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时间:2011-03-27 12:54来源:蓝天飞行翻译 作者:航空
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

 gouges 1.5 in. (38.1 mm) minimum from honeycomb core edge 
R  D. Crack  1.5 in. (38.1 mm) maximum length  Stop drill cracks.
R  Monitor at "A" check.

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R R R 
R  E. Scratch 
R R R 
R  2. Examine riveted joint for: A. Crack 
R R R R 
3. Examine the area 5 in. (127 mm) from engine attachment ring for:

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 10 in. (254 mm) minimum separation between cracks
0.005 in. (0.13 mm) maximum depth
1 in. (25.4 mm) maximum length 2 in. (50.8 mm) minimum separation from other damage
Stopped between two adjacent fasteners in joint of ten or more fasteners
10 in. (254 mm) minimum separation between cracksPermanent repair at "C" check recommended (Ref. SRM 541000).
Monitor at "A" check.
Permanent repair at "C" check recommended (Ref. SRM 541000).
Do not stop drill.
Monitor at "A" check.
Permanent repair at "C" check recommended (Ref. SRM 541000).

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R  A. Gouge  0.01 in. (0.25 mm) maximum depth  Monitor at "A" check.
R R R  Permanent repair at "C" check recommended (Ref. SRM 541000).
 0.10 in. (2.54 mm) maximum width
 1 in. (25.4 mm) maximum lenght
 1.5 in. (38.1 mm) minimum from honeycomb core edge
 10 in. (254 mm) minimum separation between gouges 
R  B. Scratch  0.005 in. (0.13 mm) maximum depth  Monitor at "A" check.
R R R  Permanent repair at "C" check recommended (Ref. SRM 541000).
 1 in. (25.4 mm) maximum length
 2 in. (50.8 mm) minimum separation from other damage

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 C. Do a Visual Inspection of the Intake Cowl Lip Structure
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1. Examine fastener areas of lip skin to intake cowl forward bulkhead for:
 A. Crack
R B. Dent
R R R
2. Examine lip skin for:
R A. Crack R No cracks permitted
No evidence of loose or pulled rivets
1 in. (25.4 mm) maximum diameter Dent must be smooth and free from sharp creases, gouges, and cracks
 0.1 in. (2.54 mm) maximum depth
 10 in. (254 mm) minimum seperation from other dents
 Maximum of three dents each segment
2 in. (50.8 mm) maximum lenght Repair before next flight (Ref. SRM 541000).
Monitor at "A" check.
Permanent repair at "C" check recommended (Ref. SRM 541000).
Stop drill before flight (Ref. SRM 541000).
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12 in. (304.8 mm)
 minimum separation from
 other damage
 Maximum of three cracks
 each segment 




R  B. Dent  2 in. (50.8 mm) maximum 
diameter 



0.2 in. (5.08 mm)
 maximum depth
 Dent must be smooth and
 free from sharp creases,
 gouges, and cracks
 10 in. (254 mm) minimum
 
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