2500-A1,-A5
NAC-70-087705/03/057INFORMATION - NACELLE - ANNOUNCEMENT OF NEW BLANK CASCADES78-32-00V2500-A1,-A5
NAC-70-088010/19/077INFORMATION - NACELLE - ANNOUNCEMENT OF NEW COMMON NOZZLE ASSEMBLY78-11-11V2500-A1,-A5
ENG-70-088607/30/047INFORMATION - ENGINE - TRANSFER NUMBER 5 BEARING PARTS TO A NON-MODULAR CHAPTER72-00-00V2500-A1
ENG-70-088705/18/05See SBINFORMATION - ENGINE - FUEL COOLED OIL COOLER (FCOC) - RE-ITEMISATION OF SHIMS FOR INSTALLATION OF THE FCOC TO THE FANCASE - MOD 70-088779-21-43V2500-A1,-A5
ENG-70-088804/08/050101/19/067ENGINE - FUEL AND CONTROL - ELECTRONIC ENGINE CONTROL (EEC) - NEW SLIMLINE CASTING73-22-00V2500-A5
ENG-70-088905/14/080105/22/088INFORMATION ENGINE - LP TURBINE - CASE FRONT RAIL WITH SHEET METAL HEATSHIELD72-50-10V2500-A1
ENG-70-089006/22/057INFORMATION - ENGINE - LP TURBINE BLADE STG 4 - DELETION OF PWA73 HOT GAS CORROSION PROTECTION COATING72-50-32V2500-A1,-A5,-D5
ENG-70-089102/15/058ENGINE - LP COMPRESSOR - TO ANNOUNCE THE ALTERNATIVE SOURCE FOR FEGV INNER PLATFORM72-32-00V2500-A5,-D5
ENG-70-089410/07/05See SBINFORMATION - ANNOUNCEMENT OF PARTS FOR REPAIR OF LP COMPRESSOR BLEED SLAVE ACTUATOR BRACKET ASSEMBLY TO REPLACE DAMMAGED/MISSING THIN WALL INSERTS, FLANGED LOCATION DOWELS75-31-43V2500-A5,-D5
ENG-70-089505/27/057INFORMATION - ENGINE - NUMBER 4 BEARING RETAINING NUT REDESIGN72-42-32V2500-A1,-A5,-D5
ENG-70-089609/30/058INFORMATION - ENGINE - PROVIDE A SALEABLE INSERT AND FITTING FOR THE REPAIR OF FUEL NOZZLE AND SUPPORT ASSEMBLIES (VRS3590)73-13-41V2500-A1,-A5,-D5
ENG-70-089706/30/05See SBINFORMATION - ANNOUNCEMENT OF CORRECT VENDOR PART NUMBER FOR THE EGT HARNESS JUNCTION BOX COVER - MOD 70-089777-21-43V2500-D5
ENG-70-089809/30/058ENGINE - IMPROVED MANIFOLD LOOP CLAMP73-11-41V2500-A5
ENG-70-090101/10/078INFORMATION - ENGINE - TO ANNOUNCE THE INTRODUCTION OF A NEW IMPROVED HYDRAULIC PRESSURE SWITCH29-11-17V2500-A1,-A5
ENG-70-090205/14/080105/26/087ENGINE - TO ANNOUNCE THE AVAILABILITY OF NEW 4W2001, 4W2002 AND 4W2003 SERIES WASHERS AS REPLACEMENTS FOR THE AN960 SERIES WASHERS THAT ARE NO LONGER AVAILABLE73-11-47V2500-A1,-A5
ENG-70-090310/28/08See SBINFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF NEW BACKSHELLS FOR THE GENERAL SERVICES HARNESS71-51-43V2500-A1,-A5
ENG-70-090408/09/077INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF TWO MODIFIED STAINLESS STEEL TAB WASHERS ON THE HYDRAULIC SYSTEM29-11-17V2500-A1,-A5
NAC-70-090811/06/070109/01/087INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW INLET COWL FITTED WITH TITANIUM REAR BULKHEAD AND HALF-LOCATING PLATES71-11-00V2500-A5
NAC-70-090909/02/087INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A NEW INLET COWL FITTED WITH TWO SEGMENT INTAKE LINERS71-11-00V2500-A5
NAC-70-091512/03/087INFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF NEW RETAINER78-30-00V2500-A1,-A5
ENG-70-092407/12/058INFORMATION - ENGINE - CLARIFY TURBINE EXHAUST CASE THERMAL BLANKET PART NUMBER72-50-52V2500-A1
ENG-70-092509/14/06See SBENGINE - TURBINE EXHAUST CASE STRUT REPLACEMENT REPAIR PARTS (VRS3064 AND VRS5396)72-50-53V2500-A1,-A5,-D5
ENG-70-092603/13/080107/07/087INFORMATION - ENGINE - PROVIDE A NEW NO. 3 BEARING72-32-24V2500-A5,-D5
ENG-70-092912/16/057INFORMATION - ENGINE - PROVIDE NEW SEALING PLUGS FOR THE DATA ENTRY PLUG73-22-35V2500-A1,-A5,-D5
ENG-70-093803/01/070106/26/077INFORMATION ENGINE - LP TURBINE ACTIVE CLEARANCE CONTROL (ACC) - INTRODUCTION OF WASHER WITH CHANGED MATERIAL75-24-49V2500-A1,-A5,-D5
ENG-70-093904/04/077ENGINE - LP COMPRESSOR - ANNOUNCEMENT OF CHANGE OF THE SPACER PART NUMBER72-32-00V2500-A1,-A5
ENG-70-094005/02/078ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF THE OVERSIZE SPACER OF THE FRONT BLADE RETAINING RING72-31-00V2500-A1,-A5,-D5
ENG-70-094104/05/077INFORMATION ENGINE - LP TURBINE ACTIVE CLEARANCE CONTROL (ACC) - INTRODUCTION OF A NEW ACC CONNECTOR TUBE WITH CHANGED MATERIAL FOR THE END FERRULES75-24-49V2500-A1,-A5,-D5
ENG-70-094201/03/080102/05/087INFORMATION - LP TURBINE - INTRODUCTION OF A NEW DISK STAGE 6 WITH ENLARGED ELONGATED STRESS RELIEF HOLES IN FRONT FLANGE72-50-31V2500-A1,-A5,-D5
ENG-70-094301/21/087INFORMATION - LP TURBINE - INTRODUCTION OF NEW ACC CONNECTOR TUBE MADE FROM STAINLESS STEEL (X10) MATERIAL75-24-49V2500-A1,-A5,-D5
ENG-70-094409/26/070109/10/107INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF A NEW 2.5 BLEED VALVE POWER ARM AND LINK ARM72-32-00V2500-A1
ENG-70-094611/19/080203/09/107INFORMATION - ENGINE - LP TURBINE - INTRODUCTION OF NEW ACTIVE CLEARANCE CONTROL (ACC) SPACER PLATES MADE FROM STAINLESS STEEL (X10) MATERIAL75-24-49V2500-A1,-A5,-D5
ENG-70-094712/13/070102/03/107ENGINE - INTRODUCTION OF ALTERNATIVE MATERIAL FOR STAGE 7 TO 11 VANE STOPS72-41-21V2500-A5,-D5
ENG-70-094806/07/117INFORMATION - EXTERNAL GEARBOX MODULE - INTRODUCTION OF ALTERNATIVE BEARINGS72-60-00V2500-A1,-A5,-D5
ENG-70-095008/08/117INFORMATION - EXTERNAL GEARBOX - INTRODUCTION OF NEW HOUSINGS WITH A CONFORMING PART NUMBER FOR SCREW THREAD INSERTS79-22-48V2500-A1,-A5,-S1
ENG-70-095111/25/088INFORMATION - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF REPAIR PARTS FOR REAR FAIRING72-32-00V2500-A5,-D5
ENG-70-095206/16/097INFORMATION - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF THE FBC OIL DISTRIBUTOR AND STRAINER HOUSING THAT PROVIDE PARTS COMMONALITY BETWEEN V2500-A1, V2500-A5 AND V2500-D5 ENGINE MODELS72-32-00V2500-A1
ENG-70-095609/28/100106/17/137INFORMATION - ENGINE - TO INTRODUCE A NEW OIL PRESSURE DIFFERENTIAL TRANSMITTER793315V2500-A1,-A5
ENG-70-096502/14/127INFORMATION - ENGINE - TO INTRODUCE A NEW OIL QUANTITY TRANSMITTER P/N 76-167-1079-31-15V2500-A1,-A5,-S1
ENG-70-097809/08/088INFORMATION - ENGINE - INTRODUCTION OF ALTERNATIVE 90 DEGREE HARNESS BACKSHELLS71-51-41V2500-A5,-D5
ENG-70-097911/14/080109/23/107INFORMATION- ENGINE - INTRODUCTION OF A NEW HP COMPRESSOR 7C BLEED VALVE NOISE ATTENUATOR75-32-52V2500-D5
ENG-70-098011/07/087INFORMATION - ENGINE - HIGH PRESSURE (HP) COMPRESSOR VARIABLE STATOR VANES (VSV) INNER SHROUD - CHANGE OF MATERIAL OF INNER SHROUD BUSHES72-41-33V2500-A1,-A5,-D5
ENG-70-098111/12/087INFORMATION - ENGINE - LP COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF THE NEW WASHER72-32-00V2500-A1
ENG-70-098212/12/087INFORMATION - ENGINE - ELECTRICAL HARNESS - ALTERNATIVE HARNESS SLEEVES FOR LASER PRINTING SYSTEM 6 MARKING PROCEDURE71-00-00V2500-A1,-A5,-D5
ENG-70-098304/27/107INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF NEW INSERTS IN THE LPC BLEED DUCT ASSEMBLY72-32-00V2500-A1,-A5,-D5
ENG-70-098411/23/097INFORMATION - ENGINE - HIGH PRESSURE (HP) COMPRESSOR VARIABLE STATOR SPLIT CASES - VSV BUSHES OF NEW MATERIAL72-41-31V2500-A5,-D5
ENG-70-098509/22/098INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF THE OVERSIZE SLEEVES OF THE LPC REAR CASE ASSEMBLY72-32-83V2500-A5,-D5
ENG-70-098712/01/117INFORMATION - ENGINE - TO ANNOUNCE THE AVAILABILITY OF THE NEW RIVET OF THE HIGH PRESSURE (HP) TURBINE CASE ASSEMBLY72-45-21V2500-A1,-A5,-D5
ENG-70-098801/27/117INFORMATION - OIL - AIR COOLED OIL COOLER - ALTERNATIVE DRAIN PLUG O-RING SEAL79-21-42V2500-A1,-A5,-S1
ENG-70-098907/29/107INFORMATION - AIR - TURBINE COOLING AIR TUBES MATERIAL CHANGE75-23-49V2500-D5
ENG-70-099001/12/118ENGINE - INFORMATION - ALTERNATIVE WELDING RINGS, SEALING RINGS AND TUBE UNION70-35-24V2500-A1,-A5,-D5
ENG-70-099107/14/110212/14/188ENGINE - HIGH PRESSURE (HP) COMPRESSOR MODULE PART NUMBER72-40-00V2500-A1,-A5,-D5
ENG-70-099210/10/137INFORMATION - INTRODUCTION OF A NEW IDLER GEAR, A NEW BONDING STRAP AND DELETION OF SOME TRANSPORTATION FITTINGS FOR THE EXTERNAL GEARBOX MODULE - INTRODUCTION OF A NEW COVER FOR THE OIL PRESSURE PUMP AND FILTER HOUSING AND THE SCAVENGE OIL PUMP72-60-00V2500-A1,-A5,-D5
ENG-70-099407/03/127INFORMATION - ENGINE - PROVIDE NEW SEALING PLUGS FOR THE DATA ENTRY PLUG73-22-35V2500-A1,-A5,-D5
ENG-70-099511/15/118INFORMATION - ENGINE - INNER AND OUTER COMBUSTION CHAMBER LINERS WITH ADDITION OF SINGLE CRYSTAL MATERIAL ON ROWS 3 AND 472-40-00V2500-A5,-S1
ENG-70-099704/30/127ENGINE - HIGH PRESSURE (HP) COMPRESSOR - REAR STATIC SEAL WITH CHANGED METHOD OF MANUFACTURING72-42-50V2500-A5,-D5
ENG-70-099910/25/128INFORMATION - LP COMPRESSOR - TO ANNOUNCE AVAILABILITY OF AN ALTERNATIVE REAR RAMP OF THE STAGE 1 FAN DISC72-31-00V2500-A1,-A5,-D5
ENG-70-100002/20/128POWER PLANT - ELECTRICAL HARNESS - ADDITIONAL ALTERNATIVE CONNECTORS FOR THE ENGINE ELECTRONIC CONTROLLER (EEC) FAN CASE HARNESS71-51-41V2500-A5,-S1
ENG-70-100111/19/127INFORMATION - LP COMPRESSOR - TO ANNOUNCE AVAILABILITY OF THE ALTERNATIVE STAGE 1 FAN DISC72-31-00V2500-A1,-A5,-D5
ENG-70-100308/23/128INFORMATION - IGNITION - INTRODUCTION OF A NEW IGNITER PLUG74-21-41V2500-A1,-A5,-D5
ENG-70-100407/23/120106/12/147INFORMATION - IGNITION - INTRODUCTION OF A MODIFIED IGNITION LEAD TO ADDRESS INSULATION DEGRADATION/CRACKING74-21-43V2500-A1,-A5
ENG-70-100503/18/147IGNITION - SHROUD, LEAD PLUG END - INTRODUCTION OF A LONGER SHROUD TO IMPROVE COOLING74-21-43V2500-A1,-A5
ENG-70-100602/23/157INFORMATION - HIGH PRESSURE (HP) COMPRESSOR BLADES - ADDITIONAL UNDERSIZE ADJUSTMENT BLADES ON STAGES 6 TO 8 FOR IMPROVED CIRCUMFERENTIAL GAPPING72-41-15V2500-A5
ENG-70-102004/10/150108/12/167INFORMATION - ENGINE - VIBRATION TRANSDUCER - INTRODUCTION OF A NEW VIBRATION TRANSDUCER THAT PROVIDES MORE ACCURATE READINGS77-32-15V2500-A1,-A5
ENG-71-000411/12/974ENGINE - OIL - OIL PRESSURE SWITCH PIPING - PIPING SUPPORT CLIPS - MODIFICATION OF71-00-00V2500-A1
ENG-71-000612/20/946ENGINE - CLIPPING POINT SUPPORT BRACKET - MODIFICATION OF71-51-42V2500-A1
NAC-71-001012/01/000103/26/024NACELLE - POWERPLANT - IDG CABLES -400VC-A CONNECTOR - PRESSURE SPRINGS - INSTALLATION OF71-00-00V2500-A1
NAC-71-001105/15/914NACELLE - POWER PLANT - CLIPPING POINTS, CORE FIRE SERVICES HARNESS - MODIFICATION OF71-00-00V2500-A1
NAC-71-001503/31/925NACELLE - POWER PLANT - MODIFICATION RECORD PLATES - REPLACEMENT OF71-11-00V2500-A1
NAC-71-001603/30/904NACELLE - POWER PLANT - HOIST POINTS - BLANKING PLUGS - INSTALLATION OF71-11-00V2500-A1
NAC-71-001703/30/905NACELLE - POWER PLANT - DRAINS MAST BOLTS - REPLACEMENT OF71-71-00V2500-A1
ENG-71-001903/09/924ENGINE - POWER PLANT - EEC AND IGNITION SUPPLY HARNESS, CLIPPING - CHANGES TO71-00-00V2500-A1
ENG-71-002109/30/964ENGINE - AIR - FIRE DETECTION, MOUNTING BRACKET - REPLACEMENT OF78-00-00V2500-A1
NAC-71-002705/15/915NACELLE - POWER PLANT - FAN COWL DOORS IDENTIFICATION PLATE - INSTALLATION OF71-11-00V2500-A1
ENG-71-002905/07/904ENGINE GENERAL - EEC AND IGNITION SUPPLY HARNESS, CLIPPING POINT - MODIFICATION OF71-00-00V2500-A1
ENG-71-003505/04/904ENGINE - EEC AND IGNITION SUPPLY HARNESS, CLIPPING POINTS - CHANGES TO71-00-00V2500-A1
NAC-71-003704/15/964NACELLE - LH FAN COWL DOORS - INCORPORATE AN OIL TANK SERVICING DECAL ON THE OIL FILL ACCESS PANEL71-13-00V2500-A1
ENG-71-003811/15/914ENGINE - FAN CASE GENERAL SERVICES HARNESS - CONNECTOR BACKSHELLS - REPLACEMENT OF71-00-00V2500-A1
NAC-71-004303/31/924NACELLE - INLET COWL - P2/T2 ROSEMOUNT PROBE, BONDING CLAMP - REPLACEMENT OF71-11-00V2500-A1
NAC-71-004607/16/934NACELLE - POWER PLANT - GEARBOX BREATHER OUTLET - OVERBOARD GEARBOX VENT - INSTALLATION OF71-13-00V2500-A1
NAC-71-004705/15/917NACELLE - POWER PLANT - INCORPORATE A REVISED OIL TANK SCUPPER DRAIN TUBE71-13-00V2500-A1
ENG-71-004806/15/900106/15/903ENGINE - EEC FAN HARNESS - INCORPORATE ADDITIONAL SPACERS AT CLIPPING POINTS CP1022 AND CP101771-00-00V2500-A1
ENG-71-004904/05/913ENGINE - INCORPORATE REVISED EEC FAN HARNESS CLIPPING REQUIREMENTS (REFERENCE CP1013)71-51-41V2500-A1
ENG-71-005004/12/910204/12/915ENGINE - INCORPORATION OF REROUTING AND MODIFICATION REQUIREMENTS FOR THE EEC FAN HARNESS24-00-00V2500-A1
ENG-71-005111/17/890204/17/924ENGINE - INTRODUCTION OF CHANGES TO ENGINE DRESSING CLEARANCES71-00-00V2500-A1
ENG-71-005201/19/904ENGINE - INCORPORATE A FUMESEAL BRACKET TO PROVIDE ADDITIONAL STRENGTH71-00-00V2500-A1
ENG-71-005306/22/905ENGINE - INCORPORATE REVISED CLIPPING REQUIREMENTS AT CP100171-00-00V2500-A1
ENG-71-005409/14/904ENGINE - EEC LINK HARNESS - CORE AND EGT HARNESS - INTRODUCTION OF IMPROVED CLIPS FOR HARNESS CLIPPING71-00-00V2500-A1
ENG-71-005510/19/905ENGINE - REWORK THE EEC FAN HARNESS ASSEMBLY TO INCORPORATE IMPROVED ANTI-CHAFING FEATURES71-00-00V2500-A1
ENG-71-005610/05/904ENGINE - INCORPORATE A SPACER AT CLIPPING POINT CP078971-00-00V2500-A1
ENG-71-005711/10/893ENGINE - PROVIDE ATTACHING BOLTS OF INCREASED LENGTH FOR AN EEC FAN HARNESS BRACKET71-00-00V2500-A1
ENG-71-005907/13/905ENGINE - INCORPORATE A REVISED RELAY BOX MOUNTING BRACKET HAVING AN ADDITIONAL SPACER AT CP101571-00-00V2500-A1
ENG-71-006001/18/916ENGINE - PROVIDE AN EEC HARNESS SUPPORT BRACKET AT FLANGE FD71-00-00V2500-A1
ENG-71-006109/21/904ENGINE - REVISE EGT HARNESS CLIPPING REQUIREMENTS AT CLIPPING POINTS CP5734, CP5735, AND CP573671-00-00V2500-A1
ENG-71-006210/19/906ENGINE - INCORPORATE REVISED BOLT LENGTH AT CP 567571-00-00V2500-A1
ENG-71-006303/29/914ENGINE - EEC HARNESS - FAN AND EEC HARNESS - CORE - INTRODUCTION OF ADDITIONAL SUPPORT FOR ELECTRICAL CONNECTORS71-00-00V2500-A1
ENG-71-006603/10/976ENGINE - POWERPLANT - INTRODUCE A SPACER AT CLIPPING POINT CP080971-00-00V2500-A1
ENG-71-006702/09/947ENGINE - INCORPORATE REVISED CUSHION-TYPE HARNESS CLIPPING71-00-00V2500-A1
NAC-71-006912/04/890103/06/903NACELLE - POWER PLANT - EEC COOLING - REMOVAL OF71-13-16V2500-A1
ENG-71-007012/04/893ENGINE - EEC COOLING - SUPPORT BRACKETS - REMOVAL/ REPLACEMENT OF71-00-00V2500-A1
NAC-71-007502/06/954NACELLE - POWERPLANT - GEARBOX BREATHER OUTLET DUCT SEAL - REPLACEMENT OF71-00-00V2500-A1
NAC-71-008205/14/900507/25/003NACELLE - POWER PLANT - MOUNTS - AFT ENGINE MOUNT BARREL NUTS - REPLACEMENT OF71-20-00V2500-A1
NAC-71-009603/10/974NACELLE - POWERPLANT - FAN COWL DOOR (LH); HOLD OPEN ROD STOWAGE BRACKET - TO REPOSITION71-00-00V2500-A1
ENG-71-009704/30/988ENGINE - POWERPLANT - GENERAL SERVICES HARNESS - CLIPPING POINTS - MODIFICATION OF71-00-00V2500-A1
NAC-71-009806/07/960108/28/986NACELLE - EXHAUST - GUIDE PIN, NO.1 OPEN LATCH INDICATOR, THRUST REVERSER - REPLACEMENTOF71-00-00V2500-A1,-A5
NAC-71-010207/01/930107/01/934NACELLE - POWER PLANT - FAN COWL DOOR - HOLD-OPEN STRUT BRACKET - REPLACEMENT OF71-00-00V2500-A1
ENG-71-010403/21/976ENGINE - POWERPLANT - FAN CASE RAFT AND BRACKET - REPLACEMENT OF71-00-00V2500-A1
ENG-71-010506/22/927ENGINE - POWERPLANT - INTRODUCE REVISED CLIPPING REQUIREMENTS AT CLIPPING POINT CP109271-00-00V2500-A1
ENG-71-010710/09/924ENGINE - POWERPLANT - INCORPORATION OF MODIFICATION REQUIREMENTS FOR THE EEC AND IGNITION SUPPLY HARNESS24-00-00V2500-A1
ENG-71-010804/12/914ENGINE - PROVIDE A P2/T2 LINE BRACKET WITH LOCKWIRE HOLES71-00-00V2500-A1
ENG-71-010912/27/966ENGINE - FAN CASE - PROVIDE IMPROVED ROUTING AND CLIPPING OF THE EEC AND IGNITION HARNESSES AND RACEWAY71-00-00V2500-A1
ENG-71-011004/01/920109/03/027ENGINE - PROVIDE REROUTED OIL TUBES FOR THE ACOC AND THE OIL TANK ASSEMBLY71-00-00V2500-A1
ENG-71-011109/06/964ENGINE - PROVIDE NEW CORE AND FAN HARNESS ASSEMBLY CONNECTORS WITH WIRE LOCKING FEATURES71-00-00V2500-A1
ENG-71-011311/08/966ENGINE - INTRODUCE A RELAY BOX MOUNTING BRACKET ASSEMBLY WITH INCREASED DURABILITY ANDAN IMPROVED ATTACHMENT DESIGN71-00-00V2500-A1,-A5
ENG-71-011411/14/976ENGINE - PROVIDE BIFURCATION PANEL BRACKETS THAT FEATURE REQUIRED BOLT HOLE PROVISIONS71-00-00V2500-D5
ENG-71-011608/01/976ENGINE - POWERPLANT - REVISE THE CLIPPING ARRANGEMENTS AT CLIPPING POINTS CP2277 AND 2432 TO IMPROVE FITMENT OF A HARNESS SUPPORT TUBE.71-00-00V2500-D5
ENG-71-011706/13/976ENGINE - POWERPLANT - REPLACE EXISTING FLOWMETER SUPPORT BRACKETS AND ADD AN ADDITIONAL FLOWMETER BONDING LEAD71-00-00V2500-D5
ENG-71-011807/15/946ENGINE - INTRODUCE REVISED CLIPPING ARRANGEMENTS TO PROVIDE INCREASED CLEARANCE BETWEEN OIL QUANTITY TRANSMITTER AND EEC HARNESS71-00-00V2500-A1,-A5
ENG-71-011908/03/940106/26/986ENGINE - INTRODUCE REVISED EEC HARNESS CLIPPING TO PROVIDE PROPER CLEARANCE BETWEEN HARNESS AND FLANGE D IN AREA ADJACENT TO EEC71-00-00V2500-A1,-A5
ENG-71-012007/15/946ENGINE - REROUTE THE CORE HARNESS TO ENSURE ADEQUATE CLEARANCE BETWEEN HARNESS ANDVARIOUS TUBES71-00-00V2500-A1,-A5
ENG-71-012104/11/976POWER PLANT - FUEL DRAIN TUBES (ENGINES) - REROUTED TUBES FROM OIL TANK FILLER DRAIN TOFAN COWL OVERBOARD VENT71-00-00V2500-D5
ENG-71-012207/21/946ENGINE - PROVIDE A LONGER BOLT AT CLIPPING POINT CP552371-00-00V2500-A1,-A5
NAC-71-012603/31/926NACELLE - POWER PLANT - INLET COWL, ACCESS PANEL NUTPLATES - REWORK OF71-00-00V2500-A1
NAC-71-012810/01/936NACELLE - POWERPLANT - GEARBOX BREATHER DUCT - REPLACEMENT OF71-13-00V2500-A1
NAC-71-013309/27/935NACELLE - POWERPLANT - GEARBOX BREATHER DUCT - SEALING COMPOUND - REPLACEMENT OF71-00-00V2500-A1
NAC-71-013508/07/950103/05/983NACELLE - POWER PLANT - FORWARD MOUNT INCREASED CLEARANCE STOP PLATE AND INCREASED STRENGTH BOLT UPGRADE71-00-00V2500-A1,-A5
NAC-71-013605/15/975NACELLE - POWERPLANT - DECAL, FAN COWL OIL SERVICING ACCESS DOOR - REPLACEMENT OF71-13-00V2500-A1
NAC-71-013706/07/968NACELLE - THRUST REVERSER - PROVIDE A LATCH INDICATOR WITH STAINLESS STEEL GUIDE PADS (FOR CONTROLLED SERVICE USE)71-00-00V2500-A1
NAC-71-013804/28/958NACELLE - POWERPLANT - CORE SERVICES HARNESS - REROUTE71-00-00V2500-A1
NAC-71-014207/16/970101/15/983NACELLE - POWERPLANT - RIGHT FAN COWL DOOR - INTRODUCTION OF A DRAIN HOLE71-00-00V2500-A5
NAC-71-014510/17/977NACELLE - POWERPLANT - CORE FIRE DETECTOR - REWORK71-52-41V2500-A1
NAC-71-014701/19/967NACELLE - POWERPLANT - DRAIN TUBES - REPLACEMENT OF71-00-00V2500-A1
ENG-71-014803/10/976ENGINE - POWERPLANT - MODIFICATION OF THE EEC HARNESS SUPPORT BRACKET71-00-00V2500-A5
ENG-71-014906/01/956POWER PLANT - ENGINE - INCORPORATION OF CLIPPING POINT 2449 AND BRACKET AT CLIPPING POINT258779-00-00V2500-D5
ENG-71-015006/01/956POWER PLANT - ENGINE - RESET EDUCTOR SYSTEM WITH REVISED HARNESS AND CLIPPING71-00-00V2500-D5
ENG-71-015106/01/957POWER PLANT - DRAINS TUBES AND MAST - RESET OIL SCUPPER DRAINS TUBE AND MODIFIED SUPPORT BRACKET AT CLIPPING POINT CP 260771-00-00V2500-D5
ENG-71-015206/01/956POWER PLANT - CORE HARNESSES - REVISED CLIPPING OF LOOMS E, F, AND G71-00-00V2500-D5
ENG-71-015306/01/950106/01/956POWER PLANT - DRAIN TUBE MAST - DRAINS COLLECTING BRACKET WITH INCREASED SEALING AREA71-00-00V2500-D5
ENG-71-015406/16/946POWER PLANT - ENGINE - EEC HARNESS FAN - LOOMS A AND B WITH SHORTENED FIRE DETECTION LIMBS AND REVISED CLIPPING71-51-00V2500-D5
ENG-71-015510/17/977ENGINE - FANCASE - SUPPORT BRACKETS, ATTACHING BOLTS - VARIOUS CHANGES71-51-00V2500-A5
ENG-71-015606/01/956POWER PLANT - EEC HARNESS FAN - REVISED CLIPPING OF LOOMS B AND D ADJACENT TO FUEL COOLEDOIL COOLER71-51-00V2500-D5
ENG-71-015808/03/94See SBENGINE - POWER PLANT - EEC HARNESS FAN - CONTROLLED SERVICE USE OF ALTERNATIVE CONNECTOR SOCKETS71-00-00V2500-A5
ENG-71-015905/03/957ENGINE - POWERPLANT - INTRODUCE A NEW FANCASE HARNESS WITH REVISED LENGTH LOOMS71-51-00V2500-D5
ENG-71-016010/05/944ENGINE - POWER PLANT - EEC FAN HARNESS - FCOC FUEL TEMPERATURE THERMOCOUPLE CONNECTOR WITH IMPROVED SOCKETS71-51-00V2500-A5
ENG-71-016103/22/956ENGINE - EGT AND FIREWIRE HARNESS - INTRODUCTION OF LONGER BOLT AT CLIPPING POINT CP780071-00-00V2500-D5
ENG-71-016206/13/970107/31/037ENGINE - INTRODUCE A NEW STAGE 10 ON/OFF VALVE AIR DEFLECTOR BRACKET72-40-00V2500-A1,-A5
ENG-71-016507/30/96See SBENGINE - INTRODUCE A NEW EEC AND IGNITION SUPPLY HARNESS FOR CONTROLLED SERVICE USE71-51-00V2500-A5
NAC-71-016612/20/947NACELLE - POWERPLANT - REPLACEMENT OF THE TAI VALVE71-51-43V2500-A1
NAC-71-016812/22/950211/20/965NACELLE - POWER PLANT - OUTER BREATHER MAST, LOWER FAN COWL DOOR - REPLACEMENT OF71-13-00V2500-D5
NAC-71-016910/17/976NACELLE - POWERPLANT - DRAIN TUBES AND COLLECTOR PLATE ASSEMBLY - REPLACEMENT OF71-00-00V2500-A5
NAC-71-017010/17/977NACELLE - POWERPLANT - REPACEMENT OF FCD LATCH HOUSING FASTENERS71-13-11V2500-A1
NAC-71-017110/17/977NACELLE - POWERPLANT - REPLACEMENT OF FASTENERS ON THE FCD LOCATOR71-13-11V2500-A1,-A5
ENG-71-017509/27/964ENGINE - EEC HARNESS - PROVIDE A NEW HARNESS THAT ELIMINATES THE THRUST REVERSER INTERLOCKCIRCUIT WIRING PROVISIONS71-51-00V2500-D5
ENG-71-017611/29/966POWER PLANT - EEC CHANNEL A AND B HARNESSES (LOOM A AND B) - INTRODUCTION OF ALTERNATIVE PLUG ASSEMBLIES71-00-00V2500-D5
ENG-71-017706/30/030504/23/093ENGINE - POWERPLANT - EEC AND IGNITION SUPPLY HARNESS - THRUST REVERSER CONTROL VALVE CABLES - REROUTE OF71-51-00V2500-A1,-A5
ENG-71-017811/01/977POWER PLANT - OIL, HYDRAULIC AND WATER DRAIN TUBES - ENGINE - NO.4 BEARING WEEP LINE RE-ROUTED71-00-00V2500-A1,-A5
ENG-71-017902/21/977POWER PLANT - GENERAL SERVICE HARNESS (LOOM E) INTRODUCTION OF REVISED CLIPPING OF EEC HARNESS71-52-51V2500-D5
ENG-71-018011/07/977POWER PLANT - EEC CHANNE "A" HARNIESS (LOOM A) - INTRODUCTION OF REVISED CLIPPING OF EEC HARNESS71-51-51V2500-D5
ENG-71-018202/14/970203/19/996POWER PLANT - EEC CHANNEL A AND B HARNESSES (LOOM A AND B) - INTRODUCTION OF REVISED ENGINE DEDICATED ALTERNATOR CONNECTORS71-51-00V2500-D5
ENG-71-018307/18/977POWER PLANT - ELECTRICAL HARNESS - INTRODUCTION OF EEC HARNESS TO SUIT FCOC FUEL TEMPERATURE THERMOCOUPLE NEW PRODUCTION71-51-00V2500-A1,-D5
NAC-71-018412/10/970109/08/994NACELLE - INLET COWL - TAI INTERBULKHEAD DUCT AND ACCESS PANEL - REPLACEMENT OF71-00-00V2500-A5
ENG-71-018506/13/970109/04/987POWER PLANT - GENERAL SERVICES HARNESS (LOOM D) - INTRODUCTION OF REVISED CLIPPING71-00-00V2500-D5
NAC-71-018606/03/994NACELLE - POWERPLANT - COWL, AIR INTAKE - ADAPTER RING ATTACHING RIVETS - INSPECTION/ REPLACEMENT OF71-00-00V2500-A5
ENG-71-018708/01/977POWER PLANT - GENERAL SERVICES HARNESS (LOOM D)-INTRODUCTION OF ICE DETECTION SYSTEM ELECTRICAL HARNESS AND CLIPPING71-51-00V2500-D5
NAC-71-019304/26/964NACELLE - NOSE COWL - FORWARD BULKHEAD ANTI-ICE DUCT CONNECTION - ADDITION OF POSITIVE RETENTION FEATURE71-00-00V2500-D5
NAC-71-A019603/28/970310/16/974NACELLE - NOSE COWL - FORWARD BULKHEAD ANTI-ICE DUCT CONNECTION - EXAMINATION OF BULKHEAD FITTING AND COUPLING NUT THREAD/RE-TORQUE OF COUPLING NUT71-00-00V2500-D5
ENG-71-019702/06/024ENGINE - POWER PLANT - EEC HARNESS FAN/CORE - INTRODUCTION OF AN ELECTRICAL INSPECTION CHECK FOR CONNECTOR SOCKET MATERIAL - NMSB71-00-00V2500-A1,-A5
ENG-71-019907/18/977POWER PLANT - ELECTRICAL HARNESS - LIGHT DUTY - EEC HARNESS - CORE - INTRODUCTION OF REVISED CLIPPING FOR EGT HARNESS ASSEMBLY71-00-00V2500-A5
ENG-71-020007/18/977POWER PLANT - EEC CHANNEL A and B - INTRODUCTION OF REVISED ENGINE DEDICATED ALTERNATOR CONNECTORS - NEW PRODUCTION71-00-00V2500-D5
ENG-71-020108/01/977POWER PLANT - ELECTRICAL HARNESS - EEC HARNESS FAN - INTRODUCTION OF REVISED NACELLE BREAK 4001VC CONNECTOR BRACKET71-00-00V2500-A1,-A5
ENG-71-020211/21/976POWER PLANT - FUEL DRAIN TUBES - ENGINE - INTRODUCTION OF SMALLER CLIPS FOR CLIP POINTSCP2607 AND CP260871-00-00V2500-D5
ENG-71-020311/07/977POWER PLANT - EEC CHANNEL A AND B HARNESS - LOOM A AND B HARNESSES WITH THRUST REVERSER CIRCUIT WIRING REMOVED71-51-00V2500-D5
ENG-71-020512/12/977POWER PLANT - GENERAL SERVICES HARNESS (LOOM E) - DELETION OF CLIP NUT AT CP784771-52-51V2500-D5
NAC-71-020609/19/000202/13/034NACELLE - POWERPLANT - COWL, AIR INTAKE - REWORK TO ACCOMMODATE LONGER P2T2 PROBE71-00-00V2500-A5
ENG-71-020706/26/987POWER PLANT - ELECTRICAL HARNESS - INTRODUCTION OF REVISED CLIP SIZES71-52-54V2500-D5
NAC-71-020803/04/990206/09/008NACELLE- POWERPLANT - SEAL, PYLON APRON, FORWARD UPPER AND LOWER - REPLACEMENT OF71-14-00V2500-D5
NAC-71-020909/12/974NACELLE - POWERPLANT - BOLTS, PYLON APRON, - REPLACEMENT OF71-14-00V2500-D5
NAC-71-021003/17/980102/04/993NACELLE - POWER PLANT - LINKS, FORWARD ENGINE MOUNT - REPLACEMENT OF71-00-00V2500-A1,-A5
NAC-71-021203/26/980206/30/984NACELLE - POWERPLANT - SEAL, PYLON APRON, AFT- MODIFICATION OF71-14-00V2500-D5
ENG-71-021606/26/980210/15/997POWER PLANT - ELECTRICAL HARNESS - EEC HARNESS - FAN - INTRODUCTION OF EEC FAN HARNESS WITH REVISED LENGTH AND CLIPPING71-5l-00V2500-A5
NAC-71-021801/18/990206/06/007NACELLE - POWERPLANT - FAN COWL - INTRODUCTION OF NEW GEARBOX BREATHER MAST (FOR CONTROLLED SERVICE USE)71-00-00V2500-A5
ENG-71-021909/18/980204/07/006POWER PLANT - ELECTRICAL HARNESSES - EEC HARNESS - FAN - INTRODUCTION OF REVISED ENGINE DEDICATED ALTERNATOR (EDA) CONNECTORS (REWORK)71-51-41V2500-A1,-A5
ENG-71-022004/10/997POWER PLANT - ELECTRICAL HARNESS - EEC HARNESS - FAN - INTRODUCTION OF REVISED ENGINE DEDICATED ALTERNATOR CONNECTORS (NEW PRODUCTION)71-51-41V2500-A5
ENG-71-022106/02/997POWER PLANT - ELECTRICAL HARNESS - EEC HARNESS - FAN - INTRODUCTION OF EEC FAN HARNESS ASSEMBLY WITH REVISED EDA CONNECTORS71-5I-00V2500-A1
ENG-71-022212/04/987POWER PLANT - ELECTRICAL HARNESSES - EEC HARNESS - FAN - INTRODUCTION OF REVISED NO.4 BEARING PRESSURE TRANSDUCER SUPPORT BRACKET71-51-41V2500-A5
NAC-71-022705/19/990108/06/084NACELLE - POWERPLANT-FAN COWL DOOR LATCH HANDLES-APPLICATION OF FLUORESCENT PAINT71-00-00V2500-A1,-A5
NAC-71-022906/28/993NACELLE - NOSE COWL - THERMAL ANTI-ICE DUCT INSTALLATION - INSPECTION OF (NON-MODIFICATION)71-00-00V2500-D5
ENG-71-023006/09/980112/18/983NACELLE-PYLON - UPPER FITTING, OPENING ACTUATOR, THRUST REVERSER71-00-00V2500-D5
NAC-71-023110/30/980205/14/994NACELLE - POWERPLANT - UPPER FITTING, THRUST REVERSER OPENING ACTUATOR - REPLACEMENT OF71-00-00V2500-D5
NAC-71-023206/18/990207/08/054NACELLE - NOSE COWL - FORWARD BULKHEAD FITTING, THERMAL ANTI-ICE DUCT-MODIFICATION OF78-00-00V2500-D5
NAC-71-023312/03/983EBU - THRUST STRUT - LOCKWIRE INSTALLATION INSPECTION71-00-00V2500-D5
NAC-71-023505/13/990205/02/004NACELLE - POWERPLANT - FAN COWL DOORS - APPLICATION OF CAUTION MARKINGS71-00-00V2500-A1,-A5
NAC-71-025606/23/990210/12/014NACELLE - POWERPLANT - RIGHT HAND FAN COWL DOOR - MODIFICATION TO LATCH ASSEMBLY71-00-00V2500-A1,-A5
NAC-71-025708/08/000104/15/097NACELLE - AIR INLET COWL - INSTALLATION OF A5 TAI OUTER DUCT AND ACCESS PANEL ON A1 AIR INLET COWLS71-11-11V2500-A1
NAC-71-025912/10/990312/11/024NACELLE - POWERPLANT - AIR INLET COWL - INSTALLATION OF A FAN COWL DOOR HOLD OPEN DEVICE71-00-00V2500-A1,-A5
NAC-71-026004/03/078NACELLE - INSTALLATION OF SPANISH DECALS ON THE AIR INTAKE COWL AND FAN COWL DOORS (SPECIAL ORDER ONLY)71-13-00V2500-A1,-A5
