from the External Power
AMM 31-60-00-860-001 EIS Start Procedure
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 34-10-00-860-004 IR Alignment Procedure
ASM 22-85/02
3. Fault Confirmation
__________________
A. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU AUTO FLT/FCU/1 9CA1 B05 49VU AUTO FLT/FMGC/1 10CA1 B02 121VU AUTO FLT/FCU/2 9CA2 M21 121VU AUTO FLT/FMGC/2 10CA2 M17
Aug 01/05R CES
B. Aircraft Maintenance Configuration
(1) Align the ADIRS (Ref. AMM TASK 34-10-00-860-004).
(2) Do the EIS start procedure (PFD and ND only) (Ref. AMM TASK 31-60-00-860-001).
C. Test
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. Make sure that the two FDs are On the upper part of the CAPT PFD: engaged. - the white FD 1 indication is in view.
On the upper part of the F/O PFD: NOTE : If they are not engaged, - the white FD 2 indication is in view.
____
push the FD pushbutton
switches on the FCU.
On the FCU:
- the two FD pushbutton switches come on.
4. Fault Isolation
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A. If the FD 2 indication comes into view on the F/O PFD and if the FD 2 pushbutton switch does not come on:
- replace the FCU (2CA) (Ref. AMM TASK 22-81-12-000-001) and (Ref. AMM TASK 22-81-12-400-001).
(1) If the fault continues:
- do a check and repair the: . wiring of the FD 2 ENGD MON OWN discrete from the FCU (2CA) to the first terminal block . wiring of the FD 2 ENGD COM OWN discrete from the FCU (2CA) to the FMGC 2 (1CA2) (Ref. ASM 22-85/02).
B. If the FD 2 pushbutton switch comes on and if the FD 2 indication does not come into view on the F/O PFD:
- 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 and repair the wiring of the FD 2 ENGD discrete from the DMC 2 (1WT2) to the first terminal block (Ref. ASM 22-85/02).
「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 ∞∞22-83-00∞∞∞∞∞∞∞∞∞∞Page 251
Aug 01/05R CES
C. If the FD 2 indication does not come into view on the F/O PFD and if the FD 2 pushbutton switch does not come on: - open the circuit breaker (9CA2)
- close this circuit breaker and after 2 minutes make sure that the FD 2 is engaged.
(1) If the fault continues:
- replace the FMGC-2 (1CA2) (Ref. AMM TASK 22-83-34-000-001) and (Ref. AMM TASK 22-83-34-400-001).
(2) If the fault continues:
- do a check and repair the wiring of the FD OWN ENGD MON OWN discrete from the FMGC 2 (1CA2) to the first terminal block (Ref. ASM 22-85/02).
D. Do the test given in Para. 3.
5. Close-up
________
A. Put the aircraft back to its initial configuration.
(1) On the overhead panel, on the ADIRS CDU, set the OFF/NAV/ATT selector switches to OFF.
(2) On the panels 301VU and 500VU, set the PFD and ND potentiometers to OFF.
(3) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
「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 ∞∞22-83-00∞∞∞∞∞∞∞∞∞∞Page 252
Aug 01/05R
CES Loss of the Reception of the Data Link by one FMGC
1. Possible Causes
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- FMGC-1 (1CA1)
- FMGC-2 (1CA2)
- wiring of the ACARS bus from the FMGC 1 (1CA1) to the first terminal block
- wiring of the ACARS bus from the FMGC 2 (1CA2) to the first terminal block 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 AUTO FLIGHT 自動飛行2(77)
