W DOC AIRBUS | TSM A320F

Pack 2 Electrical Component with Short Circuit (AIR PACK 2 REGUL FAULT)


TASK 21-61-00-810-821-A
Pack 2 Electrical Component with Short Circuit (AIR PACK 2 REGUL FAULT)


1. Possible Causes
  • FLOW CTL UNIT - PACK 2 [24HB]
  • P2 FLOW SENSOR [9HB]
  • SENSOR-DELTA P, PACK 2 [24HB2]
  • P2 RAM AIR IN ACTUATOR [28HH]
  • P2 CONTROLLER [27HH]
  • CONT-AIR COND SYSTEM 2 [57HH]
  • SENSOR-WATER EXTRACTOR TEMPERATURE [31HH]
  • VALVE-TURBINE BYPASS [30HH]
  • SENSOR-COMPRESSOR TEMPERATURE [32HH]
  • P2 FLOW CTL VALVE [8HB]
  • P2 PRESS INL SENSOR [36HH]
  • wiring
  • SENSOR-PRESS, PACK 2 INLET [24HB1]
  • SDAC
  • TEMP SENSOR RH MIXER [25HK]
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
WATER - SOAPY SOLUTION
 B. Referenced Information
REFERENCE
DESIGNATION
AMM 12-33-21-618-001
Pre-conditioning through the LP Ground Connection
ASM 215101
AMM 21-51-11-000-001
Removal of the Differential Pressure Sensor
AMM 21-51-11-400-001
Installation of the Differential Pressure Sensor
AMM 21-51-13-000-001
Removal of the Pack-Inlet Pressure Sensor
AMM 21-51-13-400-001
Installation of the Pack-Inlet 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 216101
ASM 216102
ASM 216104
AWM 216106
AWM 216107
AWM 216108
AWM 216109
AMM 21-61-11-000-001
Removal of the Compressor Outlet - Temperature Sensor
AMM 21-61-11-400-001
Installation of the Compressor Outlet - Temperature Sensor
AMM 21-61-13-000-001
Removal of the Water-Extractor Temperature Sensors
AMM 21-61-13-400-001
Installation of the Water-Extractor Temperature Sensors
AMM 21-61-16-000-001
Removal of the Pack-Inlet Pressure Sensor
AMM 21-61-16-400-002
Installation of the Pack-Inlet Pressure Sensor
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 21-61-51-000-001
Removal of the Air-Inlet Flap Actuator
AMM 21-61-51-400-001
Installation of the Air-Inlet Flap Actuator 8HH and 28HH
AMM 21-61-53-000-001
Removal of the Turbine Bypass Valve
AMM 21-61-53-400-001
Installation of the Turbine Bypass Valve
AMM 21-63-16-000-001
Removal of the Mixer Temperature Sensor
AMM 21-63-16-400-001
Installation of the Mixer Temperature Sensor
F FCV Sensor Plate Inspection Area ** ON A/C NOT FOR ALL
3. Fault Confirmation
Subtask 21-61-00-865-052-A
A. Open this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
122VUAIR COND/PACK TEMP/CTL SYS1/2/115VAC21HHW22
122VUAIR COND/PACK TEMP CTL SYS2/2/115VAC22HHY20
Subtask 21-61-00-865-053-A
B. Close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
122VUAIR COND/PACK TEMP/CTL SYS1/2/115VAC21HHW22
122VUAIR COND/PACK TEMP CTL SYS2/2/115VAC22HHY20
Subtask 21-61-00-710-090-A ** ON A/C NOT FOR ALL
C. Test
   (1) Do a read out of the post flight report and do the operational test of the pack-temperature control system AMM 21-61-00-710-001.
NOTE: If the test finds a fault the PC gives a fault code for shop maintenance and also the related CFDS message(s) (refer to chapter 21-63-00 page block 301).
Subtask 21-61-00-710-090-B ** ON A/C NOT FOR ALL
C. Test
F FCV Sensor Plate Inspection Area ** ON A/C NOT FOR ALL
   (1) Do a read out of the post flight report and do the operational test of the pack-temperature control system AMM 21-61-00-710-001.
   (2) Perform a leak check at the FCV Sensor plate.
NOTE: This procedure is only applicable for FCV P/N 1806A0000-02, 1806A0000-02 Amdt A, 1806B0000-01, 1806B0000-01 Amdt A, 1806B0000-01 Amdt AB, 1806B0000-01 Amdt B and 1806B0000-02.
     (a) On the AIR COND panel 30VU:
  • make sure that the PACK pushbutton switch is in the OFF position.
