TASK 72-00-50-420-001-B00 LPT Module - Install The LPT Module (Horizontal) - Method 1, Installation-002 - SBE 72-0063

DMC:V2500-A1-72-00-5000-01C-720A-B|Issue No:006.00|Issue Date:2020-05-01

Export Control

EAR Export Classification: Not subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3), except for the following Service Bulletins which are currently published as EAR Export Classification 9E991: SBE70-0992, SBE72-0483, SBE72-0580, SBE72-0588, SBE72-0640, SBE73-0209, SBE80-0024 and SBE80-0025.

Copyright

© IAE International Aero Engines AG (2001, 2014 - 2021) The information contained in this document is the property of © IAE International Aero Engines AG and may not be copied or used for any purpose other than that for which it is supplied without the express written authority of © IAE International Aero Engines AG. (This does not preclude use by engine and aircraft operators for normal instructional, maintenance or overhaul purposes.).

Applicability

V2500-A1 and Post SBE 72-0063

Common Information

TASK 72-00-50-420-001-B00 LPT Module - Install The LPT Module (Horizontal) - Method 1, Installation-002 - SBE 72-0063

General

This TASK gives the procedure to install the LP Turbine Module in horizontal position. Other related TASKS are:

Install the LP Turbine Module without TEC by TASK 72-00-50-420-002 (INSTALLATION-003).

Install the LP Turbine Module (vertical) by TASK 72-00-50-420-004-B00 (INSTALLATION-005) - Method 2.

Turn the LP Turbine Module from horizontal to vertical (front end down) by TASK 72-00-50-560-001 (REMOVAL-003).

Fig/item numbers in parentheses in this procedure agree with those used in the IPC. Only the primary Fig/item numbers are used. For the service bulletin alpha variants refer to the IPC.

For all parts identified in a different Chapter/Section/Subject, the applicable Chapter/Section/Subject comes before the Fig/item number.

For standard torque data and procedures, refer to the SPM TASK 70-41-01-400-501 and SPM TASK 70-41-02-400-501.

The number for each radial location must be identified in a clockwise direction. These start at the engine top position when you look from the rear of the engine, unless stated differently in the procedure.

Special torque data is identified by the symbol * after the torque value.

Special assembly tolerances are included in this procedure.

Lubricate all threads and abutment faces of nuts and bolts with CoMat 10-077 APPROVED ENGINE OILS, unless other lubricants are referred to in the procedure.

After assembly apply CoMat 07-038 AIR DRYING ENAMEL to any damaged surface protection, joint flanges and attach parts. Use the correct color of the air drying enamel. Refer to SPM TASK 70-63-02-400-501.

Transportation covers/blanks must be removed immediately before the installation of the components.

For lockwire data and procedures refer to the SPM TASK 70-42-05-400-501.

NOTE

To identify the consumable materials refer to the PCI.

NOTE

Special tools are identified in the procedure by the tool primary number.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
Dial GageLOCALDial Gage
Vernier depth gageLOCALVernier depth gage
IAE 1F10016 Mechanical wrench0AM53IAE 1F100161
IAE 1F10026 Hydraulic hand pump0AM53IAE 1F100261
IAE 1F10052 Two cables sling0AM53IAE 1F100521
IAE 1F10058 Handling fixture0AM53IAE 1F100581
IAE 1F10063 Expanding retainer0AM53IAE 1F100631
IAE 1F10080 Horizontal stand0AM53IAE 1F100801
IAE 1F10084 Support fixture0AM53IAE 1F100841
IAE 2F10418 Length gage0AM53IAE 2F104181
IAE 2F10415 Loading fixture0AM53IAE 2F104151
IAE 2F10368 Plate, Vacuum check0AM53IAE 2F103681
IAE 6F10027 Heater control unit0AM53IAE 6F100271
IAE 6F10029 Air flow test cart0AM53IAE 6F100291
IAE 6F10030 Vacuum test cart0AM53IAE 6F100301
IAE 1J12220 Hydraulic pusher/puller0AM53IAE 1J122201
IAE 1J12221 Impact hammer0AM53IAE 1J122211
IAE 1J12243 Sizing sleeve0AM53IAE 1J122431
IAE 1J12259 Seal slider0AM53IAE 1J122591
IAE 1J12260 Spanner wrench0AM53IAE 1J122601
IAE 1J12279 Grinding fixture0AM53IAE 1J122791
IAE 1J12280 Guide bar0AM53IAE 1J122801
IAE 1J12281 0AM53 heater0AM53IAE 1J122811
IAE 1J12282 Expanding pliers0AM53IAE 1J122821
IAE 1J12522 Seal slider0AM53IAE 1J125221
IAE 1M14127 Support plate0AM53IAE 1M141272
IAE 1P16354 Vacuum Test Adapter0AM53IAE 1P163541
IAE 1P16624 Slide Puller0AM53IAE 1P166241
IAE 1P17523 Blank-off Plate0AM53IAE 1P175231
IAE 1R18908 Guide plug0AM53IAE 1R189081
IAE 2R18871 Inspection bridge0AM53IAE 2R188711

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 01-119 POTASSIUM CHROMATE K2CrO4K6835CoMat 01-119
CoMat 02-119 LOCKWIRELOCALCoMat 02-119
CoMat 07-038 AIR DRYING ENAMELk3504CoMat 07-038
CoMat 10-045 LEAK CHECK FLUID, BUBBLES-TYPE03530CoMat 10-045
CoMat 10-045A LEAK CHECK FLUID, BUBBLES-TYPELOCALCoMat 10-045A
CoMat 10-077 APPROVED ENGINE OILSLOCALCoMat 10-077
CoMat 10-129 ANTI-SEIZE PASTE34568CoMat 10-129

Spares

NameManufacturerPart Number / IdentificationQuantityRemark
Sealing ring1
Packing1
Packing3
Packing1

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-00-50-420-244 Identify the LP Turbine Module

    1. Make very sure that the replacement LP Turbine Module is fully interchangeable with the module that it replaces and with the module to which it is to be installed. Refer to the SPM for module identification and interchangeability.

    2. SUBTASK 72-00-50-210-058 Examine the Module Interfaces

    1. Examine the HP System Module at interface D-45. Refer to TASK 72-00-45-220-001 (INSPECTION-001).

    2. Examine the front face of the LP Turbine Module at interface D-50/10. Refer to TASK 72-00-50-220-001 (INSPECTION-001).

    3. Examine the LP Compressor/Intermediate Case Module at interface F-32. Refer to TASK 72-00-32-220-004 (INSPECTION-004).

    4. Examine the LP Turbine Module at interface F-50. Refer to TASK 72-00-50-220-005 (INSPECTION-005).

    3. SUBTASK 72-00-50-210-059 Examine the LP Turbine Module Externally and Examine the Non-Modular Parts

    1. Examine the LP Turbine Module externally and examine the non-modular parts.

    4. SUBTASK 72-00-50-220-190 Measure that the Fits and Clearances between the LP Turbine Module and the HP System Module are in the Limits given at Location 5624

    1. Refer to Figure.

    2. Calculate the fit at Location 5624.

      Table 1. Fits and Clearances (all dimensions are in inches)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 5624

      LP Turbine Case (72-50-21, 01-010), Bore

      HP Turbine Stage 2 Support Case ENGINE-STAGE 2 HPT SUPPORT ASSEMBLY (72-45-27, 01-010), Diameter

      LP Turbine Case Bore

      28.527

      28.533

      Intf

      0.002

      28.527

      28.533

      Intf

      0.002

      HP System Case Diameter

      28.535

      28.541

      0.014

      28.529

      28.541

      0.014

      Table 2. Fits and Clearances (all dimensions are in millimeters)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 5624

      LP Turbine Case (72-50-21, 01-010), Bore

      HP Turbine Stage 2 Support Case ENGINE-STAGE 2 HPT SUPPORT ASSEMBLY (72-45-27, 01-010), Diameter

