II. INSPECTION OPTIONS - DTR CHECK FORM F-15B Around door cutout (within "Area B” and "Area C" as shown on the second illustration page).
(1) Frames, Sills, Reinforcement (Bear) Strap and Skin
(Internal) From Direction 3, including fastener locations, using visual inspection methods; at specified locations and using HFEC (Ref. NDT Manual D6-37239, Part 6, 53-10-08). 2.5 elapsed hours and
2.5 manhours are required to perform the NDT inspections.
Access: Open door 4701. Remove side panels, insulation and lower sill corner scuff plates.
Zone(s): 107, 205.
Original D6-82669 8.2 FUSELAGE SSI INFORMATION
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
N98149
F-16 -AFT GALLEY DOOR CUTOUT
Original D6-82669 8.2 FUSELAGE SSI INFORMATION
N98151
F-16 - AFT GALLEY DOOR CUTOUT (Continued)
8.2 FUSELAGE SSI INFORMATION D6-82669 Original
F-16 INSPECTION INSTRUCTIONS REFERENCES ACCESS MANHOURS
MPD CPCP OTHERS INSP MHRS ELPSD
TITLE: AFT GALLEY DOOR CUTOUT S53-22-B C53-100-01 C53-107-01 I.(1) II.(1) III.(1) III.(2) V.(1) VI.(1) 0.5 10 10 0.5 2 10 0.5 5 5 0.5 1 5
I. INSPECTION OPTIONS - DTR CHECK FORM F-16A Forward of BS 983 around door cutout (within "Area A" and “Area E” as shown on the illustration pages).
(1) Bear Strap
(Internal) From Direction 1, at specified locations, using LFEC (Ref. NDT Manual D6-37239, Part 6, 53-10-56). 0.75 elapsed hour and 0.75 manhours are required to accomplish this inspection.
Access: Open door 4301. Remove scuff plates.
Zone(s): 100, 200.
(2) Bear Strap
(Internal) From Direction 3, using HFEC (Ref. NDT Manual D6-37239, Part 6, 53-10-57).
1.25 elapsed hours and 1.25 manhours are required to accomplish this NDT inspection. Access: Open door 4301. Remove side panels, insulation and lower sill corner scuff plates. Zone(s): 108, 220.
II. INSPECTION OPTIONS - DTR CHECK FORM F-16B Forward of BS 983 around door cutout (within "Area E" and “Area F” as shown on the second illustration).
(1) Inner Chord
(Internal) From Direction 1, using visual inspection methods.
Access: Open door 4301. Remove side panels and lower sill corner scuff plates.
Zone(s): 108, 220.
Original D6-82669 8.2 FUSELAGE SSI INFORMATION
(2) Inner Chord
(Internal) From Direction 1, using HFEC (Ref. NDT Manual D6-37239, Part 6, 53-10-57).
1.25 elapsed hours and 1.25 manhours are required to accomplish this NDT inspection. Access: Open door 4301. Remove side panels and lower sill corner scuff plates. Zone(s): 108, 220. 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：737-300/400/500 補充結構檢查文件 SUPPLEMENTAL STRUCTURAL INSPECTION DOCUMENT 1(52)