     (b) Do the pre-conditioning through the HP ground connector or with the APU AMM 12-33-21-618-001.
     (c) Apply a WATER - SOAPY SOLUTION to the connections behind the sensor plate to search for a leak.
4. Fault Isolation
Subtask 21-61-00-810-273-B ** ON A/C NOT FOR ALL
A. If a leakage is found:
Subtask 21-61-00-810-113-A ** ON A/C NOT FOR ALL
B. * If the post flight report gives the warning AIR PACK 2 REGUL FAULT without a maintenance message and,
* no AIR PACK 2 REGUL FAULT shows on the ECAM upper DU and,
* no maintenance message shows:
  • replace the P2 FLOW SENSOR [9HB] AMM 21-51-11-000-001 and AMM 21-51-11-400-001.
    ** If the post flight report gives the warning AIR PACK 2 REGUL FAULT and,
    ** the ECAM upper DU gives the warning AIR PACK 2 REGUL FAULT or,
    *** If the post flight report gives the warning AIR PACK 2 REGUL FAULT with,
    *** the maintenance message NO DATA FROM P2 CONT and,
    *** the operational test of the pack-temperature control system gives the maintenance message NO TEST RECEPTION FROM P2 CONT:
  • do the work steps which follow.
NOTE: Additional Information
For wiring and pin identification used in this procedure:
ASM 215101,
ASM 216102,
ASM 216104 and,
AWM 216109.
For disconnection/reconnection of electrical connectors refer to the applicable work step AMM TASK reference in the applicable paras. 4. B, C, D and E.
Subtask 21-61-00-810-187-B ** ON A/C NOT FOR ALL
C. Check for Short Circuit at the P2 RAM AIR IN ACTUATOR [28HH] 115VAC Supply Lines
   (1) Remove the P2 CONTROLLER [27HH]
AMM 21-61-34-000-001:
   (2) Disconnect the electrical connector (28HH/A) from the P2 RAM AIR IN ACTUATOR [28HH] :
  • at the electrical connector (28HH/A) do a check for a short circuit between,
    * pins J and N and,
    * GND and pins J and N,
  • if there is a short circuit repair the related wiring between,
    * connector (28HH/A) pin J and PC connector (27HH/AB) pin 15A,
    * connector (28HH/A) pin N and PC connector (27HH/AB) pin 14B.
  • if there is no short circuit in the wiring replace the P2 RAM AIR IN ACTUATOR [28HH]
    AMM 21-61-51-000-001 and,
    AMM 21-61-51-400-001.
  • install the P2 CONTROLLER [27HH]
    AMM 21-61-34-400-001.
  • connect the electrical connector (28HH/A) to the P2 RAM AIR IN ACTUATOR [28HH] .
Subtask 21-61-00-810-188-A ** ON A/C NOT FOR ALL
D. If the fault continues:
   (1) Swap the PC 2 (27HH) and the PC 1 (7HH)
AMM 21-61-34-000-001 and,
AMM 21-61-34-400-001.
   (2) If the fault moves with the PC 2:
   (3) If the fault does not move with the PC 2:
Subtask 21-61-00-810-189-B ** ON A/C NOT FOR ALL
E. If the fault continues:
   (1) Disconnect the electrical connector (31HH/A) from the SENSOR-WATER EXTRACTOR TEMPERATURE [31HH] ,
  • make sure that the electrical connector is clean and in the correct condition,
  • at the electrical connector (31HH/A) do a check for voltage between,
    * pins E and F.
     (a) If the voltage is between 9.6VDC and 10.4VDC:
     (b) If the voltage is not between 9.6VDC and 10.4VDC:
  • disconnect the electrical connector (28HH/A) from the P2 RAM AIR IN ACTUATOR [28HH] ,
  • make sure that the electrical connector is clean and in the correct condition.
  • at the electrical connector (31HH/A) do a check for voltage again.
       1 If the voltage is between 9.6VDC and 10.4VDC:
       2 If the voltage is not between 9.6VDC and 10.4VDC:
Subtask 21-61-00-810-190-A ** ON A/C NOT FOR ALL
F. If the fault continues:
   (1) Disconnect the electrical connector (7560VC/A)
AMM 21-61-16-000-001.
  • make sure that the electrical connector is clean and in the correct condition.
  • at the electrical connector (7560VC) do a check for 15VDC from the pack controller primary channel between,
    * pins A and C (+15VDC) and,
    * pins D and C (-15VDC).
