- security of attachment
- damage
- corrosion
- oil leaks.
(2) Do the inspection of the MLG proximity sensor and target clearances (Ref. AMM TASK 32-31-73-200-001).
(3) Do the detailed visual inspection of the MLG (RH) door uplock units and pins (Ref. AMM TASK 32-31-00-200-001).
(4) Do the detailed visual inspection of the MLG (RH) door forward and aft fitting (Ref. AMM TASK 52-81-00-200-001).
(5) Correct any fault found.
(6) Do the functional test of the normal extension and retraction of the landing gear (Ref. AMM TASK 32-31-00-720-002).
(7) If the fault continues, the MLG door (RH) is slow to operate or the fault continues after the subsequent flight, replace the ACTG CYL-MLG DOOR, R (2522GM) (Ref. AMM TASK 32-31-35-000-001) and (Ref. AMM TASK 32-31-35-400-001).
「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 ∞∞32-31-00∞∞∞∞∞∞∞∞∞∞Page A229
Aug 01/05R
CES
TASK 32-31-00-810-859
NLG Doors Do Not Close Fully
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
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GEAR.
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
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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
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- UPLOCK ASSY-NLG DOOR (2534GM)
- ACTG CYL-NLG DOOR (2531GM)
- SAFETY VALVE-NLG DOOR CLOSING (2629GM)
- nose landing gear doors operating mechanism
- nose gear door gaps and mismatches
- NLG door uplock units and pins
- NLG door hinges
2. Job Set-up Information
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A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 32-22-00-220-001 Check of the Nose-Gear Doors Gaps and Mismatches AMM 32-30-00-200-001 Detailed Inspection of Nose Gear Door Operating Mechanism AMM 32-31-00-200-001 Detailed Inspection of Gear Uplock and Door Uplock Units and Pins AMM 32-31-00-720-003 Functional Test of the Normal Extension and
Retraction of the Nose Landing Gear AMM 32-31-14-000-001 Removal of the NLG Door Uplock Assy (2534GM) AMM 32-31-14-400-001 Installation of the NLG Door Uplock Assy (2534GM) AMM 32-31-16-000-001 Removal of the NLG Door Actuating Cylinder (2531GM) AMM 32-31-16-400-001 Installation of the NLG Door Actuating Cylinder
(2531GM) AMM 32-31-19-000-001 Removal of the Safety Valves 2629GM/2630GM AMM 32-31-19-400-001 Installation of the Safety Valves 2629GM/2630GM AMM 52-82-00-200-001 Detailed Inspection of NLG, Main Door Hinges, LH/RH
「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 ∞∞32-31-00∞∞∞∞∞∞∞∞∞∞Page A230
Aug 01/05R CES
3. Fault Confirmation
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A. Procedure
(1) Do a check of the post flight report. If there is LGCIU 1 and 2 FAULT ECAM messages and related NLG door-closed target-position CFDS messages, do the Fault Isolation procedure.
4. Fault Isolation
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A. Procedure
NOTE : The procedure that follows, gives the information necessary to
____
identify mechanical faults related to the NLG doors.
(1) Do the detailed visual inspection of the nose landing gear doors operating mechanism (Ref. AMM TASK 32-30-00-200-001).
(2) Do a check of the nose gear door gaps and mismatches (Ref. AMM TASK 32-22-00-220-001).
(3) Do the detailed visual inspection of the NLG door uplock units and pins (Ref. AMM TASK 32-31-00-200-001).
(4) Do the detailed visual inspection of the NLG door hinges (Ref. AMM TASK 52-82-00-200-001).
(5) Correct any fault found.
(6) Do the functional test of the normal extension and retraction of the nose landing gear (Ref. AMM TASK 32-31-00-720-003).
(7) If the fault continues replace the UPLOCK ASSY-NLG DOOR (2534GM) (Ref. AMM TASK 32-31-14-000-001) and (Ref. AMM TASK 32-31-14-400-001).
(8) If the fault continues, the NLG doors are slow to operate or the fault continues after the subsequent flight, replace the ACTG CYL-NLG DOOR (2531GM) (Ref. AMM TASK 32-31-16-000-001) (Ref. AMM TASK 32-31-16-400-001). 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 起落架 LANDING GEAR 1(51)