      LP Turbine Case Bore

      724.586

      724.738

      Intf

      0.050

      724.586

      724.738

      Intf

      0.050

      HP Turbine Case Diameter

      724.789

      724.941

      0.356

      724.637

      724.941

      0.356

    5. SUBTASK 72-00-50-220-191 Measure that the Fits and Clearances between the LP Turbine Module and the HP System Module are in the Limits given at Location 5623 (Pre SBE 72-0028)

    1. Refer to Figure.

    2. Calculate the clearance at Location 5623.

      Table 3. Fits and Clearances (all dimensions are in inches)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Select)

      REJECT IF

      MORE THAN

      LOCATION 5623

      Inner Duct Segment ENGINE-LP TURBINE INNER STATIC SEALS (72-50-24, 01-010), Honeycomb Surface

      Stage 2 HPT Blade Retaining Plate ENGINE-STAGE 2 HPT BLADE RETAINING PLATE (72-45-33, 01-010) Knife Edge Outside Diameter

      Inner Duct Segment Honeycomb Surface

      19.896

      19.925

      0.118

      Clear

      19.896

      19.925

      0.118

      Clear

      Knife Edge Outside Diameter

      19.807

      19.812

      Clear

      0.084

      19.797

      19.812

      Clear

      0.084

      Table 4. Fits and Clearances (all dimensions are in millimeters)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Select)

      REJECT IF

      MORE THAN

      LOCATION 5623

      Inner Duct Segment ENGINE-LP TURBINE INNER STATIC SEALS (72-50-24, 01-010), Honeycomb Surface

      Stage 2 HPT Blade Retaining Plate ENGINE-STAGE 2 HPT BLADE RETAINING PLATE (72-45-33, 01-010), Knife Edge Outside Diameter

      Inner Duct Segment Honeycomb Surface

      505.36

      506.10

      3.00

      Clear

      505.36

      506.10

      3.00

      Clear

      Knife Edge Outside Diameter

      503.10

      503.22

      Clear

      2.13

      502.84

      503.22

      Clear

      2.13

    6. SUBTASK 72-00-50-220-252 Measure the Fits and Clearances between the LP Turbine Module and the HP System Module are in the Limits given at Location 5623 (SBE 72-0028)

    1. Refer to Figure.

    2. Calculate the clearance at Location 5623.

      Table 5. Fits and Clearances (all dimensions are in inches)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Select)

      REJECT IF

      MORE THAN

      LOCATION 5623

      Inner Duct Segment ENGINE-LP TURBINE INNER STATIC SEALS (72-50-24, 01-010), Honeycomb Surface

      Stage 2 HPT Blade Retaining Plate ENGINE-STAGE 2 HPT BLADE RETAINING PLATE (72-45-33, 01-010), Knife Edge Outside Diameter

      Inner Duct Segment Honeycomb Surface

      19.896

      19.925

      0.121

      Clear

      19.896

      19.925

      0.121

      Clear

      Knife Edge Outside Diameter

      19.804

      19.812

      Clear

      0.084

      19.797

      19.812

      Clear

      0.084

      Table 6. Fits and Clearances (all dimensions are in millimeters)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Select)

      REJECT IF

      MORE THAN

      LOCATION 5623

      Inner Duct Segment ENGINE-LP TURBINE INNER STATIC SEALS (72-50-24, 01-010), Honeycomb Surface

      Stage 2 HPT Blade Retaining Plate ENGINE-STAGE 2 HPT BLADE RETAINING PLATE (72-45-33, 01-010), Knife Edge Outside Diameter

      Inner Duct Segment Honeycomb Surface

      505.36

      506.10

      3.07

      Clear

      505.36

      506.10

      3.07

      Clear

      Knife Edge Outside Diameter

      503.02

      503.22

      Clear

      2.13

      502.84

      503.22

      Clear

      2.13

    7. SUBTASK 72-00-50-220-192 Measure that the Fits and Clearances between the LP Turbine Module and the LP Compressor are in the Limits given at Location 5620

    1. Refer to Figure.

    2. Calculate the fit at Location 5620.

      Table 7. Fits and Clearances (all dimensions are in inches)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 5620

      LP Stub Shaft (72-32-51, 01-350), Bore

      LP Turbine Shaft ENGINE-LP TURBINE SHAFT (72-50-41, 01-200), Diameter

      Stub Shaft Bore

      3.5433

      3.5447

      Intf

      0.0006

      LP Turbine Shaft Diameter

      3.5453

      3.5462

      0.0029

      Table 8. Fits and Clearances (all dimensions are in millimeters)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 5620

      LP Stub Shaft (72-32-51, 01-350), Bore

      LP Turbine Shaft ENGINE-LP TURBINE SHAFT (72-50-41, 01-200), Diameter

      Stub Shaft Bore

      90.000

      90.035

      Intf

      0.016

      LP Turbine Shaft Diameter

      90.051

      90.073

      0.073

    8. SUBTASK 72-00-50-220-193 Measure that the Fits and Clearances between the LP Turbine Module and the LP Compressor are in the Limits given at Location 5621.

    1. Refer to Figure.

    2. Calculate the fit at Location 5621.

      Table 9. Fits and Clearances (all dimensions are in inches)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 5621

      LP Stub Shaft (72-32-51, 01-350), Bore

      LP Turbine Shaft ENGINE-LP TURBINE SHAFT (72-50-41, 01-200), Diameter

      Stub Shaft Bore

      3.9370

      3.9379

      Intf

      0.0006

      LP Turbine Shaft Diameter

      3.9385

      3.9393

      0.0023

      Table 10. Fits and Clearances (all dimensions are in millimeters)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 5621

      LP Stub Shaft (72-32-51, 01-350), Bore

      LP Turbine Shaft ENGINE-LP TURBINE SHAFT (72-50-41, 01-200), Diameter

      Stub Shaft Bore

      100.000

      100.022

      Intf

      0.015

      LP Turbine Shaft Diameter

      100.037

      100.059

      0.059

    9. SUBTASK 72-00-50-220-194 Measure that the Fits and Clearances between the LP Turbine Module and the LP Compressor are in the Limits given at Location 5622.

    1. Refer to Figure.

    2. Calculate the clearance at Location 5622.

      Table 11. Fits and Clearances (all dimensions are in inches)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 5622

      Differential Seal (72-32-26, 01-110), Bore

      To LP Turbine Shaft ENGINE-LP TURBINE SHAFT (72-50-41, 01-200), Diameter

      Seal Bore

      3.9410

      3.9449

      0.0017

      LP Turbine Shaft Diameter

      3.9385

      3.9393

      0.0064

      Table 12. Fits and Clearances (all dimensions are in millimeters)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 5622

      Differential Seal (72-32-26, 01-110), Bore

      LP Turbine Shaft ENGINE-LP TURBINE SHAFT (72-50-41, 01-200), Diameter

      Seal Bore

      100.100

      100.200

      0.041

      LP Turbine Shaft Diameter

      100.037

      100.059

      0.163

    10. SUBTASK 72-00-50-420-391 Remove the No. 5 Bearing Nozzle

    1. Refer to Figure.

    2. Remove the two bolts and key washers which attach the No. 5 Bearing Packing Transfer Tube to the No. 5 Bearing Nozzle.

    3. Install the IAE 1P16624 Slide Puller 1 off into No. 5 Bearing Packing Transfer Tube.

    4. Move the knocker puller rearwards quickly and hit the handle to remove the No. 5 Bearing Packing Transfer Tube from the No. 5 Bearing Nozzle.

    5. Remove the No. 5 Bearing Packing Transfer Tube and the three packings from the No. 5 Bearing Nozzle. Discard the packings.

    6. Remove the two bolts which attach the No. 5 Bearing Nozzle.

    7. Remove the No. 5 Bearing Nozzle and packing. Discard the packing.

    11. SUBTASK 72-00-50-420-245 Attach the LP Handling Fixture to the LP Turbine Module

    1. Refer to Figure.

    4. Install the IAE 1F10063 Expanding retainer to the inner diameter of the LP Turbine Shaft. Attach the IAE 1F10084 Support fixture to the rear inner flange of the TEC.