     (a) If the voltage is correct:
   (2) If the fault continues:
  • remove the P2 CONTROLLER [27HH]
    AMM 21-61-34-000-001,
  • disconnect the electrical connector (31HH/A) from the SENSOR-WATER EXTRACTOR TEMPERATURE [31HH] ,
  • at the electrical connector (31HH/A) do a check for a short circuit between,
    * pins E and F and,
    * GND and pins E and F.
     (a) If there is no short circuit connect the electrical connector (31HH/A).
     (b) If there is a short circuit repair the related wiring between,
* connector (31HH/A) pin E and PC 2 connector (27HH/AA) pin 14A,
* connector (31HH/A) pin F and PC 2 connector (27HH/AA) pin 14B.
  • connect the electrical connector (31HH/A).
   (3) If the fault continues:
  • disconnect the electrical connector (28HH/A) from the P2 RAM AIR IN ACTUATOR [28HH] ,
  • at the electrical connector (28HH/A) do a check for a short circuit between,
    * pins A and B, A and C, B and C and,
    * GND and pins A, B and C.
     (a) If there is no short circuit connect the electrical connector (28HH/A).
     (b) If there is a short circuit repair the related wiring between,
* connector (28HH/A) pin A and PC 2 connector (27HH/AA) pin 11D,
* connector (28HH/A) pin B and PC 2 connector (27HH/AA) pin 12A,
* connector (28HH/A) pin C and PC 2 connector (27HH/AA) pin 12B.
  • connect the electrical connector (28HH/A).
Subtask 21-61-00-810-113-B ** ON A/C NOT FOR ALL
G. * If the post flight report gives the warning AIR PACK 2 REGUL FAULT without a maintenance message and,
* no AIR PACK 2 REGUL FAULT warning shows on the ECAM upper DU and,
* no maintenance message shows:
   (1) If the fault continues:
  • replace the FLOW CTL UNIT - PACK 2 [24HB] ,
    AMM 21-51-51-000-001 and AMM 21-51-51-400-001.
  • no further action is necessary.
    ** If the post flight report gives the warning AIR PACK 2 REGUL FAULT and,
    ** the ECAM upper DU shows the warning AIR PACK 2 REGUL FAULT or:
  • do the work steps which follow.
NOTE: Additional Information
For wiring and pin identification used in this procedure:
ASM 215101,
ASM 216101,
ASM 216102,
AWM 216106,
AWM 216107,
AWM 216108and,
AWM 216109.
For disconnection/reconnection of electrical connectors refer to the applicable work step AMM TASK reference in the applicable paras. 4. B, C, D and E.
Subtask 21-61-00-810-187-C ** ON A/C NOT FOR ALL
H. Check for short circuit at the P2 RAM AIR IN ACTUATOR [28HH] 115VAC supply lines
   (1) Remove the CONT-AIR COND SYSTEM 2 [57HH] ,
AMM 21-61-34-000-002:
   (2) Disconnect the electrical connector (28HH/A) from the P2 RAM AIR IN ACTUATOR [28HH] :
  • do a check for a short circuit between,
    * pins J and K and,
    * GND and pins J and K.
  • if there is a short circuit repair the related wiring between,
    * connector (28HH/A) pin J and ACSC2 connector (57HH/AB) pin 15J,
    * connector (28HH/A) pin K and ACSC2 connector (57HH/AB) pin 15K.
  • if there is no short circuit in the wiring replace the P2 RAM AIR IN ACTUATOR [28HH] ,
    AMM 21-61-51-000-001 and,
    AMM 21-61-51-400-001.
  • install the CONT-AIR COND SYSTEM 2 [57HH]
    AMM 21-61-34-400-002.
  • connect the electrical connector (28HH/A) to the P2 RAM AIR IN ACTUATOR [28HH] .
Subtask 21-61-00-810-188-B ** ON A/C NOT FOR ALL
I. If the fault continues:
   (1) Swap the ACSC2 (57HH) and the ACSC1 (47HH)
AMM 21-61-34-000-002 and,
AMM 21-61-34-400-002.
     (a) If the fault moves with the ACSC2:
   (2) If the fault does not move with the ACSC2:
Subtask 21-61-00-810-189-D ** ON A/C NOT FOR ALL
J. If the fault continues:
   (1) Disconnect the electrical connector (31HH/A) from the SENSOR-WATER EXTRACTOR TEMPERATURE [31HH] ,
  • make sure that the electrical connector is clean and in the correct condition,
  • at the electrical connector (31HH/A) do a check for voltage between,
    * pins E and F.
     (a) If the voltage is between 9.1VDC and 9.9VDC:
     (b) If the voltage is not between 9.1VDC and 9.9VDC:
  • disconnect the electrical connector (28HH/A) from the P2 RAM AIR IN ACTUATOR [28HH] ,
  • make sure that the electrical connector is clean and in the correct condition,
  • at the electrical connector (31HH/A) do a check for voltage again.
