「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞32-31-00∞∞∞∞∞∞∞∞∞∞Page A283
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(3) Replace the initial LGCIU-1 (5GA1) or LGCIU-2 (5GA2), (Ref. AMM TASK 32-31-71-000-001) and (Ref. AMM TASK 32-31-71-400-001).
(4) Make sure that the serviceable LGCIU is installed in its initial position.
(5) Do the test given in Para 3:
- if the fault continues, do the step at Para. (7).
(6) Replace the CFDIU (1TW), (Ref. AMM TASK 31-32-34-000-001) and (Ref. AMM TASK 31-32-34-400-001).
(7) Do the test given in Para. 3.
- if the fault continues, do the next step.
(8) Do a check of the aircraft wiring ARINC-comnnection between the LGCIU 1(2) and the CFDIU (Ref. ASM 32-61/02), and repair as necessary.
(9) Do the test given in Para. 3.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞32-31-00∞∞∞∞∞∞∞∞∞∞Page A284
Aug 01/05R
CES
TASK 32-31-00-810-881
LGCIU - The EFCS Does Not Receive Data from the LGCIU
1. Possible Causes
_______________
- LGCIU-1 (5GA1)
- LGCIU-2 (5GA2)
- aircraft wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 31-60-00-860-001 EIS Start Procedure
AMM 32-31-71-000-001 Removal of the LGCIU (5GA1, 5GA2)
AMM 32-31-71-400-001 Installation of the LGCIU (5GA1, 5GA2)
ASM 32-31/03
ASM 32-31/04
3. Fault Confirmation
__________________
A. Test
(1) Do the EIS Start Procedure (Upper and Lower ECAM DU only) (Ref. AMM TASK 31-60-00-860-001).
(2) At the ECAM Control Panel set the STS page.
(3) Look at the Status Page for the message LGCIU 1 (2).
- if the message is shown, do the fault isolation procedure in Para.
4.A.
- if the message is not shown, there is no LGCIU 1 (2) fault.
4. Fault Isolation
_______________
A. Procedure
(1) Interchange LGCIU 1 with LGCIU 2, (Ref. AMM TASK 32-31-71-000-001) and (Ref. AMM TASK 32-31-71-400-001).
(2) Do the test in Para. 3.A:
- if the fault stays in the initial system (identified in the failure message), do step (5)
- if the fault moves to the opposite system, do the next step.
(3) Replace the unserviceable LGCIU-1 (5GA1) or LGCIU-2 (5GA2).
Aug 01/05R CES
(4) Make sure that the serviceable LGCIU is installed in its initial position.
(5) Do the test in Para. 3.A:
- if the fault continues do the next step.
(6) Do a check and repair the aircraft wiring between the applicable LGCIU and its related 28 VDC power supply C/B, (Ref. ASM 32-31/03) or (Ref. ASM 32-31/04).
(7) Do the test in Para. 3.A.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞32-31-00∞∞∞∞∞∞∞∞∞∞Page A286
Aug 01/05R
CES
TASK 32-31-00-810-882
L/G - GEAR NOT DOWN Message Caused by Downlock Proximity Switch Fault (14GA thru 19GA)
1. Possible Causes
_______________
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 31-60-00-860-001 EIS Start Procedure AMM 32-31-73-200-001 Inspection of the MLG Proximity Sensor and Target Clearances AMM 32-31-73-200-002 Inspection of the NLG Proximity Sensor and Target Clearances
3. Fault Confirmation
__________________
A. Test
(1) If the ECAM message L/G GEAR NOT DOWN occurs in flight, but is not shown on the Post Flight Report (PFR), there is no test:
- do the fault isolation procedure in Para. 4.A., for the six downlock proximity sensors (14GA thru 19GA).
NOTE : An incorrectly adjusted downlock proximity switch can give the
____ message L/G GEAR NOT DOWN, which can be an intermittent fault. Some intermittent faults are not recorded on the PFR.
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) 起落架 LANDING GEAR 1(74)