    5. Turn the handwheel counter clockwise until the support is installed safely in the rear end of the LP Turbine Shaft.

    6. Turn the knob counter clockwise to push the clamps against the inner diameter of the LP Turbine Shaft.

    7. Lift the IAE 1F10058 Handling fixture and install it to the IAE 1F10063 Expanding retainer. Align the guide pin of the IAE 1F10058 Handling fixture with the hole in the rear flange of the TEC.

    8. Attach the IAE 1F10058 Handling fixture to the rear flange of the TEC with the 13 screws. Tighten the screws.

    9. CAUTION

      MAKE SURE THAT THE NUTS ARE TIGHTENED. IF THE FIXTURES ARE NOT CORRECTLY SECURED THE LP TURBINE CASE AND ROTOR PARTS CAN BE DAMAGED DURING HANDLING OF THE LP TURBINE MODULE.

      Attach the IAE 1F10063 Expanding retainer to the IAE 1F10058 Handling fixture with the two nuts. Tighten the nuts.

    12. SUBTASK 72-00-50-420-246 Install the Length Gage in to the Engine

    1. Refer to Figure.

    2. Connect the front shaft and the rear shaft of the IAE 2F10418 Length gage 1 off.

    3. Compress the guiding slides of the front shaft and put the IAE 2F10418 Length gage from the rear in to the engine. Observe the top position of the front and the rear shaft.

    4. Move the IAE 2F10418 Length gage in to the engine until the locating face of the front shaft touches the adjusting ring location on the LP Turbine Stub Shaft.

    13. SUBTASK 72-00-50-420-247 Install the Beam of the Length Gage to the Rear Flange of the HP Turbine Case

    1. Refer to Figure.

    2. Install the beam (part of the IAE 2F10418 Length gage) to the rear flange of the HP Turbine Case. Safety the beam to the HP Turbine Case with the eight bolts and nuts. The end of the rear shaft must be on the beam.

    3. Safety the shaft in radial position to the beam with the safety pin.

    14. SUBTASK 72-00-50-420-248 Install the Handle to the Length Gage

    1. Install the handle to the front end of the IAE 2F10418 Length gage 1 off.

    2. Safety the handle to the IAE 2F10418 Length gage with the nut. Torque the nut to 521 lbfin (58.9 Nm).

    15. SUBTASK 72-00-50-420-249 Install the Loading Fixture to the Front Flange of the Fan Case

    1. Refer to Figure.

      2. Install the IAE 1R18908 Guide plug 1 off with the force gage and the bolt (parts of the IAE 2F10415 Loading fixture 1 off) to the curvic coupling of the LP Stub Shaft as follows:

      1. Engage the IAE 1R18908 Guide plug to the inner flange of the LP Stub Shaft.

      2. Align the four holes in the IAE 1R18908 Guide plug with the four holes in the inner flange of the LP Stub Shaft.

      3. Safety the IAE 1R18908 Guide plug to the LP Stub Shaft with the four pins (parts of the IAE 1R18908 Guide plug).

      4. Safety the four pins to the IAE 1R18908 Guide plug with the four screws (parts of the IAE 1R18908 Guide plug).

      5. Install the force gage to the IAE 1R18908 Guide plug.

      6. Attach with the socket head cap screw and nut (parts of the IAE 2F10415 Loading fixture).

      7. Install the bolt to the force gage.

      8. Attach with the socket head cap screw and nut (parts of the IAE 2F10415 Loading fixture).

    3. Install the flange (part of the IAE 2F10415 Loading fixture 1 off) to the front flange of the Fan Case. The bolt must come out through the center hole of the flange. Attach the flange to the Fan Case with eight screws, eight nuts and 16 washers.

    4. Install the support (part of the IAE 2F10415 Loading fixture 1 off) to the bolt and the flange.

    5. Install the thrust bearing (part of the IAE 2F10415 Loading fixture 1 off) on to the support. Safety all together with the ring and four screws.

    6. Install the speed ball handle (part of the IAE 2F10415 Loading fixture 1 off). Attach it to the support with two screws.

    16. SUBTASK 72-00-50-420-250 Load the No. 1 Bearing

      NOTE

      Load must be applied in rearward direction.

    1. Refer to Figure.

    2. Turn the speed ball handle of the IAE 2F10415 Loading fixture 1 off until the force gage shows the load of 900 lbf (4.0 kN).

    17. SUBTASK 72-00-50-420-251 Calibrate the Zero Position on the Dial Gage

    1. Refer to Figure.

    2. Hold the Dial Gage against the measuring base plane of the beam.

    3. Calibrate the zero position on the beam datum plane.

    18. SUBTASK 72-00-50-420-252 Measure the Dimension C

    1. Refer to Figure.

    2. Point the Dial Gage to the rear end of the IAE 2F10418 Length gage 1 off.

    3. Read the Dial Gage and write down the dimension as dimension C.

    4. Remove the Dial Gage.

    19. SUBTASK 72-00-50-420-253 Calculate the Adjusting Ring Thickness

    1. Write the dimension C in the table 1, Figure.

    2. Calculate the dimension T as shown in the table 1, Figure.

    3. Record all the necessary dimensions in a component dimension record sheet. See the example in Figure.

    20. SUBTASK 72-00-50-420-254 Adjust the Thickness of the Adjusting Ring

    1. Calculated dimension T and Figure are necessary for the selection of required adjusting ring.

      NOTE

      Figure. shows all available adjusting rings and related thickness ranges.

    2. If the calculated dimension of T is out of the limits given in Figure. the applicable adjusting ring must be machined to calculated dimension T. Refer to Figure. Use the grinding machine and IAE 1J12279 Grinding fixture 1 off.

    21. SUBTASK 72-00-50-420-255 Remove the Loading Fixture from the Engine

    1. Refer to Figure.

    2. Disassemble the speed ball handle, the ring, the thrust bearing and the support (parts of the IAE 2F10415 Loading fixture).

    3. Remove the flange from the front flange of the Fan Case.

    4. Remove the bolt, the force gage and the IAE 1R18908 Guide plug V2500-A1 1 off from the curvic coupling of the LP Stub Shaft.

    22. SUBTASK 72-00-50-420-256 Remove the Length Gage from the Engine

    1. Refer to Figure.

    2. Remove the IAE 2F10418 Length gage 1 off from the engine.

    3. Disassemble the front shaft and the rear shaft of the IAE 2F10418 Length gage.

    23. SUBTASK 72-00-50-420-257 Install the Adjusting Ring to the LP Turbine Shaft

    1. Remove the old adjusting ring from the LP Turbine Shaft and install the new adjusting ring. Use the IAE 1J12282 Expanding pliers 1 off.

    2. Make sure that the new adjusting ring is correctly fitted on the adjusting ring location.

    24. SUBTASK 72-00-50-420-258 Prepare the Engine for the Installation of the LP Turbine Module

      1. Install IAE 1J12281 0AM53 heater 1 off to the stub shaft front flange as follows: Refer to Figure.

      1. Install the IAE 1J12281 0AM53 heater to the front flange of the LP Turbine Stub Shaft.

      2. Align the four holes in the guide of the IAE 1J12281 0AM53 heater with the four slots in the flange of the LP Stub Shaft.

      3. Safety the guide of the IAE 1J12281 0AM53 heater to the LP Stub Shaft with the four pins.

      4. Safety the four pins to the guide with the four screws.

    2. Install the guide ring A1 (part of IAE 1J12280 Guide bar) on to the lock nut at the rear flange of the Stage 2 Turbine Disk. Refer to Figure.

      3. Install the IAE 1J12280 Guide bar 1 off.

      1. Connect the two IAE 1J12280 Guide bar (parts of the IAE 1J12280 Guide bar).

      2. Install the connected IAE 1J12280 Guide bar with the conical end through the guide ring A1.

      3. Make sure that the conical end of the IAE 1J12280 Guide bar is correctly engaged in to the IAE 1J12281 0AM53 heater.

    25. SUBTASK 72-00-50-420-259 Remove the LP Turbine Module from the Horizontal Stand

    1. Refer to Figure.

    2. Attach the two IAE 1F10052 Two cables sling 1 off to the front spool of the IAE 1F10058 Handling fixture 1 off which is installed at the LP Turbine Module.

