System AMM 32-43-16-000-001 Removal of the Alternate Brake Safety-Valve AMM 32-43-16-400-001 Installation of the Alternate Brake Safety-Valve TSM 32-48-00-810-801 Brake Fan Inoperative on One Brake
3. Fault Confirmation
__________________
A. Test
(1) Not applicable.
4. Fault Isolation
_______________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299,
A. If the difference of temperature between the two brakes on a same gear is more than 150.C and either the temperature of one brake is more than 600.C or the temperature of one brake is less than 60.C:
- do a check for a message related to the braking system on the POST FLIGHT REPORT (PFR).
(1) If there is a message:
- you can find the related trouble shooting procedure in the 32 fault symptoms Page Block 101.
(2) If there is no message:
- do a check of the related self-sealing coupling connection.
- do the bleeding of the corresponding brake system at the brake units (Ref. AMM TASK 32-42-00-870-001) or (Ref. AMM TASK 32-43-00-870-002)
- do an inspection/check of the brake unit for leaks and damage. (Ref. AMM TASK 32-42-27-210-006)
(a) if necessary replace the BRAKE-WHEEL 2 (2641GM) or BRAKE-WHEEL 4 (2642GM) or BRAKE-WHEEL 1 (2643GM) or BRAKE-WHEEL 3 (2644GM) (Ref. AMM TASK 32-42-27-000-001) (Ref. AMM TASK 32-42-27-400-001)
(b) if there are no leak or damage:
- refer to (Ref. TSM TASK 32-48-00-810-801) if brake fans are installed.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞32-42-00∞∞∞∞∞∞∞∞∞∞Page A214
201-299, 401-499, Aug 01/05 CES
(3) If the inspections are correct:
- replace the SAFETY VALVE-NORM BRK, WHEEL 2 (2616GM) or SAFETY VALVE-NORM BRK, WHEEL 3 (2617GM) or SAFETY VALVE-NORM BRK, WHEEL 1 (2618GM) or SAFETY VALVE-NORM BRK, WHEEL 4 (2619GM) (Ref. AMM TASK 32-42-36-000-001) (Ref. AMM TASK 32-42-36-400-001) or SAFETY VALVE-ALTN BRK, WHEEL 4 (2621GM) or SAFETY VALVE-ALTN BRK, WHEEL 2 (2622GM) or SAFETY VALVE-ALTN BRK, WHEEL 3 (2623GM) or SAFETY VALVE-ALTN BRK, WHEEL 1 (2620GM) (Ref. AMM TASK 32-43-16-000-001) (Ref. AMM TASK 32-43-16-400-001)
(4) If the fault continues:
- replace the PRESS XDCR-NORM BRK WHEEL 1 (11GG) or PRESS XDCR-NORM BRK WHEEL 3 (12GG) or PRESS XDCR-NORM BRK WHEEL 2 (13GG) or PRESS XDCR-NORM BRK WHEEL 4 (14GG) (Ref. AMM TASK 32-42-21-000-001) (Ref. AMM TASK 32-42-21-400-001)
(5) If the fault continues:
- do an inspection of the drive assy of the related tachometer
(a) If the tachometer drive is damaged:
- replace the related drive assy-tachometer (Ref. AMM TASK 32-42-68-000-003) (Ref. AMM TASK 32-42-68-400-003)
(b) If the tachometer drive is not damaged:
- replace the related TACHOMETER (Ref. AMM TASK 32-42-57-000-001) (Ref. AMM TASK 32-42-57-400-001)
(6) If the fault continues:
- replaced the related NORMAL SERVO-VALVE (Ref. AMM TASK 32-42-48-000-001) (Ref. AMM TASK 32-42-48-400-001)
R **ON A/C 401-499,
R A. If the difference of temperature between the two brakes on a same gear is
R more than 150.C and either the temperature of one brake is more than
R 600.C or the temperature of one brake is less than 60.C:
R - do a check for a message related to the braking system on the POST
R FLIGHT REPORT (PFR).
R (1) If there is a message:
R - you can find the related trouble shooting procedure in the 32 fault
R symptoms Page Block 101.
R (2) If there is no message:
R - do a check of the related self-sealing coupling connection.
R - do the bleeding of the corresponding brake system at the brake
R units (Ref. AMM TASK 32-42-00-870-001) or (Ref. AMM TASK 32-43-00-R 870-002)
R - do an inspection/check of the brake unit for leaks and damage.
R (Ref. AMM TASK 32-42-27-210-006)
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞32-42-00∞∞∞∞∞∞∞∞∞∞Page A215
201-299, 401-499, Aug 01/05 CES 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞32-42-00∞∞∞∞∞∞∞∞∞∞Page A216
R (a) if necessary replace the BRAKE-WHEEL 2 (2641GM) or BRAKE-WHEEL 4
R (2642GM) or BRAKE-WHEEL 1 (2643GM) or BRAKE-WHEEL 3 (2644GM)
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