- make sure that the guide arms are in the correct condition. Repair them if necessary.
(1) If the fault continues:
- discharge the door damper and emergency-operation cylinder (Ref. AMM TASK 52-10-00-614-001).
- and do an inspection of the door damper and emergency-operation cylinder (Ref. AMM TASK 52-13-14-200-001).
(a) If the inspection is not OK:
- replace the door damper and emergency-operation cylinder (Ref. AMM TASK 52-13-14-000-001), (Ref. AMM TASK 52-13-14-400-001).
「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 ∞∞52-13-00∞∞∞∞∞∞∞∞∞∞Page 258
Nov 01/03 CES (b) If the inspection is OK:
- do an inspection of:
. the door suspension
. the door locking mechanism
. the door escape slide release mechanism.
- Repair these items if necessary.
(2) If the fault continues:
- do an adjustment of the AFT passenger/crew door (Ref. AMM TASK 52-13-00-820-001).
(3) If the fault continues:
- replace the AFT passenger/crew door (Ref. AMM TASK 52-13-11-000-001) and (Ref. AMM TASK 52-13-11-400-001).
TASK 52-13-00-810-825
No Visual Indication of the Arming Position of the Escape Slide (Aft Passenger/Crew Door)
1. Possible Causes
_______________
- girt bar with the visual indicator
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 52-10-00-720-005 Functional Test of the Release Mechanism of the Emergency Escape Slide AMM 52-13-22-000-002 Removal of the Release Mechanism of the Emergency Escape Slide of the Aft Passenger/Crew Door AMM 52-13-22-400-001 Installation of the Release Mechanism of the Emergency Escape Slide of the Aft Passenger/Crew Door
3. Fault Confirmation
__________________
A. Test
(1) Do the functional test of the release mechanism of the emergency escape slide (Ref. AMM TASK 52-10-00-720-005)
4. Fault Isolation
_______________
A. If the test confirms the fault:
- replace only the girt bar with the visual indicator of the aft passenger/crew door. (Ref. AMM TASK 52-13-22-000-002) and (Ref. AMM TASK 52-13-22-400-001).
B. Test
- Do the test given in Para. 3.A.
TASK 52-13-00-810-826
Vibrations and Noise in the Aft Passenger/Crew Door Area
1. Possible Causes
_______________
- cover plate
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
05-50-00-810-801 Identification of the Cause of In-Flight Airframe Vibrations and/or Noises AMM 52-10-00-220-007 Check of the Preload of the Cover Plate
3. Fault Confirmation
__________________
A. Make sure that the identification of the cause of the vibrations is
correct (Ref. TASK 05-50-00-810-801).
4. Fault Isolation
_______________
A. If there are vibrations and noise at the aft passenger/crew door area:
- do a check of the cover plate of the passenger/crew door (Ref. AMM TASK 52-10-00-220-007).
PASSENGER COMPARTMENT EMERGENCY EXIT - FAULT ISOLATION PROCEDURES
_________________________________________________________________
**ON A/C 001-049, 051-099, 101-149, 201-299,
TASK 52-21-00-810-801
Sensor Monitoring Fault at the LH FWD Passenger Compartment Emergency Exit
1. Possible Causes
_______________
- PROX SW-HANDLE FLAP, L FWD EMER EXIT (19WV1)
- IND LT-SLIDE ARMED, L EMER EXIT (2WN1)
- PROX SW-HANDLE FLAP, L AFT EMER EXIT (21WV1)
- SDAC-1 (1WV1)
- SDAC-2 (1WV2)
- wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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本文链接地址：A320 Trouble Shooting Manual 排故手册 舱门 DOORS(66)
