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时间:2011-03-28 09:16来源:蓝天飞行翻译 作者:航空
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____ - PN 1303A0000-02
 (1) Do a leakage check of the sense line between the in-line-connector of the pressure-sensor (9HB) and the upstream port at the FCV (8HB), and replace if necessary.
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞21-51-00∞∞∞∞∞∞∞∞∞∞Page 249
 201-299, 301-399, Aug 01/05 CES


 (2) If the fault continues:

 - replace the SENSOR-PRESSURE (10HB) (Ref. AMM TASK 21-51-11-000-001) (Ref. AMM TASK 21-51-11-400-001)

 (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 check of the sense-line between the CPNOH (11HM9) and the FCV (8HB), and replace if necessary.

 (5) If the fault continues:

 - replace the SENSOR-COMPRESSOR PNEUMATIC OVHT (11HM9) (Ref. AMM TASK 21-61-18-000-001) (Ref. AMM TASK 21-61-18-400-001)

 (6) If the fault continues:


 - Replace the REHEATER (11HM3) (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 2 flow indicator on the ECAM BLEED page is stuck in the high position:
 - replace the PRESSURE SENSOR (24HB1) (Ref. AMM TASK 21-51-11-000-001) (Ref. AMM TASK 21-51-11-400-001).

 - replace the FLOW CONTROL SYSTEM (24HB) (Ref. AMM TASK 21-51-51-000-001) (Ref. AMM TASK 21-51-51-400-001).


 (1) If the fault continues:
 - do a check and repair the wiring (Ref. ASM 2151S01) from:

 - the FCS (24HB) to the ACSC2 (57HH) and,

 - the FCS (24HB) to ground.


 B. If the pack 2 flow indicator on the ECAM BLEED page is stuck in the low position:
 - replace the PRESSURE SENSOR (24HB1) (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 (24HB) (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 (11HM3) (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 250
 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 251
 Feb 01/05R
 CES


R **ON A/C 004-049, 055-099, 101-149, 151-199, 201-299, 301-399, 401-499,

 TASK 21-51-00-810-815
 Pack 1 High Flow Indication
 1. Possible Causes
_______________
 - VALVE-FLOW CTL (11HB)

 - FLOW CONTROL SYSTEM (23HB)

 - wiring


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 12-33-21-618-001 Pre-conditioning through the HP Ground Connection AMM 21-51-51-000-001 Removal of the Pack Flow-Control Valve AMM 21-51-51-400-001 Installation of the Pack Flow-Control Valve AMM 71-00-00-710-003 Engine Automatic Start ASM 21-51/01 ASM 21-51/02
 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.
 (1) Do the pre-conditioning through the HP ground connection (Ref. AMM TASK 12-33-21-618-001).

 (2) On the AIR COND panel 30VU:

 - push the HOT AIR pushbutton switch to the on position (the OFF legend goes off),

 - turn the COCKPIT, FWD CABIN and the AFT CABIN temperature selectors to the HOT positions and,

 - make sure that the PACK 1 and the PACK 2 pushbutton switches are in the on position (the OFF legends are off).
 
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