NAC-71-026601/19/020209/30/097NACELLE - INLET COWL - T.A.I EXHAUST ACESS PANEL - REPLACEMENT OF71-11-11V2500-A1,-A5
ENG-71-027111/20/020106/30/038ENGINE - ENGINE VIBRATION MONITOR ( E.V.M ) HARNESS - RE-ROUTING OF THE E.V.M HARNESS AT CLIPPING POINTS CP0876 AND CP 121071-51-42V2500-A1,-A5
NAC-71-027205/15/030109/20/073NACELLE - ENGINE BUILD UNIT (EBU) - REPLACEMENT AND REROUTING OF SEVERAL EBU SYSTEMS TO ACCOMMODATE THE REROUTING OF THE OIL SCAVENGE TUBES71-52-00V2500-A1
NAC-71-027311/14/030411/20/074NACELLE - ENGINE BUILD UNIT (EBU) - REPLACEMENT AND REROUTING OF SEVERAL EBU SYSTEMS TO ACCOMMODATE THE REROUTING OF THE OIL SCAVENGE TUBES71-00-00V2500-A5
ENG-71-027509/29/050206/26/156ENGINE - ENGINE BUILD UNIT (EBU) - TERMINAL MODULE ASSEMBLY - REROUTING OF THE HARNESS71-51-43V2500-A1,-A5
ENG-71-027603/31/040105/11/044ENGINE - ENGINE BUILD UNIT (EBU) - REWORK OF ELECTRICAL HARNESS AND BRACKET ASSEMBLY TO ACCOMMODATE THE REROUTING OF THE OIL SCAVENGE TUBES71-00-00V2500-A5
NAC-71-027704/13/050101/03/067NACELLE - POWERPLANT - NOSECOWL - REPLACEMENT OF THE HOIST POINT BLANKING PLUGS71-11-11V2500-A1,-A5
ENG-71-027803/17/006POWER PLANT- CORE HARNESSES - INTRODUCTION OF EEC LOOMS G AND H WITH REVISED INSULATION SHIELDING71-52-00V2500-D5
NAC-71-028006/01/000310/27/086NACELLE - POWER PLANT - BEARING ASSEMBLY FORWARD ENGINE MOUNT REPLACEMENT OF SNOUT BEARING BALL71-21-12V2500-A1,-A5
NAC-71-028108/07/000102/21/015NACELLE - EXHAUST - LIPSKIN ATTACH RIVETS, NOSE COWL - REPLACEMENT OF LIPSKIN ATTACH RIVETS71-11-00V2500-D5
NAC-71-028204/03/015NOSE COWL - FORWARD AND REAR BULKHEAD FITTINGS, THERMAL ANTI-ICE DUCT , NOSE COWL - MODIFICATION OF71-11-00V2500-D5
NAC-71-028305/21/015MODIFICATION SERVICE BULLETIN-NACELLE-PYLON APRON-NO.1 HINGE BEAM-MODIFICATION OF AND REPALCEMENT OF ATTACHING HARDWARE-FAN CASE ATTACH BRACKETS-MODIFICATION OF.71-14-00V2500-D5
NAC-71-028501/31/030412/06/043NACELLE - RIGHT HAND FAN COWL DOOR - HOLD OPEN ROD - RE-ORIENTATION OF THE HOLD OPEN ROD AND INSTALLATION OF A NEW ROD STOWAGE BRACKET71-13-12V2500-A1,-A5
ENG-71-028702/25/047POWER PLANT - RELAY BOX - INTRODUCTION OF A REVISED RELAY BOX71-00-00V2500-A1,-A5
NAC-71-028708/01/036MODIFICATION SERVICE BULLETIN - NACELLE - PYLON - UPPER ANDLOWER FITTINGS, THRUST REVERSER - ADDITION OF ACTUATOR PIN RETAINER71-00-00V2500-D5
ENG-71-028811/11/037POWER PLANT - ELECTRICAL HARNESSES - INTRODUCTION OF A COMBINED EEC FAN AND IGNITION SUPPLY HARNESS71-51-00V2500-A5
ENG-71-028903/08/046POWER PLANT - ELECTRICAL HARNESSES - LIGHT DUTY - EGT HARNESSES - INTRODUCTION OF REVISED CLIPS71-52-00V2500-A1,-A5
ENG-71-029005/09/176POWER PLANT - SOCKET CONTACT - INTRODUCTION OF TWO ALTERNATIVE SOCKET CONTACTS 71-52-43V2500-A5
NAC-71-029202/25/056NACELLE - POWERPOINT - COWL, AIR INTAKE - REPLACEMENT OF THE P2T2 MOUNTING BRACKET ASSEMBLY AND SEALING BLOC 673-22-11V2500-A1
NAC-71-029310/11/057NACELLE - POWERPLANT - FAN COWL DOOR - REWORK OF THE UPPER LOCATOR71-13-00V2500-A1,-A5
ENG-71-029408/23/057POWER PLANT - ELECTRICAL HARNESS - EEC HARNESS - FAN - DELETION OF LIGHTNING STRIKE PROTECTION SLEEVES - MOD 71-029471-51-00V2500-A5
NAC-71-029507/21/067NACELLE - POWERPLANT - CORE ENGINE - REWORK OF THE CORE FIRE DETECTOR AND THE REROUTING OF THE FIRE DETECTION HARNESSES71-52-00V2500-A5
NAC-71-029810/21/080111/10/086NACELLE - FORWARD AND AFT ENGINE MOUNT ASSEMBLIES- BOLT IDENTIFICATION71-20-00V2500-A1,-A5
NAC-71-029902/07/063NACELLE - V2500-A5 AIR INTAKE COWL SRM CHAPTER 54-10-00 REPAIR NO,4 VRS 2802 - AFT BULKHEAD HONEYCOMB REPAIR UPGRADE TO INSTALL FIRE SHEILD - NON-MODIFICATION SERVICE BULLETIN71-00-00V2500-A1,-A5
ENG-71-030305/24/060311/30/076POWER PLANT - ENGINE ELECTRONIC CONTROLLER (EEC) HARNESS-CORE - INTRODUCTION OF VOLTAGE DIVIDER HARNESS ASSEMBLY BETWEEN THE TRIM BALANCE PROBE AND ENGINE HARNESS71-00-00V2500-A1,-A5
NAC-71-030510/21/086NACELLE - FORWARD ENGINE MOUNT - BOLT PART NUMBER, INSPECTION OF71-00-00V2500-A1,-A5
NAC-71-030601/17/080108/07/088NACELLE - POWER PLANT - REPLACEMENT OF THE FAN COWL DOOR CORNER PIECES71-13-00V2500-A1,-A5
ENG-71-030701/21/167POWERPLANT - FANCASE HARNESS - HEALTH AND SAFETY MODIFICATION TO CHANGE CLAMP TYPE71-51-00V2500-A5
NAC-71-030801/22/070204/30/088NON-MODIFICATION SERVICE BULLETIN - NACELLE - FAN COWL - INSPECTION FOR FAN COWL DISBOND (FOR CONTROLLED SERVICE USE)71-13-00V2500-A1,-A5
ENG-71-031103/04/080104/07/088ENGINE - INSTALLATION OF CABLE WRAP ON THE ENGINE SYSTEM DRAIN PIPES (FOR CONTROLLED SERVICE USE) (BANGKOK AIRWAYS ONLY)71-00-00V2500-A5
NAC-71-031211/27/087NACELLE - POWERPLANT - DRAINS SYSTEM - REROUTING OF THE HYDRAULIC PUMP DRAIN TUBES71-71-00V2500-A5
ENG-71-031503/17/090104/21/094NON-MODIFICATION SERVICE BULLETIN - POWERPLANT - EBU - HUDRAULIC SUCTION LINE AND FUEL RETURN LINE HOSES - INSPECTION FOR APPLICATION OF PROPER TORQUE73-11-48V2500-A1,-A5
ENG-71-031911/19/156POWERPLANT - HARNESS CLAMP - REDUCTION OF HARNESS CLAMP SIZE REQUIREMENT AT CLIPPING POINT 240971-51-00V2500-D5
ENG-71-032002/13/188POWER PLANT -- BACKSHELL - PART NUMBER CORRECTION71-51-42V2500-A1,-A5
ENG-71-032202/13/188POWER PLANT -- BACKSHELL - PART NUMBER CORRECTION71-51-43V2500-A1,-A5
ENG-71-032402/13/188POWER PLANT - BACKSHELL - PART NUMBER CORRECTION71-51-42V2500-A1,-A5
ENG-71-032607/30/120111/08/198POWER PLANT - INTRODUCTION OF A LEASE COMPANY TITLE PLATE71-00-00V2500-A1,-A5
ENG-71-035010/23/198POWER PLANT -- BACKSHELL - PART NUMBER CORRECTION71-51-42V2500-A1,-A5
ENG-72-CN-0102/16/00See SBCONVERSION SERVICE BULLETIN - ENGINE - CONVERSION OF V2500 D528AQ04 TO D528AQ03 MODEL72-51-00V2500-D5
ENG-72-000101/19/906ENGINE - REMOVE MATERIAL FROM THE LEADING EDGE OF STAGE 2.0 COMPRESSOR BLADES TO IMPROVE CLEARANCE72-32-00V2500-A1
ENG-72-000206/15/936ENGINE - STAGE 1 TURBINE NOZZLE ASSEMBLY AND HP TURBINE ROTOR AND STATOR ASSEMBLY - INCORPORATION OF OFFSET SUPPORTS72-44-00V2500-A1
ENG-72-000306/11/927ENGINE - LP TURBINE - INTRODUCE A REVISED STAGE 7 LPT AIR SEAL72-50-00V2500-A1
ENG-72-000401/24/925ENGINE - DIFFUSER CASE ASSEMBLY - REPLACE THE NO. 4 BEARING SCAVENGE TUBE ASSEMBLY72-42-00V2500-A1
ENG-72-000512/08/897ENGINE - HP COMPRESSOR - INTRODUCTION OF WEIGHT REDUCED BORESCOPE BLANKS72-41-00V2500-A1
ENG-72-000606/28/915ENGINE - DIFFUSER AND COMBUSTOR GROUP AND STAGE 1 TURBINE NOZZLE ASSEMBLY - THERMAL BARRIER FOR COMBUSTION LINERS72-42-00V2500-A1
ENG-72-000711/22/914ENGINE - LP TURBINE - INCORPORATE REVISED EGT BRACKETS ON FLANGE P72-50-00V2500-A1
ENG-72-000805/10/917ENGINE - PROVIDE STAGES 1.5 AND 2.0 STATOR ASSEMBLIES WITH OUTER SHROUDS HAVING REDUCED THICKNESS72-32-00V2500-A1
ENG-72-000910/30/953ENGINE - INTERMEDIATE STRUCTURE - REWORK THE FAN FRAME ASSEMBLY TO INCLUDE FILLER COMPOUND IN THE REAR INNER FLANGE AREA72-32-00V2500-A1
ENG-72-001011/30/907ENGINE - PROVIDE A NO. 3 BEARING SEAL ASSEMBLY OF REDUCED WEIGHT AND REVISED MATERIAL72-32-00V2500-A1
ENG-72-001107/06/900504/04/978ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - REWORK THE STAGE 2 TURBINE HUB ASSEMBLY TO INCORPORATE A TURBINE HUB HEATSHIELD72-45-00V2500-A1
ENG-72-001209/25/956ENGINE - MAIN GEARBOX ASSEMBLY - REWORK THE IDG HOUSING ASSEMBLY AND THE RADIAL GEAR SUPPORT ASSEMBLY TO IMPROVE CLEARANCE REQUIREMENTS72-60-00V2500-A1
ENG-72-001311/22/917ENGINE - REPLACEMENT OF THE STAGE 1 HPT DUCT SEGMENT AND THE STAGE 1 HPT AIRSEAL72-44-00V2500-A1
ENG-72-001406/16/890301/15/953ENGINE - INCORPORATE REROUTED EGT HARNESS ASSEMBLY72-50-00V2500-A1
ENG-72-001512/09/916ENGINE - LP TURBINE ASSEMBLY - REPLACEMENT OF LP TURBINE ROTOR BOLTS72-50-00V2500-A1
ENG-72-001609/18/920109/18/928ENGINE - NO. 4 BEARING COMPARTMENT - NEW INNER NO. 4 BEARING AND AIRFRAME MANIFOLD ASSEMBLY72-42-00V2500-A1
ENG-72-001707/19/916ENGINE - INCORPORATE ROOT SEALING STRIPS ON STAGE 1.5,2.0, AND 2.5 LPC BLADES72-32-00V2500-A1
ENG-72-001805/03/917ENGINE - PROVIDE A NEW LP COMPRESSOR FRONT CASE ASSEMBLY AND A NEW LPC INLET GUIDE VANE ASSEMBLY72-32-00V2500-A1
ENG-72-001907/06/904ENGINE - INCORPORATE REPLACEMENT VARIABLE INLET GUIDE VANE BRACKET72-41-00V2500-A1
ENG-72-002004/15/936ENGINE - LP COMPRESSOR - FAN EXIT GUIDE VANE ASSEMBLY - INCORPORATION OF A REVISED BONDING PROCESS72-32-00V2500-A1
ENG-72-002110/19/903ENGINE - NO. 4 BEARING COMPARTMENT TUBES, REPLACEMENT OF OUTER SCAVENGE TUBE ASSEMBLY SEAL RINGS, SEALING SLEEVE, AND TUBE-TO-BOSS ELBOW72-42-00V2500-A1
ENG-72-002206/29/906ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - REPLACE THE STAGE 1 AND 2 HP TURBINE WIRESEAL72-45-00V2500-A1
ENG-72-002306/16/893ENGINE - ADDITION OF WASHERS FOR CONNECTION OF THE NF TERMINAL BLOCK AND THE EEC CORE HARNESS71-00-00V2500-A1
ENG-72-002405/31/913ENGINE - LP COMPRESSOR - INCORPORATION OF FIRE SHIELDS ON THE NO. 1 STRUT FAIRING PANELASSEMBLY72-32-00V2500-A1
ENG-72-002505/04/907ENGINE - HP COMPRESSOR - INTRODUCTION OF A WEIGHT REDUCED REAR OUTER CASE72-41-00V2500-A1
ENG-72-002601/05/907ENGINE - LP COMPRESSOR - FRONT SHAFT AND SEAL ASSEMBLY WITH STIFFENED SEAL CARRIER72-32-00V2500-A1
ENG-72-002707/05/930312/21/077ENGINE - HIGH PRESSURE COMPRESSOR - INTRODUCTION OF REDUCED WEIGHT FRONT COMPRESSOR CASING72-41-00V2500-A1
ENG-72-002804/19/917ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - INTRODUCE A REVISED STAGE 2 BLADE RETAINING PLATE72-45-00V2500-A1
ENG-72-002911/22/915ENGINE - STAGE 1 TURBINE NOZZLE ASEMBLY - REWORK THE STAGE 1 HP TURBINE OUTER AIRSEAL ASSEMBLY TO IMPROVE COOLING AIR TO THE HP TURBINE72-44-00V2500-A1
ENG-72-003002/09/906ENGINE - HP COMPRESSOR - STAGE 7 AND 8 ROTOR PATHS WITH REDUCED SPRAYED THICKNESS ABRADABLE LININGS72-41-00V2500-A1
ENG-72-003101/20/987ENGINE - PROVIDE A SEAL FOR THE BOOSTER STAGE BLEED VALVE ASSEMBLY AND A REPLACEMENT LPC INLET GUIDE VANE ASSEMBLY72-32-00V2500-A1
ENG-72-003210/19/906ENGINE - DIFFUSER AND COMBUSTION GROUP AND NO. 4 BEARING FRONT AND REAR COMPARTMENT - INCORPORATE NEW NO. 4 BEARING CARBON SEAL ASSEMBLIES MADE FROM REVISED MATERIAL72-42-00V2500-A1
ENG-72-003305/17/916ENGINE - HP COMPRESSOR - INTRODUCTION OF SCALLOPED HEAT SHIELD RETAINER - STAGE 7 BORESCOPE POSITION72-41-00V2500-A1
ENG-72-003402/01/916ENGINE - HP COMPRESSOR - STAGE 8 AND 11 REAR INNER CASING HEATSHIELD ASSEMBLIES WITH CORROSION PROTECTION72-41-00V2500-A1
ENG-72-003501/12/900305/29/986ENGINE - HPC DISKS AND BLADES - STAGE 3 TO 5 ANTI-FRET TREATMENT72-41-00V2500-A1
ENG-72-003606/14/915ENGINE - NO. 4 BEARING COMPARTMENT - REWORK NO. 4 BEARING FRONT AND REAR SEAL SEATS TO INCORPORATE REVISED SURFACE FINISH AND HARDFACE THICKNESS72-43-00V2500-A1
ENG-72-003707/26/930212/09/994ENGINE - LP TURBINE - REPLACE THE LP TURBINE SHAFT REAR END SEAL SEALING RING72-50-00V2500-A1
ENG-72-003805/17/916ENGINE - HP COMPRESSOR - INTRODUCTION OF 12 SPACERS ON THE REAR PISTON RING SEAL72-41-00V2500-A1
ENG-72-003911/10/894ENGINE - REVISED CLIPPING AT CP5737 AND THE CLIPPING BRACKET MODIFICATION72-50-00V2500-A1
ENG-72-004012/01/935ENGINE - DIFFUSER AND COMBUSTOR GROUP - SHOTPEEN THE NO. 4 BEARING SUPPORT ASSEMBLY72-42-00V2500-A1
ENG-72-004103/30/900109/27/046ENGINE - HP COMPRESSOR - INTRODUCTION OF A NEW REAR ROTATING SEAL AND A NEW REAR STATIC AIR SEAL ASSEMBLY72-00-00V2500-A1
ENG-72-004205/25/920111/16/016ENGINE - LP COMPRESSOR - REWORK THE LPC FRONT CASING ASSEMBLY TO INCORPORATE AN ENLARGED PIN HOLE DIAMETER72-32-00V2500-A1
ENG-72-004303/18/920303/18/923ENGINE - MAIN GEARBOX ASSEMBLY - INSPECT THE DEDICATED ALTERNATOR DRIVE GEAR72-60-00V2500-A1
ENG-72-004406/29/903ENGINE - LP COMPRESSOR - LPC BLEED DUCT WITH REDUCED 44 SQUARE INCH EXIT THROAT AREA72-32-00V2500-A1
ENG-72-004510/19/905ENGINE - INCORPORATE DRY FILM LUBRICANT TO THE NO. 2 AND NO. 10 STRUTS THRUST MOUNT BRACKETS71-00-00V2500-A1
ENG-72-004606/14/916ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - PROVIDE A NEW 1ST STAGE HPT BLADE AND 1ST STAGE COOLING DUCT ASSEMBLY72-44-00V2500-A1
ENG-72-004703/29/916ENGINE - LP COMPRESSOR - REWORK THE NO. 2 BEARING OIL JET ASSEMBLY TO INCORPORATE A REVISED LENGTH LOCATING PIN72-32-00V2500-A1
ENG-72-004803/15/934ENGINE - MAIN GEARBOX ASSEMBLY - INCORPORATE A DEDICATED ALTERNATOR DRIVE GEAR ASSEMBLY WITH DECREASED PINION TOOTH THICKNESS72-60-00V2500-A1
ENG-72-004908/31/916ENGINE - LPT SHAFT - RELOCATE MARKING LOCATION OF SHAFT LENGTH72-50-00V2500-A1
ENG-72-005010/19/905ENGINE - LP TURBINE - PROVIDE RECONTOURED EGT BRACKETS AND DOUBLE HEXAGONAL HEADED NUTS72-50-00V2500-A1
ENG-72-005102/22/910209/15/016ENGINE - LP COMPRESSOR - INCORPORATE A FUEL DRAIN TUBE IN THE FAN FRAME ASSEMBLY72-32-00V2500-A1
ENG-72-005204/05/915ENGINE - GENERAL - PROVIDE BOLTS OF INCREASED LENGTH AT CLIPPING POINTS CP0577, CP0560, AND CP053772-00-00V2500-A1
ENG-72-005302/11/947ENGINE - GENERAL - PROVIDE VARIOUS REPLACEMENT EXTERNAL TUBES WITH RELOCATED TUBE SLEEVES71-00-00V2500-A1
ENG-72-005402/02/94See SBENGINE - MAIN GEARBOX ASSEMBLY - CARBON SEAL MATING RINGS WITH CHROME PLATE ON THE SEALING SURFACES72-60-00V2500-A1
ENG-72-005501/05/907ENGINE - MAIN GEARBOX ASSEMBLY - INCORPORATE A TWO-PIECEOIL PRESSURE TUBE SUPPORT BRACKET72-60-00V2500-A1
ENG-72-005609/16/916ENGINE - TURBINE EXHAUST CASE ASSEMBLY - REWORK THE OIL FEED AND OIL SCAVENGE TUBE ASSEMBLIES TO INCORPORATE WEAR SLEEVES AT THE TUBE CLIPPING POINTS72-50-00V2500-A1
ENG-72-005711/02/906ENGINE - TURBINE EXHAUST CASE ASSEMBLY - REPLACE THE OIL SCAVENGE TUBE ATTACHING BOLTS72-50-00V2500-A1
ENG-72-005802/16/903ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - REMOVAL OF HP TURBINE CASE ORIFICE PLATES72-00-00V2500-A1
ENG-72-005909/07/905ENGINE - LP COMPRESSOR - REPLACE THE NO. 3 BEARING HOUSING ASSEMBLY SHOULDER STUDS WITH STUDS WHICH HAVE BEEN SHOTPEENED72-32-00V2500-A1
ENG-72-006002/08/915ENGINE - DIFFUSER AND COMBUSTION GROUP AND STAGE 1 TURBINE NOZZLE ASSEMBLY - INTRODUCE THERMAL BARRIER COATING ON INNER AND OUTER COMBUSTION CHAMBER LINERS72-42-00V2500-A1
ENG-72-006111/10/895ENGINE - LP TURBINE ROTOR AND STATOR ASSEMBLY - INCORPORATE REVISIONS TO THE MODULE IDENTIFICATION PLATE72-50-00V2500-A1
ENG-72-006211/24/894ENGINE - REWORK THE BIFURCATION DISCONNECT PANEL ASSEMBLY TO EXTEND SEALING FEATURES78-32-00V2500-A1
ENG-72-006308/15/968ENGINE - LP TURBINE ROTOR AND STATOR ASSEMBLY - INTRODUCE NEW TUBE ASSEMBLIES REQUIRED FOR MODIFIED TURBINE EXHAUST CASE72-50-00V2500-A1
ENG-72-006404/13/904ENGINE - HP COMPRESSOR - INTRODUCTION OF SUPPORT BRACKET FOR FRONT MOUNT DURING TRANSPORTATION72-41-00V2500-A1
ENG-72-006505/18/906ENGINE - DIFFUSER AND COMBUSTION GROUP - INTRODUCE A NEW NO. 4 BEARING FRONT COMPARTMENT GASKET72-42-00V2500-A1
ENG-72-006601/27/956ENGINE - LP COMPRESSOR - PROVIDE MARKING INSTRUCTIONS FOR VARIOUS MAJOR ASSEMBLIES72-32-00V2500-A1
ENG-72-006704/19/916ENGINE - LP TURBINE - DELETE THE MARKING REQUIREMENTS FOR THE STAGE 6 LP TURBINE DISK AND THE LP TURBINE SHAFT72-50-00V2500-A1
ENG-72-006811/30/906ENGINE - HPC REAR SHAFT - INCREASED LIFE REAR SHAFT72-41-00V2500-A1
ENG-72-006902/15/976ENGINE - STAGE 9 TO 12 DISK ASSEMBLY - INCREASED LIFE DISK ASSEMBLY72-41-00V2500-A1
ENG-72-007001/30/924ENGINE - MAIN GEARBOX ASSEMBLY - INCORPORATE A LAYSHAFT EXTENSION GEAR AND PMA DRIVE GEAR WITH INCREASED FACE WIDTH72-60-00V2500-A1
ENG-72-007102/23/906ENGINE - DIFFUSER AND COMBUSTOR GROUP - REPLACE THE NO. 4 BEARING OIL PRESSURE TUBE ASSEMBLY GASKET72-42-00V2500-A1
ENG-72-007209/21/904ENGINE - DIFFUSER AND COMBUSTION GROUP - REPLACE A NO. 4 BEARING COMPARTMENT TUBE BRACKET (CP5756)72-42-00V2500-A1
ENG-72-007304/19/915ENGINE - LP TURBINE ROTOR AND STATOR ASSEMBLY - INCORPORATE SERIAL NUMBER, PART NUMBER, AND ATA REFERENCE ON LP TURBINE CASE72-50-00V2500-A1
ENG-72-007401/04/914ENGINE - INCORPORATION OF REDESIGNED ACC ACTUATOR REAR MOUNT BRACKET72-40-00V2500-A1
ENG-72-007508/20/938ENGINE - INTRODUCE RECONTOURED STAGE 1 AND 2 TURBINE ROTOR HUBS72-45-00V2500-A1
ENG-72-007611/29/915ENGINE - HP TURBINE - INCORPORATE AN IMPROVED TURBINE LOCK72-45-00V2500-A1
ENG-72-007708/16/917ENGINE - LP COMPRESSOR - PROVIDE A FAN FRAME ASSEMBLY WITH REVISED ATTACHMENT FEATURES72-32-00V2500-A1
ENG-72-007803/30/920303/30/926ENGINE - HP COMPRESSOR - REWORK THE FUEL FLOW DIVIDER MOUNT BRACKET ASSEMBLIES TO PROVIDEADDITIONAL TOOL CLEARANCE72-00-00V2500-A1
ENG-72-007912/07/900103/22/916ENGINE - HP COMPRESSOR - INTRODUCE A STRENGTHENED NO. 4 BEARING BUFFER AIR TUBE BRACKET ASSEMBLY72-40-00V2500-A1
ENG-72-008012/21/905ENGINE - HP COMPRESSOR - REPLACE A BRACKET AT FLANGE FJ72-41-00V2500-A1
ENG-72-008106/22/926ENGINE - REPLACE AN960 SERIES WASHERS72-32-00V2500-A1
ENG-72-008201/18/916ENGINE - LP COMPRESSOR - REWORK THE NO. 1 BEARING SEAL ASSEMBLY TO INCORPORATE A REVISED SLEEVE SPACER AND RETAINING COLLAR72-32-00V2500-A1
ENG-72-008301/18/916ENGINE - LP COMPRESSOR - BIFURCATION PANEL - INCORPORATION OF NEW SEALING PROCESS72-38-00V2500-A1
ENG-72-008410/02/927ENGINE - HP COMPRESSOR VARIABLE STATOR VANES - REDUCED NUMBER OF RIGGING PIN BRACKETS72-41-00V2500-A1
ENG-72-008511/22/917ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - PROVIDE NEW STAGE 2 DUCT SEGMENTS INCORPORATING REVISED COATING REQUIREMENTS72-45-00V2500-A1
ENG-72-008605/24/917ENGINE - MAIN GEARBOX ASSEMBLY - PROVIDE A NEW IDG MOUNTING PAD FEATURING AN ADDED DOWEL PIN HOLE72-60-00V2500-A1
ENG-72-008704/19/915ENGINE - NO. 4 BEARING COMPARTMENT - INTRODUCE A NEW HEATSHIELDED NO. 4 BEARING SCAVENGE TUBE ASSEMBLY72-42-00V2500-A1
ENG-72-008808/30/936ENGINE - BIFURCATION PANEL - ADDITION OF STIFFENER PLATES AT RIVETED JOINT BETWEEN UPPER AND LOWER PANELS72-38-00V2500-A1
ENG-72-008909/28/906ENGINE - LP TURBINE - REMOVE THE CORRELATION MARK ON THE 6TH STAGE INNER AIRSEAL72-50-00V2500-A1
ENG-72-009009/28/906ENGINE - LP COMPRESSOR - REWORK THE NO. 1 BEARING AND NO. 3 BEARING SEAL SEATS TO INCORPORATE AN INCREASED HARDFACE THICKNESS AND A REVISED SURFACE FINISH REQUIREMENT72-32-00V2500-A1
ENG-72-009106/22/90See SBENGINE - CASE AND VANE ASSEMBLY - HP TURBINE, STAGE 1 DUCT SEGMENTS72-45-00V2500-A1
ENG-72-009205/10/918ENGINE - HP TURBINE - PROVIDE A TURBINE CASE AND VANE ASSEMBLY THAT WILL ALLOW INDIVIDUAL FIRST STAGE DUCT REPLACEMENT72-45-00V2500-A1
ENG-72-009305/17/910211/08/916ENGINE - LP COMPRESSOR - REWORK THE NO. 3 BEARING HOUSING ASSEMBLY TO INCORPORATE REVISED MATERIAL PINS72-32-00V2500-A1
ENG-72-009401/11/910101/06/926ENGINE - LP COMPRESSOR - REPLACE THE FAN EXIT GUIDE VANE ASSEMBLY PLATFORM BOLTS72-32-00V2500-A1
ENG-72-009502/10/988ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - PROVIDE A NEW HPT RETAINING NUT72-40-00V2500-A1
ENG-72-009605/01/920105/01/926ENGINE - LP COMPRESSOR - INCORPORATE ANTI-FRET COATING ON THE ANNULUS FILLER ASSEMBLY FRONT FACE72-31-00V2500-A1
ENG-72-009701/10/927ENGINE - NO. 4 BEARING COMPARTMENT - PROVIDE A NO. 4 BEARING COOLING DUCT AND HEATSHIELD WITH IMPROVED SEALING FEATURES72-43-00V2500-A1
ENG-72-009801/18/910205/29/987ENGINE - HP COMPRESSOR - TO ANNOUNCE A NEW HPC REAR SHAFT ASSEMBLY72-41-00V2500-A1
ENG-72-009909/30/930109/30/936ENGINE - DIFFUSER CASE - PROVIDE REPLACEMENT UNION AND GASKET SEAL AT ACAC AIR OFFTAKE72-42-00V2500-A1
ENG-72-010012/19/916ENGINE - HP COMPRESSOR - INTRODUCTION OF STRENGTHENED BORESCOPE BLANKING PLUG ASSEMBLIES AND GASKET SEALS AT STAGES 8, 9, AND 11 AND GASKET SEAL AT STAGE 772-41-00V2500-A1
ENG-72-010108/20/936ENGINE - HP TURBINE - PROVIDE A NEW STAGE 2 HP TURBINE HUB ASSEMBLY WITH REVISED METERING PLUGS72-45-00V2500-A1
ENG-72-010203/31/927ENGINE - HP COMPRESSOR - TO ANNOUNCE A NEW STAGE 9 TO 12 DISK ASSEMBLY72-41-00V2500-A1
ENG-72-010304/14/957ENGINE - LP COMPRESSOR - PROVIDE A NEW WEIGHT REDUCED FAN CASE ASSEMBLY72-32-00V2500-A1
ENG-72-010410/16/915ENGINE - TURBINE EXHAUST CASE ASSEMBLY - PROVIDE HEATSHIELDS FOR THE NO. 5 BEARING TUBE ELBOWS72-50-00V2500-A1
ENG-72-010512/20/910204/28/007ENGINE - LP COMPRESSOR - PROVIDE A SEGMENTED REAR FAIRING ASSEMBLY72-32-00V2500-A1
ENG-72-010612/01/97See SBCANCELLATION OF ENGINE SERVICE BULLETIN V2500-ENG-72-0106 (LP TURBINE ASSEMBLY - REPLACEMENT OF LP TURBINE ROTOR BOLTS)72-00-00V2500-A1
ENG-72-010706/23/924ENGINE - LP TURBINE - INTRODUCE NEW THRUST REVERSER HOLD OPEN ROD FITTINGS72-50-00V2500-A1
ENG-72-010811/22/916ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - INCORPORATE NEW STAGE 1 DUCT SEGMENTS WITH IMPROVED CERAMIC COATING72-45-00V2500-A1
ENG-72-010912/03/935ENGINE - HP COMPRESSOR - STAGE 9 COMPRESSOR ROTOR BLADE WITH CUTBACK PLATFORM72-41-00V2500-A1
ENG-72-011004/13/926ENGINE - LP TURBINE - PROVIDE AN OUTER DIFFUSER SUPPORT ASSEMBLY WITH SILVER PLATED CLINCH NUTS72-50-00V2500-A1
ENG-72-011101/10/927ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - NEW STAGE 1 HPT AIRSEAL72-45-00V2500-A1
ENG-72-011206/15/945ENGINE - DIFFUSER AND COMBUSTION GROUP - PROVIDE A NEW NO. 4 BEARING SUPPORT ASSEMBLY WITHINCREASED DURABILITY72-42-00V2500-A1
ENG-72-011307/31/926ENGINE - STAGE 1 TURBINE NOZZLE ASSEMBLY - PROVIDE NEW FIRST STAGE DUCT SEGMENTS AND DUCT STOPS WITH BOLT HOLE CHAMFERS72-44-00V2500-A1
ENG-72-011408/10/956ENGINE - LP COMPRESSOR - ADD PART NUMBER MARKINGS TO VARIOUS ADJUSTING WASHERS72-32-00V2500-A1,-A5,-D5
ENG-72-011504/15/926ENGINE - DIFFUSER AND COMBUSTION GROUP - PROVIDE A NEW NO. 4 BEARING PRESSURE TUBE ASSEMBLY72-42-00V2500-A1
ENG-72-011602/15/957ENGINE - DIFFUSER AND COMBUSTION GROUP AND STAGE 1 TURBINE NOZZLE ASSEMBLY - PROVIDE NEWINNER AND OUTER COMBUSTION CHAMBER ASSEMBLIES WITH GENERATION 11 LINER SEGMENTS72-00-00V2500-A1
ENG-72-011704/08/927ENGINE - LP TURBINE - PROVIDE A NEW LP TURBINE SHAFT THAT ELIMINATES NITRIDING ON THE SPLINE72-50-00V2500-A1
ENG-72-011803/24/954ENGINE - MAIN GEARBOX ASSEMBLY - PROVIDE NEW OIL SCAVENGE PUMP SPACERS WITH IMPROVED ANTIROTATION FEATURES79-22-00V2500-A1
ENG-72-011909/18/923ENGINE - DIFFUSER AND COMBUSTION GROUP - INCOPORATE REVISED FUEL DISTRIBUTION VALVE BRACKET AND ADD NEW FUEL MANIFOLD SUPPORT BRACKETS72-00-00V2500-A1
ENG-72-012007/31/920512/06/023ENGINE - NO. 4 BEARING COMPARTMENT - NEW NO. 4 BEARING SCAVENGE TUBE ASSEMBLY AND GASKET72-42-00V2500-A1
ENG-72-012101/15/948ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - PROVIDE NEW STAGE 2 HPT AIR SEAL ASSEMBLY72-45-00V2500-A1
ENG-72-012207/17/920301/15/978ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - PROVIDE NEW STAGE 2 HPT VANE ASSEMBLIES, STAGE 2 AIR SEALING RING SEGMENT ASSEMBLIES, AND STAGE 2 HPT SEALS72-45-00V2500-A1
ENG-72-012307/17/928ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - PROVIDE A NEW STAGE 1 HPT HUB METERING PLUG WITH A SMALLER METERING HOLE AND TRANSFER THE HUB DETAILS TO THE STAGE 1 TURBINE ROTOR ASSEMBLY72-45-00V2500-A1
ENG-72-012409/19/928ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - PROVIDE NEW HPT BAND SEGMENT ASSEMBLIES AND NEW HPT DUCT SUPPORT ASSEMBLIES72-45-00V2500-A1
ENG-72-012506/24/940112/04/086ENGINE - LP TURBINE - INCORPORATE LPT DISK AND DIFFUSER SUPPORT ASSEMBLY NUTS WITH REVISED COATING72-50-00V2500-A1
ENG-72-012601/15/947ENGINE - NO. 4 BEARING COMPARTMENT - PROVIDE A NEW SOURCE FOR THE NO. 4 BEARING72-43-00V2500-A1
ENG-72-012702/20/920301/18/93See SBENGINE - MAIN GEARBOX ASSEMBLY - PROVIDE A NEW DEOILER CARBON SEAL ASSEMBLY (FOR CONTROLLED SERVICE USE)72-60-00V2500-A1
ENG-72-012811/15/937ENGINE - LP COMPRESSOR - DELETION OF UNNECESSARY SCREWS ON THE ACOC INLET DUCT FAIRINGS72-32-00V2500-D5
ENG-72-012906/21/933ENGINE - INSPECT THE OIL SCAVENGE PUMP DRIVE AND DRIVEN GEARS72-60-00V2500-A1
ENG-72-013005/10/927ENGINE - HP COMPRESSOR DISKS - COMPRESSOR STAGE 3 TO 8 ROTOR DRUM ASSEMBLY WITH SPACERS INTRIPLE MELT TITANIUM72-41-00V2500-A1
ENG-72-013107/31/920107/31/928ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - NEW STAGE 1 HPT AIR SEAL72-45-00V2500-A1
ENG-72-013206/30/930105/30/978ENGINE - LP COMPRESSOR - REMOVAL OF SIXTH STAGE BUFFER AIR SYSTEM72-00-00V2500-A1
ENG-72-013304/23/998ENGINE - LP COMPRESSOR - LPC BLEED VALVE LINKAGE SYSTEM WITH IMPROVED DURABILITY72-32-00V2500-A1
ENG-72-013408/25/956ENGINE - LP TURBINE ROTOR AND STATOR ASSEMBLY - THIRD STAGE TURBINE BLADE SHROUD REWORK72-50-00V2500-A1
ENG-72-013504/10/923ENGINE - HIGH PRESSURE SYSTEM MODULE - DO A CLEARANCE INSPECTION BETWEEN THE FUEL FLOW DIVIDER VALVE REAR BRACKET ASSEMBLY AND THE FUEL N077LE SUPPLY MANIFOLD72-40-00V2500-A1
ENG-72-013606/20/958ENGINE - LP COMPRESSOR - DELETION OF POLYURETHANE COATING ON FRONT FAIRING ASSEMBLY72-32-00V2500-A1
ENG-72-013804/29/940803/19/097ENGINE - LP TURBINE - ROTOR AND STATOR ASSEMBLY - INTRODUCE NEW LP TURBINE BLADES AND VANES72-50-00V2500-A1
ENG-72-013907/30/958ENGINE - FUEL AND CONTROL - CDX MODIFIER ADJUSTMENT FOR DELIVERED ENGINES72-00-00V2500-D5
ENG-72-014011/07/944ENGINE - FAN CASE ASSEMBLY - PROVIDE SHORTER FAN EXIT GUIDE VANE BOLT TO ELIMINATE INTERFERENCE BETWEEN BOLT AND EEC MOUNT BRACKET72-32-00V2500-A1
ENG-72-014110/15/926ENGINE - HP COMPRESSOR - STAGE 10 CASE ASSEMBLY - REPLACE- MENT OF STAGE 10 PISTON RING SEAL RIVETS72-41-00V2500-A1
ENG-72-014212/15/926ENGINE - LP TURBINE ROTOR AND STATOR ASSEMBLY - INTRODUCE A NEW NO. 5 BEARING CARBON SEALASSEMBLY72-50-00V2500-A1
ENG-72-014306/30/946ENGINE - HP COMPRESSOR - DELETION OF THE HEAT SHIELD AT THE OUTLET GUIDE VANE INNER CASE LOCATION72-42-00V2500-A1
ENG-72-014401/03/947ENGINE - LP COMPRESSOR - INTRODUCE A REVISED 2.5 STATOR ASSEMBLY WITH VANES INCORPORATING A RELOCATED LOCATOR BOLT HOLE72-32-00V2500-A1,-D5
ENG-72-014502/25/947ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - PROVIDE A NEW STAGE 2 TURBINE ROTOR DISK WITH INCREASED FRONT SNAP DIAMETER72-00-00V2500-A5
ENG-72-014606/25/937ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - PROVIDE A NEW STAGE 1 HPT BLADE - CATEGORY CODE 7 - MOD.ENG-72-014672-45-00V2500-A5,-D5
ENG-72-014709/15/958ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - PROVIDE A NEW STAGE 1 HPT SUPPORT ASSEMBLY AND NEW STAGE 1 HPT VANE ASSEMBLY72-44-00V2500-A5,-D5
ENG-72-014808/20/935ENGINE - NO. 4 BEARING COMPARTMENT - REPLACE EXISTING TUBE ADAPTORS WITH TUBE ADAPTORS HAVING AN INCREASED INNER DIAMETER72-42-00V2500-A5,-D5
ENG-72-014902/27/956ENGINE - LP COMPRESSOR - PROVIDE A PART NUMBER IDENTIFICATION FOR LPC MODULES THAT HAVE THE SIXTH STAGE BUFFER AIR CONFIGURATION REMOVED72-32-00V2500-A1
ENG-72-015002/07/940310/24/007ENGINE - LP COMPRESSOR - PROVIDE A NEW WEIGHT REDUCED FAN FRAME ASSEMBLY AND ASSOCIATEDDETAILS72-32-00V2500-A1
ENG-72-015108/20/937ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - PROVIDE NEW FIRST STAGE HPT VANE PLATFORMSEALS AND ADDITIONAL CLASSES OF VANE CLUSTERS72-44-00V2500-A5,-D5
