A320飞机维护手册 AMM 时间限制/维护检查 2(97)

曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

Subtask 05-51-25-210-066
 D. Inspection of the Probes and Sensors
 NOTE : If the aircraft was on ground with the applicable protective
____ covers/devices installed (ref. AMM 10-11-00) when the dust contamination occured, this inspection is not necessary if there is no dust behind the covers.
 NOTE : Flush all the pressure lines:
____
 -
If the crew report shows an important dust storm.

 -
If the maintenance crew reports an important dust storm with probe covers in position.

R  - If a general inspection shows signs of a heavy contamination (Ref. TASK 12-24-34-600-001) (Ref. TASK 34-10-00-170-001) (Ref. TASK 34-10-00-170-002) (Ref. TASK 34-10-00-170-003)

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|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.|
 | |CODE| |  1  |  2  |  3  |SIGN|FIG.|
 |----|----|---------------------------------------|-----|-----|-----|----|----|

 |1.  |  | Inspection of the sensors and probes  |  |  |  |  |  |
 |  |  |  |  |  |  |  |  | 
R  |  A.|  | Examine all the probes and sensors  |  X  |  |  |  |  |
 |  |  |  |  |  |  |  |  |
 |  |  |(1) Examine all the probes and sensors |  |  |  |  |  |
 |  |  |  for damage and contamination (not  |  |  |  |  |  |
 |  |  |  clogged):  |  |  |  |  |  |
 |  |  |  - the pitot probes  |  |  |  |  |  |
 |  |  |  - the static probes  |  |  |  |  |  |
 |  |  |  - the TAT sensors  |  |  |  |  |  |
 |  |  |  - the AOA sensors  |  |  |  |  |  |
 |  |  |  - the ice detector probes  |  |  |  |  |  |
 |  |  |  (if installed)  |  |  |  |  |  |
 |  |  |NOTE: Make sure that the AOA sensors  |  |  |  |  |  |
 |  |  |  move freely and that the drain  |  |  |  |  |  |
 |  |  |  holes of the pitot probes are not|  |  |  |  |  |
 |  |  |  clogged.  |  |  |  |  |  |
 |  |  |  |  |  |  |  |  |
 |  |  |(2) Drain the standby static pressure  |  X  |  |  |  |  |
 |  |  |  lines and make sure that there  |  |  |  |  |  |
 |  |  |  are no signs of dust.  |  |  |  |  |  |
 |  |  |  (Ref. TASK 12-24-34-600-001)  |  |  |  |  |  |
 |  |  |  If you find contamination:  |  |  |  |  |  | 
R  |  B.|  | Flush all the pressure lines.  |  |  X  |  |  |  |
 |  |  |  (Ref. TASK 34-10-00-170-001)  |  |  |  |  |  |
 |  |  |  (Ref. TASK 34-10-00-170-002)  |  |  |  |  |  |
 |  |  |  (Ref. TASK 34-10-00-170-003)  |  |  |  |  |  |

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 Subtask 05-51-25-210-067
 E. Inspection of the Landing Gear Doors, the Landing Gears and the Landing Gear Wells (Ref. AMM 122232 PB 301)
 -------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the landing gear doors, | | | | | | | | |the landing gears and the landing gear | | | | | | | | |wells. | | | | | | | | |NOTE: If you find contamination, you | | | | | | | | | must: | | | | | | | | | (a) Remove the contamination from | | | | | | | | | surface, the moving joints | | | | | | | | | and the chromed areas of | | | | | | | | | shock absorbers and actuators | | | | | | R | | | before the subsequent flight. | | | | | | | | | (b) Do a full lubrication of | | | | | | | | | the landing gears before a | | | | | | | | | maximum of 10 flight cycles. | | | | | | | | | (Ref. AMM 12-22-32, PB 301) | | | | | | | | | | | | | | | | A.| |Inspection of the doors | | | | | | | | |(1) Examine all the doors for damage |  X  | | | | | | | | and/or contamination, specially on:| | | | | | | | | - the door skin | | | | | | | | | - the door hinges | | | | | | | | | - the proximity sensors | | | | | | | | | - the actuator bare rods. | | | | | | | | | | | | | | | | B.| |Inspection of the landing gears | | | | | | | | |(1) Examine all the landing gear |  X  | | | | | | | | structures and the components | | | | | | | | | installed on them for damage and/or| | | | | | | | | contamination, specially on: | | | | | | | | | - the attachment points of the | | | | | | | | | landing gears | | | | | | | | | - the proximity sensors | | | | | | | | | - the actuator rods | | | | | | | | | - the chromed area of the shock | | | | | | | | | absorbers | | | | | | | | | - the mechanical linkages and the | | | | | | | | | moving joints. | | | | | | | | | | | | | | | | C.| |Inspection of the landing gear wells | | | | | |
　
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