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 72-00-40-020-007-B00 HP System Module - Remove The HP System Module (Vertical), Removal-009
General
This TASK gives the procedure to remove the HP system module in the vertical position. Other related TASKS are:
TASK 72-00-40-560-005 Turn the LP compressor/intermediate case module and the HP system module from the horizontal to the vertical.
Fig/item numbers in parentheses in the procedure agree with those used in the EIPC. Only the primary Fig/item numbers are used. For the service bulletin alpha variants refer to the EIPC.
Apply the approved CoMat 10-058 PENETRATING OIL before the removal of threaded parts or parts with an interference fit. Let the parts soak before removal.
NOTE
NOTE
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| IAE 1F10052 Two cables sling | 0AM53 | IAE 1F10052 | 1 | |
| IAE 1P16046 Removal/Installation fixture | 0AM53 | IAE 1P16046 | 1 | |
| IAE 1P16285 Tie-rod adapter | 0AM53 | IAE 1P16285 | 1 | |
| IAE 1P16543 Removal/Installation fixture | 0AM53 | IAE 1P16543 | 1 | |
| IAE 1R18075 Support pedestal | 0AM53 | IAE 1R18075 | 1 | |
| IAE 1R18090 Safety support stand | 0AM53 | IAE 1R18090 | 1 | |
| IAE 1R18214 Build stand | 0AM53 | IAE 1R18214 | 1 | |
| IAE 1R18222 Support rod | 0AM53 | IAE 1R18222 | 2 | |
| IAE 1R18230 Wrench | 0AM53 | IAE 1R18230 | 1 | |
| IAE 1R18234 Support rod | 0AM53 | IAE 1R18234 | 3 | |
| IAE 1R18247 Rigging pin | 0AM53 | IAE 1R18247 | 1 | |
| IAE 1R18673 Dummy stub shaft | 0AM53 | IAE 1R18673 | 1 |
Consumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 01-002 SOLVENT, DELETED. | LOCAL | CoMat 01-002 | ||
| CoMat 10-058 PENETRATING OIL | LOCAL | CoMat 10-058 | ||
| CoMat 04-005 JOINTING COMPOUND, MEDIUM GRADE | LOCAL | CoMat 04-005 |
Spares
NONESafety Requirements
NONEProcedure
Refer to Figure.
Attach a hoist to the IAE 1F10052 Two cables sling 1 off and attach the lift sling to the remove/install fixture lift eye.
Attach IAE 1P16285 Tie-rod adapter 1 off onto the center ring (part of IAE 1P16046 Removal/Installation fixture or IAE 1P16543 Removal/Installation fixture 1 off).
SUBTASK 72-00-40-020-155 Install the Remove/Install Fixture and the Tie-Rod Adapter to the HP System Module Rear Flange
Refer to Figure.
Install IAE 1R18247 Rigging pin 1 off through the bracket and into the HP compressor cases to lock the variable stator vanes.
Install IAE 1R18234 Support rod 3 off.
SUBTASK 72-00-40-020-156 Install the HP Compressor Support Rods
Refer to Figure.
Use IAE 1R18230 Wrench 1 off to release and remove the curvic bolts from the No.3 bearing rotor center.
SUBTASK 72-00-40-020-157 Remove the Bolts from the HP Compressor Stage 3 Disk Curvic Coupling
Refer to Figure.
SUBTASK 72-00-40-020-216 Remove the Parts that Attach the LP Compressor/Intermediate Case Module and the HP System Module Joint Flanges (SBE 72-0290)
Refer to Figure.
SUBTASK 72-00-40-020-158 Remove the Parts that Attach the LP Compressor/Intermediate Case Module and the HP System Module Joint Flanges (Pre SBE 72-0290)
Refer to Figure.
SUBTASK 72-00-40-020-159 Remove the HP System Module from the LP Compressor/Intermediate Case Module
Refer to Figure.
Lower the HP system module onto IAE 1R18090 Safety support stand 1 off. The HP compressor front flange should touch the safety support stand pads. Do not release the lift sling hold.
SUBTASK 72-00-40-020-160 Prepare the HP System Module for Interface Inspection
Visually examine the HP system module and the LP compressor/intermediate case module at interfaces C-32 and C-41. Refer to TASK 72-00-00-200-002.
SUBTASK 72-00-40-220-106 Visually Examine the Interfaces
Refer to Figure.
Install the IAE 1R18673 Dummy stub shaft 1 off into the IAE 1R18673 Dummy stub shaft 1 off. Make sure the curvic protector is at the rear.

