W DOC AIRBUS | TSM A320F

Pack 2 Flow Control Valve (Pack 2 Flow Control Unit) Fault


TASK 21-51-00-810-804-A
Pack 2 Flow Control Valve (Pack 2 Flow Control Unit) Fault


1. Possible Causes
  • P2 FLOW CTL VALVE [8HB]
  • FLOW CTL UNIT - PACK 2 [24HB]
  • RELAY-R PACK CLOSE [12HB]
  • RELAY-DISAGREE (R FCV) [14HB]
  • BOARD-ANN LT TEST & INTFC [20LP]
  • P/BSW-AIR COND/PACK 2 [6HB]
  • RELAY-ENGINE START [16HB]
  • ENG/APU FIRE PNL [1WD]
  • RELAY-RAM AIR CLOSE CTL [3HZ]
  • RELAY-ENGINE START [17HB]
  • P2 CONTROLLER [27HH]
  • BOARD-ANN LT TEST & INTFC [12LP]
  • CONT-AIR COND SYSTEM 2 [57HH]
  • wiring
  • REHEATER [11HM3]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 21-51-00-200-001
Delta P Sense Lines Torque Check and Inspection
AMM 21-51-00-710-002
Operational Test of the Flow Control and Indicating System
ASM 215101
ASM 215102
AWM 215105
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 21-52-31-000-001
Removal of the Reheater
AMM 21-52-31-400-001
Installation of the Reheater
AMM 21-61-00-710-001
Operational Test of the Pack Temperature-Control System
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 73-25-34-710-040
Operational Test of the Engine Interface Unit
AMM 73-25-34-710-043
Operational Test of the Engine Interface Unit
3. Fault Confirmation
Subtask 21-51-00-710-056-A
A. Test
   (1) Do the operational test of the flow control and indication system AMM 21-51-00-710-002.
   (2) Do the operational test of the pack temperature-control system AMM 21-61-00-710-001.
4. Fault Isolation
Subtask 21-51-00-810-054-A
A. If the test is OK, no other maintenance action is necessary.
Subtask 21-51-00-810-055-B ** ON A/C NOT FOR ALL
B. If the test confirms the fault:
Subtask 21-51-00-810-055-C ** ON A/C NOT FOR ALL
B. If the test confirms the fault:
Subtask 21-51-00-810-090-A ** ON A/C NOT FOR ALL
C. If the fault continues:
- do the inspection of the delta P sense lines AMM 21-51-00-200-001.
Subtask 21-51-00-810-074-A ** ON A/C NOT FOR ALL
D. If the fault continues:
  • do a check of the RELAY-R PACK CLOSE [12HB] and replace it if necessary ASM 215102.
   (1) If the fault continues:
  • do a check of the RELAY-DISAGREE (R FCV) [14HB] and replace it if necessary ASM 215102.
   (2) If the fault continues:
  • do a check of the BOARD-ANN LT TEST & INTFC [20LP] and replace it if necessary ASM 215102.
   (3) If the fault continues:
  • do a check of the P/BSW-AIR COND/PACK 2 [6HB] and replace it if necessary ASM 215102.
   (4) If the fault continues:
     (a) If the test gives a different maintenance message refer to the Fault Symptom List.
   (5) If the fault continues:
  • do a check of the RELAY-ENGINE START [16HB] and replace it if necessary ASM 215102.
   (6) If the fault continues:
   (7) If the fault continues:
  • do a check of the RELAY-RAM AIR CLOSE CTL [3HZ] and replace it if necessary ASM 215102.
   (8) If the fault continues:
  • do a check of the RELAY-ENGINE START [17HB] and replace it if necessary ASM 215102.
   (9) If the fault continues:
Subtask 21-51-00-810-082-A ** ON A/C NOT FOR ALL
E. If the fault continues:
  • do a check and repair the wiring ASM 215101 between:
  • the FCV (8HB) and PC (27HH),
  • the FCV (8HB) and ground,
  • the RELAY (12HB) and the FCV (8HB),
  • the RELAY (14HB) and the FCV (8HB) and,
  • the RELAY (14HB) and the PC (27HH).
  • do a check and repair the wiring AWM 215105 between:
  • the circuit connection 210VT connector U and the PC (27HH) connector AB pin 7A,
  • the circuit connection 210VT connector T and RELAY (14HB) connector A pin A2.
   (1) If the fault continues:
Subtask 21-51-00-810-074-B ** ON A/C NOT FOR ALL
F. If the fault continues:
  • do a check of the BOARD-ANN LT TEST & INTFC [12LP] and replace it if necessary ASM 215101.
   (1) If the fault continues:
  • do a check of the P/BSW-AIR COND/PACK 2 [6HB] and replace it if necessary ASM 215101.
   (2) If the fault continues:
     (a) If the test gives a different maintenance message refer to the Fault Symptom List.
   (3) If the fault continues:
   (4) If the fault continues:
  • do a check of the RELAY-RAM AIR CLOSE CTL [3HZ] and replace it if necessary ASM 215101.
   (5) If the fault continues:
Subtask 21-51-00-810-082-B ** ON A/C NOT FOR ALL
G. If the fault continues:
  • do a check and repair the wiring ASM 215101 between:
  • the FCU2 (24HB) and ACSC2 (57HH) and,
  • the FCU2 (24HB) and ground.
   (1) If the fault continues:
Subtask 21-51-00-710-057-A
H. Do the test as given in the Para. 3.A.
5. Close-up
Subtask 21-51-00-860-053-A
A. Put the aircraft back to its initial configuration.
[Rev.8 from Aug 2018] 2026.04.04 04:24:46 UTC