       1 If the voltage is between 9.1VDC and 9.9VDC:
       2 If the voltage is not between 9.1VDC and 9.9VDC:
Subtask 21-61-00-810-190-B ** ON A/C NOT FOR ALL
K. If the fault continues:
   (1) disconnect the electrical connector (24HB1/A) from the SENSOR-PRESS, PACK 2 INLET [24HB1] .
  • make sure that the electrical connector is clean and in the correct condition.
  • at the electrical connector (24HB1/A) do a check for 15VDC from ACSC primary channel between,
    * pins A and C (+15VDC)
     (a) If the voltage is correct:
   (2) If the fault continues:
  • Remove the CONT-AIR COND SYSTEM 2 [57HH]
    AMM 21-61-34-000-002,
  • disconnect the electrical connector (31HH/A) from the SENSOR-WATER EXTRACTOR TEMPERATURE [31HH] ,
  • at the electrical connector (31HH/A) do a check for a short circuit between,
    * pins C and D and,
    * GND and pins C and D.
     (a) If there is no short circuit connect the electrical connector (31HH/A).
     (b) If there is a short circuit repair the related wiring between,
* connector (31HH/A) pin C and ACSC2 connector (57HH/AA) pin 4A,
* connector (31HH/A) pin D and ACSC2 connector (57HH/AA) pin 4B.
  • connect the electrical connector (31HH/A).
   (3) If the fault continues:
  • disconnect the electrical connector (28HH/A) from the P2 RAM AIR IN ACTUATOR [28HH] ,
  • at the electrical connector (28HH/A) do a check for a short circuit between,
    * pins A and B, A and C, B and C and,
    * GND and pins A, B and C.
     (a) If there is no short circuit connect the electrical connector (28HH/A).
     (b) If there is a short circuit repair the related wiring between,
* connector (28HH/A) pin A and ACSC2 connector (57HH/AA) pin 14B,
* connector (28HH/A) pin B and ACSC2 connector (57HH/AA) pin 14A,
* connector (28HH/A) pin C and ACSC2 connector (57HH/AA) pin 14C:
  • connect the electrical connector (28HH/A).
Subtask 21-61-00-810-194-B ** ON A/C NOT FOR ALL
L. If the fault continues:
   (1) Disconnect the electrical connector (30HH/A) from the VALVE-TURBINE BYPASS [30HH] ,
  • at the electrical connector (30HH/A) do a check for a short circuit between,
    * pins U and J, U and K, U and L, J and K, J and L, K and L,
    * pins C and D and,
    * GND and pins U, J, K, L and C.
     (a) If there is no short circuit connect the electrical connector (30HH/A).
     (b) If there is a short circuit repair the related wiring between,
* connector (30HH/A) pin U and PC 2 connector (27HH/AA) pin 2A,
* connector (30HH/A) pin J and PC 2 connector (27HH/AA) pin 2B,
* connector (30HH/A) pin K and PC 2 connector (27HH/AA) pin 2C,
* connector (30HH/A) pin L and PC 2 connector (27HH/AA) pin 2D,
* connector (30HH/A) pin C and PC 2 connector (27HH/AA) pin 5B:
  • connect the electrical connector (30HH/A).
Subtask 21-61-00-810-192-A ** ON A/C NOT FOR ALL
M. If the fault continues:
   (1) Disconnect the electrical connector (32HH/A),
  • at the electrical connector (32HH/A) do a check for a short circuit between,
    * pins A and B, B and C and,
    * GND and pins A, B and C.
     (a) If there is no short circuit connect the electrical connector (32HH/A).
     (b) If there is a short circuit repair the related wiring between,
* connector (32HH/A) pin A and PC 2 connector (27HH/AA) pin 15A,
* connector (32HH/A) pin B and PC 2 connector (27HH/AA) pin 14D,
* connector (32HH/A) pin C and PC 2 connector (27HH/AA) pin 14C.
  • connect the electrical connector (32HH/A).
   (2) If the fault continues:
  • disconnect the electrical connector (7560VC/A),
  • at the electrical connector (7560VC) do a check for a short circuit between,
    * pins A and B, A and C, A and D, B and C, B and D, C and D and,
    * GND and pins A, B, C and D.
     (a) If there is no short circuit connect the electrical connector (7560VC/A).
