Pack 1 and Pack 2 Flow Indication Fault
TASK 21-51-00-810-827-A
Pack 1 and Pack 2 Flow Indication Fault
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 21-51-00-860-080-A
Subtask 21-51-00-810-109-A ** ON A/C NOT FOR ALL
Subtask 21-51-00-860-083-A ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:24:49 UTC
Pack 1 and Pack 2 Flow Indication Fault
1. Possible Causes
- PRESS CONT 1 [11HL]
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| TSM TASK 21-51-00-810-807-A | FCV 1 (FCU 1) Regulation/Indication Fault |
| TSM TASK 21-51-00-810-813-A | Pack 1 Flow Indication Fault |
| TSM TASK 21-51-00-810-814-A | Pack 2 Flow Indication Fault |
| AMM 12-33-21-618-001 | Pre-conditioning through the LP Ground Connection |
| 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 71-00-00-710-003 | Engine Automatic Start |
| AMM 71-00-00-710-028 | Engine Shutdown |
Subtask 21-51-00-860-080-A
A. Bleed Air Supply Source from the HP Ground Connection
(2) On the AIR COND panel 30VU:
Subtask 21-51-00-860-081-A ** ON A/C NOT FOR ALL Subtask 21-51-00-860-082-A NOTE: The HP ground supply source must be able to give a pack inlet pressure of 24 PSI minimum. If it can not do this then you must get the bleed air supply from the engines.
The work steps which follow show the conditions necessary before you get the minimum pack-inlet pressure.
(1) Do the pre-conditioning through the HP ground connection AMM 12-33-21-618-001. The work steps which follow show the conditions necessary before you get the minimum pack-inlet pressure.
(2) On the AIR COND panel 30VU:
- push the HOT AIR pushbutton switch to the on position (the OFF legend goes off),
- turn the COCKPIT, FWD CABIN and the AFT CABIN temperature selectors to the HOT positions and,
- make sure that the PACK 1 and the PACK 2 pushbutton switches are in the on position (the OFF legends are off).
- make sure that the pack 1 inlet pressure indication shows a minimum of 24 PSI.
- make sure that the pack 2 inlet pressure indication shows a minimum of 24 PSI.
NOTE: If the indication shows less than 24 PSI you must:
- increase the ground pressure supply until the indication shows a minimum of 24 PSI.
C. Initial Test Set-up with Engines as Bleed Air Source Supply
(1) On the AIR COND panel 30VU:
Subtask 21-51-00-710-089-A (1) On the AIR COND panel 30VU:
- push the HOT AIR pushbutton switch to the on position (the OFF legend goes off),
- turn the COCKPIT, FWD CABIN and the AFT CABIN temperature selectors to the HOT positions and,
- make sure that the PACK 1 and the PACK 2 pushbutton switches are in the on position (the OFF legends are off).
- make sure that the pack 1 inlet pressure indication shows a minimum of 24 PSI.
- make sure that the pack 2 inlet pressure indication shows a minimum of 24 PSI.
NOTE: If the indication shows less than 24 PSI you must slowly adjust the throttle levers until you get the minimum indication of 24 PSI.
D. Test
4. Fault Isolation| ACTION | RESULT |
|---|---|
1.On the AIR COND panel 30VU:
| On the ECAM BLEED page:
|
2.On the AIR COND panel 30VU:
| On the AIR COND panel 30VU:
|
| | On the ECAM BLEED page:
|
3.On the AIR COND panel 30VU:
| On the AIR COND panel 30VU:
|
4.On the AIR COND panel 30VU:
| On the AIR COND panel 30VU:
|
| | On the ECAM BLEED page:
|
5.On the AIR COND panel 30VU:
| On the AIR COND panel 30VU:
|
6.On the AIR COND panel 30VU:
| On the ECAM BLEED page:
|
7.On the AIR COND panel 30VU:
| On the ECAM BLEED page:
|
Subtask 21-51-00-810-109-A ** ON A/C NOT FOR ALL
A. If the pack 1 and pack 2 flow indicator is stuck in the high position and aircraft is located at high altitude airport.
(1) Do the test of the actual pack flow values (Ref. TSM TASK 21-51-00-810-807).
(2) If the test of the pack flow values is OK and does not agree with the flow indication parameters, no other maintenance action is necessary.
Subtask 21-51-00-810-108-A (1) Do the test of the actual pack flow values (Ref. TSM TASK 21-51-00-810-807).
(2) If the test of the pack flow values is OK and does not agree with the flow indication parameters, no other maintenance action is necessary.
NOTE: This is normal system behaviour when aircraft is located at high altitude airport.
B. If the pack 1 and pack 2 flow indicator is stuck in the high or low position:
(1) replace the PRESS CONT 1 [11HL] AMM 21-31-34-000-001 AMM 21-31-34-400-001.
(2) If the fault continues:
Subtask 21-51-00-710-090-A (1) replace the PRESS CONT 1 [11HL] AMM 21-31-34-000-001 AMM 21-31-34-400-001.
(2) If the fault continues:
- do the troubleshooting procedures for single pack flow indication fault (Ref. TSM TASK 21-51-00-810-813) and (Ref. TSM TASK 21-51-00-810-814).
C. Do the test as given in the Para. 3.D.
5. Close-upSubtask 21-51-00-860-083-A ** ON A/C NOT FOR ALL
A. Stop the engines AMM 71-00-00-710-028 or the preconditioning through the HP ground connection AMM 12-33-21-618-001 (as applicable).