Excessive Cabin Altitude associated with CAB PR SYS FAULT
TASK 21-31-00-810-827-A
Excessive Cabin Altitude associated with CAB PR SYS FAULT
1. Possible Causes
2. Job Set-up Information
A. Referenced Information
3. Fault Confirmation
Subtask 21-31-00-710-103-A
Subtask 21-31-00-810-162-A
[Rev.8 from Aug 2018]
2026.04.04 04:24:43 UTC
Excessive Cabin Altitude associated with CAB PR SYS FAULT
1. Possible Causes
2. Job Set-up Information
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| AMM 21-31-00-760-001 | Resistance Check of the Return Ground Connections - Cabin Pressure Controller (CPC) 1 (11HL) and 2 (12HL) and the Electronic Modules 10HL-1 and 10HL-2 |
| CMM 213121 | |
| AMM 21-31-34-000-001 | Removal of the Cabin Pressure Controller |
| AMM 21-31-34-400-001 | Installation of the Cabin Pressure Controller |
| AMM 21-31-51-000-001 | Removal of the Outflow Valve (From Inside) |
| AMM 21-31-51-000-006 | Removal of the Outflow Valve (From Outside) |
| AMM 21-31-51-400-001 | Installation of the Outflow Valve (From Inside) |
| AMM 21-31-51-400-006 | Installation of the Outflow Valve (From Outside) |
Subtask 21-31-00-710-103-A
A. Do a read out of the POST FLIGHT REPORT.
4. Fault IsolationSubtask 21-31-00-810-162-A
A. If the POST FLIGHT REPORT gives the ECAM warnings CAB PR EXCESS CAB ALT together with CAB PR SYS 1 FAULT or CAB PR SYS 2 FAULT,
(1) Make a print out of:
AMM 21-31-34-000-001 and,
AMM 21-31-34-400-001.
(a) If possible do a print out of the NON-VOLATILE MEMORY read-out CMM 213121.
AMM 21-31-51-000-001 and,
AMM 21-31-51-400-001 or,
AMM 21-31-51-000-006 and,
AMM 21-31-51-400-006.
(1) Make a print out of:
- the POST FLIGHT REPORT,
- the CPC1 and CPC2 LAST LEG REPORTS and PREVIOUS LEG REPORTS and,
- if available the ECS REPORT 19.
AMM 21-31-34-000-001 and,
AMM 21-31-34-400-001.
(a) If possible do a print out of the NON-VOLATILE MEMORY read-out CMM 213121.
NOTE: It is recommended to:
(3) Replace the OUTFLOW VALVE [10HL] - advise Airbus Industrie in case excessive cabin altitude is experienced and,
- provide Airbus Industrie with the information provided by the reports and read-out from work steps (1) and (2)(a).
AMM 21-31-51-000-001 and,
AMM 21-31-51-400-001 or,
AMM 21-31-51-000-006 and,
AMM 21-31-51-400-006.
NOTE: It is recommended that the removed outflow valve and controllers should be returned to the vendor for a detailed examination.
(4) Do the resistance check of the ground wiring AMM 21-31-00-760-001.