2.0 elapsed hours and 2.0 manhours are required to accomplish this inspection.
Access: Same as I. (1).
Zone(s): Same as I. (1).
VI. INSPECTION OPTIONS - DTR CHECK FORM F-30F Web under each circumferential tear strap.
(1) Web
(External) From Direction 4 using LFEC (Ref. NDT Manual D6-37239, Part 6, 53-10-41).
2.0 elapsed hours and 2.0 manhours are required to accomplish this inspection.
Access: Same as I. (1).
Zone(s): Same as I. (1).
8.2 FUSELAGE SSI INFORMATION D6-82669 Original
DTR CHECK FORM
FUSELAGE BULKHEAD
TITLE:
BODY STATION 1016 OUTER RING
LOCATION:
20
10
5
2
DTR
1
.5
.2
.1
.03.05 .1.2 .5 1 2
LFEC
1
5
1
MODEL-SERIES
ITEM:
F-30A
737-300/-400/-500
OPERATOR(S)
NO. OF ELIGIBLE A/C
EXAMPLE
STRUCTURE AND INSPECTION DETAILS
LEAD CRACK: Y FRAME CHORD FLANGE
ZONE
701
10 20
50
100
N (THOUSANDS OF FLIGHTS)
NOTES:
1
S-3 TO S-7, S-13 TO S-14, 5-15 TO S-16, S-20 TO S-22, S-24 TO S-25,
S-26 TO S-27 (LEFT AND RIGHT)
STRUCTURE
DETAIL
"Y" FRAME
INSPECTION PROGRAM DETAILS
TASK REFERENCE DIREC. 1 LEVEL CHECK 4C METHOD LFEC R %PHASE o 100 F-FLIGHTS FREQUENCY 12000 100F/R N = o 12000
DAMAGE
DETECTION
PERIOD
N FLIGHTS
o
45000
FUEL LEAK DTR
ENGR. J. LO 6/6/83 REVISED
CHECK K. USUI 1/24/83 A. FOWLER 3/3/99 TOTAL DTR
APPR. APPR. R. SCHAAD 8/29/83 R. JOCHUM 3/3/99 REQUIRED DTR
DTR
N/A
10.0
10
F30A_PDF
D6-82669 8.2 FUSELAGE SSI INFORMATION
Original
8.2 FUSELAGE SSI INFORMATION D6-82669 Original
Original D6-82669 8.2 FUSELAGE SSI INFORMATION
8.2 FUSELAGE SSI INFORMATION D6-82669 Original
D6-82669 8.2 FUSELAGE SSI INFORMATION
Original
8.2 FUSELAGE SSI INFORMATION D6-82669 Original
N97795
F-31 - FUSELAGE BULKHEAD BS 1088
Original D6-82669 8.2 FUSELAGE SSI INFORMATION
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本文链接地址：737-300/400/500 补充结构检查文件 SUPPLEMENTAL STRUCTURAL INSPECTION DOCUMENT 1(61)
