(7) Replace the applicable LGCIU-1 (5GA1) or LGCIU-2 (5GA2) which identified the fault, (Ref. AMM TASK 32-31-71-000-001) and (Ref. AMM TASK 32-31-71-400-001).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞32-31-00∞∞∞∞∞∞∞∞∞∞Page 293
May 01/05R
CES TASK 32-31-00-810-839
LGCIU BITE Test Not Possible
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
1. Possible Causes
_______________
- BSCU (10GG)
- LGCIU-1 (5GA1)
- LGCIU-2 (5GA2)
- relay 24GG(25GG)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION
-------------------------------------------------------------------------------
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 32-42-34-400-001 Installation of the Braking/Steering Control Unit
(BSCU) (10GG)
AMM 32-69-00-740-001 BITE Check Landing Gear Control Interface Unit (LGCIU) using MCDU to Ensure that Continuous BITE is Operative
ASM 32-31/03
ASM 32-31/04
ASM 32-42/01
3. Fault Confirmation
__________________
A. Do a bite test on LGCIU 1 and LGCIU 2 (Ref. AMM TASK 32-69-00-740-001).
4. Fault Isolation
_______________
A. If the LGCIU 1 and LGCIU 2 display CFDS fault messages, replace the BSCU (10GG) (Ref. AMM TASK 32-42-34-400-001) and (Ref. AMM TASK 32-42-34-400-001).
(1) Do the test (Ref. Para 3. A.).
(2) If only one LGCIU displays CFDS fault messages, swap the LGCIU positions (Ref. AMM TASK 32-31-71-000-001) and (Ref. AMM TASK 32-31-71-400-001).
(3) If the fault moves with the LGCIU, swap back the LGCIU's and replace the defective LGCIU-1 (5GA1) or LGCIU-2 (5GA2) (Ref. Para 4. A. (2)).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞32-31-00∞∞∞∞∞∞∞∞∞∞Page 294
May 01/05R CES
(4) If the fault stays in the same system, do a check for ground at the LGCIU 1(2) connector AA pin 9H (Ref. ASM 32-31/03) or (Ref. ASM 32-31/04).
(5) If there is a ground, replace the LGCIU 1(2) (Ref. Para 4. A. (2)).
(6) If there is no ground, do a check for ground at the relay 24GG(25GG) connector AA pin Z (Ref. ASM 32-42/01).
(7) If there is a ground, replace the BSCU (Ref. para 4. A.).
(8) If there is no ground, replace the relay 24GG(25GG).
(9) Do a bite test of the LGCIU 1(2) (Ref. 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 295
May 01/05R
CES
TASK 32-31-00-810-840
L/G Door Fully Open Proximity Sensor TGT POS Fault (32GA thru 39GA)
1. Possible Causes
_______________
- PROX SNSR-R L/G DOOR OPEN, SYS 1 (32GA)
- PROX SNSR-L L/G DOOR OPEN, SYS 1 (33GA)
- PROX SNSR-L L/G DOOR OPEN, SYS 2 (35GA)
- 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)
- PROX SNSR-R L/G DOOR OPEN, SYS 2 (34GA)
- aircraft wiring
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific inductance meter
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R AMM 32-00-00-860-001 Flight Configuration Precautions with Electrical
R Power AMM 32-12-00-010-001 Open the Main Gear Doors for Access AMM 32-12-00-410-001 Close the Main Gear Doors after Access AMM 32-22-00-010-001 Nose Gear Doors - Ground Doors Opening AMM 32-22-00-410-001 Nose Gear Doors - Ground Doors Closing 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 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)...
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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(38)