ENG-72-015207/30/946ENGINE - LP COMPRESSOR - REPLACE THE PTO DRIVE BEARING SUPPORT SHAFT SEALING RING72-32-00V2500-A5
ENG-72-015301/30/987ENGINE - MAIN GEARBOX ASSEMBLY - INTRODUCE A NEW GEARBOX CASING ASSEMBLY AND NEW IDG HOUSING ASSEMBLY72-60-00V2500-A1,-A5
ENG-72-015409/16/946ENGINE - HP COMPRESSOR RING CASE - STAGE 10 CASE ASSEMBLY WITH INCREASED NUMBER OF RIVETS72-41-00V2500-A1,-A5
ENG-72-015503/15/946ENGINE - LP COMPRESSOR - PROVIDE A NEW 2.5 BLEED DUCT ASSEMBLY WITH IMPROVED DURABILITY FEATURES72-32-00V2500-A5,-D5
ENG-72-015609/11/956ENGINE - LP COMPRESSOR - REPLACE THE FAN CASE ASSEMBLY NO. 1 RUBBER SEAL ASSEMBLY72-32-00V2500-A1
ENG-72-015707/29/940208/16/067ENGINE - LP TURBINE ASSEMBLY - INTRODUCTION OF LP TURBINE DISKS STAGE 3 TO 7 WITH SHOTPEENED BLADE SLOTS72-50-31V2500-A1
ENG-72-015805/28/936ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - REMOVE THE STAGE 1 AND 2 TURBINE (INTERSTAGE FRONT OUTER) WIRE SEAL72-45-00V2500-A1,-A5,-D5
ENG-72-015902/25/947ENGINE - DIFFFUSER AND COMBUSTION SECTION - INTRODUCE NEW INNER AND OUTER COMBUSTION CHAMBER ASSEMBLIES72-42-00V2500-A5,-D5
ENG-72-016012/24/967ENGINE - LP COMPRESSOR - PROVIDE A NEW FAN CASE ASSEMBLY THAT ELIMINATES THE PROVISIONS FOR A TRANSITION RING72-32-00V2500-A1,-A5
ENG-72-016106/21/930409/06/966ENGINE - HP DISKS AND BLADES - STAGES 7 AND 8 ROTOR BLADES WITH DAMPING WIRES AND STAGES6,7, AND 8 BLADES WITH ANTI FRET COATING72-41-00V2500-A1
ENG-72-016209/15/936ENGINE - LP TURBINE - INTRODUCE A NO. 5 BEARING FACE SEAL ASSEMBLY WITH DECREASED THICKNESS72-50-00V2500-A1
ENG-72-016311/08/938ENGINE - NO. 4 BEARING COMPARTMENT - PROVIDE A NEW NO. 4 BEARING SEAL ASSEMBLY WITH NUTS SILVER PLATED ON THE THREADS ONLY72-42-00V2500-A1,-A5,-D5
ENG-72-016412/22/970107/20/987ENGINE - LP TURBINE ROTOR AND STATOR AND ASSEMBLY - INTRODUCE A TWO-PIECE LP TURBINE CASE ASSEMBLY72-50-00V2500-A1,-A5,-D5
ENG-72-016510/15/935ENGINE - LP TURBINE - REPLACE THE EXISTING NO. 5 BEARING SEAL SPACER WITH A SPACER INCORPORATING FOOL-PROOF INSTALLATION FEATURES72-50-00V2500-A1,-A5,-D5
ENG-72-016609/15/940408/24/066ENGINE - DIFFUSER CASE ASSEMBLY - REMOVE THE STAGE 1 HP TURBINE COOLING AIR PRESSURE SENSING TUBES72-42-00V2500-A1,-A5,-D5
ENG-72-016709/15/936ENGINE - DIFFUSER AND COMBUSTION SECTION - REPLACE THE EXISTING NO. 4 BEARING SCAVENGE TUBE CRUSH GASKET WITH A GASKET HAVING IMPROVED SEALING FEATURES72-42-00V2500-A1,-A5,-D5
ENG-72-016806/30/956ENGINE - NO. 4 BEARING COMPARTMENT - INTRODUCE A NEW NO. 4 BEARING OIL TUBE ASSEMBLY72-42-00V2500-A1,-A5,-D5
ENG-72-016907/02/936ENGINE - HP COMPRESSOR - INTRODUCE NEW STAGE 6 HP COMPRESSOR VARIABLE STATOR VANES MADE OFIMPROVED CORROSION RESISTANT MATERIAL72-41-00V2500-A1
ENG-72-017009/22/957ENGINE - LP COMPRESSOR - REMOVE UNNECESSARY BLANKING PLATES AND OIL DRAIN TUBE FROM THE FAN FRAME ASSEMBLY72-32-00V2500-D5
ENG-72-017107/13/956ENGINE - LP COMPRESSOR - PROVIDE IDENTIFICATION FOR LPC/ INTERMEDIATE CASE MODULE72-32-00V2500-A1
ENG-72-017212/03/936ENGINE - HP COMPRESSOR - PROVIDE STAGES 9 TO 12 LOCKING BLADES WITH REVISED PLATFORM CORNER PROFILES72-41-00V2500-A1,-A5,-D5
ENG-72-017308/20/936ENGINE - TURBINE EXHAUST - REPLACE THE NO. 5 BEARING COVER PACKING WITH A NEW IMPROVED SEAL72-00-00V2500-A1
ENG-72-017406/25/947ENGINE - HP COMPRESSOR - STAGE 9 ROTOR BLADES WITH MODIFIED PLATFORM PROFILE72-41-00V2500-A1
ENG-72-017501/09/956ENGINE - LP COMPRESSOR - PROVIDE LONGER ATTACHING BOLTS FOR THE OPEN LATCH INDICATOR BRACKET72-32-00V2500-A1,-A5
ENG-72-017607/26/960108/21/028ENGINE - HP COMPRESSOR - INTRODUCE AN HP SYSTEM MODULE SERIAL NUMBER IDENTIFICATION PLATE72-41-00V2500-A1,-A5
ENG-72-017708/08/976ENGINE - HP COMPRESSOR - PROVIDE AN HP COMPRESSOR REAR OUTER CASE ASSEMBLY WITH REVISED AREAS OF ANTI-WEAR COMPOUND72-41-00V2500-D5
ENG-72-017809/30/930105/29/987ENGINE - HP COMPRESSOR DISKS - STAGE 3 TO 8 ROTOR DRUM WITH THICKER STAGE 6 DISK HUB AND DAMPING WIRE LOCATING LIPS72-41-00V2500-A1,-A5,-D5
ENG-72-017909/22/970109/22/976ENGINE - LP TURBINE ROTOR AND STATOR ASSEMBLY - PROVIDE IAE PART NUMBER IDENTIFICATION FOR VARIOUS LPT ROTOR NUTS72-50-00V2500-A1,-A5,-D5
ENG-72-018002/10/986ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - INTRODUCE A NEW FIRST STAGE TURBINE OUTERAIR SEAL72-45-00V2500-A5,-D5
ENG-72-018102/07/976ENGINE - HP COMPRESSOR - INTRODUCE VARIABLE STATOR RIG PIN BRACKETS WITH SLOTTED HOLES72-41-00V2500-A1
ENG-72-018203/06/956ENGINE - HP COMPRESSOR RING CASES - STAGES 7, 9, AND 10 INNER CASES - SPACERS AT HEATSHIELD RETAINER ATTACHMENT POINTS WITH REDUCED SPIGOT LENGTHS72-41-00V2500-A1
ENG-72-018302/07/976ENGINE - PROVIDE A NEW DEOILER SEAL ASSEMBLY72-60-00V2500-A1
ENG-72-018412/20/954ENGINE - LP COMPRESSOR - BORESCOPE INSPECTION FOR NO. 1 OIL FEED TUBE72-32-00V2500-A1
ENG-72-018511/24/947ENGINE - HP COMPRESSOR - STAGE 10 COMPRESSOR CASE ASSEMBLY WITH AN INTEGRAL SEAL AND ARMAND REVISED SEAL RING72-41-00V2500-A5,-D5
ENG-72-018603/07/970206/16/006ENGINE - HP COMPRESSOR - NEW VARIABLE INLET GUIDE VANES AND NEW STAGES 3 AND 4 VARIABLE STATOR VANES REDESIGNED TO ALLOW INCREASED ANGULAR MOVEMENT72-41-00V2500-A5,-D5
ENG-72-018702/20/970102/20/977ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - PROVIDE A NEW STAGE 2 TURBINE BLADE (FOR VARIOUS MODEL PARTS COMMONALITY)72-45-00V2500-A5
ENG-72-018808/24/986ENGINE - LP COMPRESSOR - INTRODUCE A NEW LPC BLEED SCREEN WITH IMPROVED DURABILITY FEATURES72-32-00V2500-A1
ENG-72-018907/11/970204/27/018ENGINE - REPLACE VARIOUS TUBES IN THE BIFURCATION PANEL AREA TO PROVIDE ADEQUATE CLEARANCES WITH FAN COWL DOOR HOLD OPEN RODS72-00-00V2500-A5
ENG-72-019001/27/940310/31/024ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - INTRODUCE A NEW STAGE 1 HPT AIR SEAL AND A NEW NO. 4 BEARING REAR COOLING DUCT ASSEMBLY72-00-00V2500-A1,-A5,-D5
ENG-72-019107/12/966ENGINE - ATTACHING PARTS AND FITTINGS - HP SYSTEM MODULE - IMPROVED COOLING AIR DEFLECTOR FOR CABIN AIR PRESSURE REGULATING VALVE72-00-00V2500-A5
ENG-72-019203/03/940302/20/973ENGINE - TURBINE EXHAUST CASE ASSEMBLY AND FITTINGS - REMOVE THE TUBINE EXHAUST CASE FAIRING72-50-00V2500-A1,-A5,-D5
ENG-72-019307/15/946ENGINE - CORE TO FAN CASE INTERFACE SEALING OF BIFURCATION PANEL72-00-00V2500-A1,-A5
ENG-72-019406/30/958ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - INTRODUCE A NEW STAGE 1 HP TURBINE AIR SEAL72-45-00V2500-A5,-D5
ENG-72-019705/17/947ENGINE - ANGLE GEARBOX ASSEMBLY - INTRODUCTION OF MODIFIED BRACKET SUPPORT - VSCF OIL COOLING TUBES72-60-00V2500-D5
ENG-72-019802/28/956ENGINE - LP COMPRESSOR - RELOCATE THE FAN BLADE POSITION MARKING INFORMATION ON THE BLADE RETAINER71-00-00V2500-A1,-A5,-D5
ENG-72-019912/01/946ENGINE - MAIN GEARBOX ASSEMBLY - PROVIDE NEW CARBON SEAL MATING RINGS FEATURING ANTIROTATION PROVISIONS72-60-00V2500-D5
ENG-72-020112/12/946ENGINE - HP COMPRESSOR - INTRODUCE A NEW STAGE 3 HPC ROTOR BLADE WITH A CUT BACK SHROUD72-41-00V2500-A5,-D5
ENG-72-020202/14/977ENGINE - HP COMPRESSOR - INTRODUCE A STRENGTHENED HPC REAR SHAFT AND A NEW MATING REAR ROTATING SEAL72-41-00V2500-A5,-D5
ENG-72-020412/12/946ENGINE - HP COMPRESSOR - INTRODUCE A NEW STAGE 12 LH LOCKING BLADE WITH AN INCREASED PLATFORM CROP72-41-00V2500-A5,-D5
ENG-72-020501/15/954ENGINE - MAIN GEARBOX ASSEMBLY - PROVIDE A NEW HYDRAULIC PUMP DRIVE GEAR WITH GREASE LUBRICATED SPLINES72-60-00V2500-D5
ENG-72-020612/15/943ENGINE - DIFFUSER AND COMBUSTOR GROUP - PROVIDE A NEW BRACKET ASSEMBLY WHICH HAS ADDITIONAL SUPPORT FOR THE FIRE DETECTION RAIL72-42-00V2500-D5
ENG-72-020712/15/948ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - PROVIDE A NEW STAGE 2 HPT AIR SEAL ASSEMBLY FEATURING RECONTOURED ,FORWARD AND REARWARD MATING SURFACES AND A TAPERED WEB72-45-00V2500-A1,-A5,-D5
ENG-72-020807/25/950103/24/974ENGINE - LP TURBINE ROTOR AND STATOR ASSEMBLY - INCORPORATE A REVISED TORQUING PROCEDURE FOR THE NO. 5 BEARING LOCK NUT72-50-00V2500-A1,-A5,-D5
ENG-72-020903/01/95See SBENGINE - FAN CASE - PROVIDE DATA ACQUISITION INSTRUMENTATION AND HARDWARE72-32-00V2500-A1
ENG-72-021005/29/95See SBENGINE - HP COMPRESSOR - CONTROLLED SERVICE USE OF INSTRUMENTATION FOR HP COMPRESSOR AND HANDLING BLEED VALVE CHECKS36-00-00V2500-A1
ENG-72-021112/26/967ENGINE - LP COMPRESSOR - PROVIDE A NEW FAN FRAME ASSEMBLY AND ELIMINATE A T2.5 THERMOCOUPLE72-32-00V2500-A1,-A5
ENG-72-021207/25/956ENGINE - LP COMPRESSOR - PROVIDE A NEW FAN CASE-TO-MAIN GEARBOX ASSEMBLY MATING SEAL RING72-32-00V2500-A1,-A5,-D5
ENG-72-021303/28/956ENGINE - LP COMPRESSOR - TO REVISE THE MODULE ASSEMBLY NUMBER ON THE IDENTIFICATION PLATE72-32-00V2500-A1,-A5
ENG-72-021409/22/956ENGINE - LP COMPRESSOR - PROVIDE A NEW PTO SHAFT BEARING INNER RACE AND RETAINING RING72-32-00V2500-A5,-D5
ENG-72-021512/05/976ENGINE - SECURING FEATURES - HP COMPRESSOR CASES - REVISED BOLTS FOR FJ FLANGE BRACKETS72-41-00V2500-D5
ENG-72-021605/08/998ENGINE - LP COMPRESSOR - ADDITIONAL PLATE NUT ON THE NO. 1 STRUT FAIRING PANEL FOR FIRE SHIELD72-32-00V2500-A1,-A5
ENG-72-021705/03/956ENGINE - HP COMPRESSOR - REVISE REPAIR MARKING INFORMATION ON HP COMPRESSOR REAR SHAFT ASSEMBLY72-41-00V2500-A1
ENG-72-021807/30/958ENGINE - FUEL AND CONTROL - CDX MODIFIER ADJUSTMENT FOR DELIVERED ENGINES72-00-00V2500-D5
ENG-72-021908/10/956ENGINE - LP COMPRESSOR - THREAD CHANGE OF FAIRING REAR ATTACHING BOLT72-32-00V2500-A1
ENG-72-022007/30/960406/30/038ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - INTRODUCE NEW FIRST AND SECOND STAGE TURBINE BLADES WITH MORE DURABLE TIPS AND IMPROVED REPAIRABILITY72-45-00V2500-A1,-A5,-D5
ENG-72-022103/15/967ENGINE - DIFFUSER AND COMBUSTION GROUP - INTRODUCTION OF A NEW DIFFUSER CASE ASSEMBLY72-42-00V2500-A1
ENG-72-022202/10/984ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - INTRODUCE A NEW STAGE 2 TURBINE BLADE LOCK RETAINER72-45-00V2500-A1,-A5,-D5
ENG-72-022311/21/976ENGINE - HP COMPRESSOR - REPLACE HP COMPRESSOR CASE FLANGE AND FUEL COOLED OIL COOLER BRACKET ATTACHING BOLTS72-41-00V2500-A1,-A5
ENG-72-022403/20/966ENGINE - LP COMPRESSOR - REMARKING OF THE SLOT NUMBER ON THE FAN DISK72-00-00V2500-A1,-A5
ENG-72-022512/04/958ENGINE - MAIN GEARBOX ASSEMBLY - PROVIDE A REWORK FOR THE MAIN OIL SCAVENGE PUMP HOUSING ASSEMBLY TO ELIMINATE AN INTERFERENCE WITH A PUMP PACKING72-60-00V2500-D5
ENG-72-022610/17/954ENGINE - LP COMPRESSOR - ENLARGE THE HOLE DIAMETER OF THE FAN CASE REAR EXTENSION72-00-00V2500-D5
ENG-72-022710/31/950306/16/016ENGINE - LP TURBINE - PROVIDE A NEW BLIND CAP WITH DECREASED SEAL LAND HEIGHT72-50-00V2500-A1,-A5,-D5
ENG-72-022801/19/967ENGINE - DEDICATED ALTERNATOR ROTOR - INTRODUCTION OF NEW SOURCE OF SUPPLY72-60-00V2500-D5
ENG-72-022901/19/967ENGINE - DEDICATED ALTERNATOR ROTOR - INTRODUCTION OF NEW SOURCE OF SUPPLY72-60-00V2500-A1,-A5
ENG-72-023002/10/966ENGINE - SEAL, NO. 1 STRUT FIRE SHIELD - REPLACEMENT OF72-32-00V2500-A1,-A5
ENG-72-023101/15/968ENGINE - PROVIDE INSTRUCTIONS TO CHANGE THE DATA ENTRY PLUG ASSEMBLY AND THE ELECTRONIC ENGINE CONTROL TO OBTAIN A V2527E-A5 RATING72-00-00V2500-A5
ENG-72-023202/01/968ENGINE - MAIN GEARBOX ASSEMBLY - PROVIDE A MODIFIED VSCF DRIVE GEAR PLUG ASSEMBLY72-60-00V2500-D5
ENG-72-023302/28/960312/04/016ENGINE - LP COMPRESSOR - ROD ADJUSTMENT FEATURE RELOCATION OF LPC BLEED RIGGING72-32-00V2500-A1
ENG-72-023402/10/960202/21/008ENGINE - LP COMPRESSOR- TRIMMING OF ANNULUS FILLER PLATFORM EDGE72-31-00V2500-A5,-D5
ENG-72-023507/12/960111/29/966ENGINE - HP COMPRESSOR - NEW STAGES 6,7, AND 8 ROTOR PATH RINGS WITH IMPROVED ABRADABLELININGS72-41-00V2500-A1,-A5,-D5
ENG-72-023609/15/964ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - PROVIDE A NEW ORIFICE PLATE WITH AN INCREASED OPENING SIZE72-45-00V2500-A5,-D5
ENG-72-023701/25/998ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - PROVIDE NEW STAGE 2 HPT VANES72-45-00V2500-A5,-D5
ENG-72-023811/30/968ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - PROVIDE A NEW STAGE 1 TURBINE HUB72-45-00V2500-A5,-D5
ENG-72-023909/05/968ENGINE - DIFFUSER AND COMBUSTOR GROUP - PROVIDE NEW DIFFUSER GROUP ADAPTERS AND TUBE ASSEMBLIES72-42-00V2500-A5,-D5
ENG-72-024008/15/960101/15/978ENGINE - HIGH PRESSURE TURBINE ROTOR AND STATOR ASSEMBLY - PROVIDE A NEW STAGE 2 HPT AIRSEAL AND NEW STAGE 1 HIGH PRESSURE TURBINE (HPT) HUB METERING PLUGS72-45-00V2500-A1,-A5,-D5
ENG-72-024106/30/960202/20/028ENGINE - STAGE 1 TURBINE NOZZLE ASSEMBLY - PROVIDE A NEW STAGE 1 HPT COOLING DUCT ASSEMBLY AND SEGMENTS72-44-00V2500-A5,-D5
ENG-72-024207/30/960101/31/068ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - PROVIDE NEW STAGE 1 HPT BLADES72-45-00V2500-A5,-D5
ENG-72-024301/10/970102/21/025ENGINE - HP COMPRESSOR BLADES - INTRODUCTION OF INCREASED STAGE 3-6 ROTOR TIP CLEARANCES72-41-10V2500-A1
ENG-72-024402/20/985ENGINE - MAIN GEARBOX ASSEMBLY - PROVIDE AN IMPROVED FRONT DEOILER BALL BEARING AND NEW HOUSING72-60-00V2500-A1,-A5
ENG-72-024512/20/967ENGINE - LP COMPRESSOR - TO ANNOUNCE THE NEW BIFURCATION BOX COVER72-38-00V2500-D5
ENG-72-024602/17/976ENGINE - LP COMPRESSOR - BREAK THE SHARP EDGE ON THE PANEL SUPPORTING BRACKET72-32-00V2500-A1,-A5
ENG-72-024701/13/976ENGINE - LP COMPRESSOR - DELETION OF SILVER PLATING ON THE LPC INTERMEDIATE CASE MODULE ATTACHING BOLTS72-32-00V2500-D5
ENG-72-024802/28/974ENGINE - TURBINE EXHAUST CASE ASSEMBLY - INSPECTION OF THE NO. 5 BEARING SCAVENGE AND PRESSURE TUBE ASSEMBLIES FOR BRAZE AT THE INBOARD ENDS72-00-00V2500-A1
ENG-72-024912/20/966ENGINE - LP COMPRESSOR - NEW FAN CASE ASSEMBLY WITH IMPROVED ACOUSTIC LINING72-32-00V2500-A1,-A5,-D5
ENG-72-025004/16/996ENGINE - LP COMPRESSOR - RE-DESIGN OF THE LPC BLEED ACTUATING ROD72-32-00V2500-A5,-D5
ENG-72-025212/13/960105/23/977ENGINE - HP COMPRESSOR BLADES - INTRODUCTION OF STAGE 7and8 ROTOR BLADES WITH AU TIP COATING REMOVED72-00-00V2500-A1,-A5,-D5
ENG-72-025412/20/960101/16/987ENGINE - HP COMPRESSOR DISC - INTRODUCTION OF HP COMPRESSOR DRUM WITH REVISED DISC PROFILES72-41-00V2500-A1,-A5,-D5
ENG-72-025609/19/976POWER PLANT - EEC HARNESS WITH ADDITIONAL ANTI-CHAFE PROTECTION IN THE AREA OF LIGHTNING STRIKE PROTECTION SLEEVES71-51-41V2500-A1
ENG-72-025701/31/970210/14/996ENGINE - HP COMPRESSOR BLADES AND VANES - COMMONISATION OF THE PROCEDURE USED TO OBTAIN TIP CLEARANCES FOR NEW PRODUCTION AND OVERHAUL72-41-00V2500-A5,-D5
ENG-72-025802/21/970109/04/987ENGINE - HP COMPRESSOR SPLIT CASES - INTRODUCTION OF ACC ACTUATOR SUPPORT BRACKET WITHINCREASED MATERIAL THICKNESS72-41-00V2500-A1,-A5
ENG-72-025901/30/978ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - PROVIDE NEW STAGE 2 HPT VANES72-45-00V2500-A5,-D5
ENG-72-026011/07/970209/05/017ENGINE - LP COMPRESSOR BLADES AND FILLERS - INTRODUCTION OF REVISED METHOD OF ATTACHING CHOCKING PADS72-31-11V2500-A1,-A5,-D5
ENG-72-026110/27/976ENGINE - LP COMPRESSOR - CORRECT THE SERIAL NUMBER ON THE REAR RETAINING RING72-31-00V2500-A5
ENG-72-026303/28/970101/31/027ENGINE - HP COMPRESSOR REAR OUTER CASE - INTRODUCTION OF REVISED CASE WITH INTEGRAL REAR SEAL LAND72-00-00V2500-A1,-A5,-D5
ENG-72-026402/12/976ENGINE - MAIN GEARBOX ASSEMBLY - PROVIDE A NEW HYDRAULIC PUMP SHROUD72-60-00V2500-A1,-A5
ENG-72-026504/18/970209/07/016ENGINE - HP COMPRESSOR SPLIT CASES - INTRODUCTION OF REVISED STAGE 5 BOROSCOPE BLANKING FEATURES72-41-31V2500-A1,-A5,-D5
ENG-72-026603/18/978ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - PROVIDE NEW STAGE 2 HPT VANES WHICH HAVE INCREASED COOLING AIRFLOW72-45-00V2500-A5
ENG-72-026703/18/970106/30/038ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - INTRODUCE NEW SECOND STAGE TURBINE BLADES WITH MORE DURABLE TIPS AND IMPROVED REPAIRABILITY72-45-00V2500-A5
ENG-72-026812/12/977ENGINE - HP COMPRESSOR RING CASES - INTRODUCTION OF SCALLOPED STAGE 7 REAR LINER72-41-00V2500-A5,-D5
ENG-72-026903/28/970412/20/074ENGINE - ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES - INTRODUCTION OF REVISED STAGE 3 AND STAGE 4 VSV ACTUATING LEVER WITH INCREASED RADIUS72-00-00V2500-A1,-A5,-D5
ENG-72-027003/31/976ENGINE - LP COMPRESSOR - MOVE THE MARK OF THE LASH VALUE ON THE PTO PINION BEVEL GEARSHAFT72-32-00V2500-A1,-A5,-D5
ENG-72-027107/18/970304/16/037ENGINE - LP COMPRESSOR BLADES AND FILLERS - INTRODUCTION OF REVISED PRESSURE AND SUCTION AEROFOIL PANELS72-00-00V2500-A1,-A5,-D5
ENG-72-027202/28/985ENGINE - HIGH PRESSURE TURBINE ROTOR AND STATOR ASSEMBLY - PROVIDE AN INSPECTION FOR THESTAGE 2 HPT AIR SEAL72-45-00V2500-A1
ENG-72-027310/17/976ENGINE - HPC DISCS 9-12 - INTRODUCTION OF A REVISED HP COMPRESSOR STAGE 9-12 ASSEMBLY72-41-00V2500-A5,-D5
ENG-72-027606/05/978ENGINE - DIFFUSER CASE ASSEMBLY AND FITTINGS - REPLACE THE PRESSURE CAP AND FLARELESS TUBE UNION (PART MATERIAL IS CHANGED)72-42-00V2500-A1,-A5,-D5
ENG-72-027703/19/997ENGINE - ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES - CENTRALISING PADS WITH REVISED METHOD OF MANUFACTURE72-41-00V2500-A1,-D5
ENG-72-027912/15/970107/20/106ENGINE - LP COMPRESSOR - TO INTRODUCE A SMALL DIAMETER PIN ON THE LPC BLEED VALVE RING72-32-70V2500-A5,-D5
ENG-72-028010/15/017ENGINE HP COMPRESSOR RING CASES - INTRODUCTION OF HPC SYSTEM WITH STAGE 12 HEATSHIELDS DELETED72-41-21V2500-A5,-D5
ENG-72-028111/14/976ENGINE - ATTACHING PARTS AND FITTINGS - LP TURBINE MODULE - INTRODUCTION OF REVISED ECS SENSE LINE BRACKETS72-00-00V2500-D5
ENG-72-028210/26/010110/21/027ENGINE - PROVIDE NEW FRONT AND REAR NO.4 BEARING FACE SEALS.72-00-00V2500-A1,-A5,-D5
ENG-72-028309/19/977ENGINE - HP COMPRESSOR RING CASE - INTRODUCTION OF REVISED HP COMPRESSOR HEAT SHIELD ASSEMBLIES (STAGES 8 and 11)72-41-00V2500-A5,-D5
ENG-72-028411/28/976ENGINE - HP COMPRESSOR BLADES - INTRODUCTION OF REVISED LEFT HAND LOCK BLADES WITH INCREASED PLATFORM CROP72-41-00V2500-A1,-A5,-D5
ENG-72-028509/20/971203/30/168ENGINE - CONVERSION - PROVIDE INSTRUCTIONS TO CHANGE THE V2500-A5 ENGINE RATING BY MODIFYING THE DATA ENTRY PLUG72-00-00V2500-A5
ENG-72-028604/28/988ENGINE - LP COMPRESSOR - INTRODUCTION OF A REWORK PROCEDURE ON THE FAN FRAME ASSEMBLY72-32-00V2500-A1
ENG-72-028711/07/976ENGINE - FAN CASE FIRE RAIL AND ECS SENSE LINE WITH MODIFIED BRACKETS72-00-00V2500-D5
ENG-72-028812/19/970107/24/986ENGINE - MAIN GEARBOX ASSEMBLY - NEW HYDRAULIC PUMP DRIVE GEARSHAFT SEAL WITH REVISED PRESSURE CAPABILITY72-60-00V2500-A1,-A5
ENG-72-028910/24/976ENGINE - HP COMPRESSOR DISCS (STAGES 3 TO 8) - INTRODUCTION OF REVISED STAGE 7 AND 8 SEAL WIRES72-41-00V2500-A1,-A5,-D5
ENG-72-029011/28/970208/21/024ENGINE - HP SYSTEMS MODULE INSTALLATION PARTS - INTRODUCTION OF STRONGER BOLTS FOR THE HP COMPRESSOR TO INTERMEDIATE CASE FLANGE72-00-00V2500-A1,-A5,-D5
ENG-72-029101/25/980105/13/988ENGINE - STAGE 1 HP TURBINE VANE CLUSTER ASSEMBLY - PROVIDE A NEW FULLY CAST STAGE 1 HP TURBINE VANE ASSEMBLY72-40-00V2500-A5,-D5
ENG-72-029211/07/970205/08/987ENGINE - HP COMPRESSOR RING CASES - INTRODUCTION OF REVISED STAGE 12 HEAT SHIELD ASSEMBLY72-41-00V2500-A5,-D5
ENG-72-029312/19/973ENGINE - HP COMPRESSOR 9-12 DRUM - TO ANNOUNCE A REDUCTION IN CYCLIC LIFE DEPENDENT ON THRUST RATING - (NON-MODIFICATION)72-41-00V2500-A5,-D5
ENG-72-029411/25/970203/10/006ENGINE - LP TURBINE ASSEMBLY - DUCT SEGMENT INNER - REMOVAL SHEETMETAL FIN72-50-00V2500-A1,-A5,-D5
ENG-72-029508/17/016ENGINE - HP COMPRESSOR BLADES - INTRODUCTION OF A REDESIGNED STAGE 4 BLADE ASSEMBLY72-41-15V2500-A5,-D5
ENG-72-029602/13/980101/15/997ENGINE - HP COMPRESSOR - INTRODUCTION OF INTEGRAL FRONT SUPPORT-CONE STAGE 7 ROTOR PATH AND REVISED HEATSHIELD AND FASTENER CONFIGURATION72-41-00V2500-A5,-D5
ENG-72-029701/09/980612/08/063ENGINE - LP COMPRESSOR FAN BLADES - TO ANNOUNCE THE FREQUENCY OF TRANSIENT ACOUSTIC PROPOGATION (TAP) TESTS NON-MODIFICATION SERVICE BULLETIN72-00-00V2500-A1,-A5,-D5
ENG-72-029801/05/980104/24/008ENGINE - CONVERSION - PROVIDE INSTRUCTIONS TO CHANGE THE V2500-D5 ENGINE RATING BY MODIFYING THE DATA ENTRY PLUG72-00-00V2500-D5
ENG-72-029901/30/987ENGINE - MAIN GEARBOX ASSEMBLY NEW DEOILER ROLLER BEARING72-60-00V2500-A1,-A5
ENG-72-030004/03/987ENGINE - STAGE 3 TO 8 HP COMPRESSOR DISCS - INTRODUCTION OF A REVISED STAGE 3 TO 8 DISC ASSEMBLY AND REVISED STAGE 7 AND 8 SEALING WIRES72-41-00V2500-A1,-A5,-D5
ENG-72-030101/30/986ENGINE - MAIN GEARBOX ASSEMBLY - MODIFICATION OF O-RING FOR THE ANGLE GEARBOX SUPPORT72-60-00V2500-D5
ENG-72-030201/10/980701/30/044ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - INTRODUCE FIRST AND SECOND STAGE TURBINE BLADES WHICH HAVE PROTECTIVE COATING IN THE DAMPER POCKET AREA UNDER THE PLATFORM72-45-00V2500-A5,-D5
ENG-72-030411/06/986ENGINE - HP COMPRESSOR DISCS - INTRODUCTION OF A REWORKED STAGE 3 TO 8 DISC ASSEMBLY WITH REVISED L SHAPED SEALING WIRES72-41-00V2500-A1,-A5,-D5
ENG-72-030510/01/980102/29/006ENGINE - LP COMPRESSOR - TO INTRODUCE A CHROME PLATING PIN ON THE LPC BLEED VALVE RING72-32-00V2500-A5,-D5
ENG-72-030604/24/980108/03/986ENGINE - LP COMPRESSOR - TO INCORPORATE BUSHES ON THE LPC BLEED SYNCHRONIZING RING72-32-00V2500-A1
ENG-72-030704/14/987ENGINE - LP TURBINE ROTOR - INTRODUCTION OF NEW STAGE 3 AND 7 TURBINE DISKS FOR FULL LIFE72-50-00V2500-A1,-A5,-D5
ENG-72-030807/17/986ENGINE - HP COMPRESSOR SPLIT CASES - INTRODUCTION OF REVISED INNER HALF BUSH FOR THE HPC STAGE 6 VANE MANUFACTURED FROM AVIMID-N72-41-00V2500-A1
ENG-72-031001/25/997ENGINE - HIGH PRESSURE TURBINE - PROVIDE NEW STAGE 1 AND 2 HIGH PRESSURE TURBINE DUCT SEGMENTS72-45-00V2500-A1,-A5,-D5
ENG-72-031105/22/987ENGINE - HP COMPRESSOR SHAFT - REAR SHAFT ASSEMBLY - INTRODUCTION OF AN ALTERNATIVE HEATSHIELD OF HASTALLOY-X MATERIAL72-41-00V2500-A1,-A5,-D5
ENG-72-031205/13/988ENGINE - STAGE 1 HIGH PRESSURE TURBINE VANE CLUSTER ASSEMBLY - PROVIDE A MODIFICATION OF STAGE 1 HPT VANE ASSEMBLIES72-44-00V2500-A1
ENG-72-031408/31/980210/31/023ENGINE - CONVERSION - PROVIDE INSTRUCTIONS TO CHANGE THE V2500-A5 ENGINE START CRANK BY MODIFYING THE DATA ENTRY PLUG72-00-00V2500-A5
ENG-72-031506/25/980302/01/006ENGINE - DIFFUSER AND COMBUSTION GROUP AND STAGE 1 TURBINE NOZZLE ASSEMBLY - PROVIDE NEWINNER AND OUTER COMBUSTION CHAMBER LINERS WITH ADDITION OF PWA 281 COATING72-40-00V2500-A1,-A5,-D5
ENG-72-031605/15/980409/11/033ENGINE - LP COMPRESSOR FAN BLADES - ULTRASONIC INSPECTION OF FAN BLADE ROOTS - NON-MODIFICATION SERVICE BULLETIN72-00-00V2500-A1,-A5,-D5
ENG-72-031706/12/986ENGINE - HP COMPRESSOR SPLIT CASES - INTRODUCTION OF REVISED STAGE 5 AND 6 BOROSCOPE BLANKING PLUG WITH ADDITIONAL ATTACHING BOLT72-41-00V2500-A5,-D5
ENG-72-031805/12/998ENGINE - INLET CONE - INTRODUCTION OF SEALS ON THE INLET CONE FAIRING72-38-00V2500-A1,-A5,-D5
ENG-72-031903/19/997ENGINE - ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES - STAGE 4 AND 5 CENTRALISING PADS WITH REVISED METHOD OF MANUFACTURE72-41-00V2500-A5,-D5
ENG-72-032007/31/980210/01/997ENGINE - HP COMPRESSOR STATOR VANES - INTRODUCTION OF REVISED STAGE 6, 7 AND 10 STATOR VANES WITH CHORDAL MACHINING OF REAR PLATFORM LOCATION FEATURES72-41-00V2500-A5,-D5
ENG-72-032107/15/980105/29/997ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - INTRODUCE NEW FIRST AND SECOND STAGE BLADES WITH UNDER PLATFORM COATING72-45-00V2500-A1
ENG-72-032207/15/990101/29/993HPC LUBRICATION OF VSV MECHANISM WITH TRI-FLOW (NON MODIFICATION)72-41-00V2500-A1,-A5
ENG-72-032407/21/980101/29/993HPC LUBRICATION OF VSV MECHANISM WITH TRI-FLOW (NON MODIFICATION)72-41-00V2500-D5
ENG-72-032508/15/986ENGINE - HIGH PRESSURE TURBINE ASSEMBLY - INSPECT THE STAGE 1 HIGH PRESSURE TURBINE COOLING DUCT ASSEMBLY FOR CRACK INDICATIONS72-40-00V2500-A1,-A5,-D5
ENG-72-032710/25/980107/26/007ENGINE - HIGH PRESSURE TURBINE ROTOR AND STATOR ASSEMBLY - INTRODUCE NEW ROTATING PARTS WITH POTENTIAL FOR INCREASED CYCLIC LIFE72-45-00V2500-A5,-D5
ENG-72-032802/15/990102/01/027ENGINE - HIGH PRESSURE TURBINE ROTOR AND STATOR ASSEMBLY - INTRODUCE A NEW STAGE 2 HIGH PRESSURE TURBINE BLADE RETAINING PLATE72-45-00V2500-A5,-D5
ENG-72-032911/20/980207/16/124ENGINE - ATTACHING PARTS AND FITTINGS - HP SYSTEM - INTRODUCTION OF REVISED BRACKETS TO PROVIDE INCREASED CLEARANCE WITH FUEL MANIFOLDS72-40-00V2500-A1,-A5
ENG-72-033009/03/990111/07/007ENGINE - DIFFUSER AND COMBUSTION GROUP - PROVIDE NEW BULKHEAD LINER SEGMENTS72-40-00V2500-A1,-A5,-D5
ENG-72-033109/03/990303/14/027ENGINE - DIFFUSER AND COMBUSTION GROUP - PROVIDE NEW FUEL NOZZLE GUIDES72-40-00V2500-A1,-A5,-D5
ENG-72-033212/11/980211/29/994ENGINE - HP COMPRESSOR BLADES - INTRODUCTION OF STAGE 6 BLADES IN REVISED TITANIUM MATERIAL WITH RE-DEFINED ROOT GEOMETRY72-41-00V2500-A5,-D5
ENG-72-033306/29/995ENGINE - LP COMPRESSOR - INCORPORATION OF STRONGER BOLTS FOR THE LPC BLEED DUCT TO FAN FRAME72-32-00V2500-A1
ENG-72-033401/22/990412/20/074ENGINE - ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES - INTRODUCTION OF REVISED STAGE 3 AND STAGE 4 VSV ACTUATOR RING LEVERS WITH INCREASED RADIUS72-41-00V2500-A1,-A5,-D5
ENG-72-033512/15/997ENGINE - ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES - INTRODUCTION OF REVISED HP COMPRESSOR STAGES 5 VSV ACTUATOR BLEND RADIUS72-41-00V2500-A1,-A5,-D5
ENG-72-033609/29/990206/09/007ENGINE - ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES - INTRODUCTION OF REVISED VIGV AGUAATOR RING LEVERS WITH INCREASED BLEND RADIUS72-41-00V2500-A1,-A5,-D5
ENG-72-033712/18/980109/30/997ENGINE - HP COMPRESSOR SPLIT CASES - INTRODUCTION OF REVISED STAGE 5 AND 6 BOROSCOPE BLANKING PLUG WITH INCREASED STEM DIAMETER72-41-00V2500-A1,-A5,-D5
ENG-72-033803/19/996ENGINE - HP COMPRESSOR SPLIT CASES - INTRODUCTION OF REVISED STAGE 5 AND 6 BLANKING PLUG WITH ADDITIONAL FASTENER AND INCREASED STEM DIAMETER72-41-00V2500-A1
ENG-72-033911/11/987ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - PROVIDE NEW STAGE 1 HPT DUCT SEGMENTS, BAND SEGMENTS, SUPPORTS, SEALS AND BOLTS72-45-00V2500-A1
ENG-72-034011/11/980207/09/017ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - PROVIDE A NEW SINGLE FULLY CERAMIC COATED VANE AND A NEW STAGE 1 HIGH PRESSURE TURBINE COOLING DUCT ASSEMBLY72-44-00V2500-A1
ENG-72-034111/11/980110/05/006ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - PROVIDE A NEW STAGE 1 HIGH PRESSURE TURBINE SUPPORT ASSEMBLY WHICH CONTAINS A NEW SEAL72-44-00V2500-A1,-A5,-D5
ENG-72-034212/20/980112/12/008ENGINE - PROVIDE THE REQUIREMENTS FOR MODIFICATION TO THE PHOENIX STANDARD CONFIGURATION72-40-00V2500-A1
ENG-72-034308/09/997ENGINE - HP COMPRESSOR RING CASES - INTRODUCTION OF INTEGRAL HP COMPRESSOR CASES AND ROTOR PATHS72-41-00V2500-A5,-D5
