(5) Replace the applicable proximity-sensor (Ref. AMM TASK 52-71-12-000-001) and (Ref. AMM TASK 52-71-12-400-001):

 - if the fault continues, do step (6).

 (6) Replace the applicable LGCIU:

 - if the PFR shows a message related to proximity-switches 28W, 30W, 32W or 34W, replace the LGCIU-1 (5GA1), (Ref. AMM TASK 32-31-71-000-001) and (Ref. AMM TASK 32-31-71-400-001)

 - if the PFR shows a message related to proximity-switches 05MJ or 12MJ, replace the LGCIU-2 (5GA2) (Ref. AMM TASK 32-31-71-000-001) and (Ref. AMM TASK 32-31-71-400-001).

 (a) Do the test in Para 3.A.
 NOTE : To identify a TGT POS fault, the LGCIU has to be correctly
____ connected to the related proximity sensor. Thus a check of the aircraft wiring is not necessary.
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞32-31-00∞∞∞∞∞∞∞∞∞∞Page A281
 Aug 01/05R
 CES  TASK 32-31-00-810-878 Landing Gear and Doors Retract OK When Recycled WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING

_______
 GEAR.

 WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
 START A TASK ON OR NEAR:

 - THE FLIGHT CONTROLS

 - THE FLIGHT CONTROL SURFACES

 - THE LANDING GEAR AND THE RELATED DOORS

 - COMPONENTS THAT MOVE.

 1. Possible Causes
_______________
 - PROX SNSR-NLG R DOOR OPEN, SYS 1 (36GA)

 - PROX SNSR-NLG L DOOR OPEN, SYS 1 (37GA)

 - PROX SNSR-NLG R DOOR OPEN, SYS 2 (38GA)

 - PROX SNSR-NLG L DOOR OPEN, SYS 2 (39GA)

 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
32-31-00-810-854 L/G Proximity Sensor TGT POS Fault
 3. Fault Confirmation
__________________
 A. Test
 (1) You cannot create the fault condition on the ground. NOTE : The fault messages shown on the Post Flight Report occur
____ because the NLG door/s move away from the locked down position before the NLG completes the retraction cycle.
 4. Fault Isolation
_______________
 A. Procedure
 (1) Do the task (Ref. TASK 32-31-00-810-854) and make sure that these proximity sensors PROX SNSR-NLG R DOOR OPEN, SYS 1 (36GA), PROX SNSR-NLG L DOOR OPEN, SYS 1 (37GA), PROX SNSR-NLG R DOOR OPEN, SYS 2 (38GA) and PROX SNSR-NLG L DOOR OPEN, SYS 2 (39GA) and the clearance with their related targets are OK.
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞32-31-00∞∞∞∞∞∞∞∞∞∞Page A282
 Aug 01/05R CES

 TASK 32-31-00-810-879
 LGCIU - No Data from CFDS
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
 GEAR.

 1. Possible Causes
_______________
 - LGCIU-1 (5GA1)

 - LGCIU-2 (5GA2)

 - CFDIU (1TW)

 - aircraft wiring

 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 31-32-34-000-001 Removal of the CFDIU (1TW)
 AMM 31-32-34-400-001 Installation of the CFDIU (1TW)
 AMM 32-31-71-000-001 Removal of the LGCIU (5GA1, 5GA2)
 AMM 32-31-71-400-001 Installation of the LGCIU (5GA1, 5GA2)
 AMM 32-69-00-740-001 BITE Check Landing Gear Control Interface Unit

 (LGCIU) using MCDU to Ensure that Continuous BITE is Operative ASM 32-61/02
 3. Fault Confirmation
__________________
 A. Test
 (1) Do a BITE test of the applicable LGCIU 1(2) (Ref. AMM TASK 32-69-00-740-001):
 - if the test result is TEST OK, or END OF TEST, there is no fault

 - if the test does not start, do the fault isolation procedure given in Para. 4.

 4. Fault Isolation
_______________
 A. Procedure
 (1) Interchange LGCIU 1 with LGCIU 2.

 (2) Do the test given in Para 3:

 - if the test does not start, do the step at Para. (5)

 - if the test result is TEST OK, or END OF TEST, do the next step.

 
　
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