- BRAKE-R WING TIP (36CV)
- slat transmission system
- ROTARY ACTUATOR
2. Job Set-up Information______________________
A. Referenced Information
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REFERENCE DESIGNATION
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AMM 27-80-00-866-004 Extending the Slats on the Ground
AMM 27-80-00-866-005 Retracting the Slats on the Ground
AMM 27-80-00-869-004 Reset of the Wing Tip Brake (WTB) of the Slat System on the Ground
AMM 27-81-51-000-001 Removal of the Slat Wing-Tip Brake
AMM 27-81-51-400-001 Installation of the Slat Wing-Tip Brake
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.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞27-81-00∞∞∞∞∞∞∞∞∞∞Page 242
May 01/04R
CES
4. Fault Isolation
_______________
A. Procedure
(1) Do the wing tip brake (WTB) reset procedure (Ref. AMM TASK 27-80-00-869-004)
(2) Do the procedure on the wing identified by the fault message on the post flight report. If a wing is not identified, do the procedure on each wing.
(3) Do the detailed visual inspection of the slat transmission system (Ref. AMM TASK 27-84-00-200-001) repair/correct any fault 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 fault continues or no fault is found:
(a) Move the slats (Ref. AMM TASK 27-80-00-866-004) and (Ref. AMM TASK 27-80-00-866-005).
(b) If there is an incorrect noise at the WTB, replace the BRAKE-L WING TIP (35CV) or BRAKE-R WING TIP (36CV) (Ref. AMM TASK 27-81-51-000-001) and (Ref. AMM TASK 27-81-51-400-001).
(c) If there is no incorrect noise at the WTB, disconnect the transmission shafts on each side of the WTB (Ref. para (b)).
(d) Make sure that the WTB is easily turned, if it is not easily turned, replace the WTB (Ref. para (b)).
NOTE : The breakout torque of the WTB must not be more than 0.5
____
NM.
(6) If no defects have been found during this procedure, as a precaution:
(a) Replace any ROTARY ACTUATOR that has been found to have its torque limiter tripped (Ref. AMM 27-84-48 or 27-84-49).
NOTE : Any torque limiter tripped during WTB reset can be
____
ignored.
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 243
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Slat System Uncommanded Movement.
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
_______________
- SFCC-1 (21CV)
- SFCC-2 (22CV)
- POB Solenoid
- Pressure-off Brake,
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific Multimeter
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION
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AMM 27-51-34-000-001 Removal of the SFCC (21CV,22CV)
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 飛行操縱 2(70)
