Removal of the Overpressure Protector Outlet
TASK 28-12-46-000-001-A
Removal of the Overpressure Protector Outlet
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 28-12-46-941-053-A
Subtask 28-12-46-020-051-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.02 07:01:33 UTC
Removal of the Overpressure Protector Outlet
WARNING:
PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU START A TASK ON OR NEAR:
1. Reason for the Job- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE |
| No specific | AR | SAFETY BARRIER(S) |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 540 | FUEL TANK |
| 640 | FUEL TANK |
| 540PB, 640PB |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 28-10-00-910-001-A | Safety Procedures When You Do Work in a Fuel Tank |
| TASK 28-10-00-910-002-A | Access to the Fuel Tanks and the Work Areas |
| TASK 28-25-00-650-001-A | Pressure Defuel |
| TASK 28-25-00-650-003-A | To Drain Remaining Fuel from the Wing Tanks and the Center Tank |
| TASK 28-25-00-650-003-A-01 | To Drain Remaining Fuel from the Wing Tanks and the Center Tank |
| TASK 57-55-11-000-004-A | Removal of the Flap Track Fairings Nos. 2, 3 and 4 |
Subtask 28-12-46-941-053-A
A. Safety Precautions
(2) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
Subtask 28-12-46-860-051-A ** ON A/C NOT FOR ALL WARNING:
BEFORE YOU DO WORK IN OR NEAR A FUEL TANK, MAKE SURE THAT YOU OBEY ALL THE SAFETY PROCEDURES. THIS WILL PREVENT INJURY TO PERSONS AND/OR DAMAGE TO THE AIRCRAFT.
(1) You must obey the fuel safety procedures when you do work in a fuel tank (Ref. AMM TASK 28-10-00-910-001) and (Ref. AMM TASK 28-10-00-910-002). (2) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
B. Aircraft Maintenance Configuration
(1) Defuel the applicable fuel tank (Ref. AMM TASK 28-25-00-650-001).
(2) Drain the remaining fuel from the applicable fuel tank (Ref. AMM TASK 28-25-00-650-003).
(3) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE below the applicable zone 540(640).
Subtask 28-12-46-860-051-B ** ON A/C NOT FOR ALL (1) Defuel the applicable fuel tank (Ref. AMM TASK 28-25-00-650-001).
(2) Drain the remaining fuel from the applicable fuel tank (Ref. AMM TASK 28-25-00-650-003).
(3) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE below the applicable zone 540(640).
B. Aircraft Maintenance Configuration
(1) Defuel the applicable fuel tank (Ref. AMM TASK 28-25-00-650-001).
(2) Drain the remaining fuel from the applicable fuel tank (Ref. AMM TASK 28-25-00-650-003).
4. Procedure(1) Defuel the applicable fuel tank (Ref. AMM TASK 28-25-00-650-001).
(2) Drain the remaining fuel from the applicable fuel tank (Ref. AMM TASK 28-25-00-650-003).
CAUTION:
WHEN YOU PUT THE ACCESS PLATFORM IN POSITION, BE CAREFUL NOT TO CAUSE DAMAGE TO THE VORTEX GENERATOR.
(3) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE below the applicable zone 540(640). Subtask 28-12-46-020-051-A ** ON A/C NOT FOR ALL
A. Removal of the Overpressure-Protector Outlet
(2) Remove the access panel 540HB (640HB).
(3) Put a protective cover around the pressure relief outlet (1).
Subtask 28-12-46-020-051-B ** ON A/C NOT FOR ALL CAUTION:
YOU MUST REMOVE AND INSTALL THE BOLTS IN THE SPECIFIED SEQUENCE. THIS WILL PREVENT DAMAGE TO THE ACCESS PANEL.
(1) Remove the bolts (4) in the sequence AB thru A. (2) Remove the access panel 540HB (640HB).
(3) Put a protective cover around the pressure relief outlet (1).
A. Removal of the Overpressure Protector Outlet
(1) Remove the forward and the aft fixed fairings from flap track No. 4 (Ref. AMM TASK 57-55-11-000-004).
(3) Remove access panel 540PB ( 640PB).
(4) Put a protective cover around the pressure relief outlet (1).
(1) Remove the forward and the aft fixed fairings from flap track No. 4 (Ref. AMM TASK 57-55-11-000-004).
CAUTION:
YOU MUST REMOVE AND INSTALL THE BOLTS IN THE SPECIFIED SEQUENCE. THIS WILL PREVENT DAMAGE TO THE ACCESS PANEL.
(2) Remove the bolts (4) in the sequence AF thru A. (3) Remove access panel 540PB ( 640PB).
(4) Put a protective cover around the pressure relief outlet (1).
Inner Cell Overpressure-Protector Outlet, 540HB(640HB)