(a) Check that the BITE gives a "WTB,s set in this channel."
(b) Refer to the PPU DATA to identify the defective wing:
- The APPU Data that is incremented from the set control lever position by more than 5.2 deg. shows the faulty wing. Refer to page block 301 table 3 for the control lever position to APPU DATA.
(2) Do the reset of the wing tip brakes (Ref. AMM TASK 27-80-00-869-004).
(3) Do the detailed visual inspection of the slat transmission assembly (Ref. AMM TASK 27-84-00-200-001).
(a) Repair/correct any failure found (Ref. AMM chap. 27).
(4) Do the operational test of the slat system, (Ref. AMM TASK 27-84-00-710-001).
(5) If the failure continues:
(a) Refer to (Ref. AMM TASK 27-81-18-000-001) Figure 401/Task 27-81-18-991-001 and identify the APPU.
(b) Do a check of the APPU ZERO DATUM settings.
(c) If the ZERO DATUM settings are not aligned. Do (Ref. AMM TASK 27-81-18-400-001).
(6) Set the CFDS MENU MODE and access the SYSTEM STATUS SLAT and make sure that NO FAULTS is shown.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞27-81-00∞∞∞∞∞∞∞∞∞∞Page 238
May 01/04R CES
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 ∞∞27-81-00∞∞∞∞∞∞∞∞∞∞Page 239
Aug 01/03R
CES
Slat System Runaway.
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.
1. Possible Causes
_______________
- Slat Transmission System
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 27-84-00-200-001 Detailed Visual Inspection of the Slat Transmission System AMM 27-84-00-710-001 Operational Test of the Slat System
3. Fault Confirmation
__________________
A. For the fault confirmation do the fault isolation..
4. Fault Isolation
_______________
A. Procedure.
(1) Do the reset of the wing tip brakes (Ref. AMM TASK 27-80-00-869-004)
(2) Do the detailed inspection of the Slat Transmission System, (Ref. AMM TASK 27-84-00-200-001).
(a) Repair/correct any failure found (Ref. AMM chap. 27).
(3) Do the operational test of the slat system (Ref. AMM TASK 27-84-00-710-001).
(4) Set the CFDS MENU MODE and access the SYSTEM STATUS SLAT and make sure that NO FAULTS is shown.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞27-81-00∞∞∞∞∞∞∞∞∞∞Page 240
May 01/04R CES
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 ∞∞27-81-00∞∞∞∞∞∞∞∞∞∞Page 241
May 01/04R
CES Slat Overspeed Fault.
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(69)