    3. Loosen the nut of the eye bolt (part of the IAE 1F10080 Horizontal stand 1 off).

    4. Loosen the ring nut A. Turn the ring nut A to the end position.

    5. Loosen the ring nut B from the rear end of the support.

    6. Disengage the eye bolt. Turn the block in open position.

    7. Loosen and remove the 28 hex head cap screws which attach the LP Turbine Module to the rear support of the IAE 1F10080 Horizontal stand.

    8. Move the LP Turbine Module carefully to get it free from the IAE 1F10080 Horizontal stand. Lift the LP Turbine Module from the IAE 1F10080 Horizontal stand.

    9. Loosen the ring nut C and remove the shaft (part of the IAE 1F10080 Horizontal stand) from the LP Turbine Shaft.

    10. Install the shaft to the front support of the IAE 1F10080 Horizontal stand. Close the block and safety with the eye bolt and the nut.

    11. Lift the LP Turbine Module to the same level as the IAE 1J12280 Guide bar installed in the engine before. Connect the LP Turbine Shaft front end to the IAE 1J12280 Guide bar.

    26. SUBTASK 72-00-50-420-260 Remove the Guide Ring A1

    1. Refer to Figure.

    2. Remove the guide ring A1 and install the guide ring A3 (part of the IAE 1J12280 Guide bar 1 off) to the lock nut at the rear flange of the Stage 2 Turbine Disk.

    27. SUBTASK 72-00-50-420-261 Install the LP Turbine Module

    2. Move the LP Turbine Module forward until the LP Turbine Shaft is installed 1.6 ft (0.5 m) in to the engine.

    3. Remove the guide ring A3 and install the guide ring A2 (part of the IAE 1J12280 Guide bar 1 off) to the lock nut at the rear flange of the Stage 2 Turbine Disk. Refer to Figure.

    4. Continue to move the LP Turbine Module forward in to the engine. Move it forward until the front flange of the LP Turbine Case is approximately 20 in. (500 mm) behind the rear flange of the HP Turbine Case.

    5. Push the IAE 1J12281 0AM53 heater 1 off backwards, until it is against the stop position. Increase the temperature of the spline area of the LP Stub Shaft to the temperature of 275 deg F to 329 deg F (135 deg C to 165 deg C). Use the IAE 6F10027 Heater control unit 1 off.

    6. During this time remove the IAE 1M14127 Support plate 2 off from the LP Turbine Case front flange and the LP Turbine Shaft. Refer to Figure.

    7. Remove the guide ring A2 from the lock nut at the rear flange of the Stage 2 Turbine Disk.

      8. Pull the IAE 1J12281 0AM53 heater forwards. Move the LP Turbine Module in to the engine, until the LP Turbine Case front flange touches the HP Turbine Case rear flange. Refer to Figure.

      1. Make sure that the locating pin at the HP Turbine Case rear flange aligns with the locating pin hole at the LP Turbine Case front flange.

      10. Remove the IAE 1J12281 0AM53 heater from the LP Stub Shaft front mounting flange.

      1. Remove the four screws and the four pins from the guide of the IAE 1J12281 0AM53 heater.

      2. Disengage the guide of the IAE 1J12281 0AM53 heater from the four slots in the flange of the LP Stub Shaft.

    11. Remove the IAE 1J12280 Guide bar from the LP Turbine Shaft Front End.

      12. Install the IAE 1J12220 Hydraulic pusher/puller 1 off to the front flange of the LP Stub Shaft as follows: Refer to Figure.

        1. Install the inner subassembly of the IAE 1J12220 Hydraulic pusher/puller (which has the spanner, the plunger and the nut) in to the inner threaded hole of the LP Turbine Shaft.

        1. Turn the inner subassembly clockwise fully.

        2. NOTE

          The procedure in Step makes the release of the inner subassembly from the LP Turbine Shaft in Step easy.

          Hold the LP Turbine Shaft rear end and turn the inner subassembly counter clockwise by one turn to loosen it.

      2. NOTE

        Make sure that the hydraulic connection of the hydraulic cylinder is at the opposite side of the cylinder.

        Attach the outer subassembly of the IAE 1J12220 Hydraulic pusher/puller (which has the guide, the cylinder and hydraulic cylinder) to the front flange of the LP Stub Shaft. The four flanges of the guide must be in line with the scallops of the LP Stub Shaft.

      3. Turn the guide until the holes in its stoppers are in line with the slots in the front flange of the LP Stub Shaft. Put the four pins in the holes in the flanges of the guide. Safety the pins to the guide with the four screws.

      4. Install the nut D and the set screw and tighten the set screw to hold the plunger.

      5. Install the stud bolt through the hydraulic cylinder in to the nut C. Hold the stud bolt with a wrench and tighten the nut A.

      6. Loosen the set screw.

    13. Install the IAE 1F10026 Hydraulic hand pump 1 off to the hydraulic connection of the IAE 1J12220 Hydraulic pusher/puller.

    14. Install 6 work bolts and nuts through the LP Turbine front flange boltholes in opposite positioned pairs.

      NOTE

      The bolt heads and nuts must be identified by a red paint mark.

    15. Pull the LP Turbine Module in correct position. Tighten the work nut pairs at the HP/LP Turbine Flanges in opposite sequence. Apply equal force all around the flange to pull them together. In the same time operate the IAE 1F10026 Hydraulic hand pump stepwise to connect the LP Turbine Shaft with the LP Stub Shaft.

      NOTE

      Tighten the work nuts, and operate the IAE 1F10026 Hydraulic hand pump at the same time to prevent overloading of the IAE 1F10058 Handling fixture.

    16. If the HP/LP Turbine Flanges are together, loosen the two nuts which secure the IAE 1F10063 Expanding retainer 1 off to the IAE 1F10058 Handling fixture 1 off.

    17. CAUTION

      DO NOT SUPPLY THE HYDRAULIC PUSHER/PULLER WITH MORE THAN 5000 PSI (345 BAR) PRESSURE. TOO MUCH HYDRAULIC PRESSURE CAN CAUSE DAMAGE TO THE HYDRAULIC PUSHER/PULLER.

      Operate the IAE 1F10026 Hydraulic hand pump to make sure that the LP Turbine Shaft and the LP Stub Shaft are correctly engaged.

      19. Remove the IAE 1J12220 Hydraulic pusher/puller from the LP Stub Shaft as follows: Refer to Figure.

      1. Tighten the set screw.

      2. Loosen the nut A which secures the stud bolt to the hydraulic cylinder. Remove the stud bolt.

      3. Remove the set screw and the nut D.

      4. Loosen and remove the four screws which safety the pins to the guide of the IAE 1J12220 Hydraulic pusher/puller 1 off.

      5. Remove the four pins which safety the guide to the flange of the LP Stub Shaft.

      6. Remove the outer subassembly from the front flange of the LP Stub Shaft.

      7. Remove the inner subassembly from the inner thread of the LP Turbine Shaft.

      20. Install the turbine shaft front lock nut on to the front of the LP Turbine Shaft. Refer to Figure.

      1. NOTE

        If the LP Compressor Disk and fan blades are installed, do Step. and continue then with Step.

        NOTE

        If the LP Compressor Disk and fan blades are not installed, do Step. alternatively to Step.

        Install the front lock nut (01-140) to the LP Turbine Shaft.

      2. Install the support B (part of the IAE 1J12260 Spanner wrench 1 off) to the retaining ring of the LP Compressor Disk. Attach the support B with the four bolts. Refer to Figure.

      3. Install the support A (part of the IAE 1J12260 Spanner wrench) to the curvic coupling of the LP Stub Shaft. Attach the support A with the four bolts. Refer to Figure.

      4. Install the drive bar and the drive coupling of the IAE 1J12260 Spanner wrench through the support. Engage the outside spanner teeth of the wrench on to the front lock nut of the LP Turbine Shaft.

      5. Install the rod and the nut of the IAE 1J12260 Spanner wrench to the inner thread of the LP Turbine Shaft.

      6. CAUTION

        MAKE SURE THAT THE IMMOBILIZER IS FULLY ENGAGED WITH THE LOCK NUT TEETH BEFORE YOU TORQUE THE FRONT LOCK NUT.

