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 71-00-02-000-027-B00 (A5-PPBU) - Remove The LP Compressor/Intermediate Case Brackets, Removal-027
General
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.
For all the parts identified in a different Chapter/Section/Subject, the applicable Chapter/Section/Subject comes before the Fig/item number.
Apply the approved CoMat 10-058 PENETRATING OIL before the removal of threaded parts. Let the parts soak before removal.
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.
Refer to Figure for details of the module flanges given in this procedure.
NOTE
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| ACR Torq-Set bit 212-1/4-ACR | LOCAL | Torq-Set |
Consumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 10-058 PENETRATING OIL | 0AM53 | CoMat 10-058 |
Spares
NONESafety Requirements
NONEProcedure
Remove the two bolts which attach the bracket Anti-Ice Ducts (30-21-49, 01-200) to the raft.
Remove the two bolts which attach the raft to the bracket Fan Harness Support Raceways (71-51-50, 01-880).
Remove the brackets at A.
Remove the four screws and the four nuts which attach the two brackets at the holes 6, 8 and 19, 20 with the ACR Torq-Set bit 212-1/4-ACR 1 off.
Remove the brackets at B and F.
Remove the four screws and the four nuts which attach the two brackets at the holes 10, 11 and 13, 14 with the ACR Torq-Set bit 212-1/4-ACR 1 off.
Remove the brackets at C and D.
Remove the two screws and the two nuts which attach the bracket at the holes 22 and 23 with the ACR Torq-Set bit 212-1/4-ACR 1 off.
Remove the bracket at G.
Remove the bracket AIR-STAGE 10 AIR SOLENOID VALVE (75-23-52, 01-500). Refer to TASK 72-00-32-020-005-B00, SUBTASK 72-00-32-020-147-A00 or SUBTASK 72-00-32-020-147-B00, the detail on G.
Remove the two bolts and the two nuts which attach the raft AIR-STAGE 10 AIR SOLENOID VALVE (75-23-52, 01-600) at the holes 51 and 52 on the flange FA1.
Remove the brackets at I.
Remove the two bolts which attach the raft to the bracket General Services Harness (71-51-43, 05-930).
Remove the brackets at L.
Remove the two bolts which attach the raft to the attachment angle OIL-SCAVENGE OIL TUBES-ENGINE (79-22-49, 14-880).
Remove the brackets at 0.
SUBTASK 71-00-02-020-011 Remove the Brackets at the Flange FA
SBE 71-0165: Remove the bracket at A1.
Pre SBE 72-0160: Remove the four bolts and the four nuts which attach the two brackets at the holes 124, 125 and 130, 131. Refer to the detail on V and X.
SBE 72-0160: Remove the five bolts and the five nuts which attach the four brackets at the holes 123, 124, 125 and 130, 131. Refer to the detail on V and X.
Remove the brackets at V, X, Y and Z.
SBE 71-0165: Remove the bracket at Z1.
SUBTASK 71-00-02-020-012 Remove the Brackets at the Flange FA1 (Pre SBE 72-0160, SBE 72-0160 and SBE 71-0165)
Pre SBE 79-0088 and SBE 79-0088: Remove the two bolts and the two nuts which attach the bracket at the holes 51 and 52. Refer to the detail on G.
Remove the brackets at G to K.
SUBTASK 71-00-02-020-013 Remove the Brackets at the Flange FE (Pre SBE 79-0088 and SBE 79-0088)
Figure: The LP Compressor/Intermediate Case Module Flanges
The LP Compressor/Intermediate Case Module Flanges

Figure: Remove the Brackets at the Flange FA
Sheet 1

Figure: Remove the Brackets at the Flange FA
Sheet 2

Figure: Remove the Brackets at the Flange FA
Sheet 3

Figure: Remove the Brackets at the Flange FA
Sheet 4

Figure: Remove the Brackets at the Flange FA
Sheet 5

Figure: Remove theBrackets at the Flange FA
Sheet 6

Figure: Remove the Brackets at the Flange FA
Sheet 7

Figure: Remove the Brackets at the Flange FA
Sheet 8

Figure: Remove the Brackets at the Flange FA
Sheet 9

Figure: Remove the Brackets at the Flange FA
Sheet 10

Figure: Remove the Brackets at the Flange FA1
Sheet 1

Figure: Remove the Brackets at the Flange FA1
Sheet 2

Figure: Remove the Brackets at the Flange FA1
Sheet 3

Figure: Remove the Brackets at the Flange FA1
Sheet 4

Figure: Remove the Brackets at the Flange FA1
Sheet 5

Figure: Remove the Brackets at the Flange FA1
Sheet 6

Figure: Remove the Brackets at the Flange FA1
Sheet 7

Figure: Remove the Brackets at the Flange FA1
Sheet 8

Figure: Remove the Brackets at the Flange FA1
Sheet 9

Figure: Remove the Brackets at the Flange FA1
Sheet 10

Figure: Remove the Brackets at the Flange FA1
Sheet 11

Figure: Remove the brackets at the Flange FA1
Sheet 12

Figure: Remove the Brackets at the Flange FA1
Sheet 13

Figure: Remove the Brackets at the Flange FA1
Sheet 14

Figure: Remove the Brackets at the Flange FA1
Sheet 15

Figure: Remove the Brackets at the Flange FE
Sheet 1

Figure: Remove the Brackets at the Flange FE
Sheet 2

Figure: Remove the Brackets at the Flange FE
Sheet 3

Figure: Remove the Brackets at the Flange FE
Sheet 4

Figure: Remove the Brackets at the Flange FE
Sheet 5

