Removal of the Safety Valve
TASK 21-31-52-000-001-A
Removal of the Safety 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 21-31-52-861-051-A Subtask 21-31-52-865-050-A
Subtask 21-31-52-020-053-A
[Rev.10 from 2021]
2026.04.02 06:11:16 UTC
Removal of the Safety Valve
WARNING:
MAKE SURE THAT AIR IS NOT SUPPLIED TO THE AIR CONDITIONING SYSTEM FROM THE MAIN ENGINE, THE APU OR A GROUND SOURCE.
HOT COMPRESSED AIR CAN CAUSE INJURY TO PERSONNEL.
NOTE: The procedure is the same for the safety valves 6HL (7HL).
1. Reason for the JobSelf explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | CAP - BLANKING |
| No specific | AR | PLUG - BLANKING |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 811 |
| 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 52-41-00-010-002-A | Open the Avionics Compartment Doors for Access |
Subtask 21-31-52-861-051-A Subtask 21-31-52-865-050-A
B. Open, safety and tag this(these) circuit breaker(s):
Subtask 21-31-52-010-051-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 49VU | AIR COND/CAB/PRESS/CTL1 | 1HL | D09 |
| 122VU | AIR COND/CAB PRESS/CTL/2 | 2HL | Y22 |
C. Open the forward avionics access door 811 (Ref. AMM TASK 52-41-00-010-002)
(2) Remove the access panel (1).
4. ProcedureWARNING:
OPEN THE ACCESS DOOR AND MAKE SURE IT STAYS OPEN.
ATTACH A WARNING NOTICE TO THE ACCESS DOOR TO TELL PERSONS NOT TO CLOSE IT.
THIS IS TO PREVENT ACCIDENTAL PRESSURIZATION OF THE AIRCRAFT BY THE AIR CONDITIONING SYSTEM IF ALL THE OTHER CABIN OPENINGS ARE CLOSED.
PRESSURIZATION OF THE AIRCRAFT CAN BE DANGEROUS.
IT CAN CAUSE A DOOR TO OPEN WITH EXPLOSIVE FORCE WHICH CAN CAUSE INJURY AND/OR DAMAGE.
(1) Remove the food trolleys from the Aft galley. (2) Remove the access panel (1).
Subtask 21-31-52-020-053-A
A. Removal of the Safety Valve
(1) If installed remove the safety wire from the electrical connector (2).
(2) Disconnect the electrical connector (2).
(3) Put the CAP-BLANKING on each disconnected electrical connector and receptacle.
(4) Remove the nut (8), the washer (7), the screw (5) and disconnect the bonding strap (6).
(5) Disconnect the ambient-pressure sense line (4).
(6) Put the PLUG-BLANKING in each disconnected line end.
(7) Hold the safety valve (3) and remove the clamp (9).
(8) Remove the safety valve (3) and the O-ring (10).
(9) Put blanking caps on the open ends of the safety valve (3) and the mounting flange (11).
(1) If installed remove the safety wire from the electrical connector (2).
(2) Disconnect the electrical connector (2).
(3) Put the CAP-BLANKING on each disconnected electrical connector and receptacle.
(4) Remove the nut (8), the washer (7), the screw (5) and disconnect the bonding strap (6).
(5) Disconnect the ambient-pressure sense line (4).
(6) Put the PLUG-BLANKING in each disconnected line end.
(7) Hold the safety valve (3) and remove the clamp (9).
(8) Remove the safety valve (3) and the O-ring (10).
(9) Put blanking caps on the open ends of the safety valve (3) and the mounting flange (11).
Safety Valves 6HL (7HL)