      7. Carefully install the immobilizer in to the drive bar until a yellow line goes out of view.

      8. NOTE

        The immobilizer is correctly installed against the lock nut if the yellow line can not be seen.

      9. Install the center thumb nut on to the rod to safety the immobilizer.

      11. Install the spring, the anchor plate and the clamp disk on to the immobilizer and safety with the two thumb nuts.

      21. Torque the front lock nut of the LP Turbine Shaft as follows:

      1. Install the front lock nut finger tight.

      2. Apply initial tightening torque of 3150 lbfft to 3250 lbfft (4271 Nm to 4407 Nm).

      3. Loosen the front lock nut.

      4. Install the front lock nut finger tight.

      5. Apply initial tightening torque of 950 lbfft to 1050 lbfft (1288 Nm to 1424 Nm).

      6. Put an angle of turn of 26 degrees to the front lock nut.

      7. CAUTION

        DO NOT TURN THE FRONT LOCK NUT MORE THAN 3250 LBFFT (4407 NM). DAMAGE TO THE PARTS OR TOOLS CAN OCCUR.

        Apply additional turn on the front lock nut to align the slots of the nut with the slots of the LP Turbine Shaft. The maximum angle of turn is two degrees.

      22. Remove the tools as follows:

      1. Release the two thumb nuts and remove the clamp disk, the anchor plate and the spring.

      3. Release the center thumb nut from the rod and remove the immobilizer from the center of the drive bar.

      4. Release the nut from the inner thread of the LP Turbine Shaft and remove the rod.

      5. Remove the drive bar and the drive coupling assembly.

      6. Remove the support A or the support B.

    23. Safety the front lock nut of the LP Turbine Shaft with the locking cap and the Internal Retaining Ring ENGINE-LP TURBINE SHAFT (72-50-41, 01-100). Refer to Figure.

    24. Remove the red marked work bolts and nuts from the HP/LP Turbine Flange.

      25. Install the seven brackets and attach the 100 bolts and nuts which lock the LP Turbine Case to the HP Turbine Case. Refer to Figure.

      1. CAUTION

        HOLD THE BOLTS IN THEIR POSITION IF YOU INSTALL THE NUTS ON TO THE BOLTS. DO NOT TURN THE BOLTS OR MAKE TO-AND-FRO MOVEMENTS. THE LP TURBINE CASE/HP TURBINE CASE FLANGE AND/OR THE BOLTS CAN BE DAMAGED.

        Torque the 84 nuts installed on the bolts which have their heads located on the HP Turbine Flange from 180.0 lbfin to 220.0 lbfin (20.0 Nm to 25.0 Nm).

      2. Torque the 16 bolts which have their heads located on the LP Turbine Flange from 180.0 lbfin to 220.0 lbfin (20.0 Nm to 25.0 Nm) and safety the bolts with CoMat 01-119 POTASSIUM CHROMATE K2CrO4 lockwire.

    28. SUBTASK 72-00-50-420-262 Remove the Handling Fixture from the LP Turbine Module

    1. Refer to Figure.

    2. Turn the knob clockwise to disengage the clamps of the IAE 1F10063 Expanding retainer 1 off.

    3. Release the nut and turn it rearwards to the end position.

    4. Loosen and remove the 13 screws which attach the IAE 1F10058 Handling fixture 1 off to the rear flange of the TEC.

    6. Turn the handwheel of the IAE 1F10084 Support fixture 1 off clockwise to disengage the support from the LP Turbine Shaft.

    7. Release the IAE 1F10084 Support fixture from the inner rear flange of the TEC. Remove the IAE 1F10084 Support fixture cover and the IAE 1F10063 Expanding retainer from the LP Turbine Module.

    29. SUBTASK 72-00-50-420-392 Install the No. 5 Bearing Nozzle

    1. Refer to Figure.

    2. Install three new packings NO.5 BEARING OIL JET AND FILTER (72-58-02, 01-040) and the No. 5 Bearing Packing Transfer Tube in to the No. 5 Bearing Nozzle.

    3. Install a new packing NO.5 BEARING OIL JET AND FILTER (72-58-02, 01-080) on to the bearing nozzle.

    4. Install the bearing nozzle in to the No. 5 Bearing Compartment.

    5. Attach the bearing nozzle with the two bolts.

    6. Torque the bolts to 85 lbfin to 105 lbfin (9.60 Nm to 11.86 Nm).

    7. Install the two washers and the two bolts to attach the transfer tube to the bearing nozzle.

    8. Torque the bolts to 85 lbfin to 105 lbfin (9.60 Nm to 11.86 Nm).

    30. SUBTASK 72-00-50-420-263 Install the Loading Fixture and Inspection Bridge to the LP Turbine Module

    1. Install the IAE 2F10415 Loading fixture 1 off on to the front flange of the Fan Case. Refer to Step and Figure.

    2. Install the IAE 2R18871 Inspection bridge 1 off to the rear flange of the Turbine Exhaust Case.

    3. Attach the IAE 2R18871 Inspection bridge with four nuts and bolts.

    4. Push the LP Turbine rearwards from the front of the engine.

    31. SUBTASK 72-00-50-420-264 Measure the Dimension P After the Installation of the LP Turbine Module

      NOTE

      Load must be applied in rearward direction.

    1. Load the LP Turbine Module with 900 lbf (4.0 kN).

    2. Use a suitable Vernier depth gage to measure the dimension P (actual). Refer to Figure.

      DIM.P to be within 13.7988 in. to 13.8421 in. (350.49 mm to 351.59 mm).

    3. Release the load from the LP Turbine Module.

    32. SUBTASK 72-00-50-420-265 Remove the Loading Fixture and the Inspection Bridge from the LP Turbine Module

    1. Remove the IAE 2F10415 Loading fixture 1 off from the front flange of the Fan Case. Refer to Step and Figure.

    2. Remove the IAE 2R18871 Inspection bridge 1 off from the rear flange of the Turbine Exhaust Case.

    33. SUBTASK 72-00-50-420-266-B00 Install the Blind Cap to the LP Turbine Shaft (SBE 72-0037 and Pre SBE 72-0027)

      SBE 72-0037: Replacement of the LP Turbine Shaft Rear End Sealing Ring

    1. Refer to Fig. 72-00-50-990-014 , Figure, Figure, Figure, and Figure.

    2. NOTE

      Use of IAE 1J12259 Seal slider without IAE 1J12243 Sizing sleeve is not permitted.

      3. Extend the sealing ring and install it to the blind cap as follows. Refer to Figure.

      1. Put the blind cap ENGINE-LP TURBINE SHAFT (72-50-41, 01-150) with the rear end down on to a work bench.

      2. Install the IAE 1J12259 Seal slider 1 off on the blind cap.

      3. Lubricate the new ENGINE-LP TURBINE SHAFT (72-50-41, 01-160) sealing ring with CoMat 10-077 APPROVED ENGINE OILS.

      4. Lubricate the outer diameter faces of the IAE 1J12259 Seal slider and the blind cap with CoMat 10-077 APPROVED ENGINE OILS.

      5. Put the sealing ring on the IAE 1J12259 Seal slider. The open side of the sealing ring must be in down direction.

      6. CAUTION

        MOVE THE SEALING RING SMOOTHLY AND EQUALLY OVER THE ALL CIRCUMFERENCE, IF NOT SO, THE SEALING RING IS EXTENDED LOCALLY. LOCAL EXTENSION CAN CAUSE DAMAGE TO THE SEALING RING.

        Push the sealing ring down with four or more fingers until it is installed in to the groove of the blind cap.

      7. Remove the IAE 1J12259 Seal slider from the blind cap.

      4. CAUTION

        DO NOT INSTALL THE BLIND CAP AND THE SEALING RING IN TO THE LP TURBINE SHAFT BEFORE B.(6). THE SEALING RING DIAMETER IS EXTENDED. THE LP TURBINE SHAFT BORE CAN CAUSE DAMAGE TO THE EXTENDED SEALING RING.

