• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-10-31 15:52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

F-46  INSPECTION INSTRUCTIONS  REFERENCES  ACCESS MANHOURS 
MPD  CPCP  OTHERS  INSP  MHRS  ELPSD 
TITLE:  FUSELAGE BEAMS OVER MAIN WHEEL WELL  S53-08-D S53-08-E  C53-107-01  I.(1)  40  10 

I.  INSPECTION OPTIONS - DTR CHECK FORM F-46 From Body Station 662 to Body Station 666, and from Body Station 725 to Body Station 729.
(1) Upper Chord and Web (Internal) From Direction 1, including fastener locations, using visual inspection methods.
Access: Remove floor panels S1081.
Zone(s): 108.

8.2   FUSELAGE SSI INFORMATION D6-82669 Original


Original D6-82669 8.2  FUSELAGE SSI INFORMATION THIS PAGE INTENTIONALLY LEFT BLANK

8.2  FUSELAGE SSI INFORMATION D6-82669 BLANK


N98841
F-48 - SKIN LONGITUDINAL LAP SPLICES
Original D6-82669 8.2  FUSELAGE SSI INFORMATION

F-48  INSPECTION INSTRUCTIONS  REFERENCES  ACCESS MANHOURS 
MPD  CPCP  OTHERS  INSP  MHRS  ELPSD 
TITLE:  SKIN LONGITUDINAL LAP SPLICES  S53-05-A  C53-100-01 C53-212-01 

I.  INSPECTION OPTIONS - DTR CHECK FORM F-48A The upper fastener row at skin longitudinal lap splices from BS 259.5 to BS 1016.
(1)
Skin (Internal/External) From Direction 2, including fastener locations, using visual inspection methods. NOTE:  Except as covered by SB 737-53A1177.

Access: External - None required.  Internal - Remove wing-to-body fairings, as required. Zone(s): 100, 200, 222, 223, 224, 225.

(2)
Skin (Internal/External) From Direction 2, including fastener locations, using HFEC (Ref. NDT Manual D6-37239, Part 6, 53-30-05). NOTE:  Except as covered by SB 737-53A1177.


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

8.2   FUSELAGE SSI INFORMATION D6-82669 Original

II.  INSPECTION OPTIONS - DTR CHECK FORM F-48B The lower fastener row at skin longitudinal lap splices from BS 259.5 to BS 1016.
(1) Skin
(Internal) From Direction 1, including fastener locations, using MFEC (Ref. NDT Manual D6-37239, Part 6, 53-30-16).
NOTE:  Except as covered by SB 737-53A1177.
Access:  Remove cabin equipment, sidewall panels, and remove or displace insulation blankets as required.
Zone(s):  100, 101, 102, 107, 108, 200, 202, 205, 208, 210, 218, 220, 222, 223, 224, 225.
(2) Skin (Internal/External) From Direction 2, including fastener locations, using LFEC (Ref. NDT Manual D6-37239, Part 6, 53-30-17). NOTE:  Except as covered by SB 737-53A1177.
Access: Same as I. (1).
Zone(s): Same as I. (1).

Original  D6-82669 8.2  FUSELAGE SSI INFORMATION


8.2  FUSELAGE SSI INFORMATION D6-82669 Original

F48B_PDF

Original D6-82669 8.2  FUSELAGE SSI INFORMATION THIS PAGE INTENTIONALLY LEFT BLANK
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:737-300/400/500 补充结构检查文件 SUPPLEMENTAL STRUCTURAL INSPECTION DOCUMENT 1(71)