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
_______________
- SENSOR-L FLAP ATTACHMENT FAILURE DETECTION (37CV)
- SENSOR-R FLAP ATTACHMENT FAILURE DETECTION (38CV)
- SENSOR-L FLAP ATTACHMENT FAILURE DETECTION (39CV)
- SENSOR-R FLAP ATTACHMENT FAILURE DETECTION (40CV)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-51-00-810-817 Left Flap Interconnecting-Strut Attachment Failure-Detection Sensor Fault 27-51-00-810-821 Right Flap Interconnecting-Strut Attachment
Failure-Detection Sensor Fault 32-31-00-810-802 LGCIU Fault AMM 27-51-00-710-002 Operational Test of the Flap Interconnecting Strut
and the Flap-Attachment Failure-Detection Sensors AMM 27-51-44-000-002 Removal of the Proximity-Sensor of the Interconnecting Strut AMM 27-51-44-400-002 Installation of the Proximity-Sensor of the Interconnecting Strut AMM 31-32-00-860-006 Procedure to Get Access to the SYSTEM REPORT/TEST F/CTL Page
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CES
3. Fault Confirmation
__________________
A. Test
(1) Trouble shoot any LGCIU faults (Ref. TASK 32-31-00-810-802) before you continue this procedure (Ref. Chap. 32 Page block 101)
(2) Do an operational test of the failure detection sensor for the flap attachment (Ref. AMM TASK 27-51-00-710-002).
4. Fault Isolation
_______________
A. Procedure
(1) If there is a proximity sensor misadjustment failure :
(a) Refer to the (Ref. AMM TASK 27-51-44-000-002) and (Ref. AMM TASK 27-51-44-400-002), use the removal and installation procedures to do the proximity sensor adjustment.
(b) Get access to the SYSTEM REPORT/TEST (Ref. AMM TASK 31-32-00-860-006).
(c) Make sure that the SYSTEM STATUS shows NO FAULTS.
(2) If the fault continues:
(a) Replace the applicable proximity sensor
- SENSOR-L FLAP ATTACHMENT FAILURE DETECTION (37CV)
- SENSOR-R FLAP ATTACHMENT FAILURE DETECTION (38CV)
- SENSOR-L FLAP ATTACHMENT FAILURE DETECTION (39CV)
- SENSOR-R FLAP ATTACHMENT FAILURE DETECTION (40CV)
- (Ref. AMM TASK 27-51-44-000-002) and (Ref. AMM TASK 27-51-44-400-002)
(b) Repeat the test in Para. 3.A.(2).
(3) If the fault continues do the applicable task for an invalid proximity sensor (Ref. TASK 27-51-00-810-817) or (Ref. TASK 27-51-00-810-821).
(a) Repeat the test in Para. 3.A.(2), and make sure that the SYSTEM STATUS shows NO FAULTS.
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 ∞∞27-51-00∞∞∞∞∞∞∞∞∞∞Page 265
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SFCC 1 No LGCIU 1 Data or SFCC 2 No LGCIU 2 Data.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
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.
1. Possible Causes
_______________
- LGCIU-1 (5GA1)
- LGCIU-2 (5GA2)
- SFCC-1 (21CV)
- SFCC-2 (22CV)
- aircraft wiring between the LGCIU 1 ARINC connector and the SFCC 1 (2) ARINC electrical connecter. 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320 Trouble Shooting Manual 排故手册 飞行操纵 2(2)
