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时间:2011-03-28 09:13来源:蓝天飞行翻译 作者:航空
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 - replace the CONTROLLER-CABIN PRESSURE 1 (11HL) (Ref. AMM TASK 21-31-34-000-001) and (Ref. AMM TASK 21-31-34-400-001).

 

 (2) If the fault does not move with the CPC 1:

 - swap back the CPC 1 (11HL) and the CPC 2 (12HL) (Ref. AMM TASK 21-31-34-000-001) and (Ref. AMM TASK 21-31-34-400-001).

 - do the operational test of the AFS (Ref. AMM TASK 22-96-00-710-

 


001). R
R (a) If the test gives a different maintenance message, refer to the R Fault Symptom List.
 (b) If the fault continues:
 - do a check and repair the wiring of the signal ARINC 429 OUT from the FMGC 1 (1CA1) to the CPC 1 (11HL) (Ref. ASM 21-31/03).
R B. If the test with the CPC 1 (11HL) gives the maintenance message NO DATA FROM FMGS 2 (55):
 - swap the CPC 1 (11HL) and the CPC 2 (12HL) (Ref. AMM TASK 21-31-34-000-001) and (Ref. AMM TASK 21-31-34-400-001).
 (1) If the fault moves with the CPC 1:

 - swap back the CPC 1 (11HL) and the CPC 2 (12HL) (Ref. AMM TASK 21-31-34-000-001) and (Ref. AMM TASK 21-31-34-400-001).

 - replace the CONTROLLER-CABIN PRESSURE 1 (11HL) (Ref. AMM TASK 21-31-34-000-001) and (Ref. AMM TASK 21-31-34-400-001).

 

 (2) If the fault does not move with the CPC 1:

 - swap back the CPC 1 (11HL) and the CPC 2 (12HL) (Ref. AMM TASK 21-31-34-000-001) and (Ref. AMM TASK 21-31-34-400-001).

 - do the operational test of the AFS (Ref. AMM TASK 22-96-00-710-

 


001). R
R (a) If the test gives a different maintenance message, refer to the R Fault Symptom List.
 「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 ∞∞21-31-00∞∞∞∞∞∞∞∞∞∞Page 231
 Feb 01/05 CES (b) If the fault continues:


 - do a check and repair the wiring of the signal ARINC 429 OUT from the FMGC 2 (1CA2) to the CPC 1 (11HL) (Ref. ASM 21-31/03).
R C. Do the test as given in the Para. 3.A.
 5. Close-up
________
 A. Put the aircraft back to its initial configuration.

 TASK 21-31-00-810-813


 CPC 2 receives no Data from the FMGS
 1. Possible Causes
_______________
 - CONTROLLER-CABIN PRESSURE 2 (12HL)

 - wiring


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 21-31-00-710-002 Operational Test of the Pressure Control and
 Monitoring AMM 21-31-34-000-001 Removal of the Cabin Pressure Controller (11HL,12HL) AMM 21-31-34-400-001 Installation of the Cabin Pressure Controller
 (11HL,12HL) AMM 22-96-00-710-001 Operational Test of the AFS ASM 21-31/03
 3. Fault Confirmation
__________________
 A. Test
 (1) Do a read-out of the CLASS III FAULT REPORT of the cabin
 pressure-control system 2.

 NOTE : If a fault is detected, the CLASS III FAULT REPORT of the CPC
____ shows a fault code for shop maintenance in addition to the related CFDS message(s). For detailed information see the applicable Page Block 301.
 (2) Start the FMS (1+2).

 (3) Do the operational test of the pressure control and monitoring system (Ref. AMM TASK 21-31-00-710-002).


 「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 ∞∞21-31-00∞∞∞∞∞∞∞∞∞∞Page 233
 Aug 01/03R
 CES

 4. Fault Isolation
_______________

R
R A. If the test with the CPC 2 (12HL) gives the maintenance message NO DATA FROM FMGS 1 (54):
 - swap the CPC 1 (11HL) and the CPC 2 (12HL) (Ref. AMM TASK 21-31-34-000-001) and (Ref. AMM TASK 21-31-34-400-001).
 (1) If the fault moves with the CPC 2:

 - swap back the CPC 1 (11HL) and the CPC 2 (12HL) (Ref. AMM TASK 21-31-34-000-001) and (Ref. AMM TASK 21-31-34-400-001).

 - replace the CONTROLLER-CABIN PRESSURE 2 (12HL) (Ref. AMM TASK 21-31-34-000-001) and (Ref. AMM TASK 21-31-34-400-001).

 

 (2) If the fault does not move with the CPC 2:

 - swap back the CPC 1 (11HL) and the CPC 2 (12HL) (Ref. AMM TASK 21-31-34-000-001) and (Ref. AMM TASK 21-31-34-400-001).

 - do the operational test of the AFS (Ref. AMM TASK 22-96-00-710-

 


001). R
R (a) If the test gives a different maintenance message, refer to the R Fault Symptom List.
 (b) If the fault continues:
 
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