(2) Do a check of the Part Numbers (P/N) of the SFCC-1 (21CV) and the SFCC-2 (22CV):
(a) Push in the line key adjacent to SFCC-1.
(b) Push in the line key adjacent to LRU IDENT.
(c) Record the manufacturers P/N of the SFCC-1.
(d) Push in the line key adjacent to RETURN.
(e) Do steps (a) to (c) for the SFCC-2.
(f) Push in the line key adjacent to RETURN until the F/CTL SYSTEM REPORT/TEST page is shown.
(3) Compare the P/Ns of the SFCC-1 and the SFCC-2 with the permitted interchangeability given in the IPC and the permitted mixability given in the SIL 27-116:
- if the mix of SFCC P/Ns does not agree with those permitted, do the fault isolation procedure in Para 4.A.
**ON A/C 301-399,
A. Procedure
(1) Get access to the Flight Controls (F/CTL) SYSTEM REPORT/TEST page (Ref. AMM TASK 31-32-00-860-001).
(2) Do a check of the Part Numbers (P/N) of the SFCC-1 (21CV) and the SFCC-2 (22CV):
(a) Push in the line key adjacent to SFCC-1.
(b) Push in the line key adjacent to LRU IDENT.
(c) Record the manufacturers P/N of the SFCC-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 ∞∞27-51-00∞∞∞∞∞∞∞∞∞∞Page A202
Aug 01/05 CES
(d) Push in the line key adjacent to RETURN.
(e) Do steps (a) to (c) for the SFCC-2.
(f) Push in the line key adjacent to RETURN until the F/CTL SYSTEM REPORT/TEST page is shown.
(3) Compare the P/Ns of the SFCC-1 and the SFCC-2 with the permitted interchangeability given in the IPC and the permitted mixability given in the SIL 27-116:
- if the mix of SFCC P/Ns does not agree with those permitted, do the fault isolation procedure in Para 4.A.
**ON A/C ALL
4. Fault Isolation
_______________
A. Procedure
(1) Replace the SFCC1 and/or the SFCC2 with the P/N that is not permitted, with a permitted P/N, (Ref. AMM TASK 27-51-34-000-001) and (Ref. AMM TASK 27-51-34-400-001).
「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 A203
May 01/05R
CES Flaps - Torque Limiter Tripped Without a Cockpit Effect 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
_______________
- torque limiter/s
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-51-00-810-810 Flap System Jam. AMM 27-50-00-866-010 Reset of the Torque Limiters of the Flap System on the Ground AMM 27-54-00-710-001 Operational Test of the Flap System
3. Fault Confirmation
__________________
A. Test
(1) A test is not necessary, do the fault isolation procedure.
4. Fault Isolation
_______________
A. Procedure
(1) Identify and reset the applicable torque limiter/s of the flap system (Ref. AMM TASK 27-50-00-866-010).
(2) Do an operational test of the flap system (Ref. AMM TASK 27-54-00-710-001).
(3) If the fault occurs again do the task (Flap System Jam) (Ref. TASK 27-51-00-810-810).
「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 A204
May 01/05R CES
Flaps - 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
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 飛行操縱 2(15)
