(7) Do the check of the fluid level of the MLG (LH) shock absorber (Ref. AMM TASK 12-12-32-611-004).
(8) Correct any fault found.
(9) Do the functional test of the normal extension and retraction of the landing gear (Ref. AMM TASK 32-31-00-720-002).
「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 A252
Aug 01/05R
CES TASK 32-31-00-810-870
MLG (RH) Shock Absorber Does Not Extend
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
_______________
- MLG (RH) proximity sensor and target clearances
- MLG (RH) torque link damper assembly
- landing gear torque link excessive play
- MLG sliding tube.
- charge pressure of the main landing gear (RH) shock absorber
- fluid level of the MLG (RH) shock absorber
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 12-12-32-611-004 Check Fluid Level of Main Landing Gear Shock Absorber AMM 12-14-32-614-003 Check Charge Pressure of Main Landing Gear Shock
Absorber AMM 32-11-00-200-001 Inspection/Check of the Main Gear AMM 32-11-00-200-008 Detailed Inspection of MLG, Sliding Tube (Twin Wheel) AMM 32-11-27-200-001 Check Torque Links for Excessive Play AMM 32-11-27-210-001 Detailed Inspection of the Torque-Link
Damper-Assemblies AMM 32-31-00-720-002 Functional Test of the Normal Extension and Retraction of the Landing Gear AMM 32-31-73-200-001 Inspection of the MLG Proximity Sensor and Target Clearances
3. Fault Confirmation
__________________
A. Procedure
(1) Do a check of the post flight report. If there is LGCIU 1 and 2 FAULT ECAM messages and related MLG (RH) shock-absorber target-position CFDS messages, do the Fault Isolation procedure.
「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 A253
Aug 01/05R CES
4. Fault Isolation
_______________
A. Procedure NOTE : The procedure that follows, gives the information necessary to
____ identify mechanical faults related to the MLG (RH) shock absorber.
(1) Do the inspection/check of the main gear (RH) (Ref. AMM TASK 32-11-00-200-001).
(2) Do the inspection of the MLG (RH) proximity sensor and target clearances (Ref. AMM TASK 32-31-73-200-001).
(3) Do the detailed inspection of the MLG (RH) torque link damper assembly (Ref. AMM TASK 32-11-27-210-001).
(4) Do the check of the landing gear torque link excessive play (Ref. AMM TASK 32-11-27-200-001).
(5) Do the detailed visual inspection of the MLG sliding tube. (Ref. AMM TASK 32-11-00-200-008).
(6) Do the check of the charge pressure of the main landing gear (RH) shock absorber (Ref. AMM TASK 12-14-32-614-003).
(7) Do the check of the fluid level of the MLG (RH) shock absorber (Ref. AMM TASK 12-12-32-611-004).
(8) Correct any fault found.
(9) Do the functional test of the normal extension and retraction of the landing gear (Ref. AMM TASK 32-31-00-720-002).
TASK 32-31-00-810-872
LGCIU 1 (2) Fault
1. Possible Causes
_______________
- landing gear system
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 31-32-00-860-009 Procedure to Get Access to the SYSTEM REPORT/TEST/L/G Page
3. Fault Confirmation
__________________
A. Test
(1) Get access to the SYSTEM REPORT/TEST/L/G page. (Ref. AMM TASK 31-32-00-860-009).
(2) On the LGCIU main menu, Press the TROUBLE SHOOT DATA line key.
(3) Make a note of the fault codes shown.
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 起落架 LANDING GEAR 1(60)
