W DOC AIRBUS | AMM A320F

Removal of the Environmental Control System (ECS) Harness


TASK 36-11-61-000-801-A
Removal of the Environmental Control System (ECS) Harness


WARNING: MAKE SURE THAT THE PNEUMATIC SYSTEM IS DEPRESSURIZED BEFORE YOU START WORK. PRESSURIZED AIR CAN CAUSE INJURY TO PERSONNEL.
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.
WARNING: ALWAYS USE APPLICABLE GLOVES TO TOUCH HOT PARTS. HOT PARTS CAN CAUSE INJURY TO PERSONS.
WARNING: WEAR APPLICABLE PERSONAL PROTECTIVE EQUIPMENT (PPE) WHEN YOU DO THIS TASK. BEFORE YOU USE PPE, READ, UNDERSTAND AND OBEY ALL INSTRUCTIONS FOR ITS USE. THESE INSTRUCTIONS INCLUDE INSTRUCTIONS FROM THE MANUFACTURER, YOUR EMPLOYER AND GOVERNMENT REGULATIONS. YOU CAN GET INJURED IF YOU DO NOT USE PPE. GET INSTRUCTIONS FROM YOUR EMPLOYER ON WHICH PPE IS NECESSARY.
ZONE: 454
ZONE: 464
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 1M (3 FT)-ADJUSTABLE
No specific
AR
COVER - PROTECTION
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
WARNING NOTICE(S)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
454
HOT SECTION
464
HOT SECTION
191DB
FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
437AL, 438AR, 452AR
FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
447AL, 448AR, 462AR
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 24-41-00-861-002-A
Energize the Aircraft Electrical Circuits from the External Power
TASK 24-41-00-861-002-A-01
Energize the Aircraft Electrical Circuits from the APU
TASK 49-00-00-860-009-A
APU Shutdown by External Power (131-9(A))
TASK 49-00-00-860-009-A-01
APU Shutdown by Batteries (131-9(A))
TASK 71-00-00-860-833-A
Procedure to Prevent Engine Motoring
TASK 71-13-00-010-802-A
Opening of the Fan Cowl Doors
TASK 78-30-00-040-805-A
Deactivation of the Thrust Reverser System for Ground Maintenance
TASK 78-36-00-010-802-A
Opening of the Thrust Reverser Cowl-Doors
3. Job Set-up
Subtask 36-11-61-861-050-A ** ON A/C NOT FOR ALL
A. Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002) or (Ref. AMM TASK 24-41-00-861-002).
Subtask 36-11-61-941-050-A ** ON A/C NOT FOR ALL
B. Safety Precautions
   (1) On AIR COND panel 30VU:
     (a) Make sure that the ENG 1(2) BLEED pushbutton switch is released (OFF legend on).
     (b) Make sure that the APU BLEED pushbutton switch is released (ON legend off).
     (c) Put a WARNING NOTICE(S) in position to tell persons not to operate the pneumatic system.
   (2) Do the procedure to prevent engine motoring
(Ref. AMM TASK 71-00-00-860-833).
   (3) On the access door 191DB, on the HP ground connector:
     (a) Put a WARNING NOTICE(S) in position to tell persons not to pressurize the pneumatic system.
Subtask 36-11-61-865-050-A ** ON A/C NOT FOR ALL
C. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUAIR BLEED/ENG 2/MONG3HA2D12
49VUAIR BLEED/ENG 1/CTL2HA1D11
122VUAIR BLEED/ENG 1/MONG3HA1Z23
122VUAIR BLEED/ENG 2/CTL2HA2Z22
Subtask 36-11-61-010-050-A ** ON A/C NOT FOR ALL
D. 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
Subtask 36-11-61-040-050-A ** ON A/C NOT FOR ALL
E. Deactivation of the Thrust Reverser for Maintenance
WARNING: YOU MUST DEACTIVATE THE THRUST REVERSER BEFORE YOU DO WORK ON OR AROUND IT. IF YOU DO NOT, THE THRUST REVERSER CAN OPERATE ACCIDENTALLY AND CAUSE AN INJURY AND/OR DAMAGE.
   (1) Do the deactivation of the thrust reverser system for maintenance (Ref. AMM TASK 78-30-00-040-805).
Subtask 36-11-61-010-051-A ** ON A/C NOT FOR ALL
F. Get Access
   (1) Open the right thrust-reverser cowl-door (Ref. AMM TASK 78-36-00-010-802):
     (a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
452AR
     (b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
462AR
   (2) Put an ACCESS PLATFORM 1M (3 FT)-ADJUSTABLE in position below the fan cowl doors.
4. Procedure
Subtask 36-11-61-020-050-A ** ON A/C NOT FOR ALL
A. Removal of the Environmental Control System (ECS) Harness
   (1) If you use the APU to energize the electrical circuits, stop the APU:
   (2) In the cockpit, on the SD bleed page:
     (a) Make sure that the pressure and the temperature of the bleed-air duct system are in ambient conditions.
WARNING: MAKE SURE THAT THE PNEUMATIC SYSTEM IS DEPRESSURIZED BEFORE YOU START WORK. PRESSURIZED AIR CAN CAUSE INJURY TO PERSONNEL.
WARNING: DO NOT TOUCH THE UNIT UNTIL IT IS SUFFICIENTLY COOL TO PREVENT BURNS WHEN YOU DO THE MAINTENANCE TASK(S).
CAUTION: WIPE CLEAN ALL PARTS AND TOOLS AS NECESSARY TO REMOVE UNWANTED DEBRIS AND PREVENT DAMAGE TO THE ENGINE.
   (3) Disconnect the ECS harness (1) connector (450VC-A) from the pylon interface.
   (4) Disconnect the ECS harness (1) connector (4001HA-A) from the Pressure Regulating Valve (PRV).
   (5) Disconnect the ECS harness (1) connector (4000HA-A) from the High Pressure Valve (HPV).
   (6) Remove the bolt (11), two washers (12) and nut (13) that attach the clamp (14) and the ECS harness (1) to the IDG-EDP-MON and PW harnesses and the two clamps.
     (a) Remove the clamp (14) from the ECS harness (1).
NOTE: Do not remove the clamps from the IDG-EDP-MON and PW harnesses.
   (7) Attach the IDG-EDP-MON and PW harnesses and the two clamps back together.
   (8) Use the bolt (11), two washers (12) and nut (13).
   (9) Tighten the nut (13) finger-tight.
   (10) Remove the bolt (2) and washer (3) that attach the clamp (4) and the ECS harness (1) to the AOC support return fuel bracket.
     (a) Remove the clamp (4) from the ECS harness (1).
   (11) Remove the four bolts (5) and the four washers (6) that attach the four clamps (7) and the ECS harness (1) to the ECS duct brackets.
     (a) Remove the clamps (7) from the ECS harness (1).
   (12) Remove the bolt (8) and washer (9) that attach the clamp (10) and the ECS harness (1) to the ECS duct bracket.
     (a) Remove the clamp (10) from the ECS harness (1).
   (13) Remove the ECS harness (1) from the two spring clips on the electrical heatshield bracket assembly.
   (14) Remove the ECS harness (1) from the engine.
   (15) Installation of protection covers
CAUTION: INSTALL PROTECTION COVERS ON ALL THE OPENINGS IMMEDIATELY TO PREVENT DAMAGE TO THE ENGINE.
     (a) Make sure that you install COVER - PROTECTION if necessary to prevent damage to the engine.
[Rev.10 from 2021] 2026.04.01 12:38:41 UTC