        Make the sealing ring diameter smaller as follows. Refer to Figure.

      1. Put the IAE 1J12243 Sizing sleeve 1 off with the front end down on to the work bench.

      2. Lubricate the inner diameter face of the IAE 1J12243 Sizing sleeve and the outer diameter of the sealing ring with CoMat 10-077 APPROVED ENGINE OILS.

      3. Put the blind cap in to the IAE 1J12243 Sizing sleeve. Diaphragm of the blind cap must be in down direction. Refer to Figure position A.

      4. Slowly push down the blind cap until it touches the work bench. Refer to Figure position B.

      5. Keep the blind cap in the IAE 1J12243 Sizing sleeve for ten or more minutes.

      6. Remove the IAE 1J12243 Sizing sleeve from the blind cap.

      5. Examine the sealing ring.

      1. Make sure that there is no damage on the surface.

      2. CAUTION

        DO NOT CORRECT TWISTED CONDITION OF THE SEALING RING. DISCARD THE TWISTED SEALING RING.

        Make sure that the sealing ring is not twisted. Refer to Figure.

    6. Install the blind cap to the LP Turbine Shaft. Use the IAE 1J12221 Impact hammer 1 off.

      NOTE

      For fits and clearances refer to TASK 72-00-50-420-003-C00 (INSTALLATION-004, CONFIG-003),

    7. Install the Internal Retaining Ring ENGINE-LP TURBINE SHAFT (72-50-41, 01-100). Refer to Figure.

    34. SUBTASK 72-00-50-420-266-D00 Install the Blind Cap to the LP Turbine Shaft (SBE 72-0227)

      SBE 72-0227: Provide a new blind cap with decreased seal land height

    1. Refer to Figure, Figure, Figure, and Figure.

      2. Install the new ENGINE-LP TURBINE SHAFT (72-50-41, 01-160) sealing ring to the blind cap ENGINE-LP TURBINE SHAFT (72-50-41, 01-150) as follows, refer to Figure:

      1. Put the blind cap with the rear end down on to the work bench.

      2. Install the IAE 1J12522 Seal slider 1 off on the blind cap.

      3. Lubricate the sealing ring with CoMat 10-077 APPROVED ENGINE OILS.

      4. Lubricate the outer diameter face of the IAE 1J12522 Seal slider and the blind cap with CoMat 10-077 APPROVED ENGINE OILS.

      5. Put the sealing ring on the IAE 1J12522 Seal slider. The open side of the sealing ring must be in up direction.

      6. CAUTION

        MOVE THE SEALING RING SMOOTHLY AND EQUALLY OVER ALL THE CIRCUMFERENCE. IF NOT SO, THE SEALING RING IS EXTENDED LOCALLY, LOCAL EXTENSION CAN CAUSE DAMAGE TO THE SEALING RING.

        Put the sealing ring down with four or more fingers until it is installed in to the groove of the blind cap.

      7. Remove the IAE 1J12522 Seal slider from the blind cap.

      3. Examine the sealing ring.

      1. Make sure that there is no damage on the surface.

      2. CAUTION

        DO NOT CORRECT TWISTED CONDITION OF THE SEALING RING. DISCARD THE TWISTED SEALING RING.

        Make sure that the sealing ring is not twisted. Refer to Figure.

    4. Install the blind cap on to the LP Turbine Shaft. Use the IAE 1J12221 Impact hammer 1 off.

    5. CAUTION

      DO NOT USE THE INTERNAL RETAINING RING P/N RR295 WITH THE BLIND CAP P/N 5A1703.

      Install the Internal Retaining Ring ENGINE-LP TURBINE SHAFT (72-50-41, 01-100). Refer to Figure.

    35. SUBTASK 72-00-50-420-267 Install the No. 5 Bearing Compartment Cover

    1. Refer to Figure.

    2. Install a new packing ENGINE-NO.5 BEARING COMPARTMENT COVER (72-58-01, 20-160) on to the No. 5 Bearing Compartment Cover ENGINE-NO.5 BEARING COMPARTMENT COVER (72-58-01, 20-120).

    3. Install the No. 5 bearing compartment cover on to the Turbine Exhaust Case.

      4. Do a leak check of the compartment cover and oil tubes.

      1. WARNING

        IF YOU DO NOT SECURE THE COMPARTMENT COVER DURING THE LEAK TEST THERE IS A RISK OF PERSONAL INJURY FROM THE RELEASED COVER.

        Install 13 work bolts to the compartment cover. Tighten the bolts.

      2. Install the IAE 1P17523 Blank-off Plate 1 off to the No. 5 Bearing Outer Oil Feed Tube. Refer to Figure.

      3. Install the IAE 1P16354 Vacuum Test Adapter 1 off to the No. 5 Bearing Oil Scavenge Tube Outlet with three bolts (part of the IAE 1P16354 Vacuum Test Adapter). Tighten the bolts. Refer to Figure.

      5. Control the air pressure to the IAE 1P16354 Vacuum Test Adapter to 10 PSI (68.95 kPa).

      6. Apply CoMat 10-045 LEAK CHECK FLUID, BUBBLES-TYPE or CoMat 10-045 LEAK CHECK FLUID, BUBBLES-TYPE around the cover and oil tube interfaces to check for leaks. Replace the seal of any leaking interface with a new seal.

      7. Do the leak test again.

      8. Remove the 13 work bolts.

    5. Install the No.5 Bearing Shields ENGINE-NO.5 BEARING COMPARTMENT COVER (72-58-01, 20-100) and ENGINE-NO.5 BEARING COMPARTMENT COVER (72-58-01, 20-080) on to the cover. Align the boltholes.

    6. Treat threads and underside of head of the bolts with CoMat 10-129 ANTI-SEIZE PASTE at assembly.

    7. Install the 13 bolts. Torque the bolts to 62 lbfin to 72 lbfin (7.006 Nmto 8.136 Nm). Wipe off excess paste.

    36. SUBTASK 72-00-50-420-268 Install the Adapter and the Plate to the Turbine Exhaust Case

      1. Install the IAE 1P16354 Vacuum Test Adapter 1 off to No. 5 Bearing Outer Oil Scavenge Tube, Figure.

      1. Make sure that the IAE 1P16354 Vacuum Test Adapter has no damage.

      2. Lubricate the bolts, nuts and washers with CoMat 10-077 APPROVED ENGINE OILS.

      3. Attach the IAE 1P16354 Vacuum Test Adapter to No. 5 Bearing Outer Oil Scavenge Tube and safety with 4 bolts. Torque the bolts to 85 lbfin to 105 lbfin (9.604 Nm to 11.863 Nm).

      2. Install the IAE 1P17523 Blank-off Plate 1 off to No. 5 Bearing Outer Oil Feed Tube, Figure.

      1. Make sure that the IAE 1P17523 Blank-off Plate has no damage.

      2. Lubricate the bolts, nuts and washers with CoMat 10-077 APPROVED ENGINE OILS.

      3. Attach the IAE 1P17523 Blank-off Plate to No. 5 Bearing Outer Oil Feed and safety with 3 bolts. Torque the bolts to 85 lbfin to 105 lbfin (9.60 Nm to 11.86 Nm).

    37. SUBTASK 72-00-50-420-269 Do an Evacuation Check for the No. 5 Bearing Compartment

    1. Refer to Figure.

    2. Connect the hose of IAE 6F10030 Vacuum test cart 1 off to the nipple of the IAE 1P16354 Vacuum Test Adapter 1 off. Refer to Figure.

    3. Attach the cart vacuum gage hose to the plug of the IAE 1P16354 Vacuum Test Adapter.

      NOTE

      Refer to the manufacturer's manual for the operation of the IAE 6F10030 Vacuum test cart.

    4. Set the air pressure at the test port to -20inHg (-508 mmHg gage). Based on the ambient pressure, refer to the table below for the vacuum pressure in psia.

