(4) If the failure continues:
(a) Do a check of the aircraft wiring (Ref. ASM 27-51/06) and (Ref. ASM 27-51/07).
(b) Do the repair.
(c) Do the test given in Para. 3.A.(1).
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.
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Feb 01/99 CES
R FPPU Fault or FPPU to One SFCC Interface 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
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GEAR.
1. Possible Causes
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- SFCC-1 (21CV)
- SFCC-2 (22CV)
- 27CV (27CV)
- aircraft wiring
2. Job Set-up Information
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A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 27-50-00-866-008 Extension of the Flaps on the Ground AMM 27-50-00-866-009 Retraction of the Flaps on the Ground AMM 27-51-19-000-001 Removal the Feed Back Position Pick-Off Unit AMM 27-51-19-400-001 Installation of the Feed Back Position Pick-Off Unit AMM 27-51-34-000-001 Removal of the SFCC (21CV,22CV) AMM 27-51-34-400-001 Installation of the SFCC (21CV,22CV) AMM 27-54-00-710-001 Operational Test of the Flap System ASM 27-51/06 ASM 27-51/07
3. Fault Confirmation
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A. Table of the circuit breakers used in this procedure:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
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Feb 01/03 CES
INTENTIONALLY BLANK
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B. Reset and Inialization.
(1) At the circuit breakers.
(a) Open the circuit breakers.
(b) Wait for 3 seconds and close the circuit breakers.
(c) Wait for 60 seconds
(2) Move the flaps.(Ref. AMM TASK 27-50-00-866-008) (Ref. AMM TASK 27-50-00-866-009)
(a) Examine the UPPER ECAM and the SD FLT/CTL page for the fault warnings and System status.
(b) Access the FLP ON GROUND FAULTS log and do a check of the ground log.
(c) If an UPPER ECAM warning, SD FLT/CTL status and a ground log fault message, is displayed do the Fault Isolation.
(d) If the UPPER ECAM, SD FLT/CTL status and the FLP ON GROUND FAULTS log are clear.No further maintenance actions are required.
4. Fault Isolation
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A. Procedure.
(1) Set the MCDU to MENU MODE page 2 and access the submenu <FLP SYSTEM DATA.
(a) Press the line key 1R <PPU.
(b) Do a check of the PPU DATA (DEG) page. Refer to page block 301 table 2 for FPPU fault analysis.
R (c) If the no data "xxxx.x" is shown.
R (2) Swap SFCC 1 and SFCC 2, (Ref. AMM TASK 27-51-34-000-001) for (Ref. R AMM TASK 27-51-34-400-001) do Para. 2,3 and 4 only.
(a) Access the FLP ON GROUND FAULTS and do a check of the ground log.
(b) If the fault moves with SFCC 1(2).
(c) Install the SFCC 1 (2) in their initial locations.
(d) Replace the unserviceable SFCC-1 (21CV) (SFCC-2 (22CV)) Ref. Para.4.A.(2).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞27-51-00∞∞∞∞∞∞∞∞∞∞Page 209
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 飛行操縱 1(85)