ENG-72-034412/18/980102/12/994ENGINE - HIGH PRESSURE TURBINE - INSPECT CERTAIN STAGE 1 AND 2 HIGH PRESSURE TURBINE (HPT) HUBS72-40-00V2500-A1
ENG-72-034501/15/990203/07/007ENGINE - HP COMPRESSOR SPLIT CASES - INTRODUCTION OF REVISED STAGE 4 AND 5 ROTOR PATH SEAL RING SEGMENTS72-41-00V2500-A5
ENG-72-034605/13/995ENGINE - LP COMPRESSOR - INTRODUCE THE NEW NO.6 STRUT FAIRING PANEL WITH ROUNDED CORNERS72-32-00V2500-A1,-A5
ENG-72-034708/12/990101/12/007ENGINE - HP COMPRESSOR DISK (STAGES 9-12) - INTRODUCTION OF REVISED HP COMPRESSOR STAGE 9-12 DISK ASSEMBLY WITH INCREASED ABRASIVE LINING BOND COAT THICKNESS72-41-00V2500-A1,-A5,-D5
ENG-72-034806/18/997ENGINE - ACTUATING MECHANISM HP COMPRESSOR VARAIABLE VANES - INTRODUCTION OF STAGE-4 AND 5 VSV BRIDGE-PIECE ASSEMBLIES WITH REVISED METHOD OF MANUFACTURE72-41-00V2500-A1,-A5,-D5
ENG-72-034904/07/990111/30/004ENGINE - INSPECTION OF V2500-Al HIGH PRESSURE TURBINE STAGE 1 ROTOR METERING PLUGS FOR HEAT DISTRESS72-00-00V2500-A1,-A5
ENG-72-035002/07/005ENGINE - LP COMPRESSOR - INTRODUCTION OF NEW HIGH TENSION BOLT FOR NO.2 BEARING SUPPORT FLANGE72-32-00V2500-A1,-A5,-D5
ENG-72-035105/31/990410/31/023ENGINE - HP TURBINE ROTOR AND STATOR ASSEMBLY - INTRODUCE A NEW FIRST STAGE TURBINE AIR SEAL72-00-00V2500-A1
ENG-72-035303/31/000202/19/016ENGINE - LP COMPRESSOR - INTRODUCTION OF REVISED SPIRAL RING72-32-00V2500-A1
ENG-72-035410/15/995ENGINE-IDENTIFICATION OF REDUCED TOLERANCE SPIGOT FITS WITHIN THE HP COMPRESSOR72-41-00V2500-A1
ENG-72-035507/19/996ENGINE - MANUAL GEARBOX ASSEMBLY - PROVIDE A NEW VSCF SHAFT PLUG ASSEMBLY72-60-00V2500-D5
ENG-72-035607/16/990308/11/003ENGINE - LP - COMPRESSOR - INSPECTION CHECK OF INSTALLED ANNULUS FILLERS (NON-MOD)72-31-00V2500-A1
ENG-72-035708/16/990411/15/065ENGINE - HP TURBINE ROTOR ASSEMBLY - INTRODUCE NEW FIRST STAGE TURBINE BLADES WITH PROTECTIVE COATING ON THE INTERNAL CAVITIES72-45-00V2500-A5,-D5
ENG-72-035801/12/007ENGINE - HP COMPRESSOR RING CASES - INTRODUCTION OF REVISED HP COMPRESSOR STAGE 1 AND 10 CASE ASSEMBLIES WITH REDUCED QUANTITY OF BLEED SLOTS72-41-00V2500-A5,-D5
ENG-72-035906/29/010611/05/106ENGINE - LP TURBINE - INNER TRANSITION DUCT - APPLICATION OF WEAR RESISTANT COATING TO PREVENT FRETTING72-50-24V2500-A1,-A5,-D5
ENG-72-036012/01/990103/01/007ENGINE - HP COMPRESSOR SPLIT CASES - INTRODUCTION OF REVISED STAGE 5 ROTOR PATH SEGMENT72-41-00V2500-A5,-D5
ENG-72-036111/24/990204/05/047ENGINE - HP TURBINE ROTOR ASSEMBLY - INTRODUCE NEW FIRST STAGE TURBINE BLADES WITH BLADE ROOT ATTACHMENT COATING72-45-00V2500-A5,-D5
ENG-72-036201/07/004ENGINE - LP-COMPRESSOR - INCORPORATION OF HIGH STRENGTH BOLTS FOR ANNULUS FILLER ATTACHMENT72-31-00V2500-A1
ENG-72-036308/08/000109/05/007ENGINE - PROVIDE NEW FIRST AND SECOND STAGE TURBINE AIR SEALS72-45-00V2500-A1,-A5,-D5
ENG-72-036402/23/000105/12/007ENGINE - HIGH PRESSURE TURBINE - PROVIDE NEW STAGE 2 HIGH PRESSURE TURBINE DUCT SEGMENTS72-45-00V2500-A1,-A5,-D5
ENG-72-036502/23/000208/14/066ENGINE - PROVIDE PRETRENCHED SECOND STAGE HPT AIR SEALING RING SEGMENTS72-45-00V2500-A1,-A5,-D5
ENG-72-036606/22/010208/21/027ENGINE ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES-INTODUCTION OF A REVISED CRANKSHAFT ASSEMBLY72-41-34V2500-A5,-D5
ENG-72-036808/08/000109/05/007ENGINE - PROVIDE NEW SECOND STAGE HIGH PRESSURE TURBINE (HPT) VANES72-45-00V2500-A5,-D5
ENG-72-036904/07/000504/24/096MODIFICATION SERVICE BULLETIN - ENGINE - HP COMPRESSOR RING CASES - INTRODUCTION OF HP COMPRESSOR STAGES 6,7 AND 8 ROTOR PATHS WITH REVISED ABRADABLE LINING72-41-00V2500-A1,-A5,-D5
ENG-72-037003/02/000102/21/025ENGINE-HP-COMPRESSOR BLADES-INTRODUCTION OF INCREASED STAGE 4 ROTOR BLADE TIP CLEARANCE72-41-00V2500-A1
ENG-72-037104/10/005ENGINE - FAN CASE REAR EXTENSION - INTRODUCTION OF ANTI-FRET COATING OF THE V-GROOVE72-38-00V2500-D5
ENG-72-037211/03/008ENGINE - L.P. COMPRESSOR BLADES AND FILLERS - INTRODUCTION OF A REVISED WIDE CHORD FAN BLADE WITH DELETED ROOT STOP PIN AND REVISED FRONT AND REAR CHOCKING PADS72-38-00V2500-A1
ENG-72-037303/16/000706/11/044ENGINE - HP COMPRESSOR STAGE 4 ROTOR BLADES - ULTRASONIC INSPECTION OF BLADE ROOTS - NON-MODIFICATION SERVICE BULLETIN72-00-00V2500-A5,-D5
ENG-72-037407/11/000109/23/036RE-IDENTIFICATION OF SUPER POLISHED BLADES AND VANES INTRODUCED BY GIB 70-0714 - NON-MODIFICATION SERVICE BULLETIN72-41-00V2500-A5,-D5
ENG-72-037507/28/007ENGINE - LP COMPRESSOR BLADES AND FILLERS - INTRODUCTION OF A REVISED LP COMPRESSOR BLADE WITH METCO 5872-31-11V2500-A1,-A5,-D5
ENG-72-037610/28/027ENGINE - HP COMPRESSOR DISCS (STAGES 3 - 8) - INTRODUCTION OF A REVISED STAGE 3 - 8 DISC ASSEMBLY WITH INCREASED LIFE72-41-11V2500-A5,-D5
ENG-72-037710/09/006ENGINE H.P. COMPRESSOR DISCS (STAGES 9-12) - INTRODUCTION OF H.P COMPRESSOR STAGE 9-12 DISC ASSEMBLY WITH REVISED LOCATION72-41-12V2500-A1
ENG-72-037810/31/008ENGINE - L.P. COMPRESSOR - TO ANNOUNCE THE AVAILABILITY OF NEW ENGINE IDENTIFICATION PLATE WITH DESIGNATION OF ALL A5 MODEL RATINGS72-32-00V2500-A5
ENG-72-037912/11/000204/20/024ENGINE - HP COMPRESSOR VSV SYSTEM INSPECTION NMSB72-00-00V2500-A5
ENG-72-038007/10/000405/07/124NON-MODIFICATION SERVICE BULLETIN - PERMANENT MAGNET ALTERNATOR (PMA) DRIVE GEAR ASSEMBLY RETENTION NUT LOOSENING - REPLACEMENT OF THE NUT72-60-33V2500-A1,-A5
ENG-72-038101/12/010207/26/064ENGINE - PROVIDE NEW STAGE 1 HIGH PRESSURE TURBINE (HPT) COOLING AIR DUCT ASSEMBLY WITH DECREASED HONEYCOMB SURFACE72-44-50V2500-A1,-A5,-D5
ENG-72-038210/13/006MODIFICATION SERVICE BULLETIN - ENGINE - L.P. COMPRESSOR - NEW FAN CASE ASSEMBLY WITH IMPROVED ACOUSTIC LINING72-32-00V2500-A1,-A5,-D5
ENG-72-038410/03/000607/01/044ENGINE - LP COMPRESSOR BLADES AND FILLERS - INTRODUCTION OF A REVISED LP COMPRESSOR BLADE WITH METCO 58 - REWORK72-31-00V2500-A1,-A5
ENG-72-038506/22/010303/29/047ENGINE - ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES - INTRODUCTION OF REVISED BRIDGE PIECE ASSEMBLIES AND UNISON RING ASSEMBLIES WITH INCREASED DOWEL LOCATION72-41-34V2500-A1,-A5,-D5
ENG-72-038610/03/000711/07/053ENGINE - LP COMPRESSOR FAN BLADES - DOVETAIL ROOT FLANK ULTRASONIC INSPECTION AND APPLICATION OF DRY FILM LUBRICANT (ROOT FRETTING/WEAR - SCARRING) - NON-MODIFICATION SERVICE BULLETIN72-31-00V2500-A5
ENG-72-038710/03/000403/09/063ENGINE - L.P. COMPRESSOR FAN BLADES - DOVETAIL ROOT FLANK ULTRASONIC INSPECTION AND APPLICATION OF DRY FILM LUBRICANT (ROOT FRETTING/WEAR - SCARRING) NON MODIFICATION SERVICE BULLETIN72-31-00V2500-A1
ENG-72-039107/05/020111/25/087ENGINE LP COMPRESSOR - INTRODUCTION OF STEEL/ALUMINIUM NO.1 BEARING SUPPORT72-32-00V2500-A1,-A5
ENG-72-039203/13/017ENGINE - LP COMPRESSOR - IMPROVED REPAIR PARTS FOR ACOUSTIC LININGS OF FAN CASE72-32-00V2500-A1,-A5,-D5
ENG-72-039301/10/010210/07/024ENGINE - HP COMPRESSOR VSV SYSTEM INSPECTION - NON MODIFICATION SERVICE BULLETIN72-00-00V2500-D5
ENG-72-039412/20/000104/20/013ENGINE - PROVIDE NEW LOOP CLAMP BRACKET FOR USE WITH NON AT RISK FUEL MANIFOLDS72-40-00V2500-A1,-A5
ENG-72-039602/18/020211/14/08See SBENGINE - INSPECTION OF HIGH PRESSURE COMPRESSOR STAGE 3 TO 8 DRUM DAMPER WIRE RELEASE72-00-00V2500-A1,-A5,-D5
ENG-72-039702/16/010107/07/013ENGINE - MAIN GEARBOX ASSEMBLY - INSPECTION OF THE SCAVENGE PUMP DRIVE GEAR ASSEMBLY NMSB72-60-00V2500-A1
ENG-72-039804/27/015ENGINE - HP COMPRESSOR SYSTEM - RE-INTRODUCTION OF STANDARD VARIABLE STATOR VANE SCHEDULE72-41-00V2500-A1
ENG-72-039905/15/010307/15/025ENGINE - PROVIDE A NEW 2ND STAGE TURBINE ROTOR BLADE RETENTION CONFIGURATION72-45-00V2500-A5
ENG-72-040008/17/010110/16/015ENGINE HP COMPRESSOR VARIABLE VANES - INLET GUIDE STAGE 3, STAGE 4 AND STAGE 5 WITH OPTIMISED BUILD AND SETTING INSTRUCTIONS.72-41-00V2500-A5,-D5
ENG-72-040108/22/010411/29/023ENGINE - PROVIDE NICKEL PLATING ON THE NO.4 CARBON SEAL HOUSING PILOT DIAMETER72-00-00V2500-A1,-A5,-D5
ENG-72-040208/17/015ENGINE HP COMPRESSOR VARIABLE VANES-INLET GUIDE STAGE 3, STAGE 4, STAGE 5 AND STAGE 6 WITH OPTIMISED BUILD AND SETTING INSTRUCTIONS (A1 MODEL)72-41-00V2500-A1
ENG-72-040311/26/010203/01/116ENGINE - HP COMPRESSOR SHAFT - INTRODUCTION OF REVISED HPC REAR SHAFT ASSY WITH No4 BEARING LOCATION COATING A5 AND D5 MODELS72-41-13V2500-A5,-D5
ENG-72-040411/16/010103/25/116ENGINE - HP COMPRESSOR SHAFT - INTRODUCTION OF REVISED HP COMPRESSOR REARSHAFT ASSEMBLY WITH NO.4 BEARING LOCATION COATING (A1 MODEL)72-41-13V2500-A1
ENG-72-040509/20/010108/20/026ENGINE PROVIDE NEW NUMBER FOUR BEARING FRONT AND REAR SEALS72-43-00V2500-A1,-A5,-D5
ENG-72-040610/15/017ENGINE - ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES - INTRODUCTION OF A FULLY MACHINED FROM BAR CRANKSHAFT ASSEMBLY72-41-34V2500-A5,-D5
ENG-72-040708/17/014ENGINE - MAIN GEARBOX ASSEMBLY MAINTENANCE SHOP INSPECTION OF THE OIL SCAVENGE DRIVE GEARS FOR MICROPITTING AND WEAR NMSB72-60-00V2500-A1,-A5
ENG-72-040808/22/015ENGINE INTERNAL GEARBOX ASSEMBLY - FBC TROUBLESHOOTING AND TEARDOWN PROCEDURE NMSB72-32-00V2500-A1,-A5,-D5
ENG-72-040908/20/010403/08/063ENGINE - LP COMPRESSOR FAN BLADES - DOVETAIL ROOT FLANK ULTRASONIC INSPECTION AND APPLICATION OF DRY FILM LUBRICANT (ROOT FRETTING/WEAR - SCARRING) - NON-MODIFICATION SERVICE BULLETIN72-31-00V2500-D5
ENG-72-041002/08/027ENGINE - HP COMPRESSOR VARIABLE VANE INNER SHROUDS - INTRODUCTION OF REVISED ONE PIECE BUSHES72-41-32V2500-A5,-D5
ENG-72-041112/02/010108/08/026ENGINE - LP COMPRESSOR INTRODUCTION OF HYDRAULIC SEAL WITH REVISED OIL DRAIN FEATURE72-32-00V2500-A1,-A5,-D5
ENG-72-041212/17/010102/05/037ENGINE - PROVIDE ADDITIONAL OIL DRAIN HOLE IN 2nd STAGE TURBINE AIR SEAL72-45-00V2500-A5,-D5
ENG-72-041404/07/047ENGINE - PROVIDE A THIRD SOURCE FOR THE GEARBOX BEARINGS72-60-00V2500-A1,-A5,-D5
ENG-72-041503/29/020308/18/053ENGINE - PROVIDE NEW FRONT AND REAR NUMBER 4 BEARING DUCTS WITH OIL DRAIN HOLES72-00-00V2500-A1,-A5,-D5
ENG-72-041604/22/020210/19/056ENGINE - ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES - INTRODUCTION OF REVISED BRIDGE PIECE ASSEMBLIES AND UNISON RING ASSEMBLIES WITH INCREASED DOWEL LOCATION (REWORK)72-41-34V2500-A1,-A5,-D5
ENG-72-041809/16/020210/01/097ENGINE - ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES - INTRODUCTION OF UNISON RING ASSEMBLIES AND BRIDGE PIECE ASSEMBLIES WITH REVISED ONE PIECE LEVER PIN BUSHES72-41-34V2500-A1,-A5,-D5
ENG-72-041908/30/025NON-MODIFICATION SERVICE BULLETIN - ENGINE - NO. 4 COMPARTMENT OIL LOSS INVESTIGATION AND TROUBLESHOOTING GUIDE72-00-00V2500-A1,-A5,-D5
ENG-72-042008/30/020109/20/025NON-MODIFICATION SERVICE BULLETIN - ENGINE - NO. 5 COMPARTMENT OIL LOSS TROUBLESHOOTING PROCEDURE AND PROPOSED CORRECTIVE ACTIONS72-00-00V2500-A1,-A5,-D5
ENG-72-042109/04/020402/10/067ENGINE - HP COMPRESSOR FRONT STUBSHAFT - INTRODUCTION OF A REVISED HP COMPRESSOR FRONT STUBSHAFT WITH HIGH ENERGY PLASMA COATING72-32-23V2500-A5,-D5
ENG-72-042204/25/027ENGINE - HP COMPRESSOR VARIABLE VANE INNER SHROUDS - INTRODUCTION OF REVISED ONE PIECE BUSHES72-41-33V2500-A1
ENG-72-042304/30/023ENGINE - LP COMPRESSOR FAN BLADES - DOVETAIL ROOT FLANK ULTRASONIC INSPECTION (HIGH STRESS EVENT) - NON-MODIFICATION SERVICE BULLETIN72-31-00V2500-A5
ENG-72-042404/30/023ENGINE - LP COMPRESSOR FAN BLADES - DOVETAIL ROOT FLANK ULTRASONIC INSPECTION (HIGH STRESS EVENT) - NON-MODIFICATION SERVICE BULLETIN72-31-00V2500-D5
ENG-72-042504/30/020110/06/033ENGINE - LP COMPRESSOR FAN BLADES - LEADING EDGE INSPECTION REQUIREMENTS - NON-MODIFICATION SERVICE BULLETIN72-31-00V2500-A5,-D5
ENG-72-042606/28/027ENGINE - ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES - INTRODUCTION OF A REVISED CRANKSHAFT ASSEMBLY WITH REDUCED FRONT BEARING INTERFERENCE72-00-00V2500-A5,-D5
ENG-72-042704/17/020208/15/023NON MODIFICATION SERVICE BULLETIN - ENGINE - NO.5 SCAVENGE TUBE LOT NUMBER M268050S1 IDENTIFICATION AND REPLACEMENT OF72-50-00V2500-A5,-D5
ENG-72-042803/24/034NON MODIFICATION SERVICE BULLETIN - ENGINE - HPT STAGE 2 BLADE INSPECTION FOR SURFACE IMPERFECTIONS ON AIRFOIL72-45-00V2500-A5,-D5
ENG-72-042910/07/026ENGINE - LP COMPRESSOR - INTRODUCTION OF A SMALLER DIAMETER WASHER72-32-00V2500-A1,-A5
ENG-72-043006/07/020108/20/023ENGINE - HIGH PRESSURE TURBINE FIRST STAGE DISK METERING PLUG REPLACEMENT72-45-00V2500-A1
ENG-72-043111/18/020103/18/047ENGINE - ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES - INTRODUCTION OF STAGE 6 UNISON RING ASSEMBLY WITH A REVISED ONE PIECE LEVER PIN BUSH72-41-34V2500-A1
ENG-72-043206/28/027ENGINE - PROVIDE IDENTIFICATION FOR NEAR NET SHAPE CASTINGS FOR HPT DUCT SEGMENTS72-44-00V2500-A1,-A5,-D5
ENG-72-043311/04/02See SBENGINE - HP COMPRESSOR BLADES AND VANES - INTRODUCTION OF STAGE 6, 7 AND 8 BLADES AND STAGE 8 STATOR VANES WITH EROSION RESISTANT COATINGS72-41-15V2500-D5
ENG-72-043410/04/020110/31/024ENGINE - PROVIDE NEW NUMBER 4 BEARING INNER WEEP TUBE AND OUTER WEEP MANIFOLD72-42-00V2500-A1,-A5,-D5
ENG-72-043502/25/030212/01/053ENGINE - LP COMPRESSOR - INTRODUCTION OF FAN CASE , PANEL AND BRACKET SCALLOPED FOR NO 4 SCAVENGE TUBE REROUTE72-32-00V2500-A1,-A5
ENG-72-043610/02/020104/14/034ENGINE - HP COMPRESSOR, STAGE 6 ROTOR PATH, CHANGE THE COMPLIANCE CATEGORY FOR PART 2 OF IAE SERVICE BULLETIN ENG-72-0369 FROM CATEGORY 6 TO CATEGORY 4 - NON MODIFICATION SERVICE BULLETIN72-00-00V2500-A5,-D5
ENG-72-043711/29/020202/17/031ENGINE - INSPECTION OF HPC STAGE 6 METCO 313 ROTOR PATH CONDITION AFTER INACTIVE PERIOD WITHOUT ADHERANCE TO AMM STORAGE PROCEDURES ON AIRCRAFT WITH BOTH ENGINES POST ENG SB 72-0235 AND PRE ENG SB 72-036972-00-00V2500-A5,-D5
ENG-72-043810/28/020104/14/03See SBENGINE - CONVERSION - DEFINITION OF MINIMUM BILL OF MATERIAL FOR OPERATIONS AT 33,000 LBS THRUST RATING72-00-00V2500-A5
ENG-72-043911/29/020202/10/034ENGINE - NO. 4 COMPARTMENT STRAINER IMPROVEMENT72-40-00V2500-A1,-A5,-D5
ENG-72-044003/31/047ENGINE - HP COMPRESSOR REAR OUTER CASE - INTRODUCTION OF A REVISED REAR OUTER CASE72-41-23V2500-A1,-A5
ENG-72-044101/07/037ENGINE - HP COMPRESSOR STATOR VANES - DELETION OF STAGE 7,8 AND 11 RETAINING VANES72-41-22V2500-A5,-D5
ENG-72-044203/03/036ENGINE - LP COMPRESSOR - DELETION OF FLUOROSILICONE SEALS FROM THE NO. 1 BEARING SCAVENGE OIL TUBE72-32-00V2500-A5,-D5
ENG-72-044410/06/036ENGINE - ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES - INTRODUCTION OF A STAGE 4 AND 5 CONNECTOR BRACKET LOCATION DOWELS WITH REDUCED LENGTH - REWORK72-41-34V2500-A5,-D5
ENG-72-044511/29/020205/23/03See SBENGINE - HP COMPRESSOR, STAGE 6 ROTOR PATH - DUAL METCO 313 ENGINED AIRCRAFT - FLEET MANAGEMENT ACTIONS72-00-00V2500-A5
ENG-72-044611/20/023NON-MODIFICATION - ENGINE - INSPECTION OF TURBINE EXHAUST CASE LEADING EDGE PRESSURE AND TEMPERATURE VANES72-50-00V2500-A5
ENG-72-044701/31/030212/02/098ENGINE - INNER AND OUTER COMBUSTION CHAMBER LINERS WITH ADDITION OF SINGLE CRYSTAL MATERIAL ON ROWS 3 AND 472-40-00V2500-A5,-D5
ENG-72-044801/02/030105/23/03See SBENGINE - HP COMPRESSOR, STAGE 6 ROTOR PATH - DUAL METCO 313 ENGINED AIRCRAFT - FLEET MANAGEMENT ACTIONS72-00-02V2500-D5
ENG-72-044904/25/030307/12/044ENGINE - HP COMPRESSOR RING CASES - INTRODUCTION OF HPC STAGE 4 ROTOR PATH TRENCH WITH INCREASED TIP CLEARANCE72-41-00V2500-A1
ENG-72-045001/27/037ENGINE - HP COMPRESSOR DISCS ( STAGES 3-8) - INTRODUCTION OF A REVISED STAGE 3-8 DISC ASSEMBLY72-41-11V2500-A1
ENG-72-045109/01/030110/15/034ENGINE - HIGH PRESSURE TURBINE FIRST STAGE DISK METERING PLUG REDESIGN72-45-00V2500-A5,-D5
ENG-72-045205/13/030409/30/05See SBENGINE - MAGNETIC CHIP DETECTOR (MCD) INSPECTIONS FOR ENGINES WITH HIGH PRESSURE COMPRESSOR (HPC) STUBSHAFTS INSTALLED WITH LOW ENERGY STANDARD OF COATING - NON-MODIFICATION SERVICE BULLETIN72-32-20V2500-A5
ENG-72-045303/23/034ENGINE - LP TURBINE INSPECTION OF LP TURBINE SHAFTS WHICH HAVE SUFFERED FROM INTERNAL FIRE - NON MODIFICATION SERVICE BULLETIN72-00-00V2500-A1,-A5
ENG-72-045406/10/030106/03/04See SBENGINE - HP COMPRESSOR, STAGE 3 ROTOR - ACTIONS REQUIRED FOLLOWING A FOD OR BIRDSTRIKE EVENT - NON-MODIFICATION SERVICE BULLETIN72-00-00V2500-A1,-A5,-D5
ENG-72-045504/28/037ENGINE - PROVIDE NEW ADAPTER AND TUBE FOR DIFFUSER 10TH STAGE POSITIONS 72 AND 288 DEGREES72-00-00V2500-A1,-A5,-D5
ENG-72-045606/10/030106/03/04See SBENGINE - HP COMPRESSOR, STAGE 3 ROTOR - REPEAT INSPECTION OF CLAPPERS - NON-MODIFICATION SERVICE BULLETIN72-00-00V2500-A1,-A5,-D5
ENG-72-045705/15/033ENGINE - LP COMPRESSOR FAN BLADES - DOVETAIL ROOT FLANK INSPECTION AND APPLICATION OF DRY FILM LUBRICANT - NON MODIFICATION SERVICE BULLETIN72-31-00V2500-D5
ENG-72-045808/04/047ENGINE - MAIN GEARBOX ASSEMBLY - INTRODUCTION OF REDESIGNED TRANSPORTATION PLUGS AND COVERS72-60-00V2500-A1,-A5
ENG-72-045906/27/030409/26/084ENGINE - IN SHOP ACTION FOR ENGINES IN THE RANGE V10600 TO V11365 WITH P/N 2A1165 (FAG) NUMBER 3 BEARINGS INSTALLED72-00-00V2500-A5
ENG-72-046006/27/030203/04/055ENGINE - IN SHOP ACTION FOR ENGINES IN THE RANGE V10600 TO V11304 WITH P/N 2A1170 (MRC) NUMBER 3 BEARINGS INSTALLED WITH A LOW ENERGY STANDARD OF HARD FACE COATING HIGH PRESSURE COMPRESSOR (HPC) STUBSHAFT72-32-20V2500-A5
ENG-72-046107/30/030710/01/153NON-MODIFICATION SERVICE BULLETIN - ENGINE - INSPECTION OF THE NO. 5 BEARING COMPARTMENT (OIL JET) AND OIL TUBES FOR COKING72-50-00V2500-A1
ENG-72-046211/21/036ENGINE - LP COMPRESSOR - INTRODUCTION OF A REVISED HYDRAULIC SEAL AND A REVISED NO.2 BEARING OIL JET72-32-00V2500-A1,-A5,-D5
ENG-72-046301/09/040101/09/048ENGINE - HP COMPRESSOR RING CASES - INCREASE IN TIP CLEARANCE TO STAGE 6 AND STAGE 7 ROTOR PATHS72-41-00V2500-A1
ENG-72-046412/22/030107/19/048NEW FIRST STAGE BLADE OUTER AIR SEAL AND HPT VANE SUPPORT (CONTROLLED SERVICE USE)72-44-00V2500-D5
ENG-72-046601/28/040103/15/048ENGINE - LP TURBINE - DELETION OF ENGINE MANUAL REQUIREMENTS FOR MEASUREMENT OF CLEARANCES DURING LP TURBINE ASSEMBLY72-50-10V2500-A1,-A5,-D5
ENG-72-046812/22/030103/18/045NMSB - INSPECTION OF NO.3 BEARING ON PN 2A1170 FOR IMPROPER BREAK EDGE ON OIL FEED HOLES OF THE INNER BEARING RACE72-32-00V2500-A5
ENG-72-046910/25/046ENGINE - LP COMPRESSOR TO ANNOUNCE THE AVAILABILITY OF LPC FRONT CASE WITH HIGHER EROSION RESISTANT ABRADABLE SEAL72-32-00V2500-A5,-D5
ENG-72-047007/28/040210/13/057ENGINE - HP COMPRESSOR DISCS (STAGES 3-8) - INTRODUCTION OF REVISED DISC ASSEMBLY WITH REDUCED STAGE 7 REAR DAMPER WIRE RETAINING WALL DIAMETER72-41-11V2500-A1,-A5,-D5
ENG-72-047105/20/040202/19/106ENGINE - HP COMPRESSOR BLADES - INTRODUCTION OF STAGE 6 AND 7 BLADES WITH REVISED MATERIAL72-41-15V2500-A5,-D5
ENG-72-047208/26/040107/27/056ENGINE - HP COMPRESSOR DISCS (STAGES 3-8) - INTRODUCTION OF REVISED DAMPER WIRES72-41-11V2500-A1,-A5,-D5
ENG-72-047302/25/040202/19/076ENGINE - HP COMPRESSOR, STAGE 6 ROTOR - REMOVAL OF BLADES - NON-MODIFICATION SERVICE BULLETIN72-41-15V2500-A1
ENG-72-047403/12/040204/26/07See SBNON - MODIFICATION SERVICE BULLETIN - HIGH PRESSURE TURBINE (HPT) STAGE 2 HUB INSPECTION72-45-00V2500-A5
ENG-72-047507/30/040305/07/197ENGINE - HP TURBINE ROTOR ASSEMBLY - INTRODUCE NEW FIRST STAGE TURBINE BLADES AND STAGE 1 HPT COOLING DUCT ASSEMBLY WITH DECREASED FLOW72-00-00V2500-A5,-D5
ENG-72-047607/06/05See SBENGINE - HP COMPRESSOR DISCS (STAGES 3-8) - INTRODUCTION OF A DISC ASSEMBLY WITH REVISED MATERIAL STAGES 6 TO 872-41-11V2500-A1
ENG-72-047703/16/057ENGINE - HP COMPRESSOR RING CASES - DELETION OF STAGE 8 TO 11 HEATSHIELDS - MOD 72-047772-41-00V2500-A5,-D5
ENG-72-047806/07/040107/12/057ENGINE - REPLACE NUMBER 3 BEARING CARBON SEAL ASSEMBLY72-32-00V2500-A1,-A5,-D5
ENG-72-048005/18/057ENGINE - MAIN GEARBOX ASSEMBLY - TO ANNOUNCE A NEW FACE SEAL FOR THE HYDRAULIC PUMP DRIVE GEAR72-60-00V2500-A1,-A5
ENG-72-048108/04/040107/26/055ENGINE - HP COMPRESSOR BLADES - INTRODUCTION OF A PART NUMBER TO RE-IDENTIFY EDM MANUFACTURED STAGE 3 BLADES72-41-15V2500-A5,-D5
ENG-72-048205/18/057ENGINE - MAIN GEARBOX ASSEMBLY - TO ANNOUNCE A NEW TYPE OF SHIM72-60-00V2500-A1,-A5,-D5
ENG-72-048301/26/050409/19/135ENGINE- NEW FIRST STAGE DUCT SEGMENTS AND HPT VANE SUPPORT720000V2500-A5,-D5
ENG-72-048410/07/040302/14/073ENGINE - HP COMPRESSOR, STAGE 4 ROTOR - ULTRASONIC INSPECTION OF AEROFOIL, EDDY CURRENT INSPECTION OF BLADE LEADING EDGE - NON-MODIFICATION SERVICE BULLETIN72-00-00V2500-A1
ENG-72-048509/01/050203/12/098ENGINE - LP COMPRESSOR - REWORK THE INSERT HOLES OF LPC BLEED DUCT ASSEMBLY72-32-00V2500-A5,-D5
ENG-72-048604/22/050106/20/057ENGINE HP COMPRESSOR VARIABLE VANES INTRODUCTION OF A REVISED VIGV WITH AN OPTIMISED SPINDLE72-41-30V2500-A5,-D5
ENG-72-048701/04/050206/17/056ENGINE - HP COMPRESSOR BLADES - INTRODUCTION OF A STAGE 3 BLADE WITH A REVISED CLAPPER MOD 72-048772-41-15V2500-A5,-D5
ENG-72-048807/14/050202/23/067ENGINE - STATIC SEAL - INTRODUCTION OF A REVISED HP COMPRESSOR STAGE 12 REAR SEAL ASSEMBLY72-42-50V2500-A5,-D5
ENG-72-048903/10/050106/06/068ENGINE - ALLOW FOR THE USE OF REOPERATED 2ND STAGE HPT VANES IN NEWER DELIVERED CONFIGURATIONS72-45-24V2500-A5,-D5
ENG-72-049005/23/057ENGINE - HP COMPRESSOR BLADES - INTRODUCTION OF A STAGE 5 BLADE WITH REVISED ROOT GEOMETRY - MOD 72-049072-41-15V2500-A1,-A5,-D5
ENG-72-049102/08/050203/30/07See SBNON - MODIFICATION SERVICE BULLETIN - BORESCOPE INSPECTION OF HIGH PRESSURE TURBINE (HPT) STAGE 2 AIR SEAL72-20-00V2500-A1,-A5,-D5
ENG-72-049211/07/060105/31/117ENGINE - MAIN GEARBOX ASSEMBLY - TO ANNOUNCE A NEW GEARBOX WITH HELICAL COILS AND BOLTS IN PLACE OF STUDS AND LOCKING RINGS72-60-00V2500-A1,-A5
ENG-72-049305/12/050202/17/066ENGINE - NUMBER 4 COMPARTMENT SCAVENGE ELBOW REDESIGN - MOD 72-049372-42-00V2500-D5
ENG-72-049403/11/053NON - MODIFICATION - ENGINE - MAGNETIC CHIP DETECTOR (MCD) INSPECTIONS FOR ENGINE SERIAL NUMBERS V10600 TO V11250 INCLUSIVE WITH (FAG) PN 2A1165 NO. 3 BEARINGS INSTALLED WITH BEARING BALLS PROVIDED FROM AN ALTERNATE SUPPLIER. 3 BEARINGS72-32-20V2500-A5
ENG-72-049505/18/054NON - MODIFICATION - ENGINE - GEARBOX - SCAVENGE OIL FILTER HOUSING ASSEMBLY - HERMOCOUPLE THREAD INSPECTION/REWORK72-00-00V2500-A5
ENG-72-049607/01/050202/17/103ENGINE - HP COMPRESSOR, STAGE 3 - REPEAT INSPECTION OF CLAPPERS - NON-MODIFICATION SERVICE BULLETIN72-00-00V2500-A5,-D5
ENG-72-049710/10/050103/22/065ENGINE - REDESIGNED NUMBER 4 BEARING COMPARTMENT OIL NOZZLE BOLT RETENTION72-42-00V2500-A1,-A5,-D5
ENG-72-049808/02/058ENGINE - INTRODUCE PLUG AND WASHER FOR TURBINE EXHAUST CASE REPAIR (VRS3655) STRUTS 4, 7, 8, AND 1072-50-00V2500-A1
ENG-72-049907/14/050201/12/073ENGINE - HP COMPRESSOR - BOROSCOPE INSPECTION OF STAGES 6 TO 8 ROTOR BLADES AND STAGES 6 TO 7 STATOR VANES - NON-MODIFICATION SERVICE BULLETIN72-00-00V2500-D5
ENG-72-050007/25/050107/14/063NON-MODIFICATION SERVICE BULLETIN - N2 VIBRATION MONITORING FOR THE HIGH PRESSURE TURBINE (HPT) STAGE 2 AIR SEAL72-40-00V2500-A1,-A5
ENG-72-050107/25/050107/14/063NON-MODIFICATION SERVICE BULLETIN - N2 VIBRATION MONITORING FOR THE HIGH PRESSURE TURBINE (HPT) STAGE 2 AIR SEAL72-40-00V2500-D5
ENG-72-050207/22/050103/15/066NON-MODIFICATION SERVICE BULLETIN - REPLACEMENT OF HIGH PRESSURE TURBINE (HPT) STAGE 2 AIR SEAL72-40-00V2500-A1,-A5,-D5
ENG-72-050307/19/050212/01/058ENGINE - LP COMPRESSOR - INTRODUCTION OF NEW BRACKET FOR MODIFIED FB FLANGE OF FAN CASE ASSEMBLY72-32-85V2500-A1,-A5
ENG-72-050412/15/067ENGINE - MAIN GEARBOX ASSEMBLY - TO ANNOUNCE A NEW DEOILER CASING72-60-31V2500-A1,-A5
ENG-72-050507/29/050503/16/114ENGINE - HP COMPRESSOR STAGE 4 ROTOR BLADES - ULTRASONIC INSPECTION OF V2500-SB-ENG-72-0295 STANDARD BLADE ROOTS - NON MODIFICATION SERVICE BULLETIN72-00-00V2500-A5,-D5
ENG-72-050811/21/050311/30/077ENGINE - INTRODUCTION OF NEW SPEED AND TRIM BALANCE PROBES72-32-18V2500-A1,-A5
ENG-72-050903/24/060211/16/106ENGINE - HP COMPRESSOR BLADES - INTRODUCTION OF HP COMPRESSOR LOCKPLATES WITH REVISED PROFILE72-41-15V2500-A1,-A5,-D5
ENG-72-A051005/09/070212/19/073ENGINE - HIGH PRESSURE (HP) COMPRESSOR - VORTEX REDUCER INSPECTION AND OVERHAUL POLICY - ALERT NON-MODIFICATION SERVICE BULLETIN72-41-12V2500-A1,-A5,-D5
ENG-72-051110/09/067ENGINE - NEW 1ST STAGE ROTOR ASSEMBLY WITH METERING PLUGS REMOVED AND NEW 1ST STAGE HPT SEAL72-00-00V2500-A5,-D5
ENG-72-052102/06/060102/08/066ENGINE - VALUE RING ASSEMBLY - REPLACEMENT OF SEAL WHICH MAY BE DETACHED FROM VALUE RING ASSEMBLY - NON - MODIFICATION SERVICE BULLETIN72-32-00V2500-A5
ENG-72-052212/20/060306/09/106ENGINE - PROVIDE NEW SECOND STAGE VANE WITH INCREASED COOLING AIR72-45-00V2500-A5,-D5
ENG-72-052506/12/060203/12/083NON-MODIFICATION SERVICE BULLETIN - ENGINE - MAGNETIC CHIP DETECTOR (MCD) INSPECTIONS FOR ENGINES WITH A CERTAIN POPULATION OF ENGINES WITH PN 2A1170 NUMBER 3 BEARINGS INSTALLED72-32-20V2500-A5,-D5
ENG-72-052702/21/070105/07/073ENGINE - ANGLE GEARBOX ASSEMBLY - TO ANNOUNCE A NEW GEARBOX WITH PARTIAL HEAT TREATED BEARING SUPPORT - NON-MODIFICATION SERVICE BULLETIN72-60-00V2500-A5
ENG-72-052808/08/060305/14/214ENGINE - HIGH PRESSURE (HP) COMPRESSOR STAGE 6 STATOR VANES - ONE-OFF IN-SHOP INSPECTION PROCEDURE - NON-MODIFICATION SERVICE BULLETIN72-41-22V2500-A5,-D5
ENG-72-053010/24/065ENGINE - HIGH PRESSURE (HP) COMPRESSOR, REAR STATIC AIR SEAL - CONFORMITY CHECK - NON-MODIFICATION SERVICE BULLETIN72-42-50V2500-A5
ENG-72-053202/19/070102/23/076ENGINE - HIGH PRESSURE (HP) COMPRESSOR - HP COMPRESSOR STAGE 6 ROTOR BLADES WITH IMPROVED ROOT DEFINITION72-41-15V2500-A1
ENG-72-053312/21/064ENGINE - HIGH PRESSURE (HP) COMPRESSOR ROTOR BLADES AND STATOR VANES - REPLACEMENT OF BLADES AND VANES FOR SAND EROSION - NON-MODIFICATION SERVICE BULLETIN72-41-00V2500-D5
ENG-72-053405/04/070403/18/096ENGINE - PROVIDE NEW SECOND STAGE TURBINE AIR SEAL72-45-00V2500-A5,-D5
ENG-72-053510/16/060111/08/06See SBENGINE - COMPRESSOR NON MODULAR - INTRODUCTION OF A CABLE FEED - THROUGH ADAPTER FOR THE FUEL LAQUER AND TEMPERATURE SURVEY INVESTIGATION72-38-25V2500-A5
ENG-72-053611/03/060112/14/063ENGINE - HP COMPRESSOR - ONE-OFF BORESCOPE INSPECTION OF STAGES 6 TO 8 BLADES AND STAGES 6 TO 8 VANES - NON-MODIFICATION SERVICE BULLETIN72-00-00V2500-D5
ENG-72-053704/20/073ENGINE - LP COMPRESSOR - INSPECTION OF FAN CASE LINER FRONT PANEL72-32-00V2500-A5
ENG-72-053812/21/077ENGINE - HIGH PRESSURE (HP) COMPRESSOR - VARIABLE INLET GUIDE VANES (VIGV) AND VARIABLE STAGE VANES (VSV) ACTUATING MECHANISM - INTRODUCTION OF SIMPLIFIED CONTROL RODS72-41-34V2500-A5,-D5
ENG-72-053901/29/073ENGINE - LP COMPRESSOR - TAPPING INSPECTION OF FRONT ANTI ICE IMPACT PANELS OF PRE SB V2500-ENG-72-0103 STANDARD FAN CASE ASSEMBLY - NON-MODIFICATION SERVICE BULLETIN72-32-85V2500-A1
