Access: Same as I. (2).
Zone(s): Same as I. (2).
8.1 WING SSI INFORMATION D6-82669 Original
II. INSPECTION OPTIONS - DTR CHECK FORM W-6B
Typical stringers from Stringer 2 to Stringer 11 at Body Lines 41 Right, 41 Left, and from Body Line 6.5 Right to 6.5 Left.
(1) Skin and Stringers
(Internal) From Direction 1, using visual inspection methods.
Access: Defuel and purge tank (S2211). Access through left air-conditioning equipment bay access door (3303) and through left center wing tank lower forward skin access panel and spanwise beam access holes.
Zone(s): 221.
Original D6-82669 8.1 WING SSI INFORMATION
8.1 WING SSI INFORMATION D6-82669 Original
Original D6-82669 8.1 WING SSI INFORMATION THIS PAGE INTENTIONALLY LEFT BLANK
8.1 WING SSI INFORMATION D6-82669 BLANK
W-8 - WING CENTER SECTION LOWER SPLICE STRINGERS 5 AND 9
Original D6-82669 8.1 WING SSI INFORMATION
W-8 INSPECTION INSTRUCTIONS REFERENCES ACCESS MANHOURS
MPD CPCP OTHERS INSP MHRS ELPSD
TITLE: WING CENTER SECTION LOWER SPLICE STRINGERS 5 AND 9 S57-30-B C57-221-01 98 49
I. INSPECTION OPTIONS - DTR CHECK FORM W-8 Stringers 5 and 9 from right Side-of-Body to left Side-of-Body.
(1) Stringer
(Internal) From Direction 1, using visual inspection methods.
Access: Defuel and purge tank (S2211). Access through left air-conditioning equipment bay access door (3303) and through left center wing tank lower forward skin access panel and spanwise beam access holes.
Zone(s): 221.
8.1 WING SSI INFORMATION D6-82669 Original
Original D6-82669 8.1 WING SSI INFORMATION THIS PAGE INTENTIONALLY LEFT BLANK
8.1 WING SSI INFORMATION D6-82669 BLANK
N75772
W-10 - WING LOWER SURFACE SPLICE - BBL 70.85
Original D6-82669 8.1 WING SSI INFORMATION
W-10 INSPECTION INSTRUCTIONS REFERENCES ACCESS MANHOURS
MPD CPCP OTHERS INSP MHRS ELPSD
TITLE: WING LOWER SURFACE SPLICE - BBL 70.85 S57-19-A S57-19-B S57-02-A C53-212-01 C57-221-01 C57-305-01
I. INSPECTION OPTIONS - DTR CHECK FORM W-10A Mid to aft splice plate segments, inboard splice, from the Rear Spar to Stringer 11.
(1) Splice Plate
(Internal) From Direction 1, (outside the wing) using LFEC (Ref. NDT Manual D6-37239, Part 6, 57-30-04). 5.5 elapsed hours and 11.0 manhours are required to accomplish this inspection.
Access: Remove lower Wing Body Fairings 7221, 7222, 7223, 7421, 7422, and 7423.
Zone(s): 222, 223.
(2) Splice Plate
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(31)
