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时间:2011-10-31 15:52来源:蓝天飞行翻译 作者:航空
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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).
 
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