4. Fault Isolation
_______________
A. Procedure
(1) Trouble shoot the landing gear system fault codes shown (Ref. P. Block 301).
「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 A255
Aug 01/05R
CES
TASK 32-31-00-810-875
L/G Uplock Locked When L/G is Locked Down
1. Possible Causes
_______________
- Uplock Assembly
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 32-31-21-000-001 Removal of the NLG Uplock Assy (2530GM)
AMM 32-31-21-400-001 Installation of the NLG Uplock Assy (2530GM)
AMM 32-31-44-000-001 Removal of the MLG Uplock Assembly 2509GM (2510GM)
AMM 32-31-44-400-001 Installation of the MLG Uplock Assembly 2509GM
(2510GM) AMM 32-33-00-710-001 Operational Check of Gear Uplock and Door Uplock Mechanical Control
3. Fault Confirmation
__________________
A. Test
(1) Use the procedure given in the operational test that follows to open (unlock) the applicable uplock (Ref. AMM TASK 32-33-00-710-001).
4. Fault Isolation
_______________
A. Procedure
(1) If the uplock stays shut, replace the applicable Uplock Assembly:
- for the NLG Uplock Assembly (2530GM) (Ref. AMM TASK 32-31-21-000-001) and (Ref. AMM TASK 32-31-21-400-001).
- for the MLG Uplock Assembly (2509GM) or (2510GM) (Ref. AMM TASK 32-31-44-000-001) and (Ref. AMM TASK 32-31-44-400-001).
TASK 32-31-00-810-876
NLG Shock Absorber - Sliding Tube Oil Seepage or Unusual Extension (Specially when Off-loading) WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
CAUTION : DO NOT FULLY COMPRESS THE NLG AFTER A FLIGHT IN NLG LEAK CONDITIONS.
_______ FULL COMPRESSION CAN CAUSE INTERNAL DAMAGE TO THE SHOCK ABSORBER.
1. Possible Causes
_______________
- loss of gas or oil from the NLG shock absorber
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 08-10-00-200-001 Weighing and Balancing
AMM 12-12-32-611-001 Check Shock Absorber Fluid Level
32-31-00-991-016 Fig. 202
3. Fault Confirmation
__________________
A. Test
(1) Test not applicable. NOTE : If there is a loss of gas or oil from the NLG shock absorber,
____ there can be an effect on the aircraft steering or loading/unloading properties.
4. Fault Isolation
_______________
**ON A/C 001-049, 051-099, 101-149, 201-299,
A. Procedure NOTE : If a leakage from the NLG shock absorber has occurred, one return
____ flight is permitted for repair to be completed, if:
- the leak rate from the turning table drain hole is less than 10 drops/min, weight on wheels
- the servicing level of the shock absorber is done, less than one hour before a flight.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : ALL ∞∞32-31-00∞∞∞∞∞∞∞∞∞∞Page A257
Aug 01/05 CES
(1) Use the data in the tables that follow to do a check of the NLG shock absorber extension (dimension H):
(a) At the NLG measure and record the dimension H.
(Ref. Fig. 202/TASK 32-31-00-991-016)
(b) Compare the recorded dimension with the applicable dimension given in the tables that follow:
- if the shock absorber extension is not correct, do the next step.
NOTE : The recorded dimension H must be equal to, or 15 mm
____ (0.5905 in.) less than, the dimension given in the table.
NOTE : It is recommended that the complete procedure is done
____ again with a different aircraft weight and/or C of G configuration. To find the weight and C of G of the aircraft, go to (Ref. AMM TASK 08-10-00-200-001)
(2) Do a replenishment of the NLG shock absorber (Ref. AMM TASK 12-12-32-611-001).
「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 : 001-049, 051-099, 101-149, 201-299, ∞∞32-31-00∞∞∞∞∞∞∞∞∞∞Page A258
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) 起落架 LANDING GEAR 1(61)
