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R **ON A/C 151-199, 401-499,
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 : 001-049, 051-099, 101-149, 151-199, ∞∞32-31-00∞∞∞∞∞∞∞∞∞∞Page A265
201-299, 401-499, 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).
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| Dimension H (mm) |
----------------------|-----------------------------------------------| | A/C C of G | 14% | 17% | |----------------------|-----------------------|-----------------------| | Ambient Temp (Deg C) | -20 | 0 | 20 | 40 | -20 | 0 | 20 | 40 | |----------------------|-----|-----|-----|-----|-----|-----|-----|-----| | | 45000 | 66 | 63 | 101 | 119 | 71 | 89 | 108 | 126 | | |---------|-----|-----|-----|-----|-----|-----|-----|-----| | | 47500 | 62 | 79 | 97 | 114 | 67 | 85 | 103 | 121 | | |---------|-----|-----|-----|-----|-----|-----|-----|-----| | | 50000 | 58 | 75 | 93 | 110 | 63 | 81 | 98 | 116 | | |---------|-----|-----|-----|-----|-----|-----|-----|-----| | | 52500 | 56 | 72 | 89 | 106 | 60 | 77 | 91 | 112 | | |---------|-----|-----|-----|-----|-----|-----|-----|-----| | | 55000 | 52 | 69 | 85 | 102 | 56 | 73 | 91 | 108 | | |---------|-----|-----|-----|-----|-----|-----|-----|-----| | A/C Weight | 57500 | 49 | 65 | 82 | 99 | 53 | 70 | 87 | 104 |
| (Kg) |---------|-----|-----|-----|-----|-----|-----|-----|-----|
| | 60000 | 46 | 63 | 79 | 96 | 51 | 67 | 84 | 101 |
| |---------|-----|-----|-----|-----|-----|-----|-----|-----|
| | 62500 | 44 | 60 | 76 | 93 | 48 | 65 | 81 | 98 |
| |---------|-----|-----|-----|-----|-----|-----|-----|-----|
| | 65000 | 42 | 58 | 74 | 90 | 46 | 62 | 79 | 95 |
| |---------|-----|-----|-----|-----|-----|-----|-----|-----|
| | 67500 | 40 | 56 | 72 | 86 | 44 | 60 | 76 | 92 |
| |---------|-----|-----|-----|-----|-----|-----|-----|-----|
| | 70000 | 38 | 54 | 69 | 85 | 42 | 58 | 74 | 90 |
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本文链接地址：A320 Trouble Shooting Manual 排故手册 起落架 LANDING GEAR 1(65)
