TASK 72-00-00-100-001-B00 Engine General - Clean The Engine Gas Path For Performance Improvement, Cleaning-001

DMC:V2500-A5-72-00-0000-00B-251A-B|Issue No:003.00|Issue Date:2017-08-01

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-A5

Common Information

TASK 72-00-00-100-001-B00 Engine General - Clean The Engine Gas Path For Performance Improvement, Cleaning-001

General

This TASK gives the procedure to clean the engine gas path for improved performance.

Fig/item numbers in parentheses in the procedure agree with those used in the IPC.

NOTE

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

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
Potable water source at a pressure of 40 psi to 50 psi (275 kPa to 345 kPa).LOCALPotable water source - 40 psi to 50 psi (275 kPa to 345 kPa).

Refer to Potable Water Quality Specifications in SPM V2500-00-70-10-00-00A-250A-D.

Hoses and nozzles with a waterflow capacity of approximately 5 to 10 U.S. gallons (20 to 40 liters)LOCALHoses and nozzles - 5 to 10 U.S. gallons (20 to 40 liters)
Plugs or covers for the disconnectedtubesLOCALPlugs or covers for the disconnected tubes
Tank and PumpLOCALTank and Pump
IAE 4J12034 Water wash tube0AM53IAE 4J120341

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 01-007 ETHYL ALCOHOL C2H5OH (DENATURED)LOCALCoMat 01-007
CoMat 01-124 ISOPROPYL ALCOHOLLOCALCoMat 01-124

Spares

NONE

Safety Requirements

WARNING

IT IS THE RESPONSIBILITY OF THE OPERATOR TO OBTAIN AND OBSERVE THE MANUFACTURER'S MATERIAL SAFETY DATA SHEETS FOR CONSUMABLE MATERIALS. THESE CONTAIN INFORMATION SUCH AS, HAZARDOUS INGREDIENTS, PHYSICAL/CHEMICAL CHARACTERISTICS, FIRE, EXPLOSION, REACTIVITY, HEALTH HAZARD DATA, PRECAUTIONS FOR SAFE HANDLING, USE AND CONTROL MEASURES AND ALSO TO TAKE LOCAL REGULATIONS INTO CONSIDERATION.

Procedure

    1. SUBTASK 72-00-00-110-057 Makeup of Engine Gas Path Cleaning Solution

    2. Refer to SPM TASK 70-11-48-110-501 makeup of cleaning solutions for the makeup of Solution Code 181 Engine Gas Path Cleaning Solution.

    3. Water for engine gaspath cleaning must agree with the Potable Water Quality Specifications in SPM TASK 70-10-00-100-501.

    4. If the ambient temperature is 41.9 deg F (5.5 deg C) or less, use water mixed with CoMat 01-007 ETHYL ALCOHOL C2H5OH (DENATURED) or CoMat 01-124 ISOPROPYL ALCOHOL at the applicable ratio to prevent icing. Refer to Figure.

    1. SUBTASK 72-00-00-110-054 Clean the Engine Gas Path

    2. Refer to Figure, Figure, Figure and Figure.

    3. CAUTION

      DO NOT USE A DETERGENT WASH ON ENGINES WITH GAS PATHS THAT WERE EXPOSED TO DRY POWDER FIRE EXTINGUISHING AGENTS. THESE AGENTS ARE NOT WATER SOLUBLE. WATER WASHING WILL CAUSE THESE MATERIALS TO CAKE AND STICK ON ENGINE PARTS.

      CAUTION

      THE ENGINE EGT MUST BE BELOW 150 DEG F (65.6 DEG C) TO PREVENT ENGINE DAMAGE.

      Disconnect the PS3 sensing tube from the autostart probe. Install a plug. Refer to Figure.

    4. Disconnect the Air-to-P4.9 EEC tube at the fitting on the bottom of the turbine exhaust case. Install a plug. Refer to Figure.

    5. Disconnect the tenth stage cabin air bleed tube. Install a plug.

      1. Install the IAE 4J12034 Water wash tube 1 off.

        1. Install the IAE 4J12034 Water wash tube 1 off as follows. Refer to Figure.

        2. Put the two thicker wooden clamps on the front and aft sides of the No. 4 and No. 5 struts.

        3. Let the grooves in the clamps touch the strut edges and safety the clamps with the two long bolts and wing nuts.

        4. Put the tube between the No. 4 and No. 5 struts from the rear side in parallel to the engine center line, then let it go through between the fan exit guide vanes carefully so the tube does not touch the vanes.

        5. Set the square end of the tube to the aft clamps. Make sure that the front bent part of the tube does not touch the trailing edges of the fan blades. If necessary, install the spacer(s) between the aft clamps and the square end.

        6. Put the tube nozzle between the leading edges of the inlet guide vanes.

        7. Hold the tube with the thicker clamps and the thinner wooden clamps and safety them with the four short bolts and wing nuts.

        8. Connect a wash fluid supply hose to the tube.

        9. Make sure again that the front bent part of the tube does not touch the trailing edges of the fan blades, that the tube nozzle does not touch the inlet guide vanes and that the direction of the tube nozzle is at the correct angle.

        10. If necessary, use spacers to adjust the positions of the clamps and the angle of the tube correctly.

        11. Safety the clamps tightly with the wing nuts.

    6. Check the oil level on the oil tank and add oil to the engine oil tank if required.

    7. Pull the ignition circuit breaker to shut off the engine ignition system.

      1. Prepare 20 US gal to 30 US gal (80 l to 120 l) of Solution Code 181 Engine Gas Path Cleaning Solution. Refer to Step.

      2. If the ambient temperature is below 40 deg F (4.4 deg C), use the applicable potable water/alcohol mixture as an alternative to plain potable water in the solution to prevent ice. Refer to Step.