WARNING
WHEN YOU USE COMAT 01-002 INHIBITED AND STABILIZED TRICHLOROETHANE YOU MUST USE THE NECESSARY PROTECTIVE CLOTHING. DO NOT GET THE SOLVENT ON YOUR SKIN OR IN YOUR EYES. YOU MUST NOT SMOKE WHEN YOU USE THE SOLVENT AS THE VAPOR CHANGES AND BECOMES TOXIC.Use a soft brush and apply CoMat 01-002 SOLVENT, DELETED. to the curvic teeth.
Clean the curvic teeth on the dummy stub shaft and the HP compressor stage 3 disk.
SUBTASK 72-00-40-020-161 Install the Dummy Stub Shaft onto the HP System Module
Refer to Figure.
Install IAE 1R18222 Support rod 2 off onto the IAE 1R18214 Build stand 1 off.
SUBTASK 72-00-40-020-162 Install the HP System Module onto the Build Stand
Put a thin layer of CoMat 04-005 JOINTING COMPOUND, MEDIUM GRADE onto the bracket where it touches the blank.
Install one of the blanks HP COMPRESSOR SPLIT CASE (72-41-31, 01-120), the bracket HP COMPRESSOR SPLIT CASE (72-41-31, 01-118) and two of the bolts HP COMPRESSOR SPLIT CASE (72-41-31, 01-122) into the HP compressor at location C.
Put a thin layer of CoMat 04-005 JOINTING COMPOUND, MEDIUM GRADE on the bracket where it touches the blank.
Install one of the blanks HP COMPRESSOR SPLIT CASE (72-41-31, 01-120), the bracket HP COMPRESSOR SPLIT CASE (72-41-31, 01-115) and two of the bolts HP COMPRESSOR SPLIT CASE (72-41-31, 01-122) in the HP compressor at location A.
Install the other blank HP COMPRESSOR SPLIT CASE (72-41-31, 01-120) and the other bolts HP COMPRESSOR SPLIT CASE (72-41-31, 01-122) into the HP compressor at location B. Torque the bolts to 85 lbfin to 105 lbf.in (10 Nm to 12 Nm).
Remove the rigging pin installed in Step.
Remove the support rods.
SUBTASK 72-00-40-020-163 Remove the Hoist, the Remove/Install Fixture, the Tie-Rod Adapter and the HP Compressor Support Rods
Figure: Install the remove/install fixture and the tie-rod adapter onto the HP system module
Install the remove/install fixture and the tie-rod adapter onto the HP system module

Figure: Install the remove/install fixture and the tie-rod adapter to the HP system module
Install the remove/install fixture and the tie-rod adapter to the HP system module

Figure: Install the support rods into the HP compressor
Install the support rods into the HP compressor

Figure: Install the support rods into the HP compressor
Install the support rods into the HP compressor

Figure: Remove the stage 3 HP compressor curvic bolts
Remove the stage 3 HP compressor curvic bolts

Figure: LP compressor/intermediate case module to HP system module joint flange hole positions
LP compressor/intermediate case module to HP system module joint flange hole positions

Figure: Install the HP system module onto the safety support stand
Install the HP system module onto the safety support stand

Figure: Install the dummy stub shaft onto the stage 3 disk curvic coupling
Install the dummy stub shaft onto the stage 3 disk curvic coupling

Figure: Install the HP compressor/diffuser case assembly onto the build stand
Install the HP compressor/diffuser case assembly onto the build stand

