W DOC AIRBUS | TSM A320F

Bleed Control Valve Fault (APS 3200)


TASK 49-00-00-810-942-A
Bleed Control Valve Fault (APS 3200)


1. Possible Causes
  • fuel leaks
  • wiring
  • BLEED CONTROL VALVE (8051KM)
  • ELECTRONIC CONTROL BOX [59KD]
  • FUEL CONTROL UNIT (8022KM)
  • FUEL FLOW DIVIDER (8024KM)
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
ESPM 2052210
ESPM 2053210
ESPM 205321A
AMM 49-00-00-710-008
Operational Test of the APU
AMM 49-23-17-000-001
Removal of the Inlet Pressure/Temperature Sensor (APS 3200)
AMM 49-23-17-400-001
Installation of the Inlet Pressure/Temperature Sensor (APS 3200)
AMM 49-32-11-000-002
Removal of the Fuel Control Unit (APS 3200)
AMM 49-32-11-400-002
Installation of the Fuel Control Unit (APS 3200)
AMM 49-32-12-000-002
Removal of the Flow Divider (APS 3200)
AMM 49-32-12-400-002
Installation of the Flow Divider (APS 3200)
AMM 49-51-19-000-002
Removal of the Sensor - Compressor Discharge Pressure (APS 3200)
AMM 49-51-19-400-002
Installation of the Sensor - Compressor Discharge Pressure (APS 3200)
AMM 49-51-53-000-001
Removal of the Bleed Control Valve (APS 3200)
AMM 49-51-53-400-001
Installation of the Bleed Control Valve (APS 3200)
ASM 496102
AMM 49-61-34-000-002
Removal of the Electronic Control Box (ECB) (APS 3200)
AMM 49-61-34-400-002
Installation of the Electronic Control Box (ECB) (APS 3200)
AMM 49-73-00-00-
3. Fault Confirmation
Subtask 49-00-00-710-311-A ** ON A/C NOT FOR ALL
A. Do the operational test of the APU AMM 49-00-00-710-008.
NOTE: During the operational test of the APU, carefully examine the fuel lines from the fuel control unit to the bleed control valve:
  • fuel leaks are not permitted, correct/replace as necessary.
4. Fault Isolation
Subtask 49-00-00-810-297-B ** ON A/C NOT FOR ALL
A. Maintenance Action
   (1) If the APU Last Leg Report gives the maintenance message:


BLEED CTL VLV (8051KM):
Fault Code Number(s): 69 or 70


     (a) If the fault continues:
       1 If the fault continues:
   (2) If the APU Last Leg Report gives the maintenance message:


BLEED CTL VLV (8051KM):
Fault Code Number: 96


  • do a check of the IGV Actuator Guide pin with the IGV for correct installation. If the pin is disengaged, replace the pin.
     (a) If the fault continues:
       1 If the fault continues:
     (b) If the fault continues:
Interrogate CFDS for APU fault message. Use prompts (>) to go to the fault conditions screen AMM 49-73-00-00-.

Print Fault Condition Screen and do an inspection of the APU Inlet Pressure (P2A) and Bleed Air Pressure (PT).
       1 If an unusual P2A value is shown, compare with Ambient Static Pressure.
NOTE: At Standard Sea Level, P2A is 1013 mbar (14.69 psi).
         a replace the INLET PRESSURE/TEMPERATURE SENSOR (8013KM) AMM 49-23-17-000-001 and AMM 49-23-17-400-001.
       2 If an unusual PT value is shown.
NOTE: The possible values of PT must be around 1.2 bar (17.4045 psi).
         a replace the COMPRESSOR DISCHARGE-PRESSURE SENSOR (8039KM) AMM 49-51-19-000-002 and AMM 49-51-19-400-002.
     (c) If the fault continues:
   (3) If the APU Last Leg Report gives the maintenance message:


BLEED CTL VLV (8051KM):
Fault Code Number:138


     (a) If the fault continues:
       1 If the fault continues:
         a If the fault continues:
         b If the fault continues:
   (4) If the APU Last Leg Report gives the maintenance message:


BLEED CTL VLV (8051KM):
Fault Code Number: 119 or 172


     (a) If the fault continues:
       1 If the fault continues:
Subtask 49-00-00-710-312-A ** ON A/C NOT FOR ALL
B. Do the test given in Para. 3.
[Rev.8 from Aug 2018] 2026.04.04 04:34:27 UTC