Removal of the Intermediate Pressure (IP) Bleed Check Valve
TASK 36-11-41-000-040-A
Removal of the Intermediate Pressure (IP) Bleed Check Valve
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 36-11-41-861-053-A ** ON A/C NOT FOR ALL
Subtask 36-11-41-020-051-A ** ON A/C NOT FOR ALL
(a) Make sure that the pressure and the temperature of the bleed-air duct system are in ambient conditions.
(4) Remove the couplings (25), the E-seals (20) and the IP bleed check valve (30) from between the tee duct (10) and elbow duct (15).
(5) Put the PLUG-BLANKING in each disconnected line end.
(6) Keep the seals (20) for the installation procedure.
[Rev.10 from 2021]
2026.04.01 01:09:00 UTC
Removal of the Intermediate Pressure (IP) Bleed Check Valve
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 PARTS AFTER THE ENGINE SHUTDOWN. USE APPLICABLE THERMAL GLOVES. THE ENGINE PARTS CAN STAY HOT FOR ONE HOUR AFTER SHUTDOWN AND CAN BURN YOU.
FIN: 7110HM ** ON A/C NOT FOR ALL
1. Reason for the JobSelf explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | ACCESS PLATFORM 1M (3 FT)-ADJUSTABLE |
| No specific | AR | PLUG - BLANKING |
| No specific | AR | WARNING NOTICE(S) |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| FOR [1000EM1] (ENGINE-1) | |
| 437AL, 438AR, 451AL | |
| FOR [1000EM2] (ENGINE-2) | |
| 447AL, 448AR, 461AL | |
| 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 36-11-49-000-001-A | Removal of the Mid Stage Tee Duct |
| 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 71-13-00-010-040-A | Opening of the Fan Cowl Doors |
| TASK 78-30-00-481-041-A | Make the Thrust Reverser Unserviceable for Maintenance |
| TASK 78-36-00-010-040-A | Opening of the Thrust Reverser Doors |
Subtask 36-11-41-861-053-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 36-11-41-941-054-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) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.
(2) On the AIR COND panel 30VU:
Subtask 36-11-41-010-057-A ** ON A/C NOT FOR ALL (1) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.
(2) On the AIR COND panel 30VU:
- make sure that the ENG 1(2) BLEED pushbutton switch is released (the OFF legend is on),
- make sure that the APU BLEED pushbutton switch is released (the ON legend is off),
- put a WARNING NOTICE(S) to tell persons not to operate the pneumatic system.
- put a WARNING NOTICE(S) to tell persons not to start the engine 1(2).
- Put a WARNING NOTICE(S) to tell persons not to pressurize the pneumatic system.
- make sure that the ON legend of the ENG/FADEC GND PWR 1(2) pushbutton switch is off,
- put a WARNING NOTICE(S) to tell persons not to energize the FADEC 1(2).
C. Get Access
(1) Open the fan cowl doors (Ref. AMM TASK 71-13-00-010-040):
(a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
(b) FOR [1000EM2] (ENGINE-2)
447AL 448AR
(2) Put the ACCESS PLATFORM 1M (3 FT)-ADJUSTABLE in position below the engine.
Subtask 36-11-41-040-054-A ** ON A/C NOT FOR ALL Subtask 36-11-41-010-058-A ** ON A/C NOT FOR ALL (1) Open the fan cowl doors (Ref. AMM TASK 71-13-00-010-040):
(a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
(b) FOR [1000EM2] (ENGINE-2)
447AL 448AR
(2) Put the ACCESS PLATFORM 1M (3 FT)-ADJUSTABLE in position below the engine.
E. Open the left thrust reverser door (Ref. AMM TASK 78-36-00-010-040):
(1) FOR [1000EM1] (ENGINE-1)
451AL
(2) FOR [1000EM2] (ENGINE-2)
461AL
4. Procedure(1) FOR [1000EM1] (ENGINE-1)
451AL
(2) FOR [1000EM2] (ENGINE-2)
461AL
Subtask 36-11-41-020-051-A ** ON A/C NOT FOR ALL
CAUTION:
SOME PRESSURE CAN STAY IN THE DUCTING. THE PRESSURE WILL DECREASE WHEN YOU RELEASE THE CLAMPS.
A. Removal of the IP Bleed Check Valve NOTE: It may be necessary to remove the tee duct (10) in order to remove the IP bleed check valve (30). Remove the tee duct (10) only if it is very necessary (Ref. AMM TASK 36-11-49-000-001).
(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 APU (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).
(3) Remove the nuts (35), washers (40) and bolts (45) that attach the links (50) and (55) to the tee duct (10). (4) Remove the couplings (25), the E-seals (20) and the IP bleed check valve (30) from between the tee duct (10) and elbow duct (15).
(5) Put the PLUG-BLANKING in each disconnected line end.
(6) Keep the seals (20) for the installation procedure.
IP Bleed Check Valve