Removal of the Environmental Control System (ECS) Harness
TASK 36-11-61-000-801-A
Removal of the Environmental Control System (ECS) Harness
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Work Zones and Access Panels
C. Referenced Information
3. Job Set-up
Subtask 36-11-61-861-050-A ** ON A/C NOT FOR ALL
Subtask 36-11-61-020-050-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 01:14:13 UTC
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.
1. Reason for the JobSelf 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) |
| 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 | |
| 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 |
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 (Ref. AMM TASK 24-41-00-861-002) or (Ref. AMM TASK 24-41-00-861-002).
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 (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.
C. Open, safety and tag this(these) circuit breaker(s):
Subtask 36-11-61-010-050-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | AIR BLEED/ENG 2/MONG | 3HA2 | D12 |
| 49VU | AIR BLEED/ENG 1/CTL | 2HA1 | D11 |
| 122VU | AIR BLEED/ENG 1/MONG | 3HA1 | Z23 |
| 122VU | AIR BLEED/ENG 2/CTL | 2HA2 | Z22 |
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 (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
E. Deactivation of the Thrust Reverser for Maintenance
Subtask 36-11-61-010-051-A ** ON A/C NOT FOR ALL 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). 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(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.
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:
(a) Make sure that the pressure and the temperature of the bleed-air duct system are in ambient conditions.
(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).
(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
(1) If you use the APU to energize the electrical circuits, stop the APU:
- For GTCP 36-300 APU (Ref. AMM D/O 49-00-00-86)
- For APS 3200 (Ref. AMM D/O 49-00-00-86)
- For 131-9(A) APU (Ref. AMM TASK 49-00-00-860-009).
(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.
Environmental Control System (ECS) Harness