Manual System Activation Fault
TASK 35-23-00-810-805-A
Manual System Activation Fault
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 35-23-00-710-058-A 4. Fault Isolation
Subtask 35-23-00-810-057-A
Subtask 35-23-00-860-054-A
[Rev.8 from Aug 2018]
2026.04.04 04:33:39 UTC
Manual System Activation Fault
1. Possible Causes
PUSHBUTTON SW-OXYGEN/MAN ON (14WR) - wiring
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| AMM 35-23-00-710-001 | Operational Check of Manual Mask Release |
| ASM 352301 |
Subtask 35-23-00-710-058-A 4. Fault Isolation
Subtask 35-23-00-810-057-A
A. If the test confirms the fault:
(a) Do a check and repair the wiring if necessary between:
Subtask 35-23-00-710-059-A - Do a check of the
PUSHBUTTON SW-OXYGEN/MAN ON (14WR) and replace it if necessary ASM 352301.
(a) Do a check and repair the wiring if necessary between:
- PB SW (14WR) pin 8 and CB (7WR)
- PB SW (14WR) pin 7 and RELAY (25WR) connector A/B2
- PB SW (14WR) pin 6 and CB (6WR)
- PB SW (14WR) pin 5 and RELAY (25WR) connector A/B1
- PB SW (14WR) pin 4 and CB (3WR)
- PB SW (14WR) pin 3 and RELAY (25WR) connector A/A1
- PB SW (14WR) pin 2 and CB (4WR)
- PB SW (14WR) pin 1 and RELAY (25WR) connector A/A2,
ASM 352301.
B. Do the test as given in the Para. 3.A.
5. Close-upSubtask 35-23-00-860-054-A
A. Put the aircraft back to its initial configuration.