TASK 32-31-00-810-802 LGCIU Fault WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
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GEAR.
1. Possible Causes
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- LGCIU-1 (5GA1)
- LGCIU-2 (5GA2)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 31-32-00-860-009 Procedure to Get Access to the SYSTEM REPORT/TEST/L/G
Page
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 32-69-00-740-001 BITE Check Landing Gear Control Interface Unit R (LGCIU) using MCDU to Ensure that Continuous BITE is R Operative
3. Fault Confirmation
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A. Test
(1) Do the bite test of the LGCIU identified on the post flight report, (Ref. AMM TASK 32-69-00-740-001).
4. Fault Isolation
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A. Procedure
(1) If the BITE test result shows a fault message:
(a) Swop the LGCIU-1 and LGCIU-2, (Ref. AMM TASK 32-31-71-000-001) and (Ref. AMM TASK 32-31-71-400-001).
(2) If the fault moves to the other LGCIU position:
(a) Swop the LGCIU-1 and LGCIU-2 back and replace the defective LGCIU-1 (5GA1) or LGCIU-2 (5GA2), (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 204
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(3) If the fault does not move to the other LGCIU position, or TEST OK is shown:
(a) Get access to the SYSTEM REPORT/TEST/L/G page. Use the procedure (Ref. AMM TASK 31-32-00-860-009).
(b) On the MCDU at the LGCIU main menu, press the TROUBLE SHOOT DATA line key.
(c) Make a note of any fault code(s).
(d) Trouble shoot any fault code shown that occurred on the last flight, (Ref. P.Block 301), if the fault code refers to this task, replace the applicable LGCIU. Ref. Para. (2).
R (4) Make sure that the serviceable LGCIU is installed in its initial R postion.
5. Close-up
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A. Put the aircraft back to its initial configuration.
TASK 32-31-00-810-804
LGCIU Selection. Hardware/Control Determination.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
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GEAR.
1. Possible Causes
_______________
- LGCIU-1 (5GA1)
- LGCIU-2 (5GA2)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 32-31-00-440-002 Reactivation of the Landing Gear Control and
Interface Unit (LGCIU) Number 2
AMM 32-31-71-000-001 Removal of the LGCIU (5GA1, 5GA2)
AMM 32-31-71-400-001 Installation of the LGCIU (5GA1, 5GA2)
3. Fault Confirmation
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A. Message Analysis
(1) Examine the Post Flight Report (PFR) to find the flight-phase and
time-difference of the reported faults. R - if the LGCIU-1 and LGCIU-2 faults occurred during different flight R phases, do the trouble shooting procedures related to the R maintenance messages.
- if the LGCIU-1 and LGCIU-2 faults occurred at the same time, do the fault isolation procedure in Para. 4.A.
4. Fault Isolation
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A. Table of the circuit breakers used in this procedure:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU L/G/LGCIU/SYS1/NORM 1GA C09 121VU HYDRAULIC/LGCIU/SYS2 2GA Q35 121VU HYDRAULIC/LGCIU/SYS1/GRND SPLY 52GA Q34
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞32-31-00∞∞∞∞∞∞∞∞∞∞Page 206
May 01/05 CES
B. Procedure
(1) Open the C/B 2GA. This will isolate LGCIU2.
(2) Open the C/Bs 1GA and 52GA for 3 seconds and then close them. This will cause the LGCIU1 to do a power-up BITE test.
(a) Wait 60 seconds.
(3) Do a check of the UPPER ECAM and STATUS pages and check that the fault warnings go: 中國(guó)航空網(wǎng) www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) 起落架 LANDING GEAR 1(6)
