Original D6-82669 8.2 FUSELAGE SSI INFORMATION
8.2 FUSELAGE SSI INFORMATION D6-82669
Original
N98263
F-20 -ESCAPE HATCH CUTOUT
Original D6-82669 8.2 FUSELAGE SSI INFORMATION
N98589
F-20 - ESCAPE HATCH CUTOUT (Continued)
8.2 FUSELAGE SSI INFORMATION D6-82669 Original
F-20 INSPECTION INSTRUCTIONS REFERENCES ACCESS MANHOURS
MPD CPCP OTHERS INSP MHRS ELPSD
TITLE: ESCAPE HATCH CUTOUT S53-22-C C53-100-01 C53-107-01 I.(1) 1 1
I. INSPECTION OPTIONS - DTR CHECK FORM F-20
Around door cutout from Body Station 611 to Body Station 647 between Stringer 9 and Stringer 16 (for 737-300/400/500). Body Station 570 to Body Station 606 between Stringer 9 and Stringer 16 (for 737-400 only).
(1) Frame (Internal) and (External) From Direction 1, including fastener locations, using visual inspection methods.
Access: Open doors 2403 and 2404 (737-300/400/500), door 2403A and 2404A (737-400 only). Remove side panels and insulation.
Zone(s): 107, 108.
(2) Skin
(External) From Direction 2, including fastener locations, using visual inspection methods.
Access: None required.
Zone(s): 100.
Original D6-82669 8.2 FUSELAGE SSI INFORMATION
DTR CHECK FORM TITLE: CUTOUT, ESCAPE HATCH ITEM: F-20
LOCATION: 20 STRINGER - 9 TO STRINGER - 16 BODY STATION 616 TO 639
10
5
DTR 2 1
.5
.2
.1 .03 .05 NOTES: .1 .2 .5 1 2 5 N (THOUSANDS OF FLIGHTS) 10 20 50 100
MODEL-SERIES 737-300/-400/-500
OPERATOR(S) NO. OF ELIGIBLE A/C
EXAMPLE
STRUCTURE AND INSPECTION DETAILS LEAD CRACK: DOUBLER
DAMAGE
INSPECTION PROGRAM DETAILS
STRUCTURE
DETAIL
FRAME
SKIN
TASK REFERENCE
DIREC.
1 12 2
ENGR. K. USUI 9/29/83 REVISED
CHECK J. LO 9/29/83 CALZADILLA 8/19/99
APPR. FOWLER A. 8/21/99
APPR. SCHAAD 9/29/83
CHECK
LEVEL
C 4C C 4C
DETECTION
%PHASE
FREQUENCY
N =
PERIOD
METHOD
R
F-FLIGHTS
100F/R
N FLIGHTS
o
o
o
GVI
100
3000
3000
14,000
DET
100
12000
12000
14,000
GVI
100
3000
3000
14,000
DET
100
12000
12000
14,000
FUEL LEAK DTR N/A
TOTAL DTR 11.1
REQUIRED DTR 10
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(56)
