(3) If the fault continues:
- replace the VALVE-FLOW CTL (11HB) (Ref. AMM TASK 21-51-51-000-001) and (Ref. AMM TASK 21-51-51-400-001).
(4) If the fault continues:
- do a leakage check the sense-line between the CPNOH (10HM9) and the FCV (11HB), and replace if necessary.
(5) If the fault continues:
- replace the SENSOR-COMPRESSOR PNEUMATIC OVHT (10HM9) (Ref. AMM TASK 21-61-18-000-001) (Ref. AMM TASK 21-61-18-400-001)
(6) If the fault continues:
- replace the REHEATER (10HM3) (Ref. AMM TASK 21-52-31-000-001) and (Ref. AMM TASK 21-52-31-400-001).
R **ON A/C 401-499,
A. If the pack 1 flow indicator on the ECAM BLEED page is stuck in the high position:
- replace the PRESSURE SENSOR (23HB1) (Ref. AMM TASK 21-51-11-000-001) (Ref. AMM TASK 21-51-11-400-001).
(1) If the fault continues:
- replace the FLOW CONTROL SYSTEM (23HB) (Ref. AMM TASK 21-51-51-000-001) (Ref. AMM TASK 21-51-51-400-001).
(2) If the fault continues:
- do a check and repair the wiring (Ref. ASM 2151S01) from:
- the FCS (23HB) to the ACSC1 (47HH) and,
- the FCS (23HB) to ground.
B. If the pack 1 flow indicator on the ECAM BLEED page is stuck in the low position:
- replace the PRESSURE SENSOR (23HB1) (Ref. AMM TASK 21-51-11-000-001) (Ref. AMM TASK 21-51-11-400-001)
(1) If the fault continues:
- replace the FLOW CONTROL SYSTEM (23HB) (Ref. AMM TASK 21-51-51-000-001) and (Ref. AMM TASK 21-51-51-400-001).
(2) If the fault continues:
- replace the REHEATER (10HM3) (Ref. AMM TASK 21-52-31-000-001) and (Ref. AMM TASK 21-52-31-400-001).
**ON A/C ALL
C. Do the test as given in the Para. 3.E.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞21-51-00∞∞∞∞∞∞∞∞∞∞Page 242
Aug 01/05 CES 5. Close-up
________
A. Stop the engines (Ref. AMM TASK 71-00-00-710-028) or the preconditioning through the HP ground connection (Ref. AMM TASK 12-33-21-618-001) (as applicable).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞21-51-00∞∞∞∞∞∞∞∞∞∞Page 243
Feb 01/05R
CES
TASK 21-51-00-810-814
Pack 2 Flow Indication Fault
1. Possible Causes
_______________
- VALVE-FLOW CTL (8HB)
- SENSOR-PRESSURE (9HB)
- SENSOR-COMPRESSOR PNEUMATIC OVHT (11HM9)
- REHEATER (11HM3)
- VALVE-FLOW CTL (11HB)
- SENSOR-PRESSURE (10HB)
- wiring R - PRESSURE SENSOR (24HB1) R - FLOW CONTROL SYSTEM (24HB)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
ASM 2151S01 AMM 12-33-21-618-001 Pre-conditioning through the HP Ground Connection AMM 21-51-11-000-001 Removal of the Differential Pressure Sensor 9HB
(10HB) AMM 21-51-11-400-001 Installation of the Differential Pressure Sensor 9HB
(10HB) R AMM 21-51-51-000-001 Removal of the Pack Flow-Control Valve R AMM 21-51-51-400-001 Installation of the Pack Flow-Control Valve
AMM 21-51-51-600-001 Scheduled Replacement of a Pack Flow-Control Valve
Trailing-Edge Probe Filter AMM 21-52-31-000-001 Removal of the Reheater 10HM3 (11HM3) AMM 21-52-31-400-001 Installation of the Reheater 10HM3 (11HM3) AMM 21-61-18-000-001 Removal of the Compressor Pneumatic Overheat-Sensor
10HM9 (11HM9)
AMM 21-61-18-400-001 Installation of the Compressor Pneumatic
Overheat-Sensor 10HM9 (11HM9)
AMM 71-00-00-710-003 Engine Automatic Start
AMM 71-00-00-710-028 Engine Shutdown
3. Fault Confirmation
__________________
A. Bleed Air Supply Source from the HP Ground Connection
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.
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本文链接地址：A320 Trouble Shooting Manual 排故手册 AIR CONDITIONING 空调2(2)
