Pack Controller 1 (ACSC1) Fault
TASK 21-61-00-810-805-A
Pack Controller 1 (ACSC1) Fault
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 21-61-00-710-058-A ** ON A/C NOT FOR ALL
Subtask 21-61-00-810-070-A ** ON A/C NOT FOR ALL
Subtask 21-61-00-860-054-A
[Rev.8 from Aug 2018]
2026.04.04 04:24:52 UTC
Pack Controller 1 (ACSC1) Fault
1. Possible Causes
- wiring
- CONT-AIR COND SYSTEM 1 [47HH]
- P1 CONTROLLER [7HH]
- sense line
- P1 FLOW CTL VALVE [11HB]
- VALVE-TURBINE BYPASS [10HH]
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| TSM TASK 21-61-00-810-820-A | Pack 1 Electrical Component with Short Circuit (AIR PACK 1 REGUL FAULT) |
| ASM 215101 | |
| AMM 21-51-11-400-001 | Installation of the Differential Pressure Sensor |
| AMM 21-51-51-000-001 | Removal of the Pack Flow-Control Valve/ Pack Flow-Control Unit |
| AMM 21-51-51-400-001 | Installation of the Pack Flow-Control Valve/ Pack Flow-Control Unit |
| AMM 21-61-00-710-001 | Operational Test of the Pack Temperature-Control System |
| ASM 216102 | |
| ASM 216103 | |
| ASM 216104 | |
| AMM 21-61-34-000-001 | Removal of the Pack Controller |
| AMM 21-61-34-000-002 | Removal of the Air-Conditioning System Controller |
| AMM 21-61-34-400-001 | Installation of the Pack Controller |
| AMM 21-61-34-400-002 | Installation of the Air-Conditioning System Controller |
| AMM 21-61-53-000-001 | Removal of the Turbine Bypass Valve |
| AMM 21-61-53-400-001 | Installation of the Turbine Bypass Valve |
| ASM 216302 | |
| AMM 32-69-00-740-001 | BITE Check of Landing-Gear Control Interface-Unit (LGCIU) With Use of MCDU to Ensure that Continuous BITE is Operative |
Subtask 21-61-00-710-058-A ** ON A/C NOT FOR ALL
A. Do the operational test of the pack temperature-control system AMM 21-61-00-710-001.
Subtask 21-61-00-710-058-B ** ON A/C NOT FOR ALL 4. Fault IsolationNOTE: If a fault is detected, the PC gives a fault code for shop maintenance in addition to the related CFDS message(s) (refer to TSM chapter 21-63-00, page block 301).
Subtask 21-61-00-810-070-A ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message TEST FAILED with the fault code (6D):
(b) If the fault continues:
Subtask 21-61-00-810-059-B ** ON A/C NOT FOR ALL - do a check for a ground signal at the PC 1 (7HH) connector AA/9B ASM 216103.
- do the BITE test of the landing gear AMM 32-69-00-740-001.
(b) If the fault continues:
- do a check and repair the wiring if necessary between:
PC 1 (7HH) connector AA/9B and LGCIU 2 (5GA2) connector AB/G1 ASM 216103.
- do a check and repair the wiring between:
PC 1 (7HH) connector AB/6B and FCV (11HB) connector A/D,
PC 1 (7HH) connector AA/1D and FCV (11HB) connector A/E,
PC 1 (7HH) connector AA/1C and FCV (11HB) connector A/F,
PC 1 (7HH) connector AA/1B and FCV (11HB) connector A/G,
PC 1 (7HH) connector AA/1A and FCV (11HB) connector A/V,
PC 1 (7HH) connector AA/11C and FCV (11HB) connector A/J,
PC 1 (7HH) connector AA/11B and FCV (11HB) connector A/K,
PC 1 (7HH) connector AA/11A and FCV (11HB) connector A/L ASM 215101.
B. If the test gives the maintenance message ACSC1 (47HH):
Subtask 21-61-00-810-059-C ** ON A/C NOT FOR ALL - replace the CONT-AIR COND SYSTEM 1 [47HH] AMM 21-61-34-000-002 and AMM 21-61-34-400-002.
- do a check and repair the wiring ASM 216102 from:
- the ACSC1 (47HH) to the CB (49HH),
- the ACSC1 (47HH) to the CB (50HH) and,
- the ACSC1 (47HH) to ground.
- do the trouble shooting procedures for the pack 1 electrical component with short circuit (Ref. TSM TASK 21-61-00-810-820).
B. If the test gives the maintenance message P1 CONT:
Subtask 21-61-00-810-124-A ** ON A/C NOT FOR ALL - replace the P1 CONTROLLER [7HH] AMM 21-61-34-000-001 and AMM 21-61-34-400-001.
- do a check and repair the wiring if necessary between:
PC 1 (7HH) connector AA/5A and CB (1HH),
PC 1 (7HH) connector AA/5B and GND,
PC 1 (7HH) connector AB/13D and CB (2HH),
PC 1 (7HH) connector AB/14A and GND ASM 216103.
- do a check and repair if necessary the wiring of the signal:
ARINC 429 XTR (M) from the ZC (8HK) to the PC 1 (7HH),
ARINC 429 XTR (S) from the ZC (8HK) to the PC 1 (7HH),
ARINC 429 RCV (S) from the ZC (8HK) to the PC 1 (7HH) ASM 216302.
- torque the sense line connectors between the sensor (10HB) and the FCV (11HB) AMM 21-51-11-400-001 AMM 21-51-51-400-001.
- do the trouble shooting procedures for the pack 1 electrical component with short circuit (Ref. TSM TASK 21-61-00-810-820).
- do a check that the resistance of the torque motor of the FCV (11HB) measured between :
pin A/F and A/V is between 36 ohm and 44 ohm.
C. If the test gives the maintenance message NO 28V ON PACK 1 MAIN:
Subtask 21-61-00-810-125-A ** ON A/C NOT FOR ALL - do a check and repair the wiring between:
PC 1 (7HH) connector AA/8C and CB (3HH),
PC 1 (7HH) connector AA/8D and GND ASM 216103.
D. If the test gives the maintenance message NO 28V ON PACK 1 SECD:
Subtask 21-61-00-810-269-A ** ON A/C NOT FOR ALL - do a check and repair the wiring between:
PC 1 (7HH) connector AB/9A and CB (4HH),
PC 1 (7HH) connector AB/9B and GND ASM 216103.
E. If the fault continues:
Subtask 21-61-00-810-269-B ** ON A/C NOT FOR ALL - replace the VALVE-TURBINE BYPASS [10HH] AMM 21-61-53-000-001 and AMM 21-61-53-400-001.
- do a check and repair the wiring ASM 216104 from:
- the VALVE (10HH) to the PC 1 (7HH) and,
- the VALVE (10HH) to ground.
E. If the fault continues:
Subtask 21-61-00-710-059-A - replace the VALVE-TURBINE BYPASS [10HH] AMM 21-61-53-000-001 and AMM 21-61-53-400-001.
- do a check and repair the wiring ASM 216104 from:
- the VALVE (10HH) to the ACSC1 (47HH)
- the VALVE (10HH) to ground.
F. Do the test as given in the Para. 3.A.
5. Close-upSubtask 21-61-00-860-054-A
A. Put the aircraft back to its initial configuration.