     (b) If there is a short circuit repair the related wiring between,
* connector (7560VC) pin A and PC 2 connector (27HH/AB) pin 15C,
* connector (7560VC) pin B and PC 2 connector (27HH/AA) pin 10D,
* connector (7560VC) pin C and PC 2 connector (27HH/AA) pin 10C,
* connector (7560VC) pin D and PC 2 connector (27HH/AB) pin 15D.
  • connect the electrical connector (7560VC/A).
   (3) If the fault continues:
  • disconnect the electrical connector (8HB/A) from the P2 FLOW CTL VALVE [8HB] .
  • at the electrical connector (8HB/A) do a check for a short circuit between,
    * pins J and K, J and L, K and L and,
    * GND and pins J, K and L.
     (a) If there is no short circuit connect the electrical connector (8HB/A).
     (b) If there is a short circuit repair the related wiring between,
* connector (8HB/A) pin J and PC 2 connector (27HH/AA) pin 11C,
* connector (8HB/A) pin K and PC 2 connector (27HH/AA) pin 11B,
* connector (8HB/A) pin L and PC 2 connector (27HH/AA) pin 11A.
  • connect the electrical connector (8HB/A).
   (4) Install the P2 CONTROLLER [27HH]
AMM 21-61-34-400-001.
   (5) If the fault continues:
     (a) Swap the SDAC's (1WV2 and 1WV1). (Ref. AMM TASK 31-55-34-401)
     (b) If this action has solved the problem:
  • replace the SDAC which formerly was SDAC2.
Subtask 21-61-00-810-194-C ** ON A/C NOT FOR ALL
N. If the fault continues:
   (1) Disconnect the electrical connector (30HH/A) from the VALVE-TURBINE BYPASS [30HH] ,
  • at the electrical connector (30HH/A) do a check for a short circuit between,
    * pins U and J, U and K, U and L, J and K, J and L, K and L, C and D and,
    * GND and pins U, J, K, L and C.
     (a) If there is no short circuit connect the electrical connector (30HH/A).
     (b) If there is a short circuit repair the related wiring between,
* connector (30HH/A) pin U and ACSC2 connector (57HH/AB) pin 15D,
* connector (30HH/A) pin J and ACSC2 connector (57HH/AB) pin 15A,
* connector (30HH/A) pin K and ACSC2 connector (57HH/AB) pin 15B,
* connector (30HH/A) pin L and ACSC2 connector (57HH/AB) pin 15C,
* connector (30HH/A) pin C and ACSC2 connector (57HH/AB) pin 15E.
  • connect the electrical connector (30HH/A).
Subtask 21-61-00-810-192-B ** ON A/C NOT FOR ALL
O. If the fault continues:
   (1) Disconnect the electrical connector (32HH/A) from the SENSOR-COMPRESSOR TEMPERATURE [32HH] ,
  • at the electrical connector (32HH/A) do a check for a short circuit between,
    * pins B and C, B and D, C and D and,
    * GND and pins B, C and D.
     (a) If there is no short circuit connect the electrical connector (32HH/A).
     (b) If there is a short circuit repair the related wiring between,
* connector (32HH/A) pin B and ACSC2 connector (57HH/AA) pin 6B,
* connector (32HH/A) pin C and ACSC2 connector (57HH/AA) pin 6C,
* connector (32HH/A) pin D and ACSC2 connector (57HH/AA) pin 6A,
  • connect the electrical connector (32HH/A).
   (2) If the fault continues:
  • disconnect the electrical connector (24HB1/A),
  • at the connector (24HB1/A) do a check for a short circuit between,
    * pins A and B, A and C, B and C and,
    * GND and pins A, B and C.
     (a) If there is no short circuit connect the electrical connector (24HB1/A).
     (b) If there is a short circuit repair the related wiring between,
* connector (24HB1/A) pin A and ACSC2 connector (57HH/AA) pin 10H,
* connector (24HB1/A) pin B and ACSC2 connector (57HH/AA) pin 10K,
* connector (24HB1/A) pin C and ACSC2 connector (57HH/AA) pin 10J.
  • connect the electrical connector (24HB1/A).
   (3) Install the CONT-AIR COND SYSTEM 2 [57HH] ,
AMM 21-61-34-400-002.
   (4) If the fault continues:
   (5) If the fault continues:
     (a) Swap the SDAC's (1WV2 and 1WV1). (Ref.AMM TASK 31-55-34-401)
     (b) If this action has solved the problem:
  • replace the SDAC which formerly was SDAC2.
Subtask 21-61-00-710-091-A
P. Do the test as given in the Para. 3.A.
5. Close-up
Subtask 21-61-00-860-070-A
A. Put the aircraft back to its initial configuration.
[Rev.8 from Aug 2018] 2026.04.04 04:24:54 UTC