V. INSPECTION OPTIONS - DTR CHECK FORM F-16E Aft of BS 983 around door cutout (within "Area G” and “Area H” as shown on the second illustration page).
(1)
Inner Chord
(Internal) From Direction 1, at specified locations, using visual inspection methods.
Access: Open door 4301. Remove side panels.
Zone(s): 108, 220.
(2)
Inner Chord (Internal) From Direction 1, at specified locations, using HFEC (Ref. NDT Manual D6-37239, Part 6, 53-10-57). 1.25 elapsed hour and 1.25 manhours are required to accomplish this inspection.
Access: Open door 4301. Remove side panels.
Zone(s): 108, 220.
VI. INSPECTION OPTIONS - DTR CHECK FORM F-16F Aft of BS 983 around door cutout (within "Area G” and “Area H” as shown on the second illustration page).
(1) Outer Chord
(Internal) From Direction 1, using visual inspection methods.
Access: Open door 4301. Remove side panels and insulation.
Zone(s): 108, 220.
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
Original D6-82669 8.2 FUSELAGE SSI INFORMATION
8.2 FUSELAGE SSI INFORMATION D6-82669 Original
MODEL-SERIES
ITEM: F-16F
DTR CHECK FORM
737-300/-400/-500
Cutout, Aft Galley Door
OPERATOR(S)
NO. OF ELIGIBLE A/C 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(53)