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时间:2011-10-31 15:52来源:蓝天飞行翻译 作者:航空
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(3)
Inner Chord


(Internal) From Direction 3, at specified locations, using HFEC (Ref. NDT Manual D6-37239, Part 6, 53-10-60). 2.0 elapsed hours and 2.0 manhours are required to accomplish this inspection.
Access: Same as II. (1).
Zone(s): Same as II. (1).
(4)
Fail-Safe Chord (Internal) From Direction 4, using visual inspection methods.

Access: Same as II. (1).
Zone(s): Same as II. (1).


(5)
Fail-Safe Chord


(Internal) From Direction 5, at specified locations, using HFEC (Ref. NDT Manual D6-37239, Part 6, 53-10-60). 2.0 elapsed hours and 2.0 manhours are required to accomplish this inspection.
Access: Same as II. (1).
Zone(s): Same as II. (1).
Original D6-82669 8.2   FUSELAGE SSI INFORMATION


8.2   FUSELAGE SSI INFORMATION D6-82669 Original

 

Original D6-82669 8.2   FUSELAGE SSI INFORMATION


8.2   FUSELAGE SSI INFORMATION D6-82669 Original


N98716
F-36 -UPPER LOBE FRAMES BETWEEN BS 360 AND 540, AND BETWEEN BS 727 AND 1016
Original D6-82669 8.2  FUSELAGE SSI INFORMATION


N98738
F-36 - UPPER LOBE FRAMES BETWEEN BS 360 AND 540, AND BETWEEN BS 727 AND 1016 (Continued)
8.2  FUSELAGE SSI INFORMATION D6-82669 Original

F-36  INSPECTION INSTRUCTIONS  REFERENCES  ACCESS MANHOURS 
MPD  CPCP  OTHERS  INSP  MHRS  ELPSD 
TITLE:  UPPER LOBE FRAMES BETWEEN BS 360 AND 540, AND BETWEEN BS 727 AND 1016  S53-18-A S53-28-A S53-28-B S53-28-D S53-28-E S53-28-F  C53-107-01 

I. INSPECTION OPTIONS - DTR CHECK FORM F-36
Upper lobe frames between BS 360 and BS 540, and between BS 727 and BS 1016 from stringer S-13L to S-13R at stringer clips.
(1)
Frame
(Internal) From Direction 1, including fastener locations, using visual inspection methods.


Access: Remove ceiling panels S1042, S1072, S1082 and insulation.
Zone(s): 107, 108.


(2)
Frame (Internal) From Direction 2, at fastener locations and other locations specified in the NDI procedure


using HFEC (Ref. D6-37239, Part 6, 53-10-62). 4.0 elapsed hours and 4.0 manhours are required to accomplish this inspection.
Access: Same as I. (1).
Zone(s): Same as I. (1).
Original D6-82669 8.2  FUSELAGE SSI INFORMATION


F36_PDF
8.2  FUSELAGE SSI INFORMATION D6-82669 Original


N98830
F-38 -FUSELAGE CIRCUMFERENTIAL SPLICES
Original D6-82669 8.2  FUSELAGE SSI INFORMATION


N98812
F-38 - FUSELAGE CIRCUMFERENTIAL SPLICES (Continued)
8.2  FUSELAGE SSI INFORMATION D6-82669 Original

F-38  INSPECTION INSTRUCTIONS  REFERENCES  ACCESS MANHOURS 
MPD  CPCP  OTHERS  INSP  MHRS  ELPSD 
 
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本文链接地址:737-300/400/500 补充结构检查文件 SUPPLEMENTAL STRUCTURAL INSPECTION DOCUMENT 1(66)