ENG-72-054102/05/070403/12/08See SBNON-MODIFICATION SERVICE BULLETIN FOR OIL IN TURBINE FIXES72-40-00V2500-A1,-A5,-D5
ENG-72-054208/07/070101/07/095ENGINE - NEW FIRST STAGE DUCT SEGMENTS AND HPT VANE SUPPORT72-00-00V2500-A1
ENG-72-054305/14/070105/25/074ENGINE - REPLACEMENT OF PN 2A2493-01 NUMBER 4 BEARING COMPARTMENT OIL PRESSURE TUBES - NON MODIFICATION SERVICE BULLETIN72-42-20V2500-A1,-A5
ENG-72-054403/26/070207/07/086ENGINE - IN SHOP FOR ENGINES THAT HAVE A CERTAIN POPULATION OF PN 2A1170 NUMBER 3 BEARINGS INSTALLED - NON-MODIFICATION SERVICE BULLETIN72-32-24V2500-A5,-D5
ENG-72-054504/19/073ENGINE - HP COMPRESSOR, STAGE 3 ROTOR - REPEAT INSPECTION OF CLAPPERS - NON-MODIFICATION SERVICE BULLETIN72-00-00V2500-D5
ENG-72-054607/16/073ENGINE - INSPECTION OF FUEL NOZZLE AND SUPPORT ASSEMBLIES FOR CORRECT PART NUMBER INSTALLATION - NON-MODIFICATION SERVICE BULLETIN73-13-41V2500-A1,-A5
ENG-72-054801/11/080101/07/096ENGINE - PROVIDE NEW SECOND STAGE TURBINE AIR SEAL72-45-00V2500-A1
ENG-72-055111/15/078ENGINE - HIGH PRESSURE (HP) COMPRESSOR - INTRODUCTION OF STAGES 6 AND 7 STATOR VANES WITH EROSION RESISTANT COATING72-41-22V2500-D5
ENG-72-055201/22/086ENGINE - LOW PRESSURE (LP) TURBINE - INTRODUCTION OF NEW LP TURBINE CASE ASSEMBLY72-50-21V2500-A1
ENG-72-055305/25/097ENGINE - INTRODUCTION OF A NEW TRIM BALANCE PROBE AND DELETION OF RELATED POWERPLANT VOLTAGE DIVIDER HARNESS ASSEMBLY72-00-00V2500-A1,-A5
ENG-72-A055406/10/080106/27/083ALERT NON_MODIFICATION SERVICE BULLETIN - ENGINE - HP COMPRESSOR STAGE 9 TO 12 DISC ASSEMBLY - TO ANNOUNCE A REDUCTION IN CYCLIC LIFE DEPENDENT ON PART NUMBER AND THRUST RATING72-00-00V2500-A1,-A5,-D5
ENG-72-055505/22/080102/25/105ENGINE - HIGH PRESSURE (HP) COMPRESSOR - PINCH POINT REDUCTION ON STAGE 3, 4, 5 AND INTRODUCTION OF STAGE 4 SHROUDS WITH CLOSE TOLERANCE BOLTS72-41-33V2500-A5,-D5
ENG-72-055705/29/080108/12/143NON - MODIFICATION SERVICE BULLETIN - BORESCOPE INSPECTION OF HIGH PRESSURE TURBINE (HPT) STAGE 1 DUCT SEGMENTS72-00-00V2500-A1,-A5,-D5
ENG-72-055812/01/080101/19/098ENGINE - LP TURBINE - INTRODUCTION OF NEW MODULE PART NUMBERS72-50-00V2500-A5
ENG-72-056005/30/120107/19/178ENGINE - HIGH PRESSURE (HP) COMPRESSOR - V2500 SELECTONE RETROFIT AND PRODUCTION - HP COMPRESSOR UPGRADE72-00-00V2500-A5
ENG-72-056111/22/080112/11/088ENGINE - HIGH PRESSURE (HP) COMPRESSOR - V2500 SELECTONE PRODUCTION - HP COMPRESSOR UPGRADE72-00-00V2500-A5
ENG-72-056209/22/080109/19/138ENGINE - HIGH PRESSURE TURBINE (HPT) - V2500 SELECTONE PRODUCTION AND RETROFIT - HPT UPGRADE720000V2500-A5
ENG-72-056309/22/088ENGINE - LP TURBINE - INTRODUCTION OF TURBINE VANES STAGE 372-50-22V2500-A5
ENG-72-056409/22/080108/16/188ENGINE - HIGH PRESSURE (HP) COMPRESSOR - V2500 SELECTONE PRODUCTION - INTRODUCTION OF REDESIGNED VARIABLE STATOR VANE (VSV) SYSTEM72-41-00V2500-A5
ENG-72-056508/22/080203/27/17 ENGINE - PROVIDE THE REQUIREMENTS FOR MODIFICATION TO THE V2500 SELECTONE RETROFIT STANDARD72-00-00V2500-A5
ENG-72-056711/27/080406/20/138ENGINE - LOW PRESSURE (LP) TURBINE - INTRODUCTION OF A NEW INNER AIRSEAL STAGE 6 WITH 4 VENTILATION HOLES, FOR BEARING NO. 5 COMPARTMENT725000V2500-A1,-A5,-D5
ENG-72-056811/27/086ENGINE - SEAL ASSEMBLY, NO. 3 BEARING - REPLACEMENT OF THE CARBON SEAL FOR IMPROVED DURABILITY72-32-00V2500-A1,-A5,-D5
ENG-72-056906/21/087INFORMATION - ENGINE - PROVIDE NEW NO. 3 BEARING72-32-24V2500-A5,-D5
ENG-72-057001/06/097INFORMATION - ENGINE - PROVIDE NEW NO. 5 REAR BEARING HEAT SHIELD PART NUMBERS72-50-00V2500-A1
ENG-72-057109/22/086ENGINE - HIGH PRESSURE (HP) COMPRESSOR - V2500 SELECTONE PRODUCTION - INTRODUCTION OF A BAULKING FEATURE IN THE VARIABLE STATOR VANE (VSV) SYSTEM TO PREVENT MISASSEMBLY OF LEVER ARMS72-41-00V2500-A5
ENG-72-057209/22/08See SBENGINE - PROVIDE THE REQUIREMENTS FOR MODIFICATION TO THE V2500 SELECTONE PRODUCTION STANDARD72-00-00V2500-A5
ENG-72-057309/22/084ENGINE - HIGH PRESSURE (HP) COMPRESSOR - V2500 SELECTONE PRODUCTION - INCREASE OF CENRTALIZER PAD CLEARANCE TO REDUCE THE FORCE TO MOVE THE VARIABLE STATOR VANE (VSV) SYSTEM72-41-30V2500-A5
ENG-72-057509/22/080112/10/206ENGINE - ROTOR AND STATOR ASSEMBLY - PROVIDE NEW SELECTONE 2ND STAGE HIGH PRESSURE TURBINE (HPT) RESTAGGERED BLADES72-45-00V2500-A5
ENG-72-057609/22/086ENGINE - TURBINE NOZZLE - PROVIDE A SELECTONE NEW HIGH PRESSURE TURBINE (HPT) 1ST STAGE VANE ASSEMBLY72-44-00V2500-A5
ENG-72-057707/21/085NON-MODIFICATION SERVICE BULLETIN - HP COMPRESSOR - EVALUATION OF CHROMIUM NITRATE COATING EFFECTIVENESS ON HP COMPRESSOR STAGE 6 STATOR VANES72-41-22V2500-D5
ENG-72-057803/12/090111/09/097ENGINE - LP COMPRESSOR - INTRODUCTION OF FAN CASE PANELS WITH PAA ALUMINIUM HONEYCOMB72-32-85V2500-A1,-A5,-D5
ENG-72-057909/11/088ENGINE - LP COMPRESSOR - INTRODUCTION OF FAN CASE PANELS WITH PAA ALUMINIUM HONEYCOMB72-32-00V2500-A1,-A5,-D5
ENG-72-058012/19/080308/23/113NON - MODIFICATION SERVICE BULLETIN - BORESCOPE INSPECTION OF HIGH PRESSURE TURBINE (HPT) STAGE 1 DUCT SEGMENTS72-00-00V2500-A1,-A5,-D5
ENG-72-058101/15/107INFORMATION - ENGINE - PROVIDE A NEW NO. 3 BEARING OPTION72-32-24V2500-A5,-D5
ENG-72-058402/20/097ENGINE - LP COMPRESSOR - TO APPLY THE MULTI-RATING ENGINE IDENTIFICATION PLATE TO ALL A5 ENGINE MODELS72-32-85V2500-A5
ENG-72-058512/16/080203/01/104NON-MODIFICATION SERVICE BULLETIN - INSPECTION OF THE HPC STAGE 5 ROTOR BLADE RETAINING PLATE SLOT72-41-15V2500-A5,-D5
ENG-72-058601/27/090208/05/116NMSB - ENGINE - HIGH PRESSURE (HP) COMPRESSOR BLADES - SAMPLING OF THE HP COMPRESSOR STAGE 5 ROTOR BLADE RETAINING PLATE SLOT72-41-15V2500-A5,-D5
ENG-72-058704/01/090107/15/096ENGINE - HP COMPRESSOR BLADES - INTRODUCTION OF A STAGE 5 ROTOR BLADE WITH REVISED AEROFOIL POSITION72-41-15V2500-A5
ENG-72-058804/23/100202/09/187ENGINE - (LP) - INTRODUCTION OF REDUCED WEIGHT HONEYCOMBS72-50-00V2500-A1,-A5,-D5
ENG-72-058907/15/090111/24/096ENGINE - HP COMPRESSOR DISCS (STAGES 3-8) - RE-INTRODUCTION OF DAMPER WIRE STANDARD OF PRE SERVICE BULLETIN ENG-72-0472 STANDARD72-41-11V2500-A5
ENG-72-059004/09/090205/02/118ENGINE - CASE ASSEMBLY, TURBINE EXHAUST - REPLACEMENT OR MODIFICATION TO INCREASE N1 MARGIN AND IMPROVE PERFORMANCE DURING TAKE OFF72-50-53V2500-A1,-A5
ENG-72-059208/11/090102/05/106ENGINE - TUBE, NO. 4 BEARING ASSEMBLY PRESSURE - MODIFICATION TO PREVENT CRACKING OF WELD REPAIRED PARTS72-42-20V2500-A1,-A5,-D5
ENG-72-059304/28/090201/16/123NON-MODIFICATION SERVICE BULLETIN - ENGINE - HIGH PRESSURE (HP) COMPRESSOR - STAGE 3 TO 8 COMPRESSOR DRUM - ON-WING INSPECTION PROCEDURE72-41-11V2500-A5
ENG-72-059405/20/090802/13/20See SBNON-MODIFICATION - ENGINE - HIGH PRESSURE (HP) COMPRESSOR - STAGE 3 TO 8 COMPRESSOR DRUM - ULTRASONIC INSPECTION PROCEDURE AND STAGE 3 TO 8 COMPRESSOR DRUM REPLACEMENT NON-MODIFICATION SERVICE BULLETIN72-00-00V2500-A5
ENG-72-059511/20/097ENGINE - LP COMPRESSOR - DELETION OF SCREENS OF THE LPC BLEED DUCT ASSEMBLY72-32-60V2500-A1
ENG-72-059606/22/090102/17/116ENGINE - HIGH PRESSURE (HP) COMPRESSOR DISCS - INTRODUCTION OF NUTS WITH SILVER PLATING ON THREAD ONLY72-41-12V2500-A1,-A5,-D5
ENG-72-059707/21/107ENGINE - EXTERNAL GEARBOX - INTRODUCTION OF OPTIMIZED ROLLER BEARINGS FOR THE DEOILER GEAR72-60-29V2500-A1,-A5
ENG-72-059812/08/096ENGINE - SEALS, STAGE 1 HIGH PRESSURE TURBINE (HPT) VANE - PROVIDE NEW SEALS WITH IMPROVED DURABILITY72-44-20V2500-A1,-A5,-D5
ENG-72-059907/15/096NON-MODIFICATION SERVICE BULLETIN - ENGINE - HP COMPRESSOR BLADES - INSPECTION OF THE HPC STAGE 8 LOCKING BLADE CORNER RADIUS72-41-15V2500-A5
ENG-72-060110/27/090204/12/106NON-MODIFICATION SERVICE BULLETIN - ENGINE - HIGH PRESSURE (HP) COMPRESSOR - STAGE 3 TO 8 COMPRESSOR DRUM - OVERHAUL SHOP SPECIAL CLEANING PROCEDURE72-41-11V2500-A1,-A5,-D5
ENG-72-060311/24/090402/13/20See SBNON-MODIFICATION SERVICE BULLETIN - ENGINE - HIGH PRESSURE (HP) COMPRESSOR - STAGE 3 TO 8 COMPRESSOR DRUM - ULTRASONIC INSPECTION PROCEDURE72-00-00V2500-A1
ENG-72-060405/18/105NON-MODIFICATION SERVICE BULLETIN - INSPECTION OF THE INNER AND OUTER COMBUSTION CHAMBER LINER ASSEMBLIES FOR DEFECTS72-00-00V2500-A5
ENG-72-060504/19/108ENGINE - HIGH PRESSURE (HP) COMPRESSOR DISCS (STAGES 3-8) - RE- NUMBERED FRONT DRUMS WITH INCREASED REPAIR LIMITS72-41-11V2500-A5
ENG-72-060604/19/100205/24/116ENGINE - HIGH PRESSURE (HP) COMPRESSOR DISCS (STAGES 3-8) - REPLACMENT OF SILVER PLATED SHANK NUTS72-41-11V2500-A1,-A5,-D5
ENG-72-060805/05/100402/13/203NON-MODIFICATION SERVICE BULLETIN - ENGINE - HIGH PRESSURE (HP) COMPRESSOR, STAGE 3 TO 8 COMPRESSOR DRUM - ULTRASONIC INSPECTION PROCEDURE72-00-00V2500-D5
ENG-72-060904/23/100203/21/123NON-MODIFICATION SERVICE BULLETIN - ENGINE - MAINTENANCE RECOMMENDATIONS AND SAMPLING INSPECTIONS IN RESPONSE TO POTENTIAL OPERATION IN THE VICINITY OF THE VOLCANIC ASH AREA RESULTING FROM EYJAFJALLAJOEKULL VOLCANO ERUPTION IN ICELAND72-00-00V2500-A1,-A5,-D5
ENG-72-061010/08/108NON-MODIFICATION SERVICE BULLETIN - REPLACEMENT OF PRESSURE KIEL TAPS IN THE TURBINE EXHAUST CASE (TEC) TO IMPROVE THRUST AND ENGINE PRESSURE RATIO (EPR) PERFORMANCE CHARACTERISTICS72-50-53V2500-A5
ENG-72-061212/13/107ENGINE - HIGH PRESSURE (HP) COMPRESSOR RING CASES - THERMAL BLANKET STAGE 7 TO 11 RE-DESIGN72-41-21V2500-A1,-A5,-D5
ENG-72-061302/11/116ENGINE - HIGH PRESSURE (HP) COMPRESSOR - INTRODUCTION OF A NEW HP COMPRESSOR REAR SHAFT ASSEMBLY WITH A RING NUT THAT IS SILVER PLATED ON THE THREAD AND ABUTMENT FACE TO THE CUP WASHER ONLY AND NUTS WHICH ARE SILVER PLATED ON THE THREADS ONLY72-41-00V2500-A1,-A5,-D5
ENG-72-061412/06/100101/13/117ENGINE - HIGH PRESSURE (HP) COMPRESSOR - INTRODUCTION OF A NEW HP COMPRESSOR REAR SHAFT ASSEMBLY WITH A RING NUT THAT IS SILVER PLATED ON THREAD AND ABUTMENT FACE TO THE CUP WASHER ONLY72-41-13V2500-A5,-D5
ENG-72-A061507/19/100903/27/173NON-MODIFICATION SERVICE BULLETIN - ENGINE - HIGH PRESSURE (HP) COMPRESSOR - STAGE 3 TO 8 COMPRESSOR DRUM - ULTRASONIC INSPECTION (USI) FOR STRESS CORROSION CRACKING72-41-11V2500-A1,-A5,-D5
ENG-72-061605/12/120101/11/217ENGINE - FUEL AND CONTROL - DEDICATED ALTERNATOR DRIVE GEAR ASSEMBLY - INTRODUCTION OF REVISED STANDARD OF GEAR A/O PMA DRIVE AND NUT FOR THE ENGINE DEDICATED ALTERNATOR72-60-33V2500-A1,-A5
ENG-72-061712/09/100209/24/126NMSB - X-RAY INSPECTION OF THE NO.4 BEARING SCAVENGE TUBE ASSEMBLY72-42-20V2500-A1,-A5
ENG-72-061811/10/100104/12/113ENGINE - HIGH PRESSURE (HP) COMPRESSOR - ONE TIME INSPECTION OF STAGE 3 ROTOR BLADE CLAPPERS - NON-MODIFICATION SERVICE BULLETIN72-00-00V2500-A5,-D5
ENG-72-062104/14/116NMSB - INSPECTION OF THE NO.4 BEARING ASSEMBLY PRESSURE TUBE PROFILE72-42-20V2500-A1,-A5,-D5
ENG-72-062210/27/117ENGINE - SEAL ASSEMBLY, NO. 3 BEARING - REPLACE OR MODIFY TO IMPROVE DURABILITY72-32-25V2500-A1,-A5,-D5
ENG-72-062509/20/110110/08/148NON-MODIFICATION SERVICE BULLETIN - ENGINE - HIGH PRESSURE (HP) COMPRESSOR STAGE 3 TO 8 COMPRESSOR DRUM - EDDY CURRENT INSPECTION (ECI)72-41-11V2500-A1,-A5,-D5
ENG-72-062603/01/120503/03/176ENGINE - LOW PRESSURE (LP) TURBINE - INTRODUCTION OF A STAGE 6 INNER AIRSEAL WITH A DAMPER RING72-50-00V2500-A1,-A5,-D5
ENG-72-062709/22/147ENGINE - HIGH PRESSURE (HP) COMPRESSOR CASES - SIMPLIFIED REAR INNER AND OUTER CASES72-41-00V2500-A5
ENG-72-062808/31/127ENGINE - INNER AND OUTER COMBUSTION CHAMBER LINERS WITH IMPROVED CHEMISTRY TO REDUCE OXIDATION72-40-00V2500-A1,-A5,-D5
ENG-72-062905/19/150302/25/216ENGINE - SEAL ASSEMBLY, NO. 4 BRG FRONT AND HOUSING ASSEMBLY, NO. 4 BRG OIL NOZZLE BLOCK AND NO. 4 BRG OIL NOZZLE ASSEMBLY - REPLACE OR MODIFY TO STOP OIL NOZZLE BLOCK HOUSING BOLTS FROM LIBERATION72-42-00V2500-A1,-A5,-D5
ENG-72-063004/16/120109/20/125NON-MODIFICATION SERVICE BULLETIN - NO.4 BEARING SCAVENGE TUBE ASSEMBLY REPLACEMENT PROCEDURE72-42-00V2500-D5
ENG-72-063108/07/120108/16/167ENGINE - PROVIDE NEW TURBINE COOLING AIR (TCA) ORIFICE PLATE TO IMPROVE THRUST SPECIFIC FUEL CONSUMPTION (TSFC)72-45-00V2500-A1,-A5,-D5
ENG-72-063212/20/120103/23/166ENGINE - HIGH PRESSURE (HP) COMPRESSOR DISCS - INTRODUCTION OF SILVER FREE NUTS72-41-12V2500-A1,-A5,-D5
ENG-72-063311/20/124ENGINE - ACTUATING MECHANISM HIGH PRESSURE (HP) COMPRESSOR VARIABLE VANES - CONTROL ROD LOCK NUT TORQUE INCREASE75-32-41V2500-A1,-A5,-D5
ENG-72-063401/31/140102/27/147ENGINE - SEALS, BLADE OUTER AIR (DUCT SEGMENTS), 1ST AND 2ND STAGE HIGH PRESSURE TURBINE (HPT) - REPLACE OR MODIFY TO IMPROVE EFFICIENCY72-45-00V2500-A5,-D5
ENG-72-063602/14/133NON-MODIFICATION SERVICE BULLETIN - NO.4 BEARING INTERNAL SCAVENGE TUBE ASSEMBLY REPLACEMENT PROCEDURE72-42-20V2500-A1,-A5
ENG-72-063705/02/130303/01/178NON-MODIFICATION SERVICE BULLETIN - ENGINE - HIGH PRESSURE (HP) COMPRESSOR - ENHANCED FLUORESCENT PENETRANT INSPECTION (FPI)72-41-11V2500-A1,-A5,-D5
ENG-72-063804/11/138NON-MODIFICATION SERVICE BULLETIN - ENGINE - HIGH PRESSURE (HP) COMPRESSOR - STAGE 3 TO 8 COMPRESSOR DRUM - ULTRASONIC INSPECTION PROCEDURE (USI)72-00-00V2500-A1,-A5,-D5
ENG-72-063911/17/160101/06/176NON-MODIFICATION SERVICE BULLETIN - ENGINE - SHAFT, ASSEMBLY, REAR HIGH PRESSURE COMPRESSOR - REMOVAL AND REPLACEMENT72-41-13V2500-A1,-A5,-D5
ENG-72-064010/28/136NON MODIFICATION SERVICE BULLETIN - ENGINE - NO. 4 BEARING, COOLING AIR DUCT, REAR - INSPECT AND REPLACE IF SUSPECT DUCTS ARE FOUND72-43-30V2500-A5
ENG-72-064107/22/146NON-MODIFICATION SERVICE BULLETIN - ENGINE - REAR STATIC SEAL, HIGH PRESSURE COMPRESSOR (HPC) - REPLACEMENT OF SUSPECT HPC REAR STATIC SEALS72-42-50V2500-A5
ENG-72-064203/21/140105/16/174ENGINE - HIGH PRESSURE (HP) COMPRESSOR - STAGE 3 TO 8 COMPRESSOR DRUM - INTRODUCTION OF DAMPER WIRES FOR STAGES 6 TO 872-41-11V2500-A5
ENG-72-064405/05/168INFORMATION - EXTERNAL GEARBOX MODULE - INTRODUCTION OF NEW SCREWS72-60-00V2500-A1,-A5,-D5
ENG-72-064502/26/188ENGINE - EXTERNAL GEARBOX MODULE - INTRODUCTION OF AN ALTERNATIVE SOURCE OF ROLLER AND BALL BEARINGS72-60-00V2500-A1,-A5,-D5
ENG-72-064705/10/197ENGINE - BRACKET, MOUNTING - INTRODUCTION OF A MOUNTING BRACKET MADE FROM A DIFFERENT MATERIAL72-32-00V2500-A1,-A5,-D5
ENG-72-064911/24/158ENGINE - RING SEGMENT ASSEMBLIES, 2ND STAGE HIGH PRESSURE TURBINE (HPT) - INTRODUCTION OF, FOR IMPROVED EFFICIENCY72-45-24V2500-A5
ENG-72-065006/08/153ENGINE - NO. 4 BEARING SCAVENGE TUBE ASSEMBLY - REPLACEMENT OF, WITH A HIGHER STRENGTH TUBE72-42-00V2500-A1,-A5,-D5
ENG-72-A065211/17/163NON-MODIFICATION SERVICE BULLETIN - ENGINE - DISC, HIGH PRESSURE COMPRESSOR 9-12, ASSEMBLY OF - REMOVAL OF72-41-12V2500-A1,-A5,-D5
ENG-72-065302/25/157ENGINE - BLADE, SECOND STAGE HIGH PRESSURE TURBINE (HPT) - INTRODUCTION OF, TO REDUCE CORROSION72-45-32V2500-A1,-A5,-D5
ENG-72-065501/28/157ENGINE - BLADE, STAGE 4 LOW PRESSURE TURBINE (LPT) - REINTRODUCTION OF HOT GAS CORROSION PROTECTION COATING TO REDUCE SULFIDATION 72-50-32V2500-A1,-A5,-D5
ENG-72-065602/12/154NON-MODIFICATION SERVICE BULLETIN - ENGINE - BIFURCATION PANEL FIRE SEAL - INSPECTION FOR NON-CONFORMING SEALS72-38-25V2500-A5
ENG-72-066010/01/150205/10/193NON.MODIFICATION SERVICE BULLETIN - ENGINE - NO. 5 OIL PRESSURE AND SCAVENGE TUBES, OIL JET, ELBOWS, FILTERS - REPLACEMENT AT FIXED INTERVALS, TO MITIGATE COKE AND CARBON BUILDUP.72-50-50V2500-A1,-A5,-D5
ENG-72-066111/10/150505/02/174NON-MODIFICATION SERVICE BULLETIN - ENGINE - STAGE 1 AND STAGE 2 HPT HUB - OVER INSPECTION FOR MANUFACTURING DEFECTS72-45-00V2500-A5,-D5
ENG-72-066203/01/166ENGINE - LP COMPRESSOR - PROVIDE A NEW FAN CASE TO MAIN GEARBOX ASSEMBLY MATING SEAL RING72-32-00V2500-A1,-A5,-D5
ENG-72-066303/09/170110/02/176NON-MODIFICATION SERVICE BULLETIN - ENGINE - PACKING - REMOVAL OF SUSPECT PACKINGS72-60-21V2500-A5
ENG-72-066404/28/167ENGINE - AIR - RING, SEALING - REPLACEMENT OF, FOR PROCUREMENT75-00-00V2500-A1,-A5,-D5
ENG-72-066703/23/177INFORMATION - ENGINE - ROTATING RING - INTRODUCTION OF AN ALTERNATIVE ROTATING RING ON THE D5 ENGINE MODEL72-60-29V2500-D5
ENG-72-066811/24/150106/22/163NON-MODIFICATION SERVICE BULLETIN - OIL - TURBINE EXHAUST CASE (TEC) WEEP HOLE, NO. 4 BEARING WEEP LINE - INSPECTION OF, TO DETECT OIL LEAKS79-00-00V2500-A1
ENG-72-066906/02/166NON MODIFICATION SERVICE BULLETIN - ENGINE - LP COMPRESSOR - INTRODUCTION OF A NEW FRONT MOUNT TUBE STOPPER72-32-00V2500-A1,-A5
ENG-72-067003/14/163NON-MODIFICATION SERVICE BULLETIN - ENGINE - OIL CONSUMPTION MONITORING AND NO. 4 FRONT AND REAR SEAL SEAT REPLACEMENT72-00-43V2500-A1
ENG-72-067103/22/163NON-MODIFICATION SERVICE BULLETIN - NO. 3 BEARING - REDUCED MASTER MAGNETIC CHIP DETECTOR INSPECTION INTERVAL FOR SUSPECT POPULATION (LOT A)72-32-24V2500-A5
ENG-72-067203/22/163NON-MODIFICATION SERVICE BULLETIN - NO. 3 BEARING - REDUCED MASTER MAGNETIC CHIP DETECTOR INSPECTION INTERVAL FOR SUSPECT POPULATION (LOT B)72-32-24V2500-A5
ENG-72-067306/03/164NON-MODIFICATION SERVICE BULLETIN - REPLACEMENT OF NO. 3 BEARINGS FROM SUSPECT POPULATION (LOT A)72-30-00V2500-A1,-A5,-D5
ENG-72-067406/06/166NON-MODIFICATION SERVICE BULLETIN - REPLACEMENT OF NO. 3 BEARINGS FROM SUSPECT POPULATION (LOT B)72-30-00V2500-A1,-A5,-D5
ENG-72-067508/03/177ENGINE - GASKET, ASSEMBLY - INTRODUCTION OF A NEW GASKET ASSEMBLY TO MINIMIZE LEAKAGE72-40-00V2500-A1,-A5,-D5
ENG-72-067610/14/163NON-MODIFICATION SERVICE BULLETIN - HIGH PRESSURE TURBINE STAGE 2 AIR SEAL - REPLACEMENT OF72-45-00V2500-A1,-A5,-D5
ENG-72-067712/02/160101/11/173NON-MODIFICATION SERVICE BULLETIN - ENGINE - SEAL, AIR, HPT, 1 STAGE - REPLACEMENT OF72-45-12V2500-A1,-A5,-D5
ENG-72-067812/13/160101/05/176NON-MODIFICATION SERVICE BULLETIN - ENGINE - SEAL, AIR, HPT, 1 STAGE - REPLACEMENT OF72-45-12V2500-A1,-A5,-D5
ENG-72-067904/03/174NON-MODIFICATION SERVICE BULLETIN - ENGINE - NO. 2 BEARING - BORESCOPE INSPECTION OF,72-32-52V2500-A1,-A5,-D5
ENG-72-068112/13/160201/09/176NON-MODIFICATION SERVICE BULLETIN - ENGINE - PLATE, RING HPT, STAGE 2 - REPLACEMENT OF72-45-33V2500-A1,-A5,-D5
ENG-72-068212/02/163NON-MODIFICATION SERVICE BULLETIN - ENGINE - PLATE, RING HPT, STAGE 2 - CYCLIC LIFE REDUCTION72-45-33V2500-A1,-A5,-D5
ENG-72-068307/19/176ENGINE - FAN SPEED/TRIM BALANCE PROBES ELECTRICAL HARNESS - INTRODUCTION OF A NEW PART NUMBER72-32-37V2500-A1,-A5
ENG-72-068407/19/178ENGINE - FAN SPEED/TRIM BALANCE PROBES ELECTRICAL HARNESS - INTRODUCTION OF A SLEEVE FOR REPAIR72-32-37V2500-A1,-A5,-D5
ENG-72-068712/03/180112/14/186ENGINE - WASHER - REPLACE THE HIGH PRESSURE COMPRESSOR (HPC) REAR DRUM WASHERS TO REDUCE THE POTENTIAL OF 12TH STAGE ROTOR CRACKING DUE TO ASSEMBLY ERROR72-41-00V2500-A5,-D5
ENG-72-068809/06/186NON-MODIFICATION SERVICE BULLETIN - ENGINE - HIGH PRESSURE TURBINE (HPT) STAGE 2 VANE - INSPECT INTERNAL RIB AT 1ST PIECE PART INSPECTION72-45-00V2500-A5,-D5
ENG-72-068902/13/184ENGINE - BEARING, ROLLER - INSPECTION FOR SUSPECT ROLLER BEARINGS72-60-22V2500-A5
ENG-72-069110/11/177ENGINE - LP COMPRESSOR - INTRODUCTION OF NEW FAN CASE ASSEMBLY WITH NEW ACOUSTIC LINING PRIMER72-32-85V2500-A5
ENG-72-069201/12/187ENGINE - LP COMPRESSOR - INTRODUCTION OF NEW REPAIR ONLY PARTS FOR FAN CASE ACOUSTIC LININGS WITH NEW ADHESIVE PRIMER72-32-85V2500-A1,-A5,-D5
ENG-72-069301/24/187ENGINE - NO. 3 BEARING OPTION - INCORPORATION OF BEARING OPTION USING IMPROVED MANUFACTURING PROCESS72-32-24V2500-A5,-D5
ENG-72-069401/05/180207/02/183NON-MODIFICATION SERVICE BULLETIN - ENGINE - TURBINE EXHAUST CASE (TEC) - EDDY CURRENT INSPECTION (ECI)72-50-00V2500-D5
ENG-72-069601/23/187ENGINE - FAN SPEED/TRIM BALANCE PROBES ELECTRICAL HARNESS - INTRODUCTION OF A NEW PART NUMBER72-32-37V2500-D5
ENG-72-A069709/21/180111/27/183NON-MODIFICATION SERVICE BULLETIN - ENGINE - DISK STAGE 6, LOW PRESSURE TURBINE (LPT) - REMOVAL OF SUSPECT DISKS72-50-31V2500-A5
ENG-72-069806/28/186ENGINE - PACKING, PREFORMED - REPLACEMENT OF THE NO. 3 BEARING SEAL SUPPORT PREFORMED PACKING WITH A SMALLER PREFORMED PACKING TO REDUCE OIL LEAKAGE72-32-20V2500-A5,-D5
ENG-72-069910/23/199ENGINE - GASKET OPTION - ADDITION AND REMOVAL OF A NEW GASKET OPTION72-45-24V2500-A5
ENG-72-070104/12/190103/08/216ENGINE - LP COMPRESSOR - REPLACEMENT OF SEVERAL RINGS TO REDUCE OIL LEAKS72-32-00V2500-A1,-A5,-D5
ENG-72-070302/25/190106/27/194NON-MODIFICATION SERVICE BULLETIN - ENGINE - CONTROL RODS, ASSEMBLY OF - PROVIDE AN EDDY CURRENT INSPECTION (ECI) TO IDENTIFY ANY NON-CONFORMING MATERIAL WITHIN THE CONTROL RODS72-41-34V2500-A1,-A5,-D5
ENG-72-070404/26/190111/18/196ENGINE - VALVE RING ASSEMBLY - REPLACEMENT OF THE VALVE RING ASSEMBLY AND ASSOCIATED HARDWARE TO IMPROVE DURABILITY72-32-72V2500-A5,-D5
ENG-72-070504/05/196NON-MODIFICATION SERVICE BULLETIN - ENGINE - PACKING - REMOVAL OF SUSPECT PACKINGS72-60-21V2500-A5
ENG-72-A070602/14/190211/08/193NON-MODIFICATION ALERT SERVICE BULLETIN - ENGINE - DIFFUSER CASE REAR OUTER FLANGE - DIFFUSER CASE "M" FLANGE REPETITIVE VISUAL INSPECTION FOR CRACKS72-42-11V2500-A1,-A5,-D5
ENG-72-070707/01/193NON-MODIFICATION SERVICE BULLETIN - ENGINE - CASE, DIFFUSER, ASSEMBLY- REPLACEMENT OF SUSPECT DIFFUSER CASE ASSEMBLIES 72-42-11V2500-A5
ENG-72-070912/13/190102/20/203ENGINE - CASE, DIFFUSER, ASSEMBLY - MODIFICATION OF THE DIFFUSER CASE ASSEMBLY REAR OUTER FLANGE72-42-11V2500-A1,-A5,-D5
ENG-72-071312/14/200101/26/213NON-MODIFICATION SERVICE BULLETIN - ENGINE - HUB, HIGH PRESSURE TURBINE (HPT), STAGE 1 AND 2 - ANGLE SCAN ULTRASONIC INSPECTION TO FIND AN ANOMALY IN THE MATERIAL72-45-00V2500-A5,-D5
ENG-73-CN0101/17/010302/27/07See SBENGINE - CONVERSION OF V2500-A5 ENGINES FROM INSTALLATION ARRANGEMENT NUMBER AQ02 TO AQ03 STANDARD73-22-52V2500-A5
ENG-73-CN0201/17/010210/26/06See SBENGINE - CONVERSION OF V2500-A5 ENGINES FROM INSTALLATION ARRANGEMENT NUMBER AQ03 TO AQ02 STANDARD73-22-52V2500-A5
ENG-73-000104/28/936FUEL AND CONTROL - INCORPORATE A CHAMFER ON THE P4.9 PRESSURE CONTROL MANIFOLD ADAPTOR73-00-00V2500-A1
ENG-73-000211/10/894FUEL - REPLACE THE FUEL DIVERTER AND RETURN VALVE ATTACHING WASHER73-00-00V2500-A1
ENG-73-000310/06/896FUEL AND CONTROL - FUEL SYSTEM AIR TUBES, P12.5 TUBE SUPPORT BRACKET, WIRE LOCKING PROVISION73-00-00V2500-A1
ENG-73-000402/15/926ENGINE - FUEL AND CONTROL - PROVIDE NEW PRESSURE CONTROL MANIFOLDS WITH IMPROVED CLIPPING73-00-00V2500-A1
ENG-73-000512/01/896FUEL AND CONTROL - PROVIDE AN ADDITIONAL WASHER ON THE Hi- LOK PIN OF THE DATA ENTRY PLUG73-00-00V2500-A1
ENG-73-000601/26/904FUEL AND CONTROL - INCORPORATE REVISED EBU HARNESS CLIPPING REQUIREMENTS AT CP5671 AND CP109773-11-49V2500-A1
ENG-73-000712/01/894ENGINE - FUEL AND CONTROL - INCORPORATE A NEW ELECTRONIC ENGINE CONTROL (EEC) CONFIGURATION73-00-00V2500-A1
ENG-73-000801/12/904FUEL AND CONTROL - INTRODUCE A REVISED ELECTRICAL CONNECTOR COOLING SHIELD BRACKET73-00-00V2500-A1
ENG-73-000902/16/90See SBENGINE - FUEL AND CONTROL - INCORPORATE A NEW ELECTRONIC ENGINE CONTROL (EEC) CONFIGURATION73-22-34V2500-A1
ENG-73-001010/05/906FUEL AND CONTROL - INCORPORATE A RECONTOURED P2/T2 AIR TUBE ASSEMBLY73-00-00V2500-A1
ENG-73-001109/29/894FUEL AND CONTROL - REWORK THE PS3 BURNER AIR TUBE ASSEMBLY TO INCORPORATE ENLARGED MOISTURE TRAP DRAIN HOLES73-00-00V2500-A1
ENG-73-001211/16/903FUEL AND CONTROL - ELECTRONIC ENGINE CONTROL (EEC) - BURNER PRESSURE (PB) SENSOR TUBES - MOISTURE CONTAMINATION CHECK73-00-00V2500-A1
ENG-73-001309/18/924FUEL AND CONTROL - SELECTIVE REPROGRAMMING OF THE DATA ENTRY PLUG ASSEMBLY73-00-00V2500-A1
ENG-73-001411/23/903ENGINE - ELECTRONIC ENGINE CONTROL (EEC) - BURNER PRESSURE (PB) SENSOR TUBE - MOISTURE CONTAMINATION CHECK73-00-00V2500-A1
ENG-73-001506/01/900210/12/904FUEL AND CONTROL - INCORPORATE A NEW ELECTRONIC ENGINE CONTROL (EEC) CONFIGURATION AND REWORK THE DATA ENTRY PLUG ASSEMBLY TO THE SC1 1 E SOFTWARE CONFIGURATION73-22-00V2500-A1
ENG-73-001611/16/906FUEL AND CONTROL - REWORK THE EEC SUPPORT ASSEMBLY ALIGNMENT HOLES73-00-00V2500-A1
ENG-73-001704/20/906FUEL AND CONTROL - TO ANNOUNCE A FUEL METERING UNIT WITH A STRENGTHENED SPILL VALVE COVER73-00-00V2500-A1
ENG-73-001811/02/904FUEL AND CONTROL - REPLACEMENT OF FUEL FEED TUBE73-00-00V2500-A1
ENG-73-001907/05/916FUEL AND CONTROL - INCORPORATE BURNER PRESSURE (PB) SENSOR TUBES WITH REVISED MOISTURE TRAPS73-00-00V2500-A1
ENG-73-002106/01/904FUEL AND CONTROL - REPLACE THE TUBE CLIP AT CLIPPING POINT CP079573-00-00V2500-A1
ENG-73-002212/07/904FUEL AND CONTROL - REPLACE THE TUBE CLIP AT CLIPPING POINT CP030673-00-00V2500-A1
ENG-73-002311/02/903FUEL AND CONTROL - REPLACE FUEL NOZZLE ASSEMBLIES73-00-00V2500-A1
ENG-73-002407/26/916FUEL AND CONTROL - PROVIDE AN ELECTRONIC ENGINE CONTROL (EEC) WITH IMPROVED PRINTED CIRCUIT BOARDS73-00-00V2500-A1
ENG-73-002504/12/915ENGINE - FUEL AND CONTROL - MARKING OF THE EPR MODIFICATION CLASS NUMBER73-00-00V2500-A1
ENG-73-002605/24/916ENGINE - FUEL AND CONTROL - DEDICATED ALTERNATOR - DELETION OF COPPER LAMINATIONS73-00-00V2500-A1
ENG-73-002704/12/918ENGINE - FUEL AND CONTROL - TO PROVIDE A NEW ELECTRONIC ENGINE CONTROL (EEC) WITH THESCN11G/J SOFTWARE CONFIGURATION73-00-00V2500-A1
ENG-73-002805/03/913ENGINE - FUEL AND CONTROL - ENGINE DEDICATED ALTERNATOR (EDA) STATOR UNIT - INTRODUCTION OF PERIODIC INSPECTION ,FOR CARBON DEPOSITS73-00-00V2500-A1
ENG-73-002905/10/910112/06/916FUEL AND CONTROL - PROVIDE A NEW DATA ENTRY PLUG KIT ASSEMBLY AND FLANGE FC ATTACHING HARDWARE FOR THE ELECTRONIC ENGINE CONTROL (EEC)73-22-00V2500-A1
ENG-73-003002/01/936ENGINE - FUEL AND CONTROL - FUEL METERING UNIT (FMU) - TORQUE MOTOR - SEALING RING REPLACEMENT73-00-00V2500-A1
ENG-73-003106/28/916ENGINE - FUEL AND CONTROL - INCREASED LENGTH BOLTS FOR ELECTRONIC ENGINE CONTROL (EEC) GROUND CABLE STRAP73-00-00V2500-A1
ENG-73-003211/01/918ENGINE - FUEL AND CONTROL - TO PROVIDE A NEW ELECTRONIC ENGINE CONTROL (EEC) WITH THESCN11H SOFTWARE CONFIGURATION73-00-00V2500-A1
ENG-73-003303/01/935ENGINE - FUEL AND CONTROL - REPROGRAM DATA ENTRY PLUG (DEP) FOR A BUMP RATING CHANGE73-00-00V2500-A1
ENG-73-003407/26/963ENGINE - FUEL AND CONTROL - ENGINE DEDICATED ALTERNATOR (EDA) STATOR UNIT - ELECTRICAL RECEPTACLE AND CONNECTOR TIGHTENING PROCEDURE73-00-00V2500-A1,-D5
ENG-73-003505/21/938ENGINE - FUEL AND CONTROL - REWIRE THE DATA ENTRY PLUG (DEP) FOR A BUMP RATING CHANGE TO THE APPLICABLE WIRING CONFIGURATION73-00-00V2500-A1
ENG-73-003609/18/926ENGINE - FUEL AND CONTROL - REPLACE THE EXISTING FUEL NOZZLE PREFORMED PACKINGS73-00-00V2500-A1
ENG-73-003706/15/934ENGINE - FUEL AND CONTROL - TO PROVIDE A NEW ELECTRONIC ENGINE CONTROL (EEC) WITH THESCN12A SOFTWARE CONFIGURATION73-00-00V2500-A1
