F/CTL Page ASM 27-81/08
3. Fault Confirmation
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A. Test
(1) Get access to the SYSTEM REPORT/TEST F/CTL (Ref. AMM TASK 31-32-00-860-006), press the line key for the applicable SFCC menu, and press the line key for SLT class 3 faults.
(2) If you can get access to the SFCC menu, and SLT class 3 faults, the fault has gone. The system is also serviceable if "PIN PROGRAM DISAGREE INSTALLATION" is shown in class 3 faults, no further action is required. The fault has gone but it has been recorded.
(3) If you cannot get access to the SFCC menu, do the fault isolation procedure.
4. Fault Isolation
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A. Procedure NOTE : During this procedure when you interchange, remove or install an
____ SFCC, the AMM procedures (Ref. AMM TASK 27-51-34-000-001) and (Ref. AMM TASK 27-51-34-400-001) must be used.
「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 ∞∞27-81-00∞∞∞∞∞∞∞∞∞∞Page 272
May 01/05R
CES
(1) If the message "pin prog disagree slt" is shown:
(a) Interchange the SFCC-1 (21CV) with SFCC-2 (22CV).
(b) Do the test in Para. 3. A. (1).
(2) If the fault moves to the other SFCC position:
(a) Put the SFCC's back in their initial position.
(b) Replace the SFCC that has the fault.
(c) Do the test in Para. 3. A. (1).
(3) If the fault does not move to the other SFCC position:
(a) Put the SFCC's back in their initial position.
(b) Do a check of the aircraft wiring at the SFCC slat channel (Ref. ASM 27-81/08).
(c) Repair any defect found.
(d) Do the test in Para. 3. 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 : ALL ∞∞27-81-00∞∞∞∞∞∞∞∞∞∞Page 273
May 01/05R
CES Slats - WTB Applied During APU Start With the Batteries 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 TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______
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
_______________
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 27-80-00-869-004 Reset of the Wing Tip Brake (WTB) of the Slat System on the Ground AMM 27-81-00-740-002 Bite Test of the Slat and Flap Control Computers (Slat System)
3. Fault Confirmation
__________________
A. Test
(1) When you start the APU with the batteries, the warning message "F/CTL SLATS LOCKED" can show on the upper ECAM DU. Also, the Wing Tip Brakes (WTB) are applied.
NOTE : The ECAM message "F/CTL FLAPS LOCKED" can also show.
____
4. Fault Isolation
_______________
A. Procedure
(1) Do a reset of the WTBs of the Slat System (Ref. AMM TASK 27-80-00-869-004).
(2) Do a BITE test of the SFCC (Ref. AMM TASK 27-81-00-740-002): R - If the test gives a fault message, do the trouble shooting R procedure related to this 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 ∞∞27-81-00∞∞∞∞∞∞∞∞∞∞Page 274
May 01/05 CES Slats - SFCC TEST Gives the Message NO FAULTS BUT
1. Possible Causes
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2. Job Set-up Information
______________________
Not Applicable
3. Fault Confirmation
__________________
A. Test
(1) Do Para. 4. if the SLATS SFCC TEST gives the message NO FAULTS BUT, with any of the messages that follow:
- OTHER SFCC ARM SIGNAL NOT TESTED
or
- WTB SET
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 飛行操縱 2(81)
