A320飞机维护手册 AMM 时间限制/维护检查 2(108)

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

R NOTE : Flush all the pressure line :
____ R - If the crew report shows a very dense cloud of volcanic ashes R - If the maintenance reports a very dense cloud of volcanic ashes R with probe covers not in position R - If a general inspection shows evidence of heavy contamination. R (Ref. TASK 12-24-34-600-001) (Ref. TASK 34-10-00-170-001) R (Ref. TASK 34-10-00-170-002) (Ref. TASK 34-10-00-170-003)

R -------------------------------------------------------------------------------R |ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| R  | |CODE| |  1  |  2  |  3  |SIGN|FIG.| R |----|----|---------------------------------------|-----|-----|-----|----|----|
R |1.  |  | Inspection of the sensors and probes | |  |  |  |  | 
R |  |  | | |  |  |  |  | 
R  |  A.|  | Inspect all the probes and sensors |  X  |  |  |  |  | 
R |  |  | | |  |  |  |  | 
R |  |  |(1) Examine all the probes and sensors | |  |  |  |  | 
R |  |  | for damage and contamination (not | |  |  |  |  | 
R |  |  | clogged): | |  |  |  |  | 
R |  |  | - the pitot probes | |  |  |  |  | 
R |  |  | - the static probes | |  |  |  |  | 
R |  |  | - the TAT sensors | |  |  |  |  | 
R |  |  | - the AOA sensors | |  |  |  |  | 
R |  |  | - the ice detector probes | |  |  |  |  | 
R |  |  | (if installed) | |  |  |  |  | 
R |  |  |NOTE: Make sure that the AOA sensors | |  |  |  |  | 
R |  |  | move freely and that the drain | |  |  |  |  | 
R |  |  | holes of the pitot probes are not| |  |  |  |  | 
R |  |  | clogged. | |  |  |  |  | 
R |  |  | | |  |  |  |  | 
R  |  |  |(2) Drain the standby static pressure  |  X  |  |  |  |  | 
R |  |  | lines and make sure that there are | |  |  |  |  | 
R |  |  | no signs of ash. | |  |  |  |  | 
R |  |  | (Ref. TASK 12-24-34-600-001) | |  |  |  |  | 
R |  |  | If you find contamination: | |  |  |  |  | 
R  |  |  | (a) Flush all the pressure lines | |  X  |  |  |  | 
R |  |  | (Ref. TASK 34-10-00-170-001) | |  |  |  |  | 
R |  |  | (Ref. TASK 34-10-00-170-002) | |  |  |  |  | 
R |  |  | (Ref. TASK 34-10-00-170-003) | |  |  |  |  | 

R -------------------------------------------------------------------------------

R Subtask 05-51-25-210-079
R E. Inspection of the Landing Gear Doors, the Landing Gears and the Landing R Gear Wells (Ref. AMM 122232 PB 301)
R -------------------------------------------------------------------------------R |ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| R  | |CODE| |  1  |  2  |  3  |SIGN|FIG.| R |----|----|---------------------------------------|-----|-----|-----|----|----| R |1. | |Inspection of the landing gear doors, | | | | | | R | | |the landing gears and the landing gear | | | | | | R | | |wells. | | | | | | R | | |NOTE: If you find contamination, you | | | | | | R | | | must: | | | | | | R | | | (a) Remove the contamination from| | | | | | R | | | surface, the moving joints | | | | | | R | | | and the chromed areas of | | | | | | R | | | shock absorbers and actuators| | | | | | R | | | before the next flight. | | | | | | R | | | (b) Do a full lubrication of the | | | | | | R | | | landing gears before a | | | | | | R | | | maximum of 10 flight cycles. | | | | | | R | | | (Ref. AMM 12-22-32, PB 301) | | | | | | R | | | | | | | | | R | A.| |Inspection of the doors | | | | | | R  | | |(1) Examine all the doors for damage |  X  | | | | | R | | | and/or contamination, specially on:| | | | | | R | | | - the door skin | | | | | | R | | | - the door hinges | | | | | | R | | | - the proximity sensors | | | | | | R | | | - the actuator bare rods. | | | | | | R | | | | | | | | | R | B.| |Inspection of the landing gears | | | | | | R  | | |(1) Examine all the landing gear |  X  | | | | | R | | | structures and the components | | | | | | R | | | installed on them for damage and/or| | | | | | R | | | contamination, specially on: | | | | | | R | | | - the attachment points of the | | | | | | R | | | landing gears | | | | | | R | | | - the proximity sensors | | | | | | R | | | - the actuator rods | | | | | | R | | | - the chromed area of the shock | | | | | | R | | | absorbers | | | | | | R | | | - the mechanical linkages and the | | | | | | R | | | moving joints. | | | | | | R | | | | | | | | | R | C.| |Inspection of the landing gear wells | | | | | |
　
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