ENG-73-003806/20/940109/09/056ENGINE - FUEL AND CONTROL - PROVIDE A NEW P2/T2 PROBE AIR TUBE ASSEMBLY AND ATTACHMENT AT CLIPPING POINT CP060373-00-00V2500-A1
ENG-73-003912/20/936ENGINE - FUEL - INTRODUCE AN IMPROVED FUEL FILTER ELEMENT73-00-00V2500-A1
ENG-73-004010/23/920310/31/056ENGINE - FUEL AND CONTROL - FUEL TUBES - FUEL METERING UNIT TO FUEL DIVERTER VALVE SERVO TUBES REROUTED73-00-00V2500-A1
ENG-73-004201/11/933ENGINE - FUEL AND CONTROL - DO A CLEARANCE CHECK BETWEEN THE BRACKET AND THE FUEL SUPPLY MANIFOLD73-00-00V2500-A1,-A5
ENG-73-004305/21/930105/21/936ENGINE - FUEL AND CONTROL - DO A CHECK TO FIND THE SHORT DATA ENTRY PLUG BACKSHELL ASSEMBLIES73-00-00V2500-A1
ENG-73-004410/15/934ENGINE - FUEL AND CONTROL - TO PROVIDE A NEW ELECTRONIC ENGINE CONTROL (EEC) WITH THESCN12B SOFTWARE CONFIGURATION73-00-00V2500-A1
ENG-73-004512/17/936ENGINE - FUEL AND CONTROL - INTRODUCTION OF TUBES MADE OF IMPROVED FRETTAGE RESISTANT MATERIAL73-11-49V2500-A1
ENG-73-004608/19/934ENGINE - FUEL AND CONTROL - ENGINE DEDICATED ALTERNATOR STATOR POWER WINDING - INSPECTION/REPLACEMENT73-00-00V2500-A1
ENG-73-004709/30/936ENGINE - FUEL AND CONTROL - FUEL METERING UNIT - INTRODUCTION OF MOOG TORQUEMOTORS WITH IMPROVED FILTRATION73-00-00V2500-A1
ENG-73-004903/17/947ENGINE - FUEL - PROVIDE A NEW FUEL RETURN TUBE ASSEMBLY AND ASSOCIATED REVISED CLIPPING ARRANGEMENTS73-00-00V2500-A5
ENG-73-005009/01/937ENGINE - FUEL AND CONTROL - PROVIDE RE-ROUTED P4.9 PRESSURE CONTROL MANIFOLDS73-00-00V2500-A1
ENG-73-005202/25/943ENGINE - FUEL AND CONTROL - TO PROVIDE A NEW ELECTRONIC ENGINE CONTROL (EEC) WITH THESCN9A VERSION 0211121 SOFTWARE CONFIGURATION AND HARDWARE CHANGES TO ADDRESS NACELLE DRAINAGE REQUIREMENTS73-00-00V2500-A5
ENG-73-005303/07/977ENGINE - FUEL AND CONTROL - INTRODUCE A NEW FUEL SERVO-TO- BIFURCATION TUBE ASSEMBLY THAT PROVIDES IMPROVED CLEARANCES WITH ADJACENT PARTS73-00-00V2500-D5
ENG-73-005403/07/945ENGINE - FUEL AND CONTROL - NEW FUEL DIVERTER AND RETURN VALVE ASSEMBLY WITH NEW CAP SEAL AND ENLARGED SOLENOID ORIFICE73-00-00V2500-A1,-A5,-D5
ENG-73-005502/15/973ENGINE - FUEL AND CONTROL - REPLACE THE DATA ENTRY PLUG WITH ONE THAT HAS A REVISED WIRINGSCHEME73-00-00V2500-A5
ENG-73-005603/03/944ENGINE - FUEL AND CONTROL - FUEL METERING UNIT - METERING VALVE TORQUEMOTOR INTEGRITY CHECK73-00-00V2500-A5,-D5
ENG-73-005705/20/944ENGINE - FUEL AND CONTROL - FUEL METERING UNIT - INTRODUCTION OF REVISED PUSH ROD SEAL AND BEARING - PRESSURE RAISING AND OVERSPEED VALVES73-00-00V2500-A5,-D5
ENG-73-005809/30/954ENGINE - FUEL AND CONTROL - INTRODUCE NEW FUEL PUMP TO FUEL COOLED OIL COOLER TUBES WITH A REPOSITIONED RESTRICTOR ORIFICE73-00-00V2500-A1
ENG-73-005906/01/956ENGINE - FUEL AND CONTROL - FUEL SYSTEM TUBES - TUBE SUPPORT BRACKET ATTACHED WITH HEX HEAD BOLTS73-00-00V2500-D5
ENG-73-006007/28/944ENGINE - FUEL AND CONTROL - REPLACE THE TUBE CLIP AT CLIPPING POINT 079573-00-00V2500-A5
ENG-73-006107/07/957ENGINE - FUEL AND CONTROL - INCORPORATE NEW FUEL AND OIL TUBES MADE FROM IMPROVED FRETTAGE RESISTANT MATERIAL AND REVISED TUBE CLIPPING73-00-00V2500-A1,-A5
ENG-73-006201/25/956ENGINE - FUEL AND CONTROL - REPLACE THE FUEL DIVERTER AND RETURN VALVE PACKINGS WITH PACKINGS MADE FROM IMPROVED MATERIAL73-00-00V2500-A1,-A5,-D5
ENG-73-006312/20/967ENGINE - FUEL AND CONTROL - PROVIDE A NEW FCOC LP FUEL TUBE WITH A REPOSITIONED ORIFICE73-00-00V2500-D5
ENG-73-006410/24/976ENGINE - FUEL AND CONTROL - FUEL SYSTEM AIR TUBES - PROVIDE A REPOSITIONED CLIPPING POINT(CP 1080)73-00-00V2500-A1,-A5
ENG-73-006512/01/943ENGINE - FUEL AND CONTROL - TO PROVIDE A NEW ELECTRONIC ENGINE CONTROL (EEC) WITH THESCN11 SOFTWARE CONFIGURATION73-00-00V2500-D5
ENG-73-006603/24/956ENGINE - FUEL AND CONTROL - FUEL TUBES - INTRODUCTION OF SMALLER CLIP AND CLIPPING POINT 703173-00-00V2500-D5
ENG-73-006701/31/956ENGINE - FUEL AND CONTROL - REPLACE THE FUEL PUMP PACKINGS WITH PACKINGS MADE FROM IMPROVED MATERIAL73-00-00V2500-A1,-A5,-D5
ENG-73-006801/31/956ENGINE - FUEL AND CONTROL - INTRODUCTION OF AN IMPROVED FUEL PUMP73-00-00V2500-A1,-A5,-D5
ENG-73-006904/20/954ENGINE - FUEL AND CONTROL - PROVIDE A NEW ELECTRONIC ENGINE CONTROL (EEC) WITH THE SCN12C/O SOFTWARE CONFIGURATION73-00-00V2500-A1
ENG-73-007001/19/967ENGINE - FUEL AND CONTROL - DEDICATED ALTERNATOR STATOR - INTRODUCTION OF NEW SOURCE OFSUPPLY73-22-38V2500-D5
ENG-73-007110/23/954ENGINE - FUEL AND CONTROL - REPLACEMENT OF FUEL TEMPERATURE THERMOCOUPLE WITH STUD AND NUT TERMINATIONS73-35-15V2500-A5
ENG-73-007206/05/95See SBENGINE - FUEL AND CONTROL - INTRODUCE A NEW FUEL DIVERTER AMD RETURN VALVE WITH NEW TYPE OF MICROSWITCH FOR CONTROLLED SERVICE USE73-13-42V2500-A5
ENG-73-007310/29/020102/12/047ENGINE FUEL AND CONTROL - ENGINE ALTERNATOR (STATOR) - INTRODUCTION OF AN INTEGRAL COOLING SHROUD73-22-38V2500-A1,-A5,-D5
ENG-73-007503/08/964ENGINE - FUEL AND CONTROL - REPLACEMENT OF FUEL TEMPERATURE THERMOCOUPLE WITH STUD AND NUT TERMINATIONS73-35-15V2500-D5
ENG-73-007601/19/967ENGINE - FUEL AND CONTROL - TO ANNOUNCE A NEW SOURCE FOR THE ENGINE DEDICATED ALTERNATOR ROTOR AND STATOR ASSEMBLY73-22-38V2500-A1,-A5
ENG-73-007701/18/028ENGINE FUEL AND CONTROL - FUEL SYSTEM AIR TUBES - INTRODUCTION OF NON-VENTED PB SENSE LINE ASSEMBLY73-21-49V2500-D5
ENG-73-007810/04/966ENGINE - FUEL AND CONTROL - INTRODUCE A REPOSITIONED FCOC FUEL FLOW RESTRICTOR AND ASSOCIATED FUEL TUBES73-00-00V2500-A5
ENG-73-007911/14/954ENGINE - FUEL AND CONTROL - PROVIDE A NEW ELECTRONIC ENGINE CONTROL (EEC) WITH THE SCN11 BSOFTWARE CONFIGURATION73-00-00V2500-D5
ENG-73-008002/23/968ENGINE - FUEL AND CONTROL - TO PROVIDE A NEW ELECTRONIC ENGINE CONTROL (EEC) WITH THESCN10A SOFTWARE CONFIGURATION VERSION 0261026 TRIMS73-00-00V2500-A5
ENG-73-008111/30/956ENGINE - FUEL AND CONTROL - INTRODUCTION OF A NEW FUEL DIVERTER AND RETURN VALVE WITH NEW MICROSWITCH ASSEMBLIES73-00-00V2500-A1,-A5,-D5
ENG-73-008210/25/964ENGINE - FUEL AND CONTROL - ELECTRONIC ENGINE CONTROL - PROVIDE A NEW ELECTRONIC ENGINE CONTROL (EEC) WITH THE SCN12D SOFTWARE73-00-00V2500-A1
ENG-73-008306/21/964ENGINE - FUEL AND CONTROL - TO PROVIDE A NEW ELECTRONIC ENGINE CONTROL (EEC) WITH THESCN10B SOFTWARE CONFIGURATION VERSION 027/027 TRIMS73-00-00V2500-A5
ENG-73-008411/08/960107/24/986ENGINE - FUEL AND CONTROL - REPLACEMENT OF FUEL FEED TUBE73-00-00V2500-A1,-A5
ENG-73-008510/18/960109/11/018ENGINE - FUEL AND CONTROL - FUEL METERING UNIT - INTRODUCTION OF FUEL METER SUPPLIED BY WOODWARD GOVENOR COMPANY73-00-00V2500-D5
ENG-73-008601/31/974ENGINE - FUEL AND CONTROL - TO PROVIDE A NEW ELECTRONIC ENGINE CONTROL (EEC) WITH THESCN11 SOFT-WARE CONFIGURATION73-00-00V2500-A5
ENG-73-008712/12/974ENGINE - FUEL AND CONTROL - FUEL METERING UNIT - INTRODUCING A FUEL METERING UNIT BY WOODWARD GOVERNOR COMPANY73-00-00V2500-A5
ENG-73-008803/05/977ENGINE - FUEL AND CONTROL - REPLACE THE FUEL NOZZLE SUPPLY MANIFOLD ASSEMBLIES (FOR THE V2500-A1, V2527-A5 AND V2530-A5 ONLY) AND REMOVE THE GASKET OPTION AND CHANGE THE INSTALLATION PROCEDURE (FOR ALL MODELS)73-22-52V2500-A5
ENG-73-008903/05/976ENGINE - FUEL AND CONTROL - INSPECT THE FUEL NOZZLE SUPPLY MANIFOLD ASSEMBLIES FOR THE CONDITION OF THE BRAZE JOINTS73-00-00V2500-A5,-D5
ENG-73-009103/13/980103/13/987ENGINE - FUEL AND CONTROL - FMU INCREASED OVERSPEED VALVE BY - PASS FLOW73-00-00V2500-A1,-A5,-D5
ENG-73-009212/01/964POWER PLANT - EEC CHANNEL AandB HARNESSES ENGINE DEDICATED ALTERNATOR HARNESS CONNECTOR WITH IMPROVED LOCKING FEATURE71-00-00V2500-D5
ENG-73-009311/27/986ENGINE - ENGINE DEDICATED ALTERNATOR DRIVE GEAR ASSEMBLY - INTRODUCING A REVISED STANDARD OF ATTACHING BOLTS FOR THE ENGINE DEDICATED ALTERNATOR73-00-00V2500-A1,-A5,-D5
ENG-73-009411/30/960508/10/017ENGINE - FUEL AND CONTROL - REROUTE THE LEFT AND RIGHT PRESSURE CONTROL TUBE ASSEMBLIES73-00-00V2500-A1,-A5
ENG-73-009507/18/977ENGINE FUEL AND CONTROL - FUEL NOZZLE - INTRODUCTION OF REVISED TURBINE COOLING AIR SUPPORT BRACKET73-00-00V2500-D5
ENG-73-009602/14/970104/18/976ENGINE FUEL AND CONTROL - DEDICATED ALTERNATOR (STATOR) - INTRODUCTION OF REVISED RECEPTACLES73-00-00V2500-D5
ENG-73-009710/03/970110/03/977ENGINE - FUEL AND CONTROL - FMU - INTRODUCTION OF FUEL METER SUPPLIED BY WOODWARD GOVERNER COMPANY73-00-00V2500-A5
ENG-73-009804/10/97See SBENGINE - FUEL AND CONTROL - FUEL AND ADDITIVES - EVALUATION OF CIS AVIATION FUELS73-00-00V2500-A1,-A5
ENG-73-009909/19/977ENGINE - FUEL AND CONTROL - FUEL METERING UNIT - INTRODUCTION OF FUEL METERINGUNIT WITH REVISED MICROSWITCH AND PLUNGER RETURN SPRING73-00-00V2500-A5,-D5
ENG-73-010007/15/974ENGINE - FUEL AND CONTROL - TO PROVIDE A NEW ELECTRONIC ENGINE CONTROL (EEC) WITH THESCN12 SOFTWARE CONFIGURATION73-00-00V2500-D5
ENG-73-010103/28/970103/24/067ENGINE FUEL AND CONTROL - FUEL METERING UNIT - INTRODUCTION OF REVISED FUEL METERING UNITWITH INTEGRAL HOUSING STRENGTHENING FEATURE73-22-52V2500-A5,-D5
ENG-73-010210/17/976ENGINE FUEL AND CONTROL - FUEL SYSTEM TUBES - ENGINE INTRODUCTION OF REVISED TUBE ASSEMBLY WITH MATERIAL CHANGE AND REVISED CLIPPING73-11-49V2500-A1
ENG-73-010306/13/970204/15/044ENGINE FUEL AND CONTROL - FUEL SYSTEM TUBES - INTRODUCTION OF REVISED CLIPPING FOR THE HP SERVO EXTERNAL FUEL TUBE ASSEMBLY73-11-49V2500-A1
ENG-73-010409/04/984ENGINE - FUEL AND CONTROL - FUEL SYSTEM TUBES - INTRODUCTION OF REVISED CLIPPING FOR THE HP SERVO EXTERNAL FUEL TUBE ASSEMBLY,73-00-00V2500-A5
ENG-73-010504/11/970309/30/056ENGINE FUEL AND CONTROL - FUEL SYSTEM AIR TUBES - INTRODUCTION OF ADDITIONAL MOISTURE TRAP ON THE PB AIR TUBE ASSEMBLY SENSE LINE73-00-00V2500-D5
ENG-73-010607/18/977ENGINE FUEL AND CONTROL - FUEL SYSTEM AIR TUBES - INTRODUCTION OF A REVISED P2T2 TUBE ASSEMBLY73-00-00V2500-D5
ENG-73-010705/15/987ENGINE - FUEL AND CONTROL - FUEL METERING UNIT - INTRODUCTION OF FUEL METERING UNIT WITH REVISED HP SOV TORQUEMOTOR73-00-00V2500-A1,-A5,-D5
ENG-73-010806/13/977ENGINE FUEL AND CONTROL - FUEL METERING UNIT - COMMONISATION OF WOODWARD GOVERNOR COMPANY FUEL METER73-00-00V2500-D5
ENG-73-011011/12/016NMSB - ENGINE - INSPECTION OF FUEL MANIFOLDS73-11-00V2500-A1,-A5
ENG-73-011105/09/974ENGINE - FUEL AND CONTROL - TO PROVIDE A NEW SCN11/P ELECTRONIC ENGINE CONTROL (EEC)73-00-00V2500-A5
ENG-73-011205/01/984ENGINE - FUEL AND CONTROL - TO PROVIDE A NEW A1SCN131Q ELECTRONIC ENGINE CONTROL (EEC) VERSION 0841084 SOFTWARE73-00-00V2500-A1
ENG-73-011307/18/970110/18/057ENGINE FUEL AND CONTROL - FUEL FLOWMETER - INTRODUCTION OF REVISED FUEL FLOW TRANSMITTER WITH INCREASED ELECTRICAL RECEPTACLE CLEARANCE73-00-00V2500-A5,-D5
ENG-73-011508/22/977ENGINE - FUEL AND CONTROL - FUEL SYSTEM TUBES - ENGINE - INTRODUCTION OF REVISED EXTERNAL FUEL TUBE ASSEMBLY WITH WELDED-IN LUG AND AMENDED CLIPPING73-00-00V2500-A1
ENG-73-011611/07/977ENGINE - FUEL AND CONTROL - FUEL SYSTEM TUBES - INTRODUCTION OF REVISED HP SERVO EXTERNAL FUEL TUBE ASSEMBLY WITH WELDED-IN LUG AND AMENDED CLIPPING73-00-00V2500-A5
ENG-73-011706/27/977ENGINE - FUEL AND CONTROL - FUEL METERING UNIT (FMU) INTRODUCTION OF REVISED FMU WITH REDUCED FUEL FLOW73-00-00V2500-A5
NAC-73-011807/23/977NACELLE - POWERPLANT - PIPE ASSEMBLY, P2T2 - REPLACEMENT OF73-00-00V2500-D5
NAC-73-011907/23/977NACELLE - POWERPLANT - CLIP, P2T2 PIPE ASSEMBLY - ADDITION OF73-00-00V2500-D5
ENG-73-012011/07/977ENGINE FUEL AND CONTROL - FUEL SYSTEM TUBES - ENGINE INTRODUCTION OF REVISED FUEL TUBE ASSEMBLY BETWEEN FUEL FLOWMETER AND BIFURCATION PANEL73-00-00V2500-D5
ENG-73-012107/01/984ENGINE - FUEL AND CONTROL - TO PROVIDE A NEW SCN 12/Q EEC73-00-00V2500-A5
ENG-73-012205/08/986ENGINE - FUEL AND CONTROL - FUEL METERING UNIT (FMU) - INTRODUCTION OF FMU WITH REVISED MICROSWITCH MECHANISM AND OSV/PRSOV PUSH RODS73-00-00V2500-A1
ENG-73-012305/15/986ENGINE - FUEL AND CONTROL - FUEL METERING UNIT (FMU) - INTRODUCTION OF REVISED FMU WITH OSV AND PRSOV PUSH-RODS COATED WITH TUNGSTEN CARBIDE73-00-00V2500-A5,-D5
ENG-73-012410/17/970106/15/014ENGINE - WOODWARD GOVERNOR COMPANY (WGC) - FMU - SHUT-OFF VALVE AND OVERSPEED SERVOVALVE - ONE TIME INSPECTION73-00-00V2500-A5,-D5
ENG-73-012506/26/987ENGINE - FUEL AND CONTROL - LP AND HP FUEL PUMPS - INTRODUCTION OF REVISED HP BEARING CUT GEOMETRY TO REDUCE FUEL PUMP RIPPLE73-00-00V2500-A5
ENG-73-012609/25/980111/24/984INSPECTION AND REPLACEMENT OF FUEL NOZZLE LOCATION CLIPPING BRACKETS (NON MODIFICATION)73-13-41V2500-D5
ENG-73-012710/25/990210/18/057ENGINE - FUEL AND CONTROL - FUEL METERING UNIT - INTRODUCTION OF A LUCAS FUEL METERING UNIT WITH REVISED MAXIMUM FUEL FLOW STOP73-22-00V2500-A5
ENG-73-012803/06/030103/06/037ENGINE FUEL AND CONTROL - FUEL SYSTEM AIR TUBES - INTRODUCTION OF HEAT RESISTANT CLIPS FOR THE PB SENSE LINE TUBE ASSEMBLY AND THE DELETION OF A CLIP AT CP609473-00-00V2500-A5
ENG-73-012902/17/984ENGINE - FUEL AND CONTROL - TO PROVIDE A NEW ELECTRONIC ENGINE CONTROL (EEC) WITH THED5 SCN131N SOFTWARE CONFIGURATION73-00-00V2500-D5
ENG-73-013011/13/980412/06/996ENGINE - FUEL AND CONTROL - FUEL SYSTEM AIR TUBES - INTRODUCTION OF REVISED PB SENSE LINE TUBES WITH INCREASED DIAMETER73-22-00V2500-D5
ENG-73-013110/30/987ENGINE - FUEL AND CONTROL - REPLACE CERTAIN FUEL NOZZLE SUPPLY MANIFOLD ASSEMBLIES AND THE RELATED ATTACHING HARDWARE73-00-00V2500-A1,-A5
ENG-73-013204/16/980107/29/984ENGINE - FUEL AND CONTROL - SELECTIVE REPROGRAMMING OF THE DATA ENTRY PLUG ASSEMBLY73-22-00V2500-A5
ENG-73-013309/04/985ENGINE FUEL AND CONTROL - FUEL SYSTEM TUBES - INTRODUCTION OF BOLTS WITH INCREASED LENGTH TO ATTACH A FUEL TUBE ASSEMBLY TO THE FUEL DIVIDER VALVE73-00-00V2500-D5
ENG-73-013403/26/990203/26/994ENGINE - INSPECTION OF V2500-A1, A5 FUEL MANIFOLDS FOR TYPE OF BRAZE USED AT FERRULEIMAN] FOLD JOINT73-00-00V2500-A1,-A5
ENG-73-013511/30/980109/15/996ENGINE - POWERPLANT - REWORK OF THE TERMINAL BLOCK ASSEMBLY73-00-00V2500-A1,-A5
ENG-73-013604/23/990104/10/027ENGINE FUEL AND CONTROL - FUEL METERING UNIT - INTRODUCTION OF A WOODWARD FUEL METERING UNIT WITH REVISED SERVO VALVE COVER73-22-00V2500-A5,-D5
ENG-73-013712/11/980209/15/995ENGINE - POWERPLANT - INSTALLATION OF NEW TERMINAL BLOCK ASSEMBLY73-00-00V2500-A1,-A5
ENG-73-013811/20/980105/18/016ENGINE - FUEL AND CONTROL - DEDICATED ALTERNATOR STATOR - INTRODUCTION OF AN ENGINE DEDICATED ALTERNATOR WITH REVISED ELECTRICAL CONNECTORS73-22-00V2500-A1,-A5
ENG-73-013905/04/990110/27/007ENGINE - FUEL AND CONTROL - REPLACE A FUEL NOZZLE SUPPLY MANIFOLD ASSEMBLY AND THE RELATED ATTACHING HARDWARE73-00-00V2500-A1,-A5
ENG-73-014003/05/997ENGINE FUEL AND CONTROL - FUEL SYSTEM AIR TUBES - INTRODUCTION OF REVISED EEC PIPE-SUPPORT BRACKET73-22-00V2500-A1,-A5
ENG-73-014111/11/980101/25/994ENGINE - FUEL AND CONTROL - TO PROVIDE A NEW All SCN14/R ELECTRONIC ENGINE CONTROL (EEC) SOFTWARE73-22-00V2500-A1
ENG-73-014212/10/997ENGINE - FUEL AND CONTROL - FUEL TEMPERATURE THERMOCOUPLE INTRODUCTION OF A REVISED THEMOCOUPLE73-25-00V2500-A5,-D5
ENG-73-014305/05/996ENGINE FUEL AND CONTROL - LP/HP FUEL PUMPS - INTRODUCTION OF A REVISED LP/HP FUEL PUMP WITH REDUCED GEARSHAFT BENDING73-12-00V2500-A1,-A5,-D5
ENG-73-014403/19/990106/03/034ENGINE FUEL AND CONTROL - FUEL NOZZLE - INTRODUCTION OF REVISED SUPPORT BRACKETS FOR THE TURBINE COOLING AIR-PIPE73-00-00V2500-A1,-A5
ENG-73-014606/07/990104/25/024ENGINE - FUEL AND CONTROL - LP AND HP FUEL PUMP - RETURN OF PUMPS FOR INVESTIGATION TO PREVENT LP DRIVE GEAR MOUNT FRACTURES (NON MODIFICATION)73-12-00V2500-A1,-A5,-D5
ENG-73-014707/14/000410/17/127ENGINE - FUEL AND CONTROL - REPLACE CERTAIN FUEL NOZZLE SUPPLY MANIFOLD ASSEMBLIES AND THE RELATED ATTACHING HARDWARE73-00-00V2500-A1,-A5
ENG-73-014801/29/990201/12/004ENGINE FUEL AND CONTROL - FUEL NOZZLE - INTRODUCTION OF REVISED FUEL NOZZLE CLIPPING BRACKETS73-13-00V2500-D5
ENG-73-014904/11/007ENGINE - FUEL AND CONTROL - PROVIDE A NEW FUEL NOZZLE ASSEMBLY73-00-00V2500-A1,-A5,-D5
ENG-73-015005/16/990211/19/026ENGINE - FUEL AND CONTROL - FUEL METERING UNIT - INTRODUCTION OF A LUCAS FUEL METERING UNIT WITH REVISED MAXIMUM FUEL FLOW STOP73-22-00V2500-A5
ENG-73-015101/11/006ENGINE FUEL AND CONTROL-FUEL METERING UNIT-INTRODUCTION OF A WOODWARD GOVERNOR COMPANY FUEL METERING UNIT WITH REVISED MICROSWITCHES73-22-00V2500-A5,-D5
ENG-73-015206/02/990101/31/014ENGINE - INTRODUCTION OF LONGER P2T2 PROBE73-00-00V2500-A5
ENG-73-015404/10/994ENGINE FUEL AND CONTROL - FUEL NOZZLE - INTRODUCTION OF REVISED FUEL NOZZLE CLIPPING BRACKETS73-00-00V2500-D5
ENG-73-015504/20/993ENGINE - FUEL SYSTEM AIR TUBES - REVISED PB SENSE LINE - INSPECTION CHECK AND RECALL OF ANY UN-INSTALLED SB 73-0130 PIN M1550-1 SENSE LINE TUBES (NON MODIFICATION)73-22-00V2500-D5
ENG-73-015603/27/026ENGINE FUEL AND CONTROL - FUEL TUBES ENGINE - INTRODUCTION OF A REVISED FUEL TUBE SUPPORT BRACKET73-11-49V2500-D5
ENG-73-015708/06/990201/07/036ENGINE FUEL AND CONTROL - FUEL METERING UNIT - INTRODUCTION OF A WOODWARD GOVERNOR COMPANY FUEL METERING UNIT WITH REVISED MAXIMUM FUEL FLOW STOP73-22-00V2500-A5
ENG-73-015810/25/990201/07/037ENGINE FUEL AND CONTROL-FUEL METERING UNIT-INTRODUCTION OF A WOODWARD GOVERNOR COMPANY FUEL METERING UNIT WITH REVISED MAXIMUM FUEL FLOW STOP73-00-00V2500-A5
ENG-73-015907/30/998ENGINE - FUEL AND CONTROL - TO PROVIDE A NEW A5 SCN14/5 ELECTRONIC ENGINE CONTROL73-22-00V2500-A5
ENG-73-016003/06/004ENGINE-FUEL AND CONTROL-TO PROVIDE A NEW A5 SCN14B/S ELECTRICAL ENGINE CONTROL (EEC)73-22-00V2500-A5
ENG-73-016208/26/994ENGINE - WOODWARD GORVENOR COMPANY (WGC) FUEL METERING UNIT (FMU) - FUEL METERING VALVE SERVOVALVE - ONE TIME INSPECTION73-00-00V2500-A5,-D5
ENG-73-016306/16/000102/28/028ENGINE - PROVIDE NEW ELECTRONIC ENGINE CONTROL SUPPORT SHIMS73-22-00V2500-A1,-A5
ENG-73-016601/14/038ENGINE FUEL AND CONTROL - FUEL SYSTEM AIR TUBES - INTRODUCTION OF NON-VENTED BURNER TO EEC PRESSURE (PB) SENSE LINE TUBE ASSEMBLIES73-22-49V2500-A1,-A5
ENG-73-016702/21/000102/28/004MODIFICATION SERVICE BULLETIN - ENGINE - PROVIDE A5 SCN10B SOFTWARE STANDARD FOR SPECIFIC V2527-A5 DELIVERED ENGINES73-22-00V2500-A5
ENG-73-016807/28/007ENGINE - FUEL AND CONTROL - LP/HP FUEL PUMPS - INTRODUCTION OF A REVISED LP/HP FUEL PUMP WITH SAND CAST LP IMPELLER HOUSING73-12-41V2500-A5,-D5
ENG-73-016904/06/000209/05/004ENGINE - FUEL AND CONTROL - TO PROVIDE A NEW A5 SCN15/T ELECTRONIC ENGINE CONTROL (EEC)73-22-00V2500-A5
ENG-73-017010/10/000111/27/014ENGINE - FUEL AND CONTROL - TO PROVIDE A NEW A5 SCN16/U ELECTRONIC ENGINE CONTROL (EEC)73-22-00V2500-A5
ENG-73-017109/14/016ENGINE - FUEL AND CONTROL - FUEL METERING UNIT - INTRODUCTION OF A REVISED FUEL METERING UNIT SUPPLEMENTARY SOV TORQUE MOTOR CAP CLAMPING73-22-52V2500-A5,-D5
ENG-73-017208/14/017ENGINE - FUEL AND CONTROL - FUEL METERING UNIT - INTRODUCTION OF A WOODWARD GONERNOR COMPANY SWITCHABLE FUEL METERING UNIT SUITABLE FOR ALL V2500-A5 APPLICATIONS73-22-52V2500-A5
ENG-73-017308/14/017ENGINE - FUEL AND CONTROL - FUEL METERING UNIT - INTRODUCTION OF A TRW LUCAS AEROSPACE SWITCHABLE FUEL METERING UNIT SUITABLE FOR ALL V2500-A5 ENGINE MODELS73-22-52V2500-A5
ENG-73-017405/31/016ENGINE FUEL AND CONTROL - FUEL FLOWMETER - INTRODUCTION OF A REVISED FUEL FLOW TRANSMITTER SUPPORT BRACKET73-31-17V2500-D5
ENG-73-017505/22/017ENGINE - FUEL AND CONTROL - PROVIDE NEW RIGHT AND LEFT PRESSURE CONTROL MANIFOLDS73-22-51V2500-A1
ENG-73-017610/03/016ENGINE - FUEL AND CONTROL - TRW LUCAS AEROSPACE FUEL METERING UNIT (FMU) - REWORK INSTRUCTION FOR MACHINING THE MAIN METERING VALVE PLUNGER INSTALLED IN THE FMU 530, 540 AND 550 UNITS.73-22-52V2500-A5,-D5
ENG-73-017704/18/020104/25/024ENGINE - FUEL AND CONTROL - LP AND HP FUEL PUMP - INSPECTION OF TEIJIN SEIKI HOUSINGS FOR HP INLET FLANGE CRACKS - NON-MODIFICATION SERVICE BULLETIN73-12-41V2500-A5
ENG-73-017902/15/036ENGINE FUEL AND CONTROL - FUEL METERING UNIT - INTRODUCTION OF A WOODWARD AIRCRAFT ENGINE SYSTEMS (WAES) REVISED STANDARD OF VESPEL BALL73-22-52V2500-A5,-D5
ENG-73-018002/13/030104/14/037ENGINE FUEL AND CONTROL - FUEL METERING UNIT - INTRODUCTION OF A WOODWARD AIRCRAFT ENGINE SYSTEMS (WAES) FMU WITH REVISED FUEL METERING VALVE ( FMV) SERVOVALVE TORQUEMOTOR STOPSCREWS73-22-52V2500-A5,-D5
ENG-73-018103/31/046ENGINE FUEL AND CONTROL - FUEL METERING UNIT - INTRODUCTION OF A REVISED MAIN METERING VALVE (MMV) END COVER73-22-52V2500-A1
ENG-73-018210/16/027ENGINE FUEL AND CONTROL - FUEL METERING UNIT - INTRODUCTION OF A WOODWARD AIRCRAFT ENGINE SYSTEMS (WAES) FMU WITH REVISED TAMPER PROOFING FOR THE FUEL METERING VALVE (FMV) MAX. FUEL FLOW STOP AND THE FMU NAMEPLATE73-22-52V2500-A5
ENG-73-018404/04/030106/30/034ENGINE - FUEL AND CONTROL - TO PROVIDE A NEW ELECTRONIC ENGINE CONTROL (EEC) WITH A5 SCN17/V SOFTWARE73-22-00V2500-A5
ENG-73-018501/30/040208/15/066ENGINE - FUEL AND CONTROL - EEC150-40 PRESSURE BURNER SENSOR PORT SCREEN DELETION73-22-00V2500-A5
ENG-73-018603/18/040508/13/106ENGINE - FUEL AND CONTROL - EEC150-1/EEC150-20 PRESSURE BURNER SENSOR PORT SCREEN DELETION73-22-00V2500-A1,-A5
ENG-73-018801/15/040104/05/043NON-MODIFICATION SERVICE BULLETIN - ENGINE - EPR MODIFIER CLASS CORRECTION DUE TO TEST CELL CALIBRATION SHIFT73-22-00V2500-A1
ENG-73-018905/25/040301/31/114ENGINE - FUEL AND CONTROL - TO PROVIDE A NEW ELECTRONIC ENGINE CONTROL (EEC) WITH A5 SCN18/W SOFTWARE73-22-00V2500-A5
ENG-73-019010/20/044ENGINE - FUEL AND CONTROL - TO PROVIDE A NEW ELECTRONIC ENGINE CONTROL (EEC) WITH D5 SCN14/O SOFTWARE73-22-00V2500-D5
ENG-73-019108/10/050111/08/056ENGINE FUEL AND CONTROL - FUEL METERING UNIT - INTRODUCTION OF REVISED DYNAMIC SEALS AND VALVE PUSHRODS73-22-52V2500-A5,-D5
ENG-73-019601/31/063ENGINE - EXTERNALS - ACTUATOR PRESSURE FUEL SUPPLY AND ACTUATOR PRESSURE FUEL RETURN - CLIPPING POINT 7004 INSPECTION - NON-MODIFICATION SERVICE BULLETIN73-11-49V2500-D5
ENG-73-019707/20/060401/24/116ENGINE - FUEL AND CONTROL - TO PROVIDE A NEW ELECTRONIC ENGINE CONTROL (EEC) WITH A5 SCN19/X SOFTWARE73-22-00V2500-A5
ENG-73-019808/08/070205/05/086ENGINE FUEL AND CONTROL - FUEL SYSTEM AIR TUBE - INTRODUCTION OF RE-ROUTED BURNER TO ENGINE ELECTRONIC CONTROLLER (EEC) PRESSURE (PB) SENSE LINE TUBE ASSEMBLIES73-22-00V2500-A1,-A5
ENG-73-020005/15/060102/21/084ENGINE - FUEL AND CONTROL - REPLACEMENT OF RESISTORS AND TOUCH-UP OF SOLDER JOINTS FOR ENGINES WITH ECC150-40 ELECTRONIC ENGINE CONTROL (ECC) INSTALLED73-22-34V2500-A5
ENG-73-020207/24/096ENGINE - FUEL AND CONTROL - P4.9 TUBE ASSEMBLIES, PRESSURE CONTROL AND BOX AND CABLE, TC - REPLACE THE P4.9 TUBE ASSEMBLIES TO PREVENT FRACTURES AND REPOSITION THE EXHAUST GAS TEMPERATURE (EGT) CABLE TO PREVENT CHAFING73-22-51V2500-A1,-A5
ENG-73-020309/22/086ENGINE - FUEL AND CONTROL - PROVIDE A NEW ELECTRONIC ENGINE CONTROL (EEC) WITH A5 SCN20/Y SOFTWARE73-22-00V2500-A5
ENG-73-020706/29/118ENGINE - FUEL AND CONTROL - PROVIDE A NEW TWO POINT TRIM ENGINE PRESSURE RATIO (EPR) CLASSIFICATION FOR ELECTRONIC ENGINE CONTROL (EEC) UNITS WITH SCN20A SOFTWARE73-22-35V2500-A5
ENG-73-020811/20/080301/30/124ENGINE - FUEL AND CONTROL - PROVIDE A NEW ELECTRONIC ENGINE CONTROL (EEC) WITH A5 SCN20A/Z SOFTWARE73-22-00V2500-A5
ENG-73-020911/19/080209/16/138ENGINE - FUEL AND CONTROL - INTRODUCTION OF 33K BUMP RATING, MODIFICATION OF THE DATA ENTRY PLUG AND NEW ENGINE IDENTIFICATION PLATE72-32-00V2500-A5
ENG-73-021012/01/108ENGINE - FUEL AND CONTROL - PLUG, DATA ENTRY - MODIFICATION TO INCREASE THE THRUST LEVEL DURING CLIMB73-22-30V2500-A5
ENG-73-021112/11/083NON-MODIFICATION SERVICE BULLETIN - ENGINE FUEL AND CONTROL - INSPECTION OF FUEL NOZZLE AND SUPPORT ASSEMBLIES73-13-41V2500-A1,-A5
ENG-73-021307/19/100210/09/12VBNON-MODIFICATION SERVICE BULLETIN - ENGINE FUEL AND CONTROL - EEC150-1 AND EEC150-20 ELECTRONIC ENGINE CONTROL (EEC) WITH ELECTRICALLY ERASABLE PROGRAMMABLE READ-ONLY MEMORY (EEPROM) WEAR OUT73-22-34V2500-A1,-A5,-D5
ENG-73-021502/17/106ENGINE - FUEL METERING UNIT (FMU) - TURBINE OVERSPEED VALVE - INTRODUCTION OF A MODIFIED ELECTRO-HYDRAULIC SERVO VALVE COMPARTMENT HEAT SHIELD73-22-52V2500-A5,-D5
ENG-73-021801/22/100204/16/123NON-MODIFICATION SERVICE BULLETIN - ENGINE FUEL AND CONTROL - INSPECTION OF FUEL MANIFOLD FOR CHAFING BY EXHAUST GAS THERMOCOUPLE (EGT) HARNESS73-11-41V2500-A1,-A5
ENG-73-021904/15/100303/18/118ENGINE - VARIABLE STATOR VANE (VSV) ACTUATOR - LOW PRESSURE (LP) RETURN LINE REROUTE PIPEWORK73-00-00V2500-A5
ENG-73-022003/22/100203/03/116ENGINE - FUEL AND CONTROL - PRESSURE BURNER SENSOR PORT SCREEN DELETION73-22-34V2500-A5,-D5
ENG-73-022104/12/100109/14/113NON-MODIFICATION SERVICE BULLETIN - ENGINE - EPR MODIFIER CLASS CORRECTION DUE TO TEST CELL CALIBRATION SHIFT73-22-00V2500-A5
ENG-73-022210/27/110204/18/196ENGINE FUEL AND CONTROL - PROVIDE A NEW ELECTRONIC ENGINE CONTROL (EEC) WITH SCN21/AA SOFTWARE73-22-34V2500-A5
ENG-73-022302/24/110111/18/116ENGINE - FUEL METERING UNIT (FMU) - SHUT-OFF VALVE MODIFICATIONS AND CONVERSION INSTRUCTIONS BETWEEN WOODWARD GOVERNOR FUEL METERING UNITS 8061-639 AND 8061-64073-22-52V2500-A5,-D5
ENG-73-022408/12/160104/27/178ENGINE FUEL AND CONTROL - VARIABLES STATOR VANE (VSV) ACTUATOR - LOW PRESSURE (LP) RIGID FUEL TUBE - INTRODUCTION OF A BLANKING PLUG73-11-47V2500-A5,-D5
ENG-73-022503/26/128ENGINE - FUEL AND CONTROL - PLUG, DATA ENTRY - MODIFICATION TO PERMIT A MORE OPEN VARIABLE STATOR VANE SCHEDULE73-22-35V2500-A5
ENG-73-022609/13/11VBENGINE - FUEL AND CONTROL - CONTROL, ELECTRONIC ENGINE - REPLACEMENT OF THE CHANNEL A INTERCONNECT CIRCUIT CARD ASSEMBLY73-00-00V2500-A5
ENG-73-022709/12/11VBENGINE - FUEL AND CONTROL - CONTROL, ELECTRONIC ENGINE - REPLACEMENT OF THE TRANSIENT VOLTAGE SUPPRESSORS73-00-00V2500-A5
ENG-73-022807/27/110407/26/123NON-MODIFICATION SERVICE BULLETIN - ENGINE - VARIABLE STATOR VANE (VSV) ACTUATOR - LOW PRESSURE (LP) RETURN LINE RE-ROUTE PIPEWORK - FUEL TUBE INSPECTION REPLACEMENT AND HARNESS INSPECTION73-00-00V2500-A5
ENG-73-022911/20/124NON-MODIFICATION SERVICE BULLETIN - ENGINE FUEL AND CONTROL - INSPECTION OF THE VARIABLE STATOR VANE ACTUATOR (VSVA) AND THE HIGH PRESSURE (HP) SERVO FUEL TUBE FOR CHAFING75-32-00V2500-A1,-A5,-D5
ENG-73-023206/10/133NON-MODIFICATION SERVICE BULLETIN - ENGINE PRESSURE RATIO (EPR) MODIFIER CLASS CORRECTION DUE TO TEST CELL CALIBRATION SHIFT732200V2500-A5
ENG-73-023305/27/13VBENGINE- FUEL AND CONTROL - CONTROL, ELECTRONIC ENGINE (EEC) - REPLACEMENT OF BURNER PRESSURE (PB) SENSORS ON A SPECIFIC EEC POPULATIONV2500-A5
ENG-73-023407/29/137ENGINE FUEL AND CONTROL - TRANSMITTER, FUEL FLOW - SUPPLY A NEW TRANSMITTER WITH IMPROVED FUEL FLOW CALIBRATION CURVE73-31-17V2500-A1,-A5,-D5
