8.2 FUSELAGE SSI INFORMATION D6-82669 BLANK
N96132
F-13A - FORWARD ENTRY DOOR CUTOUT (WITHOUT AIRSTAIRS)
Original D6-82669 8.2 FUSELAGE SSI INFORMATION
N96367
F-13B -FORWARD ENTRY DOOR CUTOUT (WITHOUT AIRSTAIRS) (Continued)
8.2 FUSELAGE SSI INFORMATION D6-82669 Original
F-13 INSPECTION INSTRUCTIONS REFERENCES ACCESS MANHOURS
MPD CPCP OTHERS INSP MHRS ELPSD
TITLE: FORWARD ENTRY DOOR CUTOUT (WITHOUT AIRSTAIRS) S53-22-A C53-100-01 C53-107-01 I.(2) II.(1) 0.5 12 0.5 6
I. INSPECTION OPTIONS - DTR CHECK FORM F-13A Around cutout (within "Area A" as shown on the first illustration page).
(1)
Skin
(External) From Direction 1, including fastener locations, using visual inspection methods.
Access: None required.
Zone(s): 100, 200.
(2)
Reinforcement (Bear) Strap and Skin
(Internal) From Direction 2, at specified locations, using LFEC (Ref. NDT Manual D6-37239, Part 6, 53-10-67). 1.5 elapsed hours and 1.5 manhours are required to accomplish this inspection.
Access: Open door 4201, remove scuff plates.
Zone(s): 100, 200.
II. INSPECTION OPTIONS - DTR CHECK FORM F-13B Around cutout (within "Area A", “Area B”, and "Area C" as shown on the illustration pages).
(1) Frames, Sills, Bear Strap, and Skin
(Internal) From Direction 3, including fastener locations, using visual inspection methods; at specified locations, using LFEC (Ref. NDT Manual D6-37239, Part 6, 53-10-67) and at specified locations, using HFEC (Ref. NDT Manual D6-37239, Part 6, 53-10-39). 1.0 elapsed hour and 1.0 manhour are required to accomplish these NDT inspections.
Access: Open door 4201. 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
MODEL-SERIES
ITEM:
F-13B
DTR CHECK FORM
CUTOUT, FORWARD ENTRY
TITLE:
(WITHOUT AIRSTAIR)
AREA A, AREA B, AND AREA C
LOCATION:
20
10
5
2
DTR
1
.5
.2
.1
.03.05 .1 .2 .5 1 2 5 10 20 50 100
N (THOUSANDS OF FLIGHTS)
NOTES:
OPERATOR(S) NO. OF ELIGIBLE A/C 737-300/-400/-500 EXAMPLE 3
STRUCTURE AND INSPECTION DETAILS
LEAD CRACK: FRAME CHORD
2
1
GENERAL VISUAL INSPECTION IN AREA B; DETAILED INSPECTION IN AREA C; HFEC
OR LFEC INSPECTION (AS SPECIFIED IN NDT DOCUMENT) OF OUTER CHORDS IN AREA A
WHERE FRAME WEB IS NOT VISIBLE; HFEC INSPECTION OF INNER CHORDS IN AREA C
AT FRAME-TO-SILL INTERSECTIONS. 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(49)
