R (1) If the fault continue:
R - do a check and repair the wiring between the BSCU (10GG) and the
R Transducer (96GG) pin AB/7E to pin A/D and pin AB/7F to pin A/E.
R B. Do the test given in Para.3.A.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 401-499, ∞∞32-42-00∞∞∞∞∞∞∞∞∞∞Page A261
Aug 01/05 CESR **ON A/C ALL
R TASK 32-42-00-810-946
R Smoke and Dust on One Brake During Taxi with the Brakes not Operated
R 1. Possible Causes
_______________
R - WHEEL-MLG, 2 (2649GM) R - WHEEL-MLG, 4 (2650GM) R - WHEEL-MLG, 1 (2651GM) R - WHEEL-MLG, 3 (2652GM) R - BRAKE-WHEEL 2 (2641GM) R - BRAKE-WHEEL 4 (2642GM) R - BRAKE-WHEEL 1 (2643GM) R - BRAKE-WHEEL 3 (2644GM)
R 2. Job Set-up Information
______________________
R A. Referenced Information
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R AMM 07-12-00-582-002 R AMM 32-41-00-210-002 R AMM 32-41-11-000-006 R R AMM 32-41-11-400-006 R R AMM 32-42-27-000-001 R AMM 32-42-27-210-001 R R AMM 32-42-27-210-006 R AMM 32-42-27-400-001 R
R 3. Fault Confirmation
__________________
R A. Test Jacking for Main Gear Wheel Change Inspection/Check of the Wheels and Tires Removal of the MLG Wheel (2649GM,2650GM,2651GM,2652GM) Installation of the MLG Wheel (2649GM,2650GM,2651GM,2652GM) Removal of the Brake (2641GM,2642GM,2643GM,2644GM) Inspection/Check of the Brake with the Wheel Installed Inspection/Check of the Brake with the Wheel Removed Installation of the Brake (2641GM,2642GM,2643GM,2644GM)
R Not applicable, the fault is evident. R 4. Fault Isolation
_______________ R A. If there is smoke and dust during taxi with the brakes not operated: R (1) Lift the related axle with a jack (Ref. AMM TASK 07-12-00-582-002). R (2) Do a visual inspection/check of the related wheel (Ref. AMM TASK 32-
R 41-00-210-002).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞32-42-00∞∞∞∞∞∞∞∞∞∞Page A262
Feb 01/05 CES
R (3) If the visual inspection/check of the wheel is OK:
R (a) Turn the wheel and do the inspection/check of the brake with the
R wheel installed (Ref. AMM TASK 32-42-27-210-001) and make sure
R during rotation that:
R - there is no vibration and abnormal noise
R - no metallic or carbon pieces fall down from the brake or the
R wheel
R - there is no dust on the brake.
R (4) If the inspection/check of the brake with the wheel installed is OK:
R - do the steps (7)(b) and (c).
R - after the subsequent flight, make sure that the fault does not
R continue.
R (5) If you are not sure of the condition or if the inspection of the
R brake with the wheel installed is not OK:
R (a) Remove the related WHEEL-MLG, 2 (2649GM) or WHEEL-MLG, 4 (2650GM)
R or WHEEL-MLG, 1 (2651GM) or WHEEL-MLG, 3 (2652GM) (Ref. AMM TASK
R 32-41-11-000-006).
R (b) Do the inspection/check of the related brake with the wheel
R removed (Ref. AMM TASK 32-42-27-210-006).
R (6) If the inspection/check of the related brake with the wheel removed
R is not OK:
R (a) Replace the defective BRAKE-WHEEL 2 (2641GM) or BRAKE-WHEEL 4
R (2642GM) or BRAKE-WHEEL 1 (2643GM) or BRAKE-WHEEL 3 (2644GM)
R (Ref. AMM TASK 32-42-27-000-001) (Ref. AMM TASK 32-42-27-400-001)
R and do the steps that follow.
R (7) If the inspection/check of the related brake with the wheel removed
R is OK:
R (a) Install the related wheel (Ref. AMM TASK 32-41-11-400-006).
R (b) Lower the aircraft on its wheels (Ref. AMM TASK 07-12-00-582-R 002).
R (c) Make sure that the work area is clean and clear of tool(s) and
R other items.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞32-42-00∞∞∞∞∞∞∞∞∞∞Page A263
Feb 01/05 CES NORMAL BRAKING - TASK SUPPORTING DATA
_____________________________________
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-220, 301-399,
1. TROUBLE SHOOTING DATA of the BSCU
_________________________________
A. CFDS BSCU Messages decoding:
(1) On the center pedestal, on the MCDU, get the MCDU MENU page: - on the MCDU MENU page, push the line key adjacent to the CFDS indication - on the CFDS MENU page, push the line key adjacent to the SYSTEM REPORT/TEST indication - on the SYSTEM REPORT/TEST page, push the line key adjacent to the L/G indication - on the SYSTEM REPORT/TEST/L/G page, push the line key adjacent to the BSCU1 indication
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) 起落架 LANDING GEAR 2(31)