ENG-73-023504/14/143ENGINE FUEL AND CONTROL - VARIABLE STATOR VANE (VSV) ACTUATOR - REVERSAL OF SERVICE BULLETIN V2500-ENG-73-0219 (LOW PRESSURE (LP) RETURN LINE RE-ROUTE PIPEWORK)73-11-00V2500-A1,-A5,-D5
ENG-73-023612/19/140105/07/196ENGINE FUEL AND CONTROL - CONTROL, ELECTRONIC ENGINE (EEC) - REPLACEMENT OR MODIFICATION OF, TO INCORPORATE SCN22/AB SOFTWARE CONFIGURATION73-22-34V2500-A5
ENG-73-023712/19/146ENGINE FUEL AND CONTROL - DATA ENTRY PLUG (DEP) - REPLACEMENT OR MODIFICATION OF, TO PROVIDE SCN22/AB SOFTWARE AND REDUCED GROUND IDLE (RGI) CAPABILITY73-22-35V2500-A5
ENG-73-023812/19/140206/14/198ENGINE - FUEL AND CONTROL - OPERATING PROCEDURES FOR V2500 SOFTWARE LOADER (SOFTWARE LOADER AND DATA ENTRY PLUG (DEP) READER)73-00-00V2500-A1,-A5,-D5
ENG-73-023912/19/148ENGINE FUEL AND CONTROL - INTRODUCTION OF A5 SELECTTWO™ ENGINE WITH REDUCED GROUND IDLE (RGI)73-22-35V2500-A5
ENG-73-024009/08/156ENGINE FUEL AND CONTROL - FUEL DIVERTER AND RETURN VALVE - REPLACEMENT OF, TO IMPROVE RELIABILITY73-13-42V2500-A1,-A5,-D5
ENG-73-024203/18/166ENGINE FUEL AND CONTROL - FUEL TEMPERATURE THERMOCOUPLE - REPLACEMENT OF, TO IMPROVE RELIABILITY73-35-15V2500-A5,-D5
ENG-73-024412/05/170112/15/173NON-MODIFICATION SERVICE BULLETIN - ENGINE FUEL AND CONTROL - PUMP, FUEL, LOW PRESSURE, HIGH PRESSURE - INSPECTION FOR SUSPECT LP/HP FUEL PUMPS73-12-41V2500-A5
ENG-73-024604/08/196ENGINE FUEL AND CONTROL - FUEL SYSTEM AIR TUBE - INTRODUCTION OF PB SENSE LINE73-22-49V2500-A5
ENG-73-024712/14/187ENGINE FUEL AND CONTROL - FUEL DIVERTER AND RETURN VALVE - REPLACEMENT OF THE FUEL DIVERTER AND RETURN VALVE TO DECREASE SERVICE INTERRUPTIONS73-13-42V2500-A1,-A5,-D5
ENG-73-024810/31/196ENGINE FUEL AND CONTROL - CONTROL, ELECTRONIC ENGINE (EEC) - REPLACEMENT OR MODIFICATION TO INCORPORATE SCN23/AC SOFTWARE CONFIGURATION73-22-34V2500-A5
ENG-73-A024903/29/193NON MODIFICATION ALERT SERVICE BULLETIN - ENGINE FUEL AND CONTROL - FUEL METERING UNIT - REPLACEMENT OF THE FUEL METERING VALVE DYNAMIC SEAL ON FUEL METERING UNITS MANUFACTURED BY WOODWARD73-22-52V2500-D5
ENG-73-025004/09/208ENGINE FUEL AND CONTROL - CONTACT, SOCKET - INTRODUCTION OF AN ALTERNATIVE SOCKET CONTACT71-00-00V2500-A1,-A5,-D5
ENG-73-A025111/19/193NON-MODIFICATION ALERT SERVICE BULLETIN - ENGINE FUEL AND CONTROL - REPLACEMENT OF FUEL METERING VALVE DYNAMIC SEAL ON FUEL METERING UNITS MANUFACTURED BY WOODWARD73-22-52V2500-D5
ENG-73-025203/02/206NON-MODIFICATION SERVICE BULLETIN - ENGINE FUEL AND CONTROL - VALVE, FUEL DIVERT & RETURN - REPLACE THE TORQUE MOTOR ON THE FUEL DIVERTER AND RETURN VALVE73-13-42V2500-A5,-D5
ENG-73-025305/27/208ENGINE FUEL AND CONTROL - CLIP - INTRODUCTION OF ALTERNATIVE CLIPS73-22-49V2500-A5
ENG-73-025408/18/200103/09/213NON-MODIFICATION SERVICE BULLETIN - ENGINE FUEL AND CONTROL - CONTROL, ELECTRONIC ENGINE (EEC) - DO AN INSPECTION OF THE EEC SERIAL NUMBER FOR POSSIBLY UNSERVICEABLE CIRCUIT BOARDS WITH A Q854 SOLDER ISSUE73-22-34V2500-A5
ENG-74-000112/20/967ENGINE - IGNITION - INTRODUCE NEW IGNITION EXCITER MOUNTING BRACKETS74-00-00V2500-A5
ENG-74-000203/24/955ENGINE - IGNITION - INTRODUCTION OF IMPROVED IGNITION LEAD, COOLING SHROUD, AND IGNITION COOLING BOX74-00-00V2500-A1,-A5,-D5
ENG-74-000303/25/955ENGINE - IGNITION - INTRODUCTION OF A REDIMENSIONED IGNITION LEAD COOLING SHROUD AND THE DELETION OF IGNITION COOLING BOX SUPPORT BRACKETS74-00-00V2500-A1,-A5,-D5
ENG-74-000401/31/974ENGINE - IGNITION - INTRODUCE IGNITER PLUG INSERTS WITH AN INCREASED WALL THICKNESS AND IMPROVED THREAD REQUIREMENTS74-00-00V2500-A1,-A5,-D5
ENG-74-000507/29/027IGNITION - EXCITER IGNITION UNITS - INTRODUCTION OF A REVISED ENGINE EXCITER BOX MOUNTING BRACKET74-11-38V2500-A5
ENG-74-000612/06/127NON-MODIFICATION SERVICE BULLETIN - IGNITION - INSTALLATION REQUIREMENTS FOR IGNITER PLUGS OF SERVICE BULLETIN V2500-ENG-70-1003 STANDARD74-21-41V2500-A5
ENG-74-000707/03/176IGNITION - PLUG, IGNITER - REPLACE WITH A MORE DURABLE IGNITER PLUG74-21-41V2500-A1,-A5,-D5
ENG-74-000902/27/207IGNITION - PLUG, IGNITER - INTRODUCTION OF A NEW IGNITER PLUG TO INCREASE PART DURABILITY74-21-41V2500-A1,-A5
ENG-74-001005/15/207IGNITION - PLUG, IGNITER - INTRODUCE A NEW IGNITER PLUG TO INCREASE DURABILITY74-21-41V2500-D5
ENG-75-000104/13/900411/17/117AIR - INTRODUCE A REVISED LPT ACC SUPPORT ASSEMBLY CONFIGURATION75-24-49V2500-A1
ENG-75-000202/23/900112/13/056AIR - PROVIDE REPLACEMENT LP TURBINE CASE - TO - ACC MANIFOLD ATTACHING BOLTS75-00-00V2500-A1
ENG-75-000307/07/893AIR - REWORK OF STAGE 10 AIR SOLENOID VALVE MOUNT BRACKET75-00-00V2500-A1
ENG-75-000411/10/894AIR - PROVIDE REVISED MATERIAL TUBE CLIP AT CLIPPING POINT LOCATION CP577675-00-00V2500-A1
ENG-75-000506/30/893AIR - INTRODUCTION OF TWO ZONE 2 AIR DEFLECTOR BRACKETS75-00-00V2500-A1
ENG-75-000611/10/894AIR - INCORPORATION OF ACC VALVE BRACKETS AND STATOR ROD FEATURING CHROME PLATED BEARING DETAILS75-00-00V2500-A1
ENG-75-000708/09/917AIR - VARIABLE STATOR VANE ACTUATOR - INTRODUCTION OF A STATOR VANE ACTUATOR WITH IMPROVED TORQUE MOTOR WIRE SEPARATION75-00-00V2500-A1
ENG-75-000811/02/904AIR - HPT/LPT ACC ACTUATOR ASSEMBLY - NEW LVDT COVER INTRODUCTION AND REWORK OF LVDT COVER AND ACTUATOR BODY BOSS75-00-00V2500-A1
ENG-75-000909/21/904AIR - HPT/LPT ACC SYSTEM - IMPROVED CONNECTION OF THE ACC ACTUATOR AND THE STATOR ROD75-00-00V2500-A1
ENG-75-001001/31/925ENGINE - DEDICATED ALTERNATOR - COOLING AIR SUPPLY75-00-00V2500-A1
ENG-75-001109/07/906AIR - INTRODUCE A SUPPORT BRACKET FOR THE FBC BUFFER AIR TUBE ASSEMBLY75-00-00V2500-A1
ENG-75-001201/11/914AIR - HPT/LPT ACC AIR VALVE ASSEMBLY - REMOVAL OF SEAL RINGS75-00-00V2500-A1
ENG-75-001304/18/917AIR - PROVIDE HPT ACC TUBES WITH IMPROVED MAINTAINABILITY FEATURES75-00-00V2500-A1
ENG-75-001405/24/916AIR - HP COMPRESSOR - INTRODUCTION OF SOLENOID VALVES WITH IMPROVED ELECTRICAL BONDING75-00-00V2500-A1
ENG-75-001503/08/914AIR - HP COMPRESSOR VARIABLE STATOR VANE ACTUATOR (VSVA) AND LP COMPRESSOR BLEED MASTER ACTUATOR - TORQUE MOTOR - SEALING RING REPLACEMENT75-00-00V2500-A1
ENG-75-001609/06/917AIR - HPC BLEED AIR TUBES - REVISED CORE ENGINE TUBES TO IMPROVE CLEARANCE WITH HARNESS IN BIFURCATION AREA - R.H. SIDE75-00-00V2500-A1
ENG-75-001703/03/936AIR - ACC MANIFOLD - DELETE THE USE OF CERTAIN ACC MANIFOLD SPACERS75-00-00V2500-A1
ENG-75-001805/29/90See SBAIR - REPLACE THE HPT/LPT ACC AIR VALVE (FOR CONTROLLED SERVICE USE)75-00-00V2500-A1
ENG-75-001901/06/924AIR - INCORPORATE A NON-RETURN VALVE INTO THE LPC BLEED MASTER ACTUATOR LP RETURN LINE75-00-00V2500-A1
ENG-75-002012/07/924AIR - HP COMPRESSOR VARIABLE STATOR VANE ACTUATOR (VSVA) - INTRODUCTION OF RETURN PORT, NON RETURN VALVE75-00-00V2500-A1
ENG-75-002103/08/964AIR - HP/LP TURBINE ACC SYSTEM - VALVE VANE REPLACEMENT AND ADDITION OF PLUG STORAGE PLATE TO HPT/LPT ACC AIR VALVE75-00-00V2500-A1
ENG-75-002206/10/938ENGINE - AIR - INTRODUCE A NEW TURBINE COOLING AIR VALVE WITH AN IMPROVED SWITCH MECHANISM75-00-00V2500-A1,-A5,-D5
ENG-75-002301/15/926AIR - LPC BLEED MASTER ACTUATOR - NEW FUEL DRAIN PASSAGE75-00-00V2500-A1
ENG-75-002411/05/91See SBENGINE - AIR - INTRODUCTION OF ADDITIONAL ACC VALVE SUPPORTS AND NEW SLIDE TYPE HPT MANIFOLD JOINT (FOR CONTROLLED SERVICE USE)75-00-00V2500-A1
ENG-75-002501/25/91See SBAIR - HPT/LPT ACTIVE CLEARANCE CONTROL DUCTS - TO PROVIDE A FRONT DUCT COVER ASSEMBLY FORCONTROLLED SERVICE USE75-00-00V2500-A1
ENG-75-002604/16/938ENGINE - AIR - REVISED HPT ACC MANIFOLD SUPPORT BRACKET75-00-00V2500-A1
ENG-75-002710/30/913AIR - HPT/LPT ACC VALVE ACTUATOR - INSTALLATION OF PIN RETAINER ON SERVO VALVE75-00-00V2500-A1
ENG-75-002811/08/923AIR - HP COMPRESSOR VARIABLE STATOR VANE ACTUATOR (VSVA) LINEAR VARIABLE DIFFERENTIAL TRANSFORMER (LVDT) SEALING75-00-00V2500-A1
ENG-75-002904/25/920106/26/984AIR - VARIABLE STATOR VANE ACTUATOR - INTRODUCTION OF A LINEAR VARIABLE DIFFERENTIAL TRANSFORMER (LVDT) WITH IMPROVED EXTERNAL SEALING75-32-00V2500-A1
ENG-75-003005/25/924AIR - HPT/LPT ACC SYSTEM - INTRODUCTION OF ADDITIONAL ACC VALVE SUPPORTS AND NEW SLIDE TYPE HPT MANIFOLD JOINT75-00-00V2500-A1
ENG-75-003109/27/935AIR - HP/LP TURBINE ACC SYSTEM - ADDITION OF ANTI-ROTATION BUSHING TO HPT/LPT ACC AIR VALVE75-00-00V2500-A1
ENG-75-003206/12/924AIR - HP COMPRESSOR VALVE SOLENOIDS - STAGE 7 HPC AND STAGE 10 HPC - INSPECTION OF TORQUEVALUES ON SOLENOID BODY UNION CONNECTIONS75-00-00V2500-A1
ENG-75-003304/20/938ENGINE - AIR - INCORPORATE A CHAMFER OF THE ACAC INLET/ OUTLET DUCT LUG75-00-00V2500-A1,-A5
ENG-75-003406/25/946ENGINE - AIR - REPLACE THE HP COMPRESSOR VARIABLE STATOR VANE ACTUATOR MOUNTING BRACKET ASSEMBLY75-00-00V2500-A1
ENG-75-003508/03/946ENGINE - AIR - REVISE THE ORIENTATION OF THE CLIPPING POINT AT CP 556075-00-00V2500-A1,-A5
ENG-75-003602/11/946ENGINE - AIR - INCORPORATE A REVISED SOLENOID SUPPORT BRACKET TO PROVIDE IMPROVED CLEARANCES BETWEEN BRACKET AND FAN CASE ASSEMBLY75-00-00V2500-A1,-A5
ENG-75-003710/24/010103/27/026AIR TURBINE COOLING CONTROLLED AIR TUBES - REVISED STAGE 10 MAKE-UP AIR ADAPTOR MOUNTED CLIPPING BRACKET75-23-48V2500-A5
ENG-75-003812/03/933ENGINE - AIR - INSPECTION AND REWORK OF THE HP COMPRESSOR STAGES 7 AND 10 BLEED VALVES75-00-00V2500-A1
ENG-75-003901/12/00See SBCANCELLATION OF ENGINE SERVICE BULLETIN V2500-75-0039 (AIR-INTRODUCTION OF A SHROUD TO THE HP COMPRESSOR STAGE 7 BLEEDVALVES)75-00-00V2500-A1,-A5,-D5
ENG-75-004012/24/934AIR - HP COMPRESSOR STAGE 7 AND STAGE 10 BLEED VALVES - INTRODUCTION OF AN IMPROVED CENTER BUSH75-00-00V2500-A1,-A5,-D5
ENG-75-004105/26/944ENGINE - AIR - INTRODUCE A NEW LPC BLEED MASTER ACTUATOR FEATURING A LINEAR VARIABLE DIFFERENTIAL TRANSFORMER (LVIDT) WITH IMPROVED WIRE TERMINATION75-00-00V2500-A1,-A5,-D5
ENG-75-004201/17/977ENGINE - AIR - TO ANNOUNCE THE INTRODUCTION OF A SPACER AT CLIPPING POINT CP 2423 (NO. 4BEARING SCAVENGE VALVE AIR SERVO TUBE)75-00-00V2500-D5
ENG-75-004301/12/956ENGINE - AIR - IGNITION COOLING LEADS - INTRODUCTION OF NEW IGNITION EXCITER COOLING TUBES75-00-00V2500-D5
ENG-75-004412/20/966ENGINE - AIR - INTRODUCE A NEW BRACKET AT CLIPPING POINT CP556075-00-00V2500-A1,-A5
ENG-75-004510/28/946ENGINE - AIR - ADDITION OF DETUNING HOLES ON THE ACC FRONT DUCT75-00-00V2500-D5
ENG-75-004608/10/950108/10/956AIR - HIGH PRESSURE (HP)/LOW PRESSURE (LP) TURBINE ACTIVE CLEARANCE CONTROL (ACC) VALVE ACTUATOR - INTRODUCTION OF A NEW ROD END TO THE HP/LP TURBINE ACC VALVE ACTUATOR75-24-52V2500-A1,-A5,-D5
ENG-75-004701/21/030106/22/047AIR - HP COMPRESSOR STAGE 7 SOLENOID VALVE - INTRODUCTION OF A REVISED HP COMPRESSOR BLEED CONTROL VALVE SOLENOID MOUNTING BRACKET75-32-51V2500-A1,-A5
ENG-75-004903/07/944ENGINE - AIR - BEARING COMPARTMENT COOLING HPC AIR BLEED TUBES - SERVO AIR TO HANDLINGBLEED VALVES75-00-00V2500-A1,-A5
ENG-75-005007/14/946ENGINE - AIR - PROVIDE NEW HP SYSTEM BLEED AIR TUBES WITH REVISED CLIPPING LUGS FOR SUPPORT OF REROUTED FIRERAIL75-00-00V2500-A1,-A5
ENG-75-005107/10/960310/17/116AIR - ACTIVE CLEARANCE CONTROL (ACC) - REVISED CONNECTOR TUBE ASSEMBLY WITH NEW PERISEAL HOUSING CLAMPS75-24-49V2500-A1,-A5,-D5
ENG-75-005206/28/960104/11/976ENGINE - AIR - INTRODUCE A VARIABLE STATOR VANE ACTUATOR (VSVA) HAVING A LINEAR DIFFERENTIAL TRANSDUCER WITH EXTENDED TRAVEL75-00-00V2500-A5,-D5
ENG-75-005303/19/994ENGINE - AIR - INTRODUCE A NEW HP COMPRESSOR STAGE 7 BLEED VALVE CHEVRON SEAL CONFIGURATION75-00-00V2500-A1,-A5,-D5
ENG-75-005405/12/954AIR - HP COMPRESSOR STAGE 10 BLEED VALVES - INTRODUCTION OF CHEVRON SEALS AND NEW VALVE CENTER STEM BUSHING75-00-00V2500-A1,-A5,-D5
ENG-75-005505/26/954AIR - VARIABLE STATOR VANE ACTUATOR LINKAGE - INTRODUCTION OF A NEW SETTING PROCEDURE FOR THE RE-SCHEDULING OF THE HP COMPRESSOR VARIABLE VANES75-00-00V2500-A1
NAC-75-005602/28/965NACELLE - OVER HEAT CORE DETECTOR, SUPPORT CLIPS - REPLACEMENT OF75-00-00V2500-A5
ENG-75-005803/15/96See SBENGINE - AIR - INTRODUCTION OF A NEW HPT/LPT ACC AIR VALVE WITH NEW TYPE ROD END AND SLEEVE BEARINGS FOR CONTROLLED SERVICE USE75-00-00V2500-A1,-A5
NAC-75-005812/02/960208/06/976NACELLE - EXHAUST - SEAL, ACAC DUCT - REPLACEMENT OF75-00-00V2500-A1,-A5
ENG-75-005901/15/966AIR - HPT/LPT ACC VALVE ACTUATOR - INTRODUCTION OF A NEW SEAL RING75-00-00V2500-A1,-A5,-D5
ENG-75-006005/15/960403/05/995ENGINE - AIR - ACTIVE CLEARANCE CONTROL SYSTEM - INTRODUCTION OF REVISED (ACC) MOUNTING BRACKET AND LINK ASSEMBLIES WITH SLOTTED ENTRY BEARINGS72-40-00V2500-A1,-A5
ENG-75-006106/28/960108/21/984ENGINE - AIR - INTRODUCE A VARIABLE STATOR VANE ACTUATOR (VSVA) WITH REVISED SOLDERED TERMINATION JOINTS AND SLEEVE MATERIAL75-32-00V2500-A1,-A5,-D5
NAC-75-006201/15/974ACAC EXHAUST DUCT REDESIGN - 58PCT INCREASE IN EXHAUST AREA75-00-00V2500-A1,-A5
ENG-75-006301/31/970112/15/006ENGINE - AIR - INTRODUCTION OF A HPT/LPT ACC AIR VALVE WITH NEW SLOTTED ENTRY TYPE ROD END ASSEMBLY75-00-00V2500-A1,-A5,-D5
ENG-75-006511/07/977AIR - COOLING - IGNITION COOLING LEADS - INTRODUCTION OF REINFORCED AND ABRASIVE RESISTANT COOLING HOSES FOR THE IGNITOR BOX75-00-00V2500-D5
ENG-75-006610/24/970107/07/007AIR - ENGINE AIR OFF-TAKE DUCTS - INTRODUCTION OF STAGE 7 HP COMPRESSOR BLEED-VALVE SUPPORT AIR DUCTS MANUFACTURED BY CASTING75-00-00V2500-A1,-A5
ENG-75-006804/24/986AIR - LPC BLEED, MASTER ACTUATOR - INTRODUCTION OF A LINEAR VARIABLE - DIFFERENTIAL TRANSFORMER WITH DIFFERENT ADHESIVE TAPE75-00-00V2500-A1,-A5,-D5
ENG-75-006910/31/970101/12/007AIR - HPC STAGE 10 BLEED VALVES - INTRODUCTION OF BLEED VALVE SILENCERS WITH INTEGRALSEAL LAND75-00-00V2500-D5
ENG-75-007011/07/977AIR - HPC STAGE 10 BLEED VALVES - INTRODUCTION OF A STAGE 10 BLEED VALVE SUPPLIED BY PARKER HANNIFIN FOR THE HP COMPRESSOR75-00-00V2500-D5
ENG-75-007106/19/987AIR - HP COMPRESSOR STAGE 7 BLEED VALVES - INTRODUCTION OF REVISED BLEED VALVE SILENCER WITH INTEGRAL SEAL LAND75-00-00V2500-A1,-A5
ENG-75-007204/24/980103/15/047AIR - HPC STAGE 10 BLEED VALVE - INTRODUCTION OF REVISED BLEED VALVE SILENCER WITH INTEGRAL SEAL LAND75-32-54V2500-A1,-A5
ENG-75-007306/19/987AIR - HP COMPRESSOR STAGE 7 BLEED VALVES - INTRODUCTION OF REVISED BLEED-VALVE SILENCER WITH INTEGRAL SEAL LAND75-32-00V2500-D5
ENG-75-007407/24/00See SBAIR - HPC STAGE 10 BLEED VALVE - INTRODUCTION OF A BLEED VALVE SUPPLIED BY PARKER HANNIFIN CORPORATION75-32-00V2500-A5
ENG-75-007504/24/980107/31/986AIR - HP COMPRESSOR VARIABLE STATOR VANE ACTUATOR - INTRODUCTION OF REVISED TORQUE MOTOR STRAINERS75-32-00V2500-A1,-A5,-D5
ENG-75-007604/24/986AIR - LP COMPRESSOR BLEED MASTER ACTUATOR- INTRODUCTION OF REVISED TORQUE MOTOR STRAINERS75-00-00V2500-A1,-A5,-D5
ENG-75-007704/10/997AIR - LP COMPRESSOR BLEED, SLAVE ACTUATOR - INTRODUCTION OF REVISED MOUNTING BRACKET FOR THE SLAVE BSBVA75-00-00V2500-A5
ENG-75-007804/16/997AIR - HP COMPRESSOR VARIABLE STATOR VANE ACTUATOR - INTRODUCTION OF A LINEAR VARIABLE DIFFERENTIAL TRANSFORMER WITH REVISED ADHESIVE TAPE75-00-00V2500-A1,-A5,-D5
ENG-75-007910/13/996AIR-HP COMPRESSOR STAGE 10 BLEED VALVE- INTRODUCTION OF A REVISED PARKER HANNIFIN BLEED VALVE WITH INCREASED LENGTH RELIEF IN THE PISTON BORE75-32-54V2500-D5
ENG-75-008003/12/997AIR - LP COMPRESSOR MASTER ACTUATOR - INTRODUCTION OF REVISED BSBVA MASTER MOUNTINGBRACKET75-31-00V2500-A5
ENG-75-008105/04/010404/21/117AIR - STAGE 10 TO HPT AIR VALVE - DELETION OF THE HPC STAGE 10 MAKE-UP AIR VALVE AND ASSOCIATED HARDWARE75-23-51V2500-A5
ENG-75-008210/15/990111/05/99See SBAIR - HP COMPRESSOR STAGE 10 BLEED VALVE - INTRODUCTION OF A REVISED PARKER HANNIFIN BLEED VALVE WITH INCREASED LENGTH RELIEF IN THE PISTON BORE75-32-00V2500-A5
ENG-75-008311/10/990208/23/008AIR - HPC HANDLING BLEED VALVES - CLEANING DUNLOP BLEED VALVES FITTED TO 10TH AND 7TH HPC STAGES NON-MOD SERVICE BULLETIN75-00-00V2500-A1,-A5,-D5
ENG-75-008408/12/000703/13/138ENGINE - AIR ACTIVE CLEARANCE CONTROL (ACC) - REPLACEMENT OF TITANIUM TUBES MADE FROM X10 MATERIAL FOR REWORK/REPAIR BY TUBE REPLACEMENT75-24-49V2500-A1,-A5,-D5
ENG-75-008505/26/006AIR - HP COMPRESSOR STAGE BLEED VALVE - INTRODUCTION OF PARKER HANNIFIN CORPORATION SUPPLIED BLEED VALVE75-32-54V2500-A1,-A5
ENG-75-008606/23/006AIR - HP COMPRESSOR STAGE 10 BLEED VALVE - INTRODUCTION OF A REVISED PARKER HANNIFIN BLEED VALVE WITH ADDITIONAL CARBON BEARING REDESIGNED SPRING AND ADDITIONAL SPRING GUIDE75-32-54V2500-D5
ENG-75-008701/31/016AIR - HP COMPRESSOR STAGE 7 SOLENOID VALVE - INTRODUCTION OF A REVISED MOUNTING BRACKET ASSEMBLY AND SUPPORT BRACKETS75-32-51V2500-D5
ENG-75-008910/11/026AIR-TURBINE COOLING CONTROLLED AIR TUBES - INTRODUCTION OF A REVISED STAGE 10 MAKE-UP AIR BRACKET75-23-48V2500-A5
ENG-75-009002/20/046AIR - ACTIVE CLEARANCE CONTROL VALVE - INTRODUCTION OF AN ACC VALVE WITH REVISED ACTUATING ROD SLEEVE BEARINGS75-24-51V2500-A1,-A5,-D5
ENG-75-009102/02/040209/11/068ENGINE - LP TURBINE - RELEASE OF SALEABLE DETAIL PARTS FOR ACC DUCT REPAIR75-24-49V2500-A1,-A5,-D5
ENG-75-009205/12/046AIR - HP COMPRESSOR STAGE 7 BLEED VALVE - INTRODUCTION OF A BLEED VALVE SPACER75-32-52V2500-A1,-A5
ENG-75-009305/05/040111/18/046ENGINE - HP COMPRESSOR - INTRODUCTION OF A REVISED HPC STAGE 7A AND 10 BLEED VALVE SILENCER WITH INCREASED HEIGHT75-32-52V2500-A1,-A5
ENG-75-009403/20/080106/14/118AIR - ACTIVE CLEARANCE CONTROL (ACC) - TO INCORPORATE THE OVERSIZE BUSHES OF THE ACC HOUSING ASSEMBLY75-24-51V2500-A1,-A5
ENG-75-009504/07/056ENGINE - LP TURBINE - INTRODUCTION OF SPACER PLATES WITH INCREASED DIAMETER75-24-49V2500-A1,-A5,-D5
ENG-75-009608/10/060104/27/076AIR - ACTIVE CLEARANCE CONTROL (ACC) ACTUATOR - INTRODUCTION OF AN ACC ACTUATOR WITH A REVISED SERVO VALVE75-24-52V2500-A1,-A5,-D5
ENG-75-009708/27/050910/01/193NON-MODIFICATION SERVICE BULLETIN - VARIABLE STATOR VANE ACTUATOR AND BOOSTER STAGE BLEED VALVE MASTER ACTUATOR - RECOMMENDED LACQUER/FUEL DEPOSITS CLEANING INTERVAL FOR AFFECTED OPERATORS75-31-42V2500-A1,-A5,-D5
ENG-75-010304/18/080105/06/088ENGINE - LP TURBINE - ACTIVE CLEARANCE CONTROL C-TUBE WITH CHANGED MATERIAL FOR END FERRULES75-24-49V2500-A1,-A5,-D5
ENG-75-010408/14/070112/19/07See SBENGINE - NON-MODIFICATION - ADDITIONAL ENGINE RUNNING REQUIREMENT AFTER INSTALLATION OF A NEW OR ZERO TIME SINCE REPAIR VARIABLE STATOR VANE ACTUATOR75-32-41V2500-A1,-A5,-D5
ENG-75-010509/30/080106/30/117AIR - HP COMPRESSOR STAGE 7 BLEED VALVES - INTRODUCTION OF AN ALTERNATIVE BLEED VALVE WITH NEW DESIGN75-32-52V2500-A1,-A5
ENG-75-010610/12/070101/23/096NON-MODIFICATION SERVICE BULLETIN - AIR - REQUIREMENT TO FLUSH A VARIABLE STATOR VANE ACTUATOR (VSVA) 1685 UNIT FOLLOWING OVERHAUL OR REPAIR AT AN APPROVED MAINTENANCE FACILITY75-00-00V2500-A1,-A5,-D5
ENG-75-010710/12/070201/23/096NON-MODIFICATION SERVICE BULLETIN - AIR - REQUIREMENT TO FLUSH A VARIABLE STATOR VANE ACTUATOR (VSVA) 2607 UNIT FOLLOWING OVERHAUL OR REPAIR AT AN APPROVED MAINTENANCE FACILITY75-00-00V2500-A1,-A5,-D5
ENG-75-010809/04/080210/17/117AIR - ACTIVE CLEARANCE CONTROL (ACC) - INTRODUCTION OF A PERISEAL HOUSING WITH INCREASED INNER LIP DIAMETER75-24-49V2500-A1,-A5,-D5
ENG-75-010909/30/080203/22/197AIR - HIGH PRESSURE COMPRESSOR (HPC) STAGE 7 AND 10 SOLENOID VALVES - INTRODUCTION OF ALTERNATIVE SOLENOID VALVE WITH IMPROVED RELIABILITY75-32-51V2500-A1,-A5,-D5
ENG-75-011002/09/096AIR - VARIABLE STATOR VANE ACTUATOR (VSVA) - INTRODUCTION OF SEAL HOUSING WHICH INCLUDES A CONSTANT PRESSURE VALVE (CPV) PISTON TRAVEL STOP75-32-41V2500-A1,-A5,-D5
ENG-75-011102/09/098AIR - VARIABLE STATOR VANE ACTUATOR (VSVA) - CHANGE TO SERVO VALVE PORT FILTERS75-32-41V2500-A1,-A5,-D5
ENG-75-011207/08/096AIR - VARIABLE STATOR VANE (VSV) ACTUATOR - INTRODUCTION OF NEW VSV ACTUATOR MARK NUMBER DUE TO MODIFIED SERVO VALVE PORT FILTERS AND REDESIGNED HOUSING SEAL FOR THE CONSTANT PRESSURE VALVE75-32-41V2500-A1,-A5,-D5
ENG-75-011308/27/096AIR - LOW PRESSURE (LP) COMPRESSOR MASTER BLEED ACTUATOR - INTRODUCTION OF SEAL HOUSING WHICH INCLUDES A CONSTANT PRESSURE VALVE (CPV) PISTON TRAVEL STOP75-31-42V2500-A1,-A5,-D5
ENG-75-011408/27/098AIR - LOW PRESSURE (LP) COMPRESSOR MASTER BLEED ACTUATOR - CHANGE TO SERVO VALVE PORT FILTERS75-31-42V2500-A1,-A5,-D5
ENG-75-011508/27/096AIR - LOW PRESSURE (LP) COMPRESSOR BLEED MASTER ACTUATOR - INTRODUCTION OF NEW LP COMPRESSOR BLEED MASTER ACTUATOR MARK NUMBER DUE TO MODIFIED SERVO VALVE PORT FILTERS AND REDESIGNED HOUSING FOR THE CONSTANT PRESSURE VALVE75-31-42V2500-A1,-A5,-D5
ENG-75-011608/18/097ENGINE - AIR COOLED AIR COOLER - INTRODUCTION OF A MODIFIED AIR COOLED AIR COOLER (ACAC)75-22-41V2500-A1,-A5,-D5
ENG-75-011711/18/107ENGINE - AIR - TURBINE COOLING AIR TUBES - INTRODUCTION OF NEW COOLING AIR TUBES WITH REVISED ELBOW FITTING CONNECTIONS75-23-49V2500-A1,-A5,-S1
ENG-75-011904/04/126AIR - ACTIVE CLEARANCE CONTROL - INTRODUCTION OF MOUNTING BUSHES WITH COUNTERBORE75-00-00V2500-A1,-A5,-D5
ENG-75-012004/02/127AIR - TURBINE COOLING CONTROLLED AIR TUBES - STAGE 10 MAKE UP AIR ADAPTOR WITH REVISED MACHINING PROFILE75-23-48V2500-A5
ENG-75-012205/02/140407/02/197AIR - VARIABLE STATOR VANE ACTUATOR - INTRODUCTION OF VARIABLE STATOR VANE ACTUATOR WITH IMPROVED FORCE CAPABILITY75-32-41V2500-A5
ENG-75-012303/24/150111/06/186AIR - BLEED VALVES, 7TH STAGE HIGH PRESSURE COMPRESSOR (HPC) - REPLACE THE BLEED VALVES TO IMPROVE RELIABILITY75-32-52V2500-A1,-A5,-D5
ENG-75-012412/03/153NON-MODIFICATION SERVICE BULLETIN - TURBINE COOLING AIR (TCA) TUBES - INSPECTION FOR CABLE OR LOCKWIRE INSTALLATION75-23-49V2500-A1,-A5,-D5
ENG-75-012504/20/160203/11/198AIR - BLEED VALVE, 10TH STAGE HIGH PRESSURE COMPRESSOR (HPC) - INTRODUCTION OF ALTERNATE BLEED VALVE75-32-54V2500-A1,-A5,-D5
ENG-75-012605/03/178BLEED AIR - STAGE 7 AND 10 SILENCER ASSEMBLY - SPAREABILITY OF RETAINING RING75-32-52V2500-A1,-A5
ENG-75-012702/12/180106/27/197AIR - VARIABLE STATOR VANE ACTUATOR - INTRODUCTION OF IMPROVED SERVO VALVE TO PN G4000VSVA01 VARIABLE STATOR VANE ACTUATOR75-32-41V2500-A5
ENG-75-012804/01/216AIR - ENGINE AIR-ACTUATOR, VARIABLE STATOR VANE - INTRODUCTION OF PRODUCT IMPROVEMENTS TO TYPE G4000 SERIES ACTUATOR75-32-41V2500-A5
ENG-77-000101/24/927ENGINE - LP TURBINE MODULE AND EXHAUST GAS TEMPERATURE (EGT) INDICATING SYSTEM - REPLACEMENT OF TURBINE EXHAUST CASE AND INSTALLATION OF A REVISED EGT BRACKET CONFIGURATION77-00-00V2500-A1
ENG-77-000202/23/903ENGINE INDICATING - REPLACEMENT OF EGT LOOP CLAMP BRACKETS AND ATTACHING BOLTS77-00-00V2500-A1
ENG-77-000301/11/910201/11/915ENGINE INDICATING - REPLACEMENT OF EGT LOOP CLAMP BRACKETS77-00-00V2500-A1
ENG-77-000404/27/907IGNITION - INCORPORATE AN EGT HARNESS AND JUNCTION BOX FEATURING IMPROVED WIRING BETWEEN THE ELECTRONIC ENGINE CONTROL (EEC) CHANNELS77-00-00V2500-A1
ENG-77-000505/17/916ENGINE INDICATING -ADD WASHERS AT CLIPPING POINTS CP6004 AND CP600977-00-00V2500-A1
ENG-77-000601/25/916ENGINE INDICATING - REPLACE THE EGT HARNESS CLAMP BOLTS AT FLANGE FP77-00-00V2500-A1
ENG-77-000705/24/916ENGINE INDICATING - PROVIDE PERMANENTLY ATTACHED WASHERS TO BRACKET AT CLIPPING POINTS CP6004 AND CP600977-00-00V2500-A1
ENG-77-000811/24/946ENGINE INDICATING - EGT HARNESS AND JUNCTION BOX - INTRODUCTION OF LONGER BOLT AT CLIPPING POINT 786077-00-00V2500-D5
ENG-77-000912/21/010202/28/026ENGINE - PROVIDE NEW EGT HARNESS JUNCTION BOX TERMINAL NUTS77-21-00V2500-A1,-A5
ENG-77-001003/12/030104/23/036ENGINE INDICATING - EGT HARNESS AND JUNCTION BOX - INTRODUCTION OF A EGT HARNESS JUNCTION BOX ASSEMBLY WITH REVISED SELF LOCKING NUTS77-21-43V2500-D5
ENG-77-001103/04/136ENGINE INDICATING - THERMOCOUPLE, EXHAUST GAS TEMPERATURE (EGT) - INTRODUCTION OF77-21-15V2500-A1,-A5,-D5
ENG-77-001206/18/130107/19/177ENGINE INDICATING - HARNESS AND JUNCTION BOX ASSEMBLY, EXHAUST GAS TEMPERATURE (EGT) - INTRODUCTION OF77-21-43V2500-A1,-A5
ENG-77-001405/11/205ENGINE INDICATING - ENGINE VIBRATION MONITOR (EVM) HARNESS - MODIFICATION OF CLIPPING POINTS CP0877, CP0879 AND CP121071-51-42V2500-A1,-A5
ENG-77-001503/08/170108/03/176ENGINE INDICATING - EXHAUST GAS TEMPERATURE (EGT) WIRING HARNESS AND JUNCTION BOX ASSEMBLY - REPLACE WITH THERMOCOUPLE WIRING HARNESS ASSEMBLY77-21-43V2500-A5
ENG-77-001609/21/170107/16/187ENGINE INDICATING - THERMOCOUPLE, IMMERSION - INTRODUCTION OF NEW IMMERSION THERMOCOUPLE FOR IMPROVED DURABILITY77-21-15V2500-A1,-A5,-D5
NAC-78-000106/23/924NACELLE - EXHAUST - THRUST REVERSER - HOLD-OPEN ROD AND FITTING - REPLACEMENT OF78-00-00V2500-A1
NAC-78-000601/08/914NACELLE - EXHAUST - INSTALLATION OF HOIST POINT BLANKS (SETSCREWS)78-00-00V2500-A1
NAC-78-001610/01/954NACELLE - EXHAUST - THRUST REVERSER ATTACH HARDWARE AT NO. 4 HINGE LOCATION - REPLACEMENT OF78-32-00V2500-A1
NAC-78-001806/17/924NACELLE - EXHAUST - THRUST REVERSER OPENING ACTUATOR, COOLING HOSE - REPLACEMENT OF78-32-00V2500-A1
NAC-78-002705/25/938NACELLE - EXHAUST - THRUST REVERSER CASCADE - IDENTITY OF78-32-00V2500-A1
NAC-78-003810/01/950102/20/974NACELLE - EXHAUST - THRUST REVERSER NO. 4 HINGE WASHERS - REPLACEMENT OF78-32-00V2500-A1
NAC-78-004706/13/910101/12/006NACELLE - EXHAUST - COMMON NOZZLE ASSEMBLY - REIDENTIFICATION OF/TRANLATING SLEEVE-ANNOUNCE AVAILABILITY OF NEW CONFIGURATION78-00-00V2500-A1
NAC-78-005009/09/966NACELLE - THRUST REVERSER - REVISED P.C. DUCT/ACTUATOR HOSE CLAMPING, REVISION OF78-00-00V2500-A1
NAC-78-005406/07/966NACELLE - EXHAUST - NO. 1 OPEN LATCH INDICATOR THRUST REVERSER - MODIFICATION OF78-32-00V2500-A1
NAC-78-006606/22/936NACELLE - EXHAUST - EXHAUST CONE INSTALLATION BOLTS - REPLACEMENT OF78-11-12V2500-A1
NAC-78-008112/15/956NACELLE - EXHAUST - THRUST REVERSER - INNER BARREL HEAT- SHIELD PANDOWN, ENLARGEMENT OF78-32-00V2500-A1
NAC-78-008510/23/960201/27/984NACELLE - EXHAUST - FLUID DRAINAGE, THRUST REVERSER - MODIFICATION OF78-32-00V2500-A1,-A5
NAC-78-008706/18/960112/05/974NACELLE - EXHAUST - VENT HOLES, LEFT THRUST REVERSER DOOR - MODIFICATION AND ADDITION OF78-32-00V2500-A5
NAC-78-009206/07/966NACELLE - EXHAUST - NO. 1 LATCH OPEN INDICATOR STAINLESS GUIDE PAD INSTLLATION, THRUST REVERSER - MODIFICATION OF - CATEGORY CODE 6 - MOD.NAC-78-009278-32-00V2500-A1,-A5
NAC-78-009501/26/966NACELLE - EXHAUST - THRUST REVERSER, UNIQUE V2500-A5 CONFIGURATION - REIDENTIFICATION OF78-30-00V2500-A5
NAC-78-009710/15/956NACELLE - EXHAUST - LUG, THRUST REVERSER LOWER OUTBOARD TRACK ASSEMBLY LANYARD ATTACH- MODIFICATION OF78-32-00V2500-D5
NAC-78-009810/01/950202/06/986NACELLE - EXHAUST - BLANK CASCADES, THRUST REVERSER - REPLACEMENT OF78-32-00V2500-A1,-A5
NAC-78-009906/30/950209/26/964NACELLE - EXHAUST - ACTUATORS AND MANIFOLDS, THRUST REVERSER DOOR OPENING - REPLACEMENT OF78-30-00V2500-D5
