3. Fault Confirmation
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A. SFCC system peripherals test.
(1) Do the SFCC1 (2) SYSTEM TEST (BITE) (Ref. AMM TASK 27-51-00-740-002). The fault data "FPPU disconnected or faulty and WTB's set" is displayed. Page block 301 Table 7 gives the SFCC test menu selection details.
(2) Do the fault isolation.
4. Fault Isolation
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A. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
B. Procedure
(1) Go to the maintenance procedure (Ref. AMM TASK 27-51-19-000-001) Figure 401/TASK 27-51-19 991 001 and find the FPPU 27CV (27CV).
(a) Swap the connectors 27CV-A and 27CV-B.
(b) Remove the safety clips and the tags and close the circuit breakers Ref.Para 4.A.
(c) Wait 60 seconds for SFCC initialization.
(d) Set the MENU MODE and access the FLP ON GROUND FAULTS and check the ground log.
(e) If the fault moves to SFCC 1 (2). Swap back the connectors 27CV-B and 27CV-A.
(f) Replace the 27CV (27CV), (Ref. AMM TASK 27-51-19-000-001) (Ref. AMM TASK 27-51-19-400-001)
(2) If the fault does not move
(3) Open, safety and tag the circuit breakers Ref.Para 4.A.
(4) Use ARINC connector breakout box and do a check of the aircraft wiring. Between the SFCC 1 (2) and the FPPU (Ref. ASM 27-51/06) (Ref. ASM 27-51/07)
(5) Do the repair
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞27-51-00∞∞∞∞∞∞∞∞∞∞Page 219
Feb 01/03R CES
(6) Connect the electrical connectors 27CV-A and 27CV-B to the FPPU.
(7) Remove the safety clips and the tags and close the circuit breakers Ref.Para.4.A.
(8) Wait 60 seconds for SFCC initialization.
(9) Set the MENU MODE and access the FLP ON GROUND FAULTS and check that the ground log is clear.
5. Close-up
________
A. Remove the ground support and maintenance equipment, the special and standard tools and all other items.
B. Put the aircraft back to its initial configuration.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞27-51-00∞∞∞∞∞∞∞∞∞∞Page 220
Feb 01/03R
CES APPU FLAP LH/RH Fault.
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
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START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
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CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
1. Possible Causes
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- SFCC-1 (21CV)
- SFCC-2 (22CV)
- APPU-L(R) FLAP 29CV (30CV)
- A/C Wiring between the SFCC 1 (2) and the APPU connectors 29CV-A (30CV-B)
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific ARINC Connector Breakout Box
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 27-51-00-740-002 Bite Test of the Slat and Flap Control Computers (Flap System) AMM 27-51-18-000-001 Removal of the Asymmetry-Position Pick-Off Unit 29CV (30CV) AMM 27-51-18-400-001 Installation of the Asymmetry-Position Pick-Off Unit
29CV (30CV)
AMM 27-51-34-000-001 Removal of the SFCC (21CV,22CV)
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 飛行操縱 1(89)