    8. Disconnect the variable stator vane actuator from the crankshaft and manually set the stator vanes to full open and fit rigging pin. Refer to TASK 72-00-40-050-001 (REMOVAL-011).

      1. Do the subsequent wash-and-soak procedure two times/cycles and let the engine soak for 10 minutes minimum between the wash-and-soak procedure cycles:

      2. Motor the engine with the starter until N2 is at 2000 RPM minimum.

      3. While you continue to motor the engineat N2 of 2000 RPM minimum, spray 10 gal to 15 gal (40 l to 60 l) of Solution Code 181 Engine Gas Path Cleaning Solution in two minutes into the low pressure compressor.

        1. Stop motoring the engine.

        2. Let the engine soak for 30 minutes minimum after each third wash-and-soak procedure cycle to let the starter become cool.

        3. Let the engine soak for 10 minutes minimum after all other wash-and-soak procedure cycles.

      1. If the solution that comes out of the tailpipe continues to look dirty, an added wash-and-soak procedure cycle will help to increase the benefit of the gas path wash. Operators are permitted to do the wash-and-soak procedure again at their discretion.

      2. Let the engine soak for 30 minutes minimum after each second (2nd) wash-and-soak procedure cycle to let the starter become cool.

      1. Exchange the detergent source for one that has a similar amount of potable water or potable water/alcohol mixture (refer to Step and see Figure). Do the subsequent rinse procedure two times/cycles and let the engine drain for 10 minutes minimum between the rinse procedure cycles:

      2. Motor the engine with the starter until a minimum of 2000 RPM is reached.

      3. While you motor the engine, spray 10 gal to 15 gal (40 l to 60 l) of the potable water or potable water/alcohol mixture in two minutes into the low pressure compressor.

      4. Stop motoring the engine.

      1. Use one of the procedures in the subsequent list to clean the LPC 1st Stage (fan) Blades:

        1. Aqueous Degreaser Solution Procedure.

        2. Clean the blades by SPM TASK 70-11-03-300-503 SUBTASK 70-11-03-300-002 Aqueous Spray or Wipe (with Rinsing) Method.

        1. Engine Gas Path Cleaner Solution Procedure.

        2. Clean the blades with Solution Code 181 Engine Gas Path Cleaning Solution and a clean cloth.

        3. Rinse the blades thoroughly with potable water.

    9. Motor the engine with the starter for approximately 30 seconds to remove water.

    10. Disconnect the P2.5 at the EEC and purge the line. Remove all the plugs and the rigging pin, purge and connect all the lines and connect the variable stator vane actuator control rod. Refer to TASK 72-00-40-450-001 (INSTALLATION-011).

      1. Set the ignition circuit breakers again and start the engine. Refer to 71-00-00-700-053-A01, 71-00-00-700-B01 (TESTING-000 CONFIG-001 and CONFIG-002) or 71-00-00-700-053-A02, 71-00-00-700-B02 (TESTING-000, CONFIG-001 and CONFIG-002). Operate the engine at a power setting that is sufficient to keep the oil temperature at a minimum of 220 deg F (104.5 deg C) for no less than 10 minutes. If the minimum oil temperature cannot be reached, it is necessary to do an oil check for water content.

      2. Take a 4 oz. (100 ml) sample of oil from the engine.

      3. Do a Karl Fisher ASTMD-1744 Water Analysis to find the water content of the oil.

      4. If the water content is above 800 parts per million (ppm) by weight or by volume, drain the engine oil system. Refer to TASK 71-00-00-600-003 (SERVICING-003). Fill the system with new oil. Refer to TASK 71-00-00-600-002 (SERVICING-002).

        .

  1. Figure: Alcohol and water mixture ratio

    Alcohol and water mixture ratio

    Figure: Remove the PS3 sense line air tube assembly

    Remove the PS3 sense line air tube assembly

    Figure: Remove the P4.9 air tube assembly

    Remove the P4.9 air tube assembly

    Figure: Install the IAE 4J12034 water wash tube

    Install the IAE 4J12034 water wash tube

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Revised the procedure. (16VC449)

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:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:LOCAL
Supply Number:CoMat 01-007
Type:sp01
Supply Short Name:CoMat 01-007 ETHYL ALCOHOL C2H5OH (DENATURED)
Supply Name:CoMat 01-007 ETHYL ALCOHOL C2H5OH (DENATURED)
Specification Groups:
Doc NumberType
PMC 9009 (PW REF)Reagent grade
MTH 133 (94%) (MTU REF)Reagent grade
Suppliers:
ManufacturerRemarks
LOCAL
K6835
IE441
24853
Manufacturer Code:LOCAL
Supply Number:CoMat 01-124
Type:sp01
Supply Short Name:CoMat 01-124 ISOPROPYL ALCOHOL
Supply Name:CoMat 01-124 ISOPROPYL ALCOHOL
Specification Groups:
Doc NumberType
OMAT:1/40GPR TECHNICAL GRADE
PMC 9094GPR TECHNICAL GRADE
JCR-011GPR TECHNICAL GRADE
Suppliers:
ManufacturerRemarks
LOCAL
U1185
24853
K6835
Link not Found
Manufacturer Code:0AM53
Tool Number:IAE 4J12034
Tool Name:IAE 4J12034 Water wash tube
Manufacturer Code:LOCAL
Tool Number:Plugs or covers for the disconnected tubes
Tool Name:Plugs or covers for the disconnectedtubes
Link not Found
Manufacturer Code:LOCAL
Tool Number:Tank and Pump
Tool Name:Tank and Pump