NAC-78-010305/08/970107/24/976NACELLE - EXHAUST - BOLT, PRESSURE RELIEF DOOR LANYARD - REPLACEMENT OF78-32-00V2500-D5
NAC-78-010407/15/950109/26/963NACELLE - EXHAUST - TAIL CONE - INTRODUCTION OF PERIODIC INSPECTIONS FOR CRACKING78-11-00V2500-D5
NAC-78-010507/15/950108/08/956NACELLE - EXHAUST - BOLT CUPS, EXHAUST CONE - INSTALLATION OF DOUBLERS; REWELD OF78-10-00V2500-D5
NAC-78-010607/10/954NACELLE - EXHAUST - LEVER ASSEMBLY, THRUST REVERSER OUTER LOCKING ACTUATOR - REPLACEMENT OF78-30-00V2500-D5
NAC-78-010710/28/954NACELLE - EXHAUST - TRACK LINERS AND DEPLOY TUBE AND FLEXSHAFT, THRUST REVERSER ACTUATION - REPLACEMENT OF78-30-00V2500-D5
NAC-78-010912/13/950404/27/964NACELLE - EXHAUST - CASCADES, THRUST REVERSER - MODIFICATION AND REPLACEMENT OF78-00-00V2500-D5
NAC-78-011012/14/950210/02/965NACELLE - THRUST REVERSER - DOOR, PRESSURE RELIEF - LATCHES - MODIFICATION OF78-00-00V2500-D5
NAC-78-011308/23/965NACELLE - EXHAUST - THRUST REVERSER LOCKOUT FEATURE - MODIFICATION OF78-32-00V2500-D5
NAC-78-011406/19/960305/09/175NACELLE - THRUST REVERSER - DOORS, PRESSURE RELIEF, AND LATCH ACCESS - MODIFICATION OF78-32-00V2500-D5
NAC-78-011601/02/964NACELLE - EXHAUST - COMMON NOZZLE ASSEMBLY - BIFURCATION FAIRING - MODIFICATION OF78-32-00V2500-D5
NAC-78-011712/15/950106/15/965NACELLE - THRUST REVERSER - FAIRING ASSEMBLY, THRUST REVERSER ACTUATOR, MODIFICATION OF78-32-00V2500-D5
NAC-78-011905/07/970205/16/996NACELLE - EXHAUST - OUTER SKIN, EXIT NOZZLE, COMMON NOZZLE ASSEMBLY (CNA) - MODIFICATIONOF78-11-00V2500-D5
NAC-78-012401/17/964NACELLE - EXHAUST - THRUST REVERSER - PIN, QUICK RELEASE - HOLD OPEN, PRESSURE RELIEF DOOR - RELOCATION OF78-32-00V2500-D5
NAC-78-012504/12/960101/22/974NACELLE - EXHAUST - THRUST REVERSER LOWER CROSS TIE ASSEMBLY - MODIFICATION OF78-32-00V2500-D5
NAC-78-012704/27/984NACELLE - EXHAUST - VENT, COOLING, SLAVE BOOSTER STAGE BLEED VALVE ACTUATOR (BSBVA) COOLING VENT, RIGHT THRUST REVERSER ,HALF - ADDITION OF FOR COOLING COMMONALITY ACROSS ALL A320/A321 /A31 9-A5 AIRCRAFT78-32-00V2500-A5
NAC-78-012804/12/960106/19/964NACELLE - EXHAUST - COMMON NOZZLE ASSEMBLY, STRUT ATTACH BOLT, - REPLACEMENT OF78-11-00V2500-D5
NAC-78-013203/27/970605/20/996NACELLE - EXHAUST - BLOCKER DOOR HINGE, TRANSLATING SLEEVE - REPLACEMENT OF78-32-00V2500-D5
NAC-78-013403/21/974NACELLE - EXHAUST - ATTACH HARDWARE, BLOCKER DOOR - TO LINK ASSEMBLY REPLACEMENT OF78-32-00V2500-D5
NAC-78-013704/03/970201/29/984NACELLE - EXHAUST - BLOCKER DOOR BUSHINGIBUSHING RETAINER PIN INSTALLATION - MODIFICATION OF78-32-00V2500-D5
NAC-78-013812/04/970104/17/984NACELLE - EXHAUST - LOWER THRUST REVERSER, CORE DRAIN MAST MODIFICATION OF78-00-00V2500-D5
NAC-78-014004/03/970303/26/984NACELLE - EXHAUST - CASCADE-TO-AFT CASCADE SUPPORT RING ATTACHMENT - MODIFICATION OF78-32-00V2500-D5
NAC-78-014106/10/970110/30/974NACELLE - EXHAUST - ACTUATION SYSTEM HARNESS RE-ROUTE AND CLIPPING POINT HARDWARE REPLACEMENT78-32-00V2500-D5
NAC-78-014209/12/976NACELLE POWERPLANT - STOWAGE, STOW LOCKOUT PIN, THRUST REVERSER - MODIFICATION OF78-00-00V2500-D5
NAC-78-014409/09/990101/21/004NACELLE - EXHAUST - ACTUATOR FAIRINGS, THRUST REVERSER - REPLACEMENT OF78-00-00V2500-D5
NAC-78-014603/26/980308/24/984NACELLE - POWERPLANT - TRANSLATING SLEEVE, THRUST REVERSER - MODIFICATION OF - SEAL, THRUST REVERSER - REPLACEMENT OF78-00-00V2500-D5
NAC-78-014701/13/984NACELLE - EXHAUST - BLOCKER DOORS, THRUST REVERSER - INSPECTION/REPAIR78-00-00V2500-D5
NAC-78-014909/19/974NACELLE - EXHAUST - OVERHEAT DETECTOR HARNESS INSTALLATION, UPPER THRUST REVERSER HALF - MODIFICATION OF78-00-00V2500-D5
NAC-78-015001/28/980505/26/994NACELLE - POWERPLANT - TRANSLATING SLEEVE, THRUST REVERSER - MODIFICATION OF78-00-00V2500-D5
NAC-78-015101/22/990208/08/004NACELLE - THRUST REVERSER - DOOR, LATCH ACCESS AND LOWER OUTBOARD TRACK BEAM - MODIFICATION OF78-00-00V2500-D5
NAC-78-015503/26/980408/25/984NACELLE - EXHAUST - RUB BLOCKS, COMMON NOZZLE ASSEMBLY - MODIFICATION OF78-00-00V2500-D5
NAC-78-015712/11/977NACELLE - POWERPLANT - LATCH BRACKET, NO. 1, LOWER, THRUST REVERSER - REPLACEMENT OF78-00-00V2500-D5
NAC-78-015806/04/984NACELLE - EXHAUST - HOIST POINT, TRANSLATING SLEEVE - MODIFICATION OF78-30-00V2500-A1,-A5
NAC-78-016110/11/984NACELLE - EXHAUST - MANUAL DRIVE, THRUST REVERSER - REPLACEMENT OF78-00-00V2500-D5
NAC-78-016207/06/984NACELLE - EXHAUST -PRESSURE RELIEF DOOR LATCH LOAD, THRUST REVERSER, INSPECTION OF78-00-00V2500-D5
NAC-78-016501/22/994NACELLE - EXHAUST - COMMON NOZZLE ASSEMBLY, STRUT ATTACH BOLTS - REPLACEMENT OF78-00-00V2500-D5
NAC-78-016607/24/000105/02/016NACELLE - EXHAUST - LOCKOUT FEATURE AFT CASCADE SUPPORT RING, THRUST REVERSER - INSPECTION/REWORK78-00-00V2500-A1,-A5
NAC-78-016701/22/990207/20/994NACELLE - EXHAUST - LATCH ACCESS DOOR, THRUST REVERSER - SEALING IMPROVEMENT78-00-00V2500-D5
NAC-78-016806/07/996NACELLE - EXHAUST - C.N.A BIFURCATION FAIRING78-00-00V2500-D5
NAC-78-017010/05/000103/12/034NACELLE - EXHAUST - TRANSLATING SLEEVE AFT LATCH - HEAT SHIELD MODIFICATION/LATCH ACCESS DOOR HINGE MODIFICATION, THRUST REVERSER78-00-00V2500-D5
NAC-78-017312/22/004NACELLE - EXHAUST - ACTUATOR, THRUST REVERSER - REPLACEMENT OF78-00-00V2500-D5
NAC-78-017406/29/996NACELLE - EXHAUST - PROXIMITY SWITCH, THRUST REVERSER ACTUATOR -INSPECTION/RE-IDENTIFICATION OR REPLACEMENT OF78-00-00V2500-A1,-A5
NAC-78-017508/07/008NACELLE - EXHAUST - THRUST REVERSER - LOWER OUTBOARD TRACK BEAM - MODIFICATION OF78-00-00V2500-D5
NAC-78-017607/30/993NACELLE - EXHAUST - MINOR TRACK LINER, THRUST REVERSER-REPLACEMENT/ MAJOR TRACK LINER - INSPECTION78-00-00V2500-D5
NAC-78-018010/05/004NACELLE - EXHAUST - DRAIN MAST, THRUST REVERSER78-32-00V2500-D5
NAC-78-A018211/19/990407/06/003NACELLE - EXHAUST - OUTER V-BLADE, THRUST REVERSER - INSPECTION FOR CRACKS AND/OR MISSING PIECES78-00-00V2500-D5
NAC-78-018305/19/000208/31/004NACELLE- EXHAUST- OUTER V-BALDE, THRUST REVERSER - APPLICATION OF DRY FILM LUBRICANT78-30-00V2500-D5
NAC-78-018402/16/010409/04/034NACELLE - EXHAUST - LANYARD, PRESSURE RELIEF DOOR, THRUST REVERSER - REPLACEMENT OF78-00-00V2500-D5
NAC-78-018610/26/000102/26/014COMMON NOZZLE ASSEMBLY (CAN) ACAC EXHAUST EXIT AREA MODIFICATION/THRUST RECOVERY DUCT MODIFICATION78-11-11V2500-D5
NAC-78-018712/20/000102/23/016COMMON NOZZLE ASSEMBLY (CAN) PEN NIB FAIRING AFT SEGMENT REPLACEMENT78-11-11V2500-D5
NAC-78-018910/26/000103/16/014NACELLE - THRUST REVERSER ASSEMBLY COMPRESSION STRUT ADJUSTMENT AND RIGGING MODIFICATION78-30-00V2500-D5
NAC-78-019104/24/014MODIFICATION SERVICE BULLETIN - NACELLE - EXHAUST - THRUST REVERSER OPENING ACTUATOR SAFETY PINS REPLACEMENT OF78-30-00V2500-D5
NAC-78-019204/12/016NACELLE - EXHAUST - THRUST REVERSER COMPRESSION STRUT - ADDITION OF PROTECTIVE SLEEVE78-30-00V2500-D5
NAC-78-019611/18/020103/17/046COMMON NOZZLE ASSEMBLY (CNA) - OUTER BARREL - MODIFICATION TO PREVENT ELONGATION OF UPPER AND LOWER STRUT ATTACH HOLES78-30-00V2500-D5
NAC-78-019711/06/016MODIFICATION SB - NACELLE - EXHAUST - COMMON NOZZLE ASSEMBNLY - APPLICATION OF ABRASION RESISTANT PAINT TO THE INBOARD SIDE78-30-00V2500-D5
NAC-78-019805/14/014NACELLE - EXHAUST - THRUST REVERSER - BLOCKER DOOR LINKS - INSPECTION OF NON MODIFICATION SERVICE BULLETIN78-30-00V2500-D5
NAC-78-019911/05/030104/26/068NACELLE - THRUST REVERSER - AFT SUPPORT RING REPLACEMENT - BLANK CASCADE REPLACEMENT- ACTUATOR COVER REPLACEMENT78-30-00V2500-A1,-A5
NAC-78-020309/20/028THRUST REVERSER ASSEMBLY - BLOCKER DOOR - REPLACE THREADED BEARINGS WITH SWAGED BEARINGS78-30-00V2500-D5
NAC-78-020805/09/036NACELLE - EXHAUST - COMMON NOZZLE ASSEMBLY (CNA) - ADDITION OF NUTPLATES FOR ATTACHMENT TO ENGINE78-11-11V2500-A1
NAC-78-021003/19/048NACELLE - EXHAUST - THRUST REVERSER - CASCADE ASSEMBLY - MODIFICATION OF78-30-00V2500-A1,-A5
NAC-78-021306/07/058NACELLE - EXHAUST - THRUST REVERSER - SLEEVE - ADDITION OF IDENTIFICATION PLATE78-30-00V2500-A1,-A5
NAC-78-021406/20/057NACELLE - THRUST REVERSER - UPPER BIFURCATION - INTRODUCTION OF A THREE-PIECE SEAL DEPRESSOR ON THE SEAL LAND ASSEMBLY78-30-00V2500-A1,-A5
NAC-78-021803/31/050112/13/066EXHAUST - THRUST REVERSER - RIGHT THRUST REVERSER HALF - FIXED STRUCTURE - 7TH STAGE BLEED PORT MODIFICATION78-30-00V2500-A1,-A5
NAC-78-021901/07/050102/27/078NACELLE - FIXED DUCT ASSEMBLY - LOWER BIFURCATION SEAL LAND GAP INSPECTION78-00-00V2500-A1,-A5
NAC-78-022001/13/068EXHAUST - THRUST REVERSER - RIGHT THRUST REVERSER LOWER HALF - FIXED STRUCTURE - 7TH STAGE BLEED PORT MODIFICATION78-32-00V2500-D5
NAC-78-022502/07/068NACELLE - EXHAUST - LUG, THRUST REVERSER LOWER OUTBOARD TRACK ASSEMBLY LANYARD ATTACH - MODIFICATION OF78-00-00V2500-D5
NAC-78-022907/05/070109/17/073NACELLE - EXHAUST - TRANSLATING SLEEVE, LOWER - DRAIN TUBE MODIFICATION, THRUST REVERSER78-30-00V2500-D5
NAC-78-023210/08/084NACELLE - THRUST REVERSER - BLOCKER DOOR LINK ASSEMBLY - INSPECTION OF CHAMFER78-30-00V2500-D5
NAC-78-023310/02/083NACELLE - COMMON NOZZLE ASSEMBLY - EXIT NOZZLE INNER SKIN - INSPECTION OF RIVETS78-11-11V2500-D5
ENG-78-026304/25/187INFORMATION - NACELLE - THRUST REVERSER - TO ANNOUNCE THE AVAILABILITY OF NEW THERMAL BLANKETS78-30-00V2500-D5
ENG-79-000106/16/893OIL - INCORPORATE REVISED NO. 4 AND NO. 5 BEARING OIL SCAVENGE TUBE ASSEMBLIES79-00-00V2500-A1
ENG-79-000206/09/893OIL - REPLACEMENT OF THE SCAVENGE OIL FILTER ASSEMBLY79-00-00V2500-A1
ENG-79-000302/16/903OIL - PROVIDE A NEW OIL TANK CAP PLACARDED WITH THE CORRECT TANK CAPACITY79-00-00V2500-A1
ENG-79-000407/07/893OIL - REPLACE THE CLIPPING BRACKETS ON THE OIL TANK AT CP0787 AND CP078879-00-00V2500-A1
ENG-79-000507/07/893OIL - REPLACE THE CLIPPING BRACKET ON THE AIR COOLED OIL COOLER AT CP053379-00-00V2500-A1
ENG-79-000605/01/980105/01/988ENGINE - OIL - TO INTRODUCE A NEW OIL PUMP WITH INCREASED FLOW RATE79-00-00V2500-A1
ENG-79-000710/15/923ENGINE - OIL SYSTEM - REVISED METHOD OF MARKING PART NUMBER AND SERIAL NUMBER ON THE PRESSURE AND SCAVENGE OIL PUMPS79-00-00V2500-A1
ENG-79-000808/09/913OIL - INCORPORATE A DEOILER IMPELLER ASSEMBLY WITH LARGER OIL PASSAGE HOLES79-00-00V2500-A1
ENG-79-000910/13/893OIL - REWORK THE ACOC INLET DUCT ASSEMBLY BY ADDING FILLER MATERIAL TO PREVENT FLUID ENTRAPMENT79-00-00V2500-A1
ENG-79-001002/10/925OIL - REWORK THE ACOC INLET DUCT ASSEMBLY BY INCORPORATING DRAIN HOLES TO PREVENT FLUID ENTRAPMENT79-00-00V2500-A1
ENG-79-001101/05/906OIL - REVISE THE NO. 5 BEARING OIL SCAVENGE TUBE ASSEMBLY ATTACHING PARTS79-00-00V2500-A1
ENG-79-001203/02/904OIL - INCORPORATE NEW NO. 5 BEARING OIL FEED TUBE SUPPORT BRACKET ATTACHING BOLTS79-00-00V2500-A1
ENG-79-001305/24/918OIL - PROVIDE A NEW OIL TANK LEVEL INDICATOR79-11-00V2500-A1
ENG-79-001410/12/907OIL - INTRODUCE AN OIL TANK WITH A REVISED FILLER NECK LOCATION79-00-00V2500-A1
ENG-79-001510/14/927ENGINE - OIL - INTRODUCE OIL PRESSURE PUMP AND OIL SCAVENGE PUMP IDENTIFICATION PLATES AND ATTACHING SCREWS79-00-00V2500-A1
ENG-79-001608/30/934ENGINE - OIL FEED TUBE RESTRICTOR - INSPECTION/CHECK79-00-00V2500-A1
ENG-79-001711/13/894OIL - INCORPORATION OF A SPACER AT OIL QUANTITY TRANSMITTER MOUNT79-00-00V2500-A1
ENG-79-001801/18/915OIL - INCORPORATE LONGER BOLTS TO ATTACH NO. 4 BEARING COMPARTMENT SCAVENGE VALVE79-00-00V2500-A1
ENG-79-001907/05/914OIL - REPLACE THE FUEL COOLED OIL COOLER ATTACHING BOLTS79-00-00V2500-A1
ENG-79-002004/05/916OIL - FUEL COOLED OIL COOLER - INTRODUCTION OF LONGER UPPER BONDING STRAP79-00-00V2500-A1
ENG-79-002112/14/904OIL - REPLACE THE FUEL COOLED OIL COOLER (FCOC) MOUNT BRACKET79-00-00V2500-A1
ENG-79-002210/07/916OIL - OIL TANK ASSEMBLY - ADD A BRACKET FOR SECURING THE DUST COVERS LANYARDS79-00-00V2500-A1
ENG-79-002305/31/914OIL - OIL TANK ASSEMBLY - PROVIDE AN OIL TANK OVERFILL WARNING PLATE79-00-00V2500-A1
ENG-79-002411/15/964OIL - AIR COOLED OIL COOLER AIR MODULATING VALVE - ACTUATOR ASSEMBLY - INSPECTION CHECK OF CONCENTRICITY OF PISTON LOCATING BORES79-00-00V2500-A1
ENG-79-002505/11/938ENGINE - OIL - PROVIDE A SIGHT GLASS OIL LEVEL INDICATOR FOR THE OIL TANK ASSEMBLY79-11-00V2500-A1
ENG-79-002610/11/914OIL - REPLACEMENT OF TWO SCAVENGE TUBES ON THE EXTERNAL GEARBOX79-22-00V2500-A1
ENG-79-002708/10/936ENGINE - OIL - NEW OIL TANK CAP ASSEMBLY WITH REVISED TANK CAPACITY INFORMATION79-00-00V2500-A1
ENG-79-002804/02/935ENGINE - MAIN GEARBOX ASSEMBLY - MAGNETIC CHIP DETECTOR PACKINGS, REPLACEMENT OF79-00-00V2500-A1
ENG-79-002902/18/945ENGINE - POWERPLANT - OIL MAGNETIC CHIP DETECTOR INSPECTION FOR WEAR79-00-00V2500-A1,-A5
ENG-79-003009/22/947ENGINE - OIL - PROVIDE AN IMPROVED DESIGN OIL TANK SIGHT GLASS ASSEMBLY79-00-00V2500-A1
ENG-79-003104/20/935ENGINE - OIL - A NEW REINFORCED FUEL COOLED OIL COOLER TO PROVIDE IMPROVED DURABILITY79-00-00V2500-A5
ENG-79-003206/01/935ENGINE - OIL SYSTEM - APPLY JOINTING COMPOUND TO THE ACOC INLET DUCT AND FAN CASE ASSEMBLY79-00-00V2500-A1
ENG-79-003303/01/94See SBENGINE - OIL - SAMPLING INSPECTION OF SCAVENGE OIL FILTER .ELEMENT FOR EXTENDED SERVICE USE79-22-00V2500-A1
ENG-79-003512/16/947ENGINE - OIL - PROVIDE A REROUTED NO. 4 BEARING OIL SCAVENGE TUBE ASSEMBLY79-22-00V2500-A1
ENG-79-003602/12/968ENGINE - OIL - ADD A SPACER AT CLIPPING POINTS CP0919 AND CP092679-22-00V2500-A1
ENG-79-003810/10/976ENGINE - PROVIDE A NEW IDG POWER CABLE BRACKET TO ACCOMMODATE A REROUTED RACEWAY79-21-00V2500-A5
ENG-79-003910/07/945ENGINE - OIL - INTRODUCE A NEW OIL PRESSURE PUMP OUTLET - TO ACOC TUBE SEALING RING79-00-00V2500-A1,-A5,-D5
ENG-79-004007/27/970106/27/007ENGINE - OIL SYSTEM - INTRODUCE A NEW NO. 4 BEARING OIL SCAVENGE TUBE ASSEMBLY79-00-00V2500-D5
ENG-79-004102/10/957OIL - AIR COOLED OIL COOLER AIR MODULATING VALVE - INTRO- DUCTION OF A VALVE FEATURING IMPROVED SPRING DURABILITY, IMPROVED, LINKAGE, IMPROVED LINEAR VARIABLE DIFFERENTIAL TRANSFORMER, AND IMPROVED SEALING OF THE ACTUATOR ASSEMBLY79-00-00V2500-D5
ENG-79-004206/16/950110/19/997ENGINE - INTRODUCE A NEW MAGNETIC CHIP DETECTOR ASSEMBLY FOR CONTROLLED SERVICE USE79-00-00V2500-A1,-A5
ENG-79-004302/10/957OIL - AIR COOLED OIL COOLER AIR MODULATING VALVE - ACTUATOR ASSEMBLY - INTRODUCTION OF IMPROVED SEALING79-00-00V2500-A1,-A5
ENG-79-004406/15/955ENGINE - OIL - INTRODUCE A NEW NO. 4 BEARING SCAVENGE VALVE WITH AN IMPROVED VALVE SEAL79-23-00V2500-A1
ENG-79-004510/17/976ENGINE - OIL - INTRODUCE A NEW IDG BRACKET AND A NEW SUPPORT BRACKET79-21-00V2500-A5
ENG-79-004601/30/986ENGINE - OIL - INTRODUCE NEW MAIN OIL SCAVENGE PUMP ATTACHMENT BOLTS79-22-00V2500-D5
ENG-79-004704/30/986ENGINE - OIL - INTRODUCE A NEW OIL LUBRICATION TUBE, AND NEW OIL PRESSURE AND OIL SCAVENGETUBES79-00-00V2500-A5
ENG-79-004807/21/956ENGINE - OIL - TO REMOVE THE INLET DUCT RIB OF THE ACOC INLET DUCT ASSEMBLY79-00-00V2500-D5
ENG-79-004906/26/956ENGINE - REPLACE MAIN OIL SCAVENGE PUMP MOUNTING FLANGE PACKINGS79-00-00V2500-A1,-A5,-D5
ENG-79-005003/13/980103/13/986ENGINE - OIL - INTRODUCTION OF PARTIAL BLANKING OF THE AIR COOLED OIL COOLER (ACOC) MATRIX79-00-00V2500-A1,-A5
ENG-79-005109/10/950407/10/998ENGINE - OIL - TO INTRODUCE A NEW MAIN OIL SCAVENGE PUMP FEATURING IMPROVED SPACERS AND COVERS79-00-00V2500-A1,-A5,-D5
ENG-79-005201/29/966ENGINE - OIL - INTRODUCE A NEW ACOC INLET DUCT WITH A REVISED DUCT FACE SURFACE TREATMENT79-00-00V2500-D5
ENG-79-005309/06/964ENGINE - OIL - PROVIDE REROUTED NO. 5 BEARING OIL SCAVENGE TUBE ASSEMBLIES79-22-00V2500-D5
ENG-79-005411/29/965ENGINE - AIR MODULATING VALVE - INTRODUCTION OF A -P- SEAL HAVING REDUCED COMPRESSIVE LOAD79-21-00V2500-D5
ENG-79-005507/29/967OIL - AIR COOLED OIL COOLER MODULATING VALVE - INTRODUCTION OF AIR MODULATING VALVE WITH REVISED"P"SEAL MATERIAL79-21-00V2500-D5
ENG-79-005602/06/986OIL - SCAVENGE TUBES - ENGINE - INTRODUCTION OF RE-ROUTED SCAVENGING OIL PUMP TUBE ASSEMBLIES FOR THE NO. 5 BEARING COMPARTMENT AND ANGLE GEARBOX79-22-00V2500-A1,-A5
ENG-79-005710/05/010103/07/037ENGINE-OIL-NO.4 BEARING COMPARTMENT SCAVENGE VALVE-INTRODUCTION OF A NO.4 BEARING SCAVENGE VALVE SUPPLIED BY TECHSPACE AERO79-23-51V2500-A1,-A5
ENG-79-005807/18/970208/03/017ENGINE - OIL - ACOC TO SCAVENGE OIL FILTER AND SCAVENGE PUMP TO NO. 8 STRUT OIL TUBES RESET IN REGION OF OIL SCAVENGE PUMP79-00-00V2500-D5
ENG-79-005906/13/970208/07/987OIL - AIR COOLED OIL COOLER MODULATING VALVE - INTRODUCTION OF REVISED"P"SEAL79-21-00V2500-A1,-A5
ENG-79-006011/07/977OIL - PRESSURE OIL TUBES - INTRODUCTION OF REVISED OIL TUBE BETWEEN FCOC AND BEARINGS WITH BRAZED-ON LUGS79-21-00V2500-A1,-A5
ENG-79-006111/07/976OIL PRESSURE OIL TUBES - INTRODUCTION OF BOLT FOR CLIPPING POINT CP2180 WITH DECREASED LENGTH79-21-00V2500-D5
ENG-79-006204/27/980111/24/007ENGINE - FUEL, AIR AND OIL TUBES - TO ANNOUNCE THE INTRODUCTION OF MODIFIED RIGID TUBE ASSEMBLIES75-22-00V2500-D5
ENG-79-006312/19/975ENGINE - MAIN GEARBOX ASSEMBLY - SWAPPED SCAVENGE OIL TUBE MODIFICATION79-22-00V2500-D5
ENG-79-006404/17/980109/20/998ENGINE - MAIN GEARBOX ASSEMBLY - INTRODUCTION OF REVISED OIL SCAVENGE TUBES TO STOP OIL LEAKS79-22-00V2500-A1,-A5,-D5
ENG-79-006501/25/030102/10/037NACELLE - POWEPLANT - INTRODUCTION OF IMPROVED OIL QUANTITY TRANSMITTER79-00-00V2500-A1,-A5
ENG-79-006610/02/987OIL - PRESSURE OIL TUBES - INTRODUCTION OR RE-RUN TUBE ASSEMBLY WITH REVISED ADJACENT BRACKET ASSEMBLIES79-21-00V2500-D5
ENG-79-006709/18/980205/26/997OIL - MAGNETIC CHIP DETECTOR - INTRODUCTION OF A REVISED MAGNETIC CHIP DETECTOR SUPPLIED BY VICKERS - TEDECO DIVISION79-22-00V2500-D5
ENG-79-006802/12/996OIL - AIR COOLED OIL COOLER - INTRODUCTION OF REVISED ACOC WITH PARTIAL MATRIX BLANKING79-21-00V2500-D5
ENG-79-006912/23/990104/14/006OIL-PRESSURE OIL TUBES - ENGINE-INTRODUCTION OF RE-ROUTED OIL TUBES AND REVISED CLIPPING ABOVE THE EXTERNAL GEARBOX79-21-00V2500-A1,-A5
ENG-79-007004/16/990101/28/004OIL - PRESSURE OIL TUBES - ENGINE - INTRODUCTION OF REVISED OIL FEED SYSTEM RESTRICTORS79-21-00V2500-A1
ENG-79-007104/03/990106/28/994ENGINE - OIL - INTRODUCE AN UPGRADED OIL PRESSURE PUMP79-21-00V2500-A1
ENG-79-007304/02/990104/28/005ENGINE - OIL - INTRODUCTION OF OIL RESTRICTOR OF FBC OIL LINE WITH REVISED THROAT SIZE72-32-00V2500-A1
ENG-79-007406/11/997OIL - ENGINE OIL SCAVENGE PUMP COUPLING REDESIGN79-22-41V2500-A1,-A5,-D5
ENG-79-007503/12/990201/28/007OIL - FUEL COOLED OIL COOLER - INTRODUCTION OF REVISED FCOC UPPER MOUNT79-21-00V2500-A1,-A5
ENG-79-007602/05/990101/28/007OIL - FUEL COOLED OIL COOLER - INTRODUCTION OF AN FCOC WITH REVISED TOP MOUNT ASSEMBLY79-21-00V2500-A1,-A5
ENG-79-007705/23/000110/23/006ENGINE - OIL - INTRODUCTION OF A NEW OIL SCAVENGER PUMP WITH IMPROVED CASING, SPACERS AND COVERS79-00-00V2500-A1,-A5,-D5
ENG-79-007806/16/995OIL - OIL PRESSURE TRANSMITTER - RETURN OF POTENTIALLY DEFECTIVE TRANSMITTER UNITS (NON-MODIFICATION)79-33-15V2500-A1,-A5
ENG-79-007906/19/004ENGINE - OIL - TO ANNOUNCE THE AVAILABILITY OF A COATED FUEL COOLED OIL COOLER THREADED INSERT79-21-00V2500-A1
ENG-79-008001/15/016OIL - AIR COOLED OIL COOLER MODULATING VALVE - INTRODUCTION OF AN AIR MODULATING VALVE WITH REVISED ACTUATOR END CAP RETAINING WASHERS79-21-51V2500-A1
ENG-79-008202/14/027OIL - AIR COOLED OIL COOLER MODULATING VALVE - INTRODUCTION OF AN AIR MODULATING VALVE SUPPLIED BY WOODWARD AIRCRAFT ENGINE SYSTEM79-21-51V2500-A1,-A5
ENG-79-008310/05/010108/01/023ENGINE - OIL - REPLACEMENT OF 1648MK2 NO.4 BEARING SCAVENGE VALVES NMSB - NON-MODIFICATION SERVICE BULLETIN79-23-51V2500-A1
ENG-79-008405/17/027OIL - OIL QUANTITY TRANSMITTER - INTRODUCTION OF AN IMPROVED OIL QUANTITY TRANSMITTER79-31-02V2500-D5
ENG-79-008506/19/020205/09/124OIL - FUEL COOLED OIL COOLER - INTRODUCTION OF A REVISED FCOC WITH STIFFENED FUEL FILTER CAP79-21-43V2500-A1
ENG-79-008608/08/020205/09/124OIL - FUEL COOLED OIL COOLER - INTRODUCTION OF A REVISED FCOC WITH STIFFENED FUEL FILTER CAP (A5 ENGINES)79-21-43V2500-A5
ENG-79-008705/15/030109/11/033OIL - SCAVENGE OIL TUBES - RE-ROUTE OF NUMBER 4 BEARING SCAVENGE TUBE79-00-00V2500-A1
ENG-79-008811/12/034OIL - SCAVENGE OIL TUBES - RE-ROUTE OF NUMBER 4 BEARING SCAVENGE TUBE79-00-00V2500-A5
ENG-79-008909/16/034OIL - SCAVENGE OIL TUBES - ENGINE - INTRODUCTION OF FLUOROCARBON SEALS79-22-49V2500-A1,-A5,-D5
ENG-79-009102/20/073ENGINE - EXTERNALS - INSPECTION OF OIL SCAVENGE TUBE AND CLIPPING POINT79-00-00V2500-D5
ENG-79-009210/26/070106/11/087ENGINE - OIL TANK ASSEMBLY - TO ANNOUNCE AN OIL TANK PLATE WITH REVISED WORDING79-11-41V2500-A1,-A5,-D5
ENG-79-009311/27/080108/05/207ENGINE - OIL - TO ANNOUNCE A NEW SCAVENGE OIL PUMP WITH IMPROVED COMPARTMENT NO. 5 SCAVENGING PERFORMANCE79-22-41V2500-A1,-A5,-D5
ENG-79-009406/09/087ENGINE - OIL - INTRODUCTION OF A REDESIGNED DOUBLE HEADER AIR COOLED OIL COOLER79-21-42V2500-A1,-A5
ENG-79-009509/28/100105/27/117ENGINE - OIL - NO.4 BEARING OIL PRESSURE TRANSDUCER RE-DESIGN79-33-16V2500-A1,-A5
ENG-79-009707/21/103NON-MODIFICATION SERVICE BULLETIN - ENGINE - FUEL COOLED OIL COOLER (FCOC) HOUSING - THIN WALL SECTIONS79-21-43V2500-A1
ENG-79-009804/27/116ENGINE - EXHAUST GAS TEMPERATURE (EGT) HARNESS CLIPPING MODIFICATION TO PREVENT CHAFING ON FUEL MANIFOLD TUBE79-21-49V2500-A1,-A5
ENG-79-009911/09/100501/28/133NON-MODIFICATION SERVICE BULLETIN - OIL - AIR COOLED OIL COOLER (ACOC) - REPLACEMENT OF LOCALLY INSUFFICIENT BRAZED UNITS79-21-42V2500-A1,-A5
ENG-79-010002/18/110111/03/117OIL - INTRODUCTION OF V2500-A5 FUEL COOLED OIL COOLER ON V2500-A1 ENGINES79-21-43V2500-A1
ENG-79-010109/02/140111/17/168OIL - INTRODUCTION OF OPTIMIZED DESIGN FEATURES TO THE OIL TANK, THE PRESSURE PUMP AND FILTER HOUSING, THE SCAVENGE OIL PUMP, THE SCAVENGE OIL FILTER ASSEMBLY AND THE TRANSPORTATION FITTINGS.79-00-00V2500-A1,-A5,-D5
ENG-79-010205/21/138ENGINE - BOLT LENGTH CORRECTION TO SOLVE BUILD ISSUES731100V2500-A5
ENG-79-010312/20/116NON-MODIFICATION SERVICE BULLETIN - OIL - AIR COOLED OIL COOLER (ACOC) - ACOUSTIC EMISSION TEST FOR UNITS NOT TESTED DURING NEW PRODUCTION79-21-41V2500-A1,-A5
ENG-79-010508/06/144NON-MODIFICATION SERVICE BULLETIN - OIL - SCAVENGE OIL PUMP - INSPECTION FOR INTERNAL RETAINING RING INSTALLATION79-22-41V2500-A1,-A5,-D5
ENG-79-010610/17/147OIL - TUBE ASSY, FRONT BEARING COMPARTMENT OIL VENT - INTRODUCTION OF A NEW TUBE ASSY WITH A VENT LINE RESTRICTOR FOR REDUCED GROUND IDLE79-22-49V2500-A5
ENG-79-010711/23/150106/22/163NON-MODIFICATION SERVICE BULLETIN - A1 OIL CONSUMPTION MONITORING GUIDELINES79-00-00V2500-A1
ENG-79-010812/14/168NON-MODIFICATION SERVICE BULLETIN - OIL - ENGINE OIL - INTRODUCE ALTERNATIVE ENGINE OIL LUBRICANTS79-00-00V2500-A1,-A5,-D5
ENG-79-010906/29/176OIL - OIL COOLER, AIR COOLED - REPLACE WITH A MORE DURABLE OIL COOLER79-21-42V2500-A1,-A5
ENG-80-000207/05/916STARTING - INSTALLATION OF SHOTPEENED PAWL SPRINGS IN PNEUMATIC STARTER80-13-00V2500-A1
ENG-80-000305/17/914STARTING - PNEUMATIC STARTER - INTRODUCTION OF OIL SIGHT GLASS AND INCREASED OIL QUANTITY80-13-00V2500-A1
ENG-80-000407/12/916STARTING - PNEUMATIC STARTER VALVE - INTRODUCTION OF IMPROVED SEALING OF THE VALVEDISC80-13-00V2500-A1
ENG-80-000507/05/916STARTING - INTRODUCTION OF A STARTER INCORPORATING IMPROVED CLAMPING OF THE TURBINE ASSEMBLY (L7), INCREASED OIL FLOW (L9), AND ADDITIONAL OVERFLOW TUBE (L10)80-00-00V2500-A1
NAC-80-000605/14/934NACELLE - STARTING - AIR SUPPLY DUCT- ALIGNMENT MARK - ALTERATION OF - CATEGORY CODE 4 - MOD.NAC-80-000680-00-00V2500-A1
ENG-80-000712/17/937ENGINE - STARTING - INTRODUCE A PNEUMATIC STARTER FEATURING A HOUSING WITH INCREASED OILCAPACITY80-13-00V2500-A1
ENG-80-000809/30/957ENGINE - STARTING - INTRODUCTION OF A SYNCHRONOUS ENGAGEMENT STARTER80-13-00V2500-A1,-A5
ENG-80-000911/07/970211/07/974ENGINE - STARTING - PNEUMATIC STARTER - INTRODUCTION OF A STARTER FEATURING A SYNCHRONOUS ENGAGEMENT CLUTCH AND AN OIL PRESSURE FILL FACILITY80-00-00V2500-D5
ENG-80-001003/13/980103/13/987STARTING - PNEUMATIC STARTER VALVE - INTRODUCTION OF STARTER CONTROL VALVE WITH REVISED SOLENOID AND PLUNGER SPOOL COATING80-00-00V2500-A1,-A5,-D5
ENG-80-001112/12/970112/12/977STARTING - PNEUMATIC STARTER VALVE - INTRODUCTION OF REVISED EXTERNAL WIRING80-00-00V2500-A1
ENG-80-001207/18/977STARTING - PNEUMATIC STARTER VALVE - INTRODUCTION OF STARTER CONTROL VALVE WITH REVISED MATERIAL FOR ACTUATOR LINK PIN80-00-00V2500-A1,-A5,-D5
ENG-80-001306/12/987STARTING - PNEUMATIC STARTER - INTRODUCTION OF STARTER WITH REVISED CARBON SEAL RETENTION80-00-00V2500-A1,-A5,-D5
ENG-80-001406/09/006STARTING - PNEUMATIC STARTER - INTRODUCTION OF REVISED STARTER WITH MODIFIED TURBINE RETENTION NUT REWORK OF THE PINION GEAR80-00-00V2500-A1,-A5,-D5
ENG-80-001512/10/000103/07/116STARTING - PNEUMATIC STARTER - INTRODUCTION OF A REVISED PNEUMATIC STARTER WITH A MODIFIED SYNCHRONOUS ENGAGEMENT CLUTCH ASSEMBLY80-00-00V2500-A1,-A5,-D5
ENG-80-001611/15/026STARTING - PNEUMATIC STARTER - INTRODUCTION OF A REVISED STARTER WITH MODIFIED PLANET GEAR SETSCREW RETENTION80-13-41V2500-A1,-A5,-D5
ENG-80-001904/07/046STARTING - PNEUMATIC STARTER - INTRODUCTION OF A PNEUMATIC STARTER WITH REVISED DYNAMIC "O" RING SEALS80-13-41V2500-A1,-A5,-D5
ENG-80-002007/08/040108/04/046STARTING - PNEUMATIC STARTER - INTRODUCTION OF A PNEUMATIC STARTER WITH A VENTED INLET HOUSING80-13-41V2500-A5
ENG-80-002104/08/080112/17/088STARTER/TAI DUCT SYSTEM - REPLACEMENT OF BEARING LINK ASSEMBLIES (FOR CONTROLLED SERVICE USE)80-13-00V2500-A5
ENG-80-002204/28/140110/29/148ENGINE - STARTER AND TAI DUCT SYSTEM - INTRODUCTION OF NEW MORE DURABLE BEARING LINK ASSEMBLIES80-00-00V2500-A5
ENG-80-002301/16/120103/28/13NON-MODIFICATION SERVICE BULLETIN - STARTING - PNEUMATIC STARTER - REPLACEMENT OF NON CONFORMANCE PHEUMATIC STARTER UNITS80-13-41
ENG-80-002409/16/130212/18/137STARTING - PNEUMATIC STARTER - INTRODUCTION OF A REVISED PNEUMATIC STARTER WITH AN IMPROVED MAGNETIC SEAL AND NEW GEAR CAGE STEEL SLEEVES80-13-41V2500-A1,-A5,-D5
ENG-80-002509/16/138STARTING - PNEUMATIC STARTER - INTRODUCTION OF A NEW STARTER WITH THE REMOVAL OF THE OIL SIGHT GLASS80-13-41V2500-A1,-A5
ENG-80-002609/17/206STARTING - STARTER, PNEUMATIC - INSPECTION OF THE PNEUMATIC STARTER FOR AN INCORRECT FAA-PMA LABEL80-13-41V2500-A1,-A5
NAC-29-026502/22/178 NACELLE - HYDRAULIC SYSTEM - INTRODUCTION OF AN EXTERNAL DAMPENER FOR EATON ENGINE DRIVEN PUMPS (EDP)29-11-49V2500-A5
NAC-70-058903/16/98See SBINFORMATION - NACELLE - TO ANNOUNCE THE AVAILABILITY OF A SPECIAL ORDER ONLY FIRE DETECTION SYSTEM26-00-00V2500-A5
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