      Ambient pressure of the Day (psia)

      Vacuum Pressure (psia)

      14.7

      4.9

      14.5

      4.7

      14.3

      4.5

      14.1

      4.3

      13.9

      4.1

      13.7

      3.9

      13.5

      3.7

      13.3

      3.5

      13.1

      3.3

      Vacuum pressure (psia) = Ambient pressure of the day (psia) - 9.8 psia

    5. Read the airflow indicated by the rotor meters on the IAE 6F10030 Vacuum test cart.

    6. Record the indicated airflow.

    7. If the indication is more than 10 PPH (4.536 kg per hour) reject the module.

    8. Stop the vacuum pump.

    38. SUBTASK 72-00-50-420-270 Remove the Vacuum Test Cart, the Adapter and the Plate

    1. Disconnect the hoses of the IAE 6F10030 Vacuum test cart from the adapter. Refer to Figure.

    2. Remove the plate and the adapter. Refer to Figure and Figure.

    39. SUBTASK 72-00-50-420-271 Install the Module Dressings

    1. Install the Module Dressings. Refer to TASK 72-00-50-420-005 (INSTALLATION-007).

    40. SUBTASK 72-00-50-420-272 Install the Inlet Cone

    1. Install the Inlet Cone. Refer to TASK 72-38-11-420-001 (INSTALLATION-001).

    41. Figure: Fits and Clearances at Interface D-45 and D-50/10

    Fits and Clearances at Interface D-45 and D-50/10

    Figure: Fits and Clearances at Interface F-32 and F-50

    Fits and Clearances at Interface F-32 and F-50

    Figure: Attachment of the Handling Fixture and the Expanding Retainer

    Attachment of the Handling Fixture and the Expanding Retainer

    Figure: Installation of the Heater and the Guide Bar

    Installation of the Heater and the Guide Bar

    Figure: Installation of the Guide Rings

    Installation of the Guide Rings

    Figure: Calculate the Adjusting Ring Thickness

    Sheet 1

    Legend
    Calculate the Adjusting Ring Thickness

    Sheet 1

    Close

    Figure: Calculate the Adjusting Ring Thickness

    Sheet 2

    Legend
    Calculate the Adjusting Ring Thickness

    Sheet 2

    Close

    Figure: Calculate the Adjusting Ring Thickness

    Sheet 3

    Legend
    Calculate the Adjusting Ring Thickness

    Sheet 3

    Close

    Figure: Calculate the Adjusting Ring Thickness

    Sheet 4

    Legend
    Calculate the Adjusting Ring Thickness

    Sheet 4

    Close

    Figure: Calculate the Adjusting Ring Thickness

    Sheet 5

    Legend
    Calculate the Adjusting Ring Thickness

    Sheet 5

    Close

    Figure: Example of a Component Dimension Record Sheet

    Sheet 1

    Legend
    Example of a Component Dimension Record Sheet

    Sheet 1

    Close

    Figure: Example of a Component Dimension Record Sheet

    Sheet 2

    Legend
    Example of a Component Dimension Record Sheet

    Sheet 2

    Close

    Figure: Example of a Component Dimension Record Sheet

    Sheet 3

    Legend
    Example of a Component Dimension Record Sheet

    Sheet 3

    Close

    Figure: Example of a Component Dimension Record Sheet

    Sheet 4

    Legend
    Example of a Component Dimension Record Sheet

    Sheet 4

    Close

    Figure: Connect the LP Shaft Front End with the LP Stub Shaft

    Connect the LP Shaft Front End with the LP Stub Shaft

    Figure: Install the LP Turbine Shaft Front Lock Nut

    Sheet 1

    Legend
    Install the LP Turbine Shaft Front Lock Nut

    Sheet 1

    Close

    Figure: Install the LP Turbine Shaft Front Lock Nut

    Sheet 2

    Legend
    Install the LP Turbine Shaft Front Lock Nut

    Sheet 2

    Close

    Figure: Safety the Front Lock Nut of the LP Turbine Shaft

    Safety the Front Lock Nut of the LP Turbine Shaft

    Figure: Removal of the Support Plate

    Removal of the Support Plate

    Figure: Pre SBE 75-0013 Installation of the Bolts and the Brackets at the LP Turbine Module Front Flange

    Sheet 1

    Legend
    Pre SBE 75-0013 Installation of the Bolts and the Brackets at the LP Turbine Module Front Flange

    Sheet 1

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    Figure: Pre SBE 75-0013 Installation of the Bolts and the Brackets at the LP Turbine Module Front Flange

    Sheet 2

    Legend
    Pre SBE 75-0013 Installation of the Bolts and the Brackets at the LP Turbine Module Front Flange

    Sheet 2

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    Figure: SBE 75-0013 Installation of the Bolts and the Brackets at the LP Turbine Module Front Flange

    Sheet 3

    Legend
    SBE 75-0013 Installation of the Bolts and the Brackets at the LP Turbine Module Front Flange

    Sheet 3

    Close

    Figure: SBE 75-0013 Installation of the Bolts and the Brackets at the LP Turbine Module Front Flange

    Sheet 4

    Legend
    SBE 75-0013 Installation of the Bolts and the Brackets at the LP Turbine Module Front Flange

    Sheet 4

    Close

    Figure: Installation of the No.5 Bearing Compartment Cover

    Installation of the No.5 Bearing Compartment Cover

    Figure: Install the Blind Cap

    Install the Blind Cap

    Figure: Remove the LP Turbine Module from the Horizontal Stand

    Sheet 1

    Legend
    Remove the LP Turbine Module from the Horizontal Stand

    Sheet 1

    Close

    Figure: Remove the LP Turbine Module from the Horizontal Stand

    Sheet 2

    Legend
    Remove the LP Turbine Module from the Horizontal Stand

    Sheet 2

    Close

    Figure: Installation of the Adapter to No.5 Bearing Outer Oil Scavenge Tube

    Installation of the Adapter to No.5 Bearing Outer Oil Scavenge Tube

    Figure: Installation of the Plate to No.5 Bearing Outer Oil Feed Tube

    Installation of the Plate to No.5 Bearing Outer Oil Feed Tube

    Figure: Connect the Fitting of the Vacuum Test Cart to the Adapter

    Connect the Fitting of the Vacuum Test Cart to the Adapter

    Figure: Install/Remove the Loading Fixture

    Install/Remove the Loading Fixture

    Figure: SBE 72-0037 and Pre SBE 72-0227: Installation of the Sealing Ring on to the Blind Cap

    Sheet 1

    Legend
    SBE 72-0037 and Pre SBE 72-0227: Installation of the Sealing Ring on to the Blind Cap

    Sheet 1

    Close

    Figure: SBE 72-0227: Installation of the Sealing Ring on to the Blind Cap

    Sheet 2

    Legend
    SBE 72-0227: Installation of the Sealing Ring on to the Blind Cap

    Sheet 2

    Close

    Figure: Installation of the Sealing Ring on to the Blind Cap - Method 2

    Sheet 3

    Legend
    Installation of the Sealing Ring on to the Blind Cap - Method 2

    Sheet 3

    Close

    Figure: SBE 72-0037 and Pre SBE 72-0227: Installation of the Sealing Ring in to the Sizing Sleeve

    SBE 72-0037 and Pre SBE 72-0227: Installation of the Sealing Ring in to the Sizing Sleeve

    Figure: SBE 72-0037: Installed Condition of the Sealing Ring

    SBE 72-0037: Installed Condition of the Sealing Ring

    Figure: Example of Incorrect Installation of the Sealing Ring onto the Blind Cap

    Example of Incorrect Installation of the Sealing Ring onto the Blind Cap

    Figure: SBE 72-0037: Installation of Blind Cap and Retaining Ring

    SBE 72-0037: Installation of Blind Cap and Retaining Ring

    Figure: Install the No.5 Bearing Nozzle

    Install the No.5 Bearing Nozzle

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Revised fits and clearance values and added subtask. (13VC121)

