TITLE:
AREA G and AREA H
EXAMPLE
LOCATION:
(Aft of Body Station 983)
20
STRUCTURE AND INSPECTION DETAILS
LEAD CRACK: Outer Chord
10
ZONE
5
108
220
2
DTR
1
.5
.2
.1
.03.05.1 .2 .5 1 2 5 10 20 50100
N (THOUSANDS OF FLIGHTS)
NOTES:
STRUCTURE
DETAIL
CHORD
CHORD
TASK REF.
ABRAMOVA
07/15/02
ENGR.
REVISED
CHECK
APPR.
APPR.
INSPECTION PROGRAM DETAILS
DIREC.CHECK METHOD%PHASE FREQUENCY N =
LEVEL Ro F-FLIGHTS 100F/Ro
1 GVI
1 D DET 100 24000 24000
F16F_PDF
Original D6-82669
DAMAGE
DETECTION
PERIOD
N FLIGHTS
o
>100000
>100000
FUEL LEAK DTR N/A
TOTAL DTR 15.6
REQUIRED DTR 10
DTR
15.6
8.2 FUSELAGE SSI INFORMATION THIS PAGE INTENTIONALLY LEFT BLANK
8.2 FUSELAGE SSI INFORMATION D6-82669 BLANK
N96974
F-17 -AFT ENTRY DOOR CUTOUT
Original D6-82669 8.2 FUSELAGE SSI INFORMATION
N96970
F-17 - AFT ENTRY DOOR CUTOUT (Continued)
8.2 FUSELAGE SSI INFORMATION D6-82669 Original
F-17 INSPECTION INSTRUCTIONS REFERENCES ACCESS MANHOURS
MPD CPCP OTHERS INSP MHRS ELPSD
TITLE: AFT ENTRY 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-17A Forward of BS 983 around door cutout (within "Area A" as shown on the first illustration page).
(1) Reinforcement (Bear) Strap and Skin
(External) 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 4601. Remove scuff plates.
Zone(s): 100, 200.
II. INSPECTION OPTIONS - DTR CHECK FORM F-17B Forward of BS 983 around door cutout (within "Area C" as shown on the second illustration page).
(1) Inner Chord
(Internal) From Direction 1, at specified locations, using HFEC (Ref. NDT Manual D6-37239, Part 6, 53-10-57). 1.25 elapsed hours and 1.25 manhours are required to accomplish the NDT inspections.
Access: Open door 4601. Remove side panels and lower sill corner scuff plates.
Zone(s): 108, 220.
Original D6-82669 8.2 FUSELAGE SSI INFORMATION
III. INSPECTION OPTIONS - DTR CHECK FORM F-17C Forward of BS 983 around door cutout (within "Area A" and “Area C” as shown on the illustration pages). 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(54)