「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞32-31-00∞∞∞∞∞∞∞∞∞∞Page 298
 May 01/05R CES

 (7) Do the test in para 3.B.

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞32-31-00∞∞∞∞∞∞∞∞∞∞Page 299
 May 01/05R
 CES

 TASK 32-31-00-810-842

 L/G Shock Absorber Extended Proximity Sensor TGT POS Fault (20GA thru 25GA)
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
 GEAR.

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

 - LGCIU-2 (5GA2)

 - shock-absorber proximity-sensor

 - 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
 -------------------------------------------------------------------------------
32-31-00-810-885 L/G - Lever Does Not Move - Retraction Inhibit Baulk Solenoid Does Not Release AMM 32-31-00-720-002 Functional Test of the Normal Extension and Retraction of the Landing Gear AMM 32-31-00-720-003 Functional Test of the Normal Extension and
 Retraction of the Nose Landing Gear
 AMM 32-31-71-000-001 Removal of the LGCIU (5GA1, 5GA2)
 AMM 32-31-71-400-001 Installation of the LGCIU (5GA1, 5GA2)

R AMM 32-31-73-000-001 Removal of the Proximity-Sensors 9GA(8GA), 11GA(10GA), 27GA(26GA), 29GA(28GA), 15GA(14GA), 17GA(16GA), 21GA(20GA), 23GA(22GA), 33GA(32GA), 35GA(34GA) AMM 32-31-73-000-005 Removal of the NLG Proximity-Sensors 12GA, 13GA, 18GA, 19GA, 24GA, 25GA, 30GA, 31GA, 37GA (36GA), 39GA (38GA) 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
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞32-31-00∞∞∞∞∞∞∞∞∞∞Page A200
 May 01/05 CES

 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
AMM 32-31-73-400-001  Installation of the Proximity-Sensors 9GA(8GA), 11GA(10GA), 27GA(26GA), 29GA(28GA), 15GA(14GA), 17GA(16GA), 21GA(20GA), 23GA(22GA), 33GA(32GA)...
 AMM 32-31-73-400-005  Installation of the NLG Proximity-Sensors 12GA, 13GA, 18GA, 19GA, 24GA, 25GA, 30GA, 31GA, 37GA (36GA), 39GA (38GA)
R  AMM 32-31-73-820-008 Inductance Check of the Proximity Sensors/Switches ASM 32-31/03 ASM 32-31/04
 3. Fault Confirmation
__________________
 A. Test
 (1) If a shock-absorber proximity-sensor (20GA thru 25GA) target position message is shown on the Post Flight Report (PFR), do the applicable functional test of the Main L/G (Ref. AMM TASK 32-31-00-720-002), or Nose L/G (Ref. AMM TASK 32-31-00-720-003):
 - if the initial test is OK, continue and do the inductance check in Para. 4.A., for all the shock-absorber proximity-sensors

 - if during the initial test, the L/G control lever does not move to the UP position, do the fault isolation procedures in Para. 4.A., then do the trouble shooting for the L/G control-lever baulk-solenoid (Ref. TASK 32-31-00-810-885)

 - if a subsequent test is OK, after the fault isolation procedure(s) has been done, no more maintenance work is necessary.

 NOTE : If the L/G lever does not move to the UP position there will
____ be two faults, one in System 1 and one in System 2. If the shock-absorber proximity-sensors are serviceable and the L/G lever does not move, then the two faults are in the L/G lever unit, or the LGCIU, or the related aircraft wiring. If one of the two faults goes, the L/G lever will operate correctly, but the fault in the opposite system stays. Thus it is also necessary to do the L/G lever trouble shooting task to find the other fault.
 4. Fault Isolation
_______________
 A. Procedure
 (1) For the applicable proximity sensor shown on the Post Flight Report (PFR), do the inspection of the gap between the proximity-sensor and its target, (Ref. AMM TASK 32-31-73-200-001) or (Ref. AMM TASK 32-31-73-200-002).
　
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 起落架 LANDING GEAR 1(40)