Link not Found
Manufacturer Code:03530
Enterprise Name:AMERICAN GAS AND CHEMICAL CO LTD
BU Name:AMERICAN GAS AND CHEMICAL CO LTD
Street:220 PEGASUS AVE
City:NORTHVALE
State:NJ
Zip Code:07647
Country:USA
Phone Number:1-201-767-7300, 1-800-526-1008
Fax Number:1-201-767-1741
Internet:www.amgas.com
Manufacturer Code:0AM53
Enterprise Name:IAE INTERNATIONAL AERO ENGINES AG
BU Name:NULL
Building:SUITE 400
Street:628 HEBRON AVENUE
City:GLASTONBURY
State:CT
Zip Code:06033
Country:USA
Manufacturer Code:34568
Enterprise Name:TIODIZE CO., INC.
BU Name:TIODIZE CO., INC.
Street:5858 ENGINEER DRIVE
City:HUNTINGTON BEACH
State:CA
Zip Code:92649
Country:USA
Phone Number:1-714-898-4377
Fax Number:1-714-891-7467
Internet:www.tiodize.com
Manufacturer Code:K6835
Enterprise Name:MED-LAB LTD
BU Name:MED-LAB LTD
Street:COPELAND ST
City:DERBY
Zip Code:DE1 2PU
Country:GREAT BRITAIN
Phone Number:44-1332-349094
Fax Number:44-1332-371237
Email:sales@med-lab.co.uk
Internet:www.med-lab.co.uk
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Link not Found
Link not Found
Manufacturer Code:U1185
Supply Number:CoMat 01-119
Type:sp01
Supply Short Name:CoMat 01-119 POTASSIUM CHROMATE K2CrO4
Supply Name:CoMat 01-119 POTASSIUM CHROMATE K2CrO4
Specification Groups:
Doc NumberType
OMAT:1/128 (RR REF)GPR
Suppliers:
ManufacturerRemarks
U1185
K6835
24853
LOCAL
Manufacturer Code:LOCAL
Supply Number:CoMat 02-119
Type:sp01
Supply Short Name:CoMat 02-119 LOCKWIRE
Supply Name:CoMat 02-119 LOCKWIRE
Specification Groups:
Doc NumberType
SAE AS9226 Part Number MS-9226-04 (0.032 IN DIA.)
Suppliers:
ManufacturerRemarks
LOCAL
51563
81343
V508V
Manufacturer Code:00BB6
Supply Number:CoMat 07-038
Type:sp01
Supply Short Name:CoMat 07-038 AIR DRYING ENAMEL
Supply Name:CoMat 07-038 AIR DRYING ENAMEL
Specification Groups:
Doc NumberType
OMAT:7/22B (RR REF)IP9138 R1
JCR-029 (JAEC REF)
Suppliers:
ManufacturerRemarks
00BB6
K3504
Manufacturer Code:03530
Supply Number:CoMat 10-045
Type:sp01
Supply Short Name:CoMat 10-045 LEAK CHECK FLUID, BUBBLES-TYPE
Supply Name:CoMat 10-045 LEAK CHECK FLUID, BUBBLES-TYPE
Specification Groups:
Doc NumberType
LEAK TEC 372E
Suppliers:
ManufacturerRemarks
03530
Manufacturer Code:02570
Supply Number:CoMat 10-045A
Type:sp01
Supply Short Name:CoMat 10-045A LEAK CHECK FLUID, BUBBLES-TYPE
Supply Name:CoMat 10-045A LEAK CHECK FLUID, BUBBLES-TYPE
Specification Groups:
Doc NumberType
SNOOP LIQUID LEAK DETECTOR
Suppliers:
ManufacturerRemarks
02570
U9113
Manufacturer Code:X333X
Supply Number:CoMat 10-077
Type:sp01
Supply Short Name:CoMat 10-077 APPROVED ENGINE OILS
Supply Name:CoMat 10-077 APPROVED ENGINE OILS
Specification Groups:
Doc NumberType
For V2500-A1/A5/D5 models - Refer to V2500 Service Bulletin ENG-79-0108
For V2500-E5 model - Refer to Service Bulletin E5-79-0001
Suppliers:
ManufacturerRemarks
X333X
Manufacturer Code:34568
Supply Number:CoMat 10-129
Type:sp01
Supply Short Name:CoMat 10-129 ANTI-SEIZE PASTE
Supply Name:CoMat 10-129 ANTI-SEIZE PASTE
Specification Groups:
Doc NumberType
TIODIZE T8E PASTE
Suppliers:
ManufacturerRemarks
34568
Manufacturer Code:LOCAL
Tool Number:Dial Gage
Tool Name:Dial Gage
Manufacturer Code:0AM53
Tool Number:IAE 1F10016
Tool Name:IAE 1F10016 Mechanical wrench
Manufacturer Code:0AM53
Tool Number:IAE 1F10026
Tool Name:IAE 1F10026 Hydraulic hand pump
Manufacturer Code:0AM53
Tool Number:IAE 1F10052
Tool Name:IAE 1F10052 Two cables sling
Manufacturer Code:0AM53
Tool Number:IAE 1F10058
Tool Name:IAE 1F10058 Handling fixture
Manufacturer Code:0AM53
Tool Number:IAE 1F10063
Tool Name:IAE 1F10063 Expanding retainer
Manufacturer Code:0AM53
Tool Number:IAE 1F10080
Tool Name:IAE 1F10080 Horizontal stand
Manufacturer Code:0AM53
Tool Number:IAE 1F10084
Tool Name:IAE 1F10084 Support fixture
Manufacturer Code:0AM53
Tool Number:IAE 1J12220
Tool Name:IAE 1J12220 Hydraulic pusher/puller
Manufacturer Code:0AM53
Tool Number:IAE 1J12221
Tool Name:IAE 1J12221 Impact hammer
Manufacturer Code:0AM53
Tool Number:IAE 1J12243
Tool Name:IAE 1J12243 Sizing sleeve
Manufacturer Code:0AM53
Tool Number:IAE 1J12259
Tool Name:IAE 1J12259 Seal slider
Manufacturer Code:0AM53
Tool Number:IAE 1J12260
Tool Name:IAE 1J12260 Spanner wrench
Manufacturer Code:0AM53
Tool Number:IAE 1J12279
Tool Name:IAE 1J12279 Grinding fixture
Manufacturer Code:0AM53
Tool Number:IAE 1J12280
Tool Name:IAE 1J12280 Guide bar
Manufacturer Code:0AM53
Tool Number:IAE 1J12281
Tool Name:IAE 1J12281 0AM53 heater
Manufacturer Code:0AM53
Tool Number:IAE 1J12282
Tool Name:IAE 1J12282 Expanding pliers
Manufacturer Code:0AM53
Tool Number:IAE 1J12522
Tool Name:IAE 1J12522 Seal slider
Manufacturer Code:0AM53
Tool Number:IAE 1M14127
Tool Name:IAE 1M14127 Support plate
Manufacturer Code:0AM53
Tool Number:IAE 1P16354
Tool Name:IAE 1P16354 Vacuum Test Adapter
Manufacturer Code:0AM53
Tool Number:IAE 1P16624
Tool Name:IAE 1P16624 Slide Puller
Manufacturer Code:0AM53
Tool Number:IAE 1P17523
Tool Name:IAE 1P17523 Blank-off Plate
Manufacturer Code:0AM53
Tool Number:IAE 1R18908
Tool Name:IAE 1R18908 Guide plug
Manufacturer Code:0AM53
Tool Number:IAE 2F10368
Tool Name:IAE 2F10368 Plate, Vacuum check
Manufacturer Code:0AM53
Tool Number:IAE 2F10415
Tool Name:IAE 2F10415 Loading fixture
Manufacturer Code:0AM53
Tool Number:IAE 2F10418
Tool Name:IAE 2F10418 Length gage
Manufacturer Code:0AM53
Tool Number:IAE 2R18871
Tool Name:IAE 2R18871 Inspection bridge
Manufacturer Code:0AM53
Tool Number:IAE 6F10027
Tool Name:IAE 6F10027 Heater control unit
Manufacturer Code:0AM53
Tool Number:IAE 6F10029
Tool Name:IAE 6F10029 Air flow test cart
Manufacturer Code:0AM53
Tool Number:IAE 6F10030
Tool Name:IAE 6F10030 Vacuum test cart
Manufacturer Code:LOCAL
Tool Number:Vernier depth gage
Tool Name:Vernier depth gage