5. Close-up
________
A. Put the aircraft back to its initial configuration.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞32-31-00∞∞∞∞∞∞∞∞∞∞Page 278
May 01/05R
CES
TASK 32-31-00-810-833
Cargo Door (Aft) Safety Mechanism Proximity Sensor Fault (32WV)
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
1. Possible Causes
_______________
- LGCIU-1 (5GA1)
- 32WV
- aircraft wiring.
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific Multimeter
No specific 50Vdc Isolation Tester
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
ASM 315400S05
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 AMM 52-71-12-000-002 Removal of the Proximity Switches 30WV and 32WV AMM 52-71-12-400-002 Installation of the Proximity Switches 30WV and 32WV
3. Fault Confirmation
__________________
A. Message Analysis.
(1) Do a BITE test on the LGCIU-1 (Ref. AMM TASK 32-69-00-740-001)
(a) Access LGCIU-1 TROUBLE SHOOTING (ground) and read the BITE test fault number(s) for fault confirmation (refer to AMM 326900 table 4).
NOTE : The table 4 shows the fault messages approximate to the
____
CFDS message
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞32-31-00∞∞∞∞∞∞∞∞∞∞Page 279
May 01/05R CES
(2) Do the fault isolation.
4. Fault Isolation
_______________
A. Cargo Compartment Control.
(1) The proximity sensor 32WV is installed in the AFT cargo door.
(a) Refer to (Ref. AMM TASK 52-71-12-000-002) Figure 402/TASK 52-71-12-991-002-A for the proximity sensor 32WV location and:
(b) Refer (Ref. AMM TASK 52-71-12-000-002) to and find the proximity sensor 32WV
(c) Release the electrical connector for 32WV. NOTE : If the ELDEC proximity sensor test unit is available. Go
____ to page block 301 and do the procedure in table 5.
(2) Use a Multimeter and do a check of the resistance between the pins A and B of the PROX. SNSR, (Ref. ASM 315400S05) the resistance must be approximately 13ohms.
(3) On the PROX SNSR do a check of circuit isolation.
(a) Connect the pins A & B together.
(b) Connect one test lead of the 50Vdc Isolation Tester to the pins AB and the other test lead to the case.
(c) Supply a test signal for 5 seconds and read the resistance value shown.
(d) The resistance value must be more than 400Megohms.
(4) If the 32WV fails one of the two (2) test at Para.4.A.(2) or (3) replace the unserviceable proximity sensor(Ref. AMM TASK 52-71-12-000-002) (Ref. AMM TASK 52-71-12-400-002).
(5) If the tests at Para.4.A.(2) and (3) are satisfactory then do a check of the aircraft wiring. between the applicable proximity sensor electrical connector and the LGCIU- 1 ARINC tray
(6) If there is no continuity repair the wiring/interface.
(7) Do the L/G BITE test as in Para.3.A.(1).
(8) If no fault is found at Para.4.A.(5), replace the LGCIU-1 (5GA1) (Ref. AMM TASK 32-31-71-000-001) (Ref. AMM TASK 32-31-71-400-001).
(9) Do the GROUND SCANNING to check that there are no fault entries in the ground log.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞32-31-00∞∞∞∞∞∞∞∞∞∞Page 280
May 01/05R CES
5. Close-up
________
A. Put the aircraft back to its initial configuration.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞32-31-00∞∞∞∞∞∞∞∞∞∞Page 281
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320 Trouble Shooting Manual 排故手册 起落架 LANDING GEAR 1(33)
