W DOC AIRBUS | AMM A320F

Removal of the Inlet Cowl T2-Probe Harness [PW11]


TASK 71-61-51-000-801-A
Removal of the Inlet Cowl T2-Probe Harness


WARNING: BE CAREFUL WHEN YOU DO WORK ON THE ENGINE AFTER SHUTDOWN. THE ENGINE CAN STAY HOT FOR A LONG TIME. IF YOU DO NOT OBEY THIS INSTRUCTION, INJURY CAN OCCUR.
FIN: 4110KS ** ON A/C NOT FOR ALL
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE
No specific
AR
COVER - PROTECTION
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
437AL, 438AR
FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
447AL, 448AR
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 71-00-00-860-832-A
Procedure to Prevent Engine Motoring and to Stop the Electrical Supply to the EEC
TASK 71-13-00-010-802-A
Opening of the Fan Cowl Doors
TASK 71-61-11-000-801-A
Removal of the Aft Bulkhead T2 Panel
TASK 71-61-12-000-801-A
Removal of the T2 Probe
3. Job Set-up
Subtask 71-61-51-941-050-A ** ON A/C NOT FOR ALL
A. Safety Precautions
   (1) Do the procedure to prevent engine motoring and to stop the electrical supply to the Electronic Engine Control (EEC)
(Ref. AMM TASK 71-00-00-860-832).
Subtask 71-61-51-010-050-A ** ON A/C NOT FOR ALL
B. Get Access
   (1) Open the fan cowl doors (Ref. AMM TASK 71-13-00-010-802):
     (a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
437AL 438AR
     (b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
447AL 448AR
   (2) Put an ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position.
   (3) Remove the aft bulkhead T2 panel (Ref. AMM TASK 71-61-11-000-801).
4. Procedure
Subtask 71-61-51-020-050-A ** ON A/C NOT FOR ALL
A. Removal of the Inlet Cowl T2-Probe Harness
   (1) Remove the inlet cowl T2-probe harness (3).
     (a) Disconnect the T2 jumper harness from the inlet cowl T2-probe harness (3) (D1001P) (Ref. AMM TASK 71-61-11-000-801).
     (b) Disconnect the inlet cowl T2-probe harness (3) (D1000P) from the T2-probe (Ref. AMM TASK 71-61-12-000-801).
     (c) Remove the four bolts (1) and the four washers (2) that attach the inlet cowl T2-probe harness (3) to the T2 disconnect panel.
     (d) Remove the bolt (4) and washer (5) that attach the clamp (6) and the inlet cowl T2-probe harness (3) to the T2 harness bracket.
     (e) Remove the inlet cowl T2-probe harness (3).
     (f) Remove the clamp (6) from the inlet cowl T2-probe harness (3).
     (g) Installation of the protection covers
CAUTION: INSTALL PROTECTION COVERS ON ALL THE OPENINGS IMMEDIATELY TO PREVENT DAMAGE TO THE ENGINE.
       1 Make sure that you install COVER - PROTECTION as necessary to prevent damage to the engine.
[Rev.10 from 2021] 2026.04.01 02:33:48 UTC