Removal of the ACT Pressurization Check Valve
TASK 28-28-38-000-001-A
Removal of the ACT Pressurization 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 28-28-38-860-050-A ** ON A/C NOT FOR ALL
Subtask 28-28-38-020-050-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.02 06:17:57 UTC
Removal of the ACT Pressurization Check Valve
WARNING:
BE CAREFUL NOT TO GET AIRCRAFT FUEL IN YOUR MOUTH OR IN YOUR EYES.
IF YOU GET FUEL ON YOUR SKIN OR ON YOUR CLOTHES, FLUSH IT IMMEDIATELY WITH WATER.
IF NECESSARY, GET MEDICAL HELP.
AIRCRAFT FUEL IS POISONOUS.
WARNING:
DO NOT GET YOUR CLOTHES SOAKED WITH FUEL.
WARNING:
MAKE SURE THAT YOU HAVE THE CORRECT FIRE FIGHTING EQUIPMENT AVAILABLE.
WARNING:
OBEY THE FUEL SAFETY PROCEDURES.
FIN: 178QM ** 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 | 1 | ACCESS PLATFORM 2M (6 FT) |
| No specific | AR | PLUG - BLANKING |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| No specific | 1 | WARNING NOTICE(S) |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 151BC |
| 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 24-41-00-861-002-A-02 | Energize the Aircraft Electrical Circuits from Engine 1(2) |
| TASK 25-55-11-000-002-A | Removal of the Ceiling Panels in the Aft Cargo-Compartment - FR47/FR59 |
| TASK 28-00-00-910-001-A | Fuel Safety Procedures |
| TASK 52-30-00-860-001-A | Open the FWD or Aft Cargo-Compartment Door with the Yellow Electric Pump |
Subtask 28-28-38-860-050-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
(1) Obey the fuel safety procedures (Ref. AMM TASK 28-00-00-910-001).
(2) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(3) Put a WARNING NOTICE(S) in position on the panels that follow:
Subtask 28-28-38-010-051-A ** ON A/C NOT FOR ALL (1) Obey the fuel safety procedures (Ref. AMM TASK 28-00-00-910-001).
(2) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(3) Put a WARNING NOTICE(S) in position on the panels that follow:
- Refuel/defuel panel 801VU
- Fuel panel 28VU and 40VU
to tell persons not to operate the refuel/defuel system.
B. Get Access
(1) Open the aft cargo-compartment door (Ref. AMM TASK 52-30-00-860-001).
(2) Put an ACCESS PLATFORM 2M (6 FT) in position at the opening of the aft cargo compartment.
(3) In the aft cargo compartment, remove cargo ceiling panel 151BC (Ref. AMM TASK 25-55-11-000-002).
Subtask 28-28-38-865-050-A ** ON A/C NOT FOR ALL (1) Open the aft cargo-compartment door (Ref. AMM TASK 52-30-00-860-001).
(2) Put an ACCESS PLATFORM 2M (6 FT) in position at the opening of the aft cargo compartment.
(3) In the aft cargo compartment, remove cargo ceiling panel 151BC (Ref. AMM TASK 25-55-11-000-002).
C. Open, safety and tag this(these) circuit breaker(s):
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 121VU | ACT1/REFUEL & SPLY | 33QU | L29 |
| 121VU | FUEL/HI/LVL/SPLY | 1QJ | L25 |
| 121VU | FUEL/RFL/DFL/SPLY | 2QU | L24 |
| 121VU | FUEL/RFL/DFL/XFR/DEFUEL/VALVE | 1QU | L23 |
| 121VU | ACT XFR VALVE MAN CTL | 30QH | N29 |
| 121VU | ACT1/CTL & SPLY | 9QH | P29 |
| 121VU | ACT PUMP SUPPLY | 25QH | Q29 |
Subtask 28-28-38-020-050-A ** ON A/C NOT FOR ALL
A. Removal of the ACT Pressurization Check-Valve
(1) Loosen the union nut (2) from the check valve (4) and remove the pipe (3).
(2) Loosen the union nut (5) of the check valve (4).
(3) Remove the check valve (4) from the T-pipe section (6).
(4) Put the PLUG-BLANKING in each disconnected line end.
(1) Loosen the union nut (2) from the check valve (4) and remove the pipe (3).
(2) Loosen the union nut (5) of the check valve (4).
(3) Remove the check valve (4) from the T-pipe section (6).
(4) Put the PLUG-BLANKING in each disconnected line end.
ACT Pressurization Check Valve