「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : 401-499, ∞∞32-43-00∞∞∞∞∞∞∞∞∞∞Page 250
Aug 01/05 CES
R (8) If the fault continues:
R - replace the HYDR. PRESSURE TRANSMITTER (3068GN) (Ref. AMM TASK 29-
R 32-11-000-004) (Ref. AMM TASK 29-32-11-400-004).
R (9) If the fault continues:
R - replace the MANIFOLD (3016GM) (Ref. AMM TASK 32-44-17-000-001)
R (Ref. AMM TASK 32-44-17-400-001).
R (10) If the fault continues:
R - replace the ABCU (95GG) (Ref. AMM TASK 32-43-34-000-001) (Ref. AMM
R TASK 32-43-34-400-001).
R TASK 32-43-00-810-836 R Failure of ABCU R 1. Possible Causes
_______________
R - PRESS XDCR-NORM BRK SPLY (96GG)
R - ABCU (95GG)
R 2. Job Set-up Information
______________________
R A. Referenced Information
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R AMM 31-32-00-869-002 R AMM 32-42-22-000-001 R R AMM 32-42-22-400-001 R R AMM 32-43-34-000-001 R R AMM 32-43-34-400-001 R R AMM 32-46-00-740-001
R 3. Fault Confirmation
__________________
R A. Test
Procedure for Class 3 Faults Reading
Removal of the Normal-Brake Supply
Pressure-Transducer (96GG)
Installation of the Normal-Brake Supply
Pressure-Transducer (96GG)
Removal of the Alternate Braking Control Unit (ABCU)
(95GG)
Installation of the Alternate Braking Control Unit
(ABCU) (95GG)
BITE Test of the BSCU
R On the CFDS MENU page, get access to the AVIONICS STATUS page (Ref. AMM R TASK 31-32-00-869-002).
R 4. Fault Isolation
_______________
R A. If the test gives the maintenance message BRK NORM SELECTOR VALVE PRESS
R TRANSDUCER (96GG):
R - replace the PRESS XDCR-NORM BRK SPLY (96GG) (Ref. AMM TASK 32-42-22-R 000-001) and (Ref. AMM TASK 32-42-22-400-001).
R (1) If the test does not give the maintenance message BRK NORM SELECTOR
R VALVE PRESS TRANSDUCER (96GG):
R - do the BITE test of the BSCU (Ref. AMM TASK 32-46-00-740-001).
R (2) If the BITE test gives the maintenance message ABCU (95GG)
R - replace the ABCU (95GG) (Ref. AMM TASK 32-43-34-000-001) and (Ref.
R AMM TASK 32-43-34-400-001).
R B. Do the test given in para. 4.A.(1)
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : 401-499, ∞∞32-43-00∞∞∞∞∞∞∞∞∞∞Page 252
Aug 01/05 CES
ALTERNATE BRAKING WITHOUT ANTI SKID - FAULT ISOLATION PROCEDURES
________________________________________________________________
TASK 32-44-00-810-801
Loss of the Right Yellow Pressure Indication on the Triple Indicator (Electrical Failure)
1. Possible Causes_______________
R R R R R - PRESS XDCR-BRK,YELLOW R (62GG) - PRESS XDCR-BRK, YELLOW R (100GG) - wiring from the right Yellow brake pressure-transducer 62GG pins A/D, E to the first terminal block - wiring from the right Yellow brake pressure-transducer 62GG pin A/A to the first terminal block - wiring from the right Yellow brake pressure-transducer 100GG pins A/D, E to the first terminal block - wiring from the right Yellow brake pressure-transducer 100GG pin A/A to the first terminal block
2. Job Set-up Information______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R AMM AMM AMM AMM AMM ASM 31-50-00-710-001 32-44-18-000-001 32-44-18-400-001 32-44-19-000-001 32-44-19-400-001 32-44/01 Ground Scanning of the Central Warning SystemRemoval of the Pressure Transducers 62GG, 63GGInstallation of the Pressure Transducers 62GG, 63GG Removal of the Pressure Transducer 100GG(101GG) Installation of the Pressure Transducer 100GG(101GG)
3. Fault Confirmation__________________
A. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
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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(49)
