WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
1. Possible Causes
_______________
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 27-50-00-869-006 Reset of the Wing Tip Brake (WTB) of the Flap System on the Ground AMM 27-51-00-740-002 Bite Test of the Slat and Flap Control Computers (Flap System)
3. Fault Confirmation
__________________
A. Test
(1) When you start the APU with the batteries, the warning message "F/CTL FLAPS LOCKED" can show on the upper ECAM DU. Also, the Wing Tip Brakes (WTB) are applied.
NOTE : The ECAM message "F/CTL SLATS LOCKED" can also show.
____
4. Fault Isolation
_______________
A. Procedure
(1) Do a reset of the WTBs of the Flap System (Ref. AMM TASK 27-50-00-869-006).
(2) Do a BITE test of the SFCC (Ref. AMM TASK 27-51-00-740-002): R - If the test gives a fault message, do the trouble shooting R procedure related to this fault message.
「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 A205
May 01/05 CES Flaps - SFCC TEST Gives the Message NO FAULTS BUT
1. Possible Causes
_______________
2. Job Set-up Information
______________________
Not Applicable
3. Fault Confirmation
__________________
A. Test
(1) Do Para. 4. if the FLAPS SFCC TEST gives the message NO FAULTS BUT, with any of the messages that follow:
- OTHER SFCC ARM SIGNAL NOT TESTED
or
- WTB SET
and/or
- NO WTB POWER
- LH WTB SOLENOID S/C (or O/C)
- RH WTB SOLENOID S/C (or O/C)
- LH APPU FAULT
- FPPU FAULT
- RH APPU FAULT
4. Fault Isolation
_______________
A. Procedure
(1) At the MCDU access the CFDS MENU then LAST LEG REPORT to see if a related fault message was given during normal system operation. The table that follows shows the relationship between the messages given during the SFCC TEST and normal mode, it also gives the related trouble shooting task. Do Para. 4.A. of the applicable task.
NOTE : A fault message given during normal mode will make sure that
____ the fault identified during the SFCC TEST is correct. It will also give the FIN of the defective component.
「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 A206
May 01/05R
CES ---------------------------------------------------------------------------SFCC TEST CFDS LAST LEG REPORT TS TASK IN
MESSAGE MESSAGE 27-51-00 ----------------------------------------------------------------------------OTHER SFCC FLP 1 (2) NO SFCC 2 (1) DATA
804 SIGNAL NOT TESTED
NO WTB POWER FLP 1 (2) WTB C/B 10CV (12CV) 835
LH WTB SOLENOID FLP LH WTB BLU (YEL) SOLENOID
836 S/C (or O/C) 33CV OR WIRING TO FLP 1 (2)
RH WTB SOLENOID FLP RH WTB BLU (GRN) SOLENOID 837 S/C (or O/C) 34CV OR WIRING TO SLT 1 (2)
LH APPU FAULT LH FLP APPU 29CV OR WIRING TO 809 FLP 1 (2) FPPU FAULT FLP FPPU 27CV OR WIRING TO 808 FLP 1 (2) RH APPU FAULT RH FLP APPU 30CV OR WIRING TO 809 FLP 1 (2) ----------------------------------------------------------------------------
NOTE : The LAST LEG REPORT messages shown are for SFCC1, the items in
____
( ) are for SFCC 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 A207
May 01/05R
CES Flaps - SFCC 1 and SFCC 2 Show PCU Valveblock Fault Message (23CV, 24CV)
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
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 GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 飛行操縱 2(16)
