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时间:2011-03-28 22:55来源:蓝天飞行翻译 作者:航空
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 (a) If the fault continues:
 - replace the CDU-ADIRS (2FP) (Ref. AMM TASK 34-12-12-000-001) and (Ref. AMM TASK 34-12-12-400-001).
 1 If the fault continues:
_
 - do a check and repair the wiring of the annunciator light test and interface board (4LP) . from pin A/17 to ADIRS CDU (4FP) pin C/14 . from pin A/31 to the ground point (Ref. ASM 34-14/02).
 B. Do the test given in Para. 3.B.
 5. Close-up
________
 A. Put the aircraft back to its initial configuration.
 (1) On the panel 25VU, set the ANN LT switch to BRT.

 (2) Do the ADIRS stop procedure (Ref. AMM TASK 34-10-00-860-005).


 「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 ∞∞34-14-00∞∞∞∞∞∞∞∞∞∞Page A214
 May 01/05R
 CES  Attitude Discrepancy Warning on the Upper ECAM Display Unit


 1. Possible Causes
_______________
 - DMC-1 (1WT1)

 - ADIRU-1 (1FP1)

 - DMC-2 (1WT2)

 - ADIRU-2 (1FP2)

 - wiring of the INERTIAL REFERENCE OUTPUT BUS 1 bus from the ADIRU1 (1FP1) to the DMC1 (1WT1)

 - wiring of the INERTIAL REFERENCE OUTPUT BUS 1 bus from the ADIRU2 (1FP2) to the DMC2 (1WT2)


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
AMM 31-63-34-000-001 Removal of the DMC (1WT1,1WT2,1WT3)
 AMM 31-63-34-400-001 Installation of the DMC (1WT1,1WT2,1WT3)
 AMM 34-12-34-000-001 Removal of the ADIRU (1FP1, 1FP2, 1FP3)
 AMM 34-12-34-400-001 Installation of the ADIRU (1FP1, 1FP2, 1FP3)
 ASM 34-14/01

 3. Fault Confirmation
__________________
 A. Test
 (1) Not applicable, the fault is evident.
 4. Fault Isolation
_______________
 A. If the NAV ATT DISCREPANCY message comes into view on the upper ECAM DU:
 - make sure that the CHECK ATT message is in view on the CAPT PFD or on the F/O PFD.
 (1) If the CHECK ATT message is in view on the CAPT PFD:
 - on the center pedestal, on the SWITCHING panel 8VU, set the EIS DMC selector switch to CAPT 3.
 (a) If the messages go out of view:
 - replace the DMC-1 (1WT1) (Ref. AMM TASK 31-63-34-000-001) and (Ref. AMM TASK 31-63-34-400-001).
 「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 ∞∞34-14-00∞∞∞∞∞∞∞∞∞∞Page A215
 May 01/05R
 CES  a If there is no continuity:


 1_ If the fault continues:
 - do a check of the wiring of the INERTIAL REFERENCE OUTPUT
 BUS 1 bus from the ADIRU1 (1FP1) to the DMC1 (1WT1) (Ref.
 ASM 34-14/01).

_ - repair the above wiring.
 b If there is continuity:
_
 - replace the ADIRU-1 (1FP1) (Ref. AMM TASK 34-12-34-000-001) and (Ref. AMM TASK 34-12-34-400-001).
 (b) If the messages stay in view:
 - replace the ADIRU-1 (1FP1) (Ref. AMM TASK 34-12-34-000-001) and (Ref. AMM TASK 34-12-34-400-001).
 (2) If the CHECK ATT message is in view on the F/O PFD:
 - on the center pedestal, on the SWITCHING panel 8VU, set the EIS DMC selector switch to F/O 3.
 (a) If the messages go out of view:
 - replace the DMC-2 (1WT2) (Ref. AMM TASK 31-63-34-000-001) and (Ref. AMM TASK 31-63-34-400-001).
 1 If the fault continues:
_
 - do a check of the wiring of the INERTIAL REFERENCE OUTPUT BUS 1 bus from the ADIRU2 (1FP2) to the DMC2 (1WT2) (Ref. ASM 34-14/01).
 a If there is no continuity:
_ - repair the above wiring.
 b If there is continuity:
_
 - replace the ADIRU-2 (1FP2) (Ref. AMM TASK 34-12-34-000-001) and (Ref. AMM TASK 34-12-34-400-001).
 (b) If the messages stay in view:
 - replace the ADIRU-2 (1FP2) (Ref. AMM TASK 34-12-34-000-001) and (Ref. AMM TASK 34-12-34-400-001).
 5. Close-up
________
 A. Put the aircraft back to its initial configuration.
 (1) On the center pedestal, on the SWITCHING panel 8VU, set the EIS DMC selector switch to NORM.
 「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 ∞∞34-14-00∞∞∞∞∞∞∞∞∞∞Page A216
 May 01/05R
 CES  Heading Discrepancy Warning on the Upper ECAM Display Unit
 
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