A. Fowler
04/06/99
ENGR.
REVISED CHECK
M. Morgan
7/22/04 APPR. APPR.
Original
F41_PDf
DAMAGE
DETECTION
PERIOD
N FLIGHTS
o
>100000
>100000
FUEL LEAK DTR N/A
TOTAL DTR 11.6
REQUIRED DTR 10
DTR
11.6
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N98670
F-45 - CREW CABIN WINDOW POSTS
Original D6-82669 8.2 FUSELAGE SSI INFORMATION
F-45 INSPECTION INSTRUCTIONS REFERENCES ACCESS MANHOURS
MPD CPCP OTHERS INSP MHRS ELPSD
TITLE: CREW CABIN WINDOW POSTS *Plus sealant cure time -variable dependent on mixture used. S53-09-A C53-100-01 C53-101-01 I.(1) I.(2) 10 12 5 6*
I. INSPECTION OPTIONS - DTR CHECK FORM F-45A Cabin window, posts A-B.
(1)
Left and Right Chord
(Internal) From Direction 1, using visual inspection methods.
NOTE: Both left and right chords must be inspected.
Access: Remove left/right No. 1 window.
Zone(s): 101, 102.
(2)
Left and Right Chord
(Internal) From Direction 3, using visual inspection methods.
NOTE: Both left and right chords must be inspected.
Access: Remove glare shield (not necessary if adjacent window has been removed). Zone(s): Same as I. (1).
II. INSPECTION OPTIONS - DTR CHECK FORM F-45B Cabin window, posts C-D.
(1) Skin and Chord
(External) From Direction 1, using visual inspection methods.
Access: Sliding window open.
Zone(s): 100, 101, 102.
8.2 FUSELAGE SSI INFORMATION D6-82669 Original
III. INSPECTION OPTIONS - DTR CHECK FORM F-45C Cabin window, posts E-F, upper part.
(1)
Skin and Chord
(External/Internal) From Direction 1, using visual inspection methods.
Access: Same as II. (1).
Zone(s): Same as II. (1).
(2)
Skin and Chord (External) From Direction 5, at specified locations, using X-Ray inspection method (Ref. NDT Manual D6-37239, Part 2, 53-10-14).
Access: None required.
Zone(s): 100.
Original D6-82669 8.2 FUSELAGE SSI INFORMATION
8.2 FUSELAGE SSI INFORMATION D6-82669 Original
Original D6-82669 8.2 FUSELAGE SSI INFORMATION
8.2 FUSELAGE SSI INFORMATION D6-82669 Original
N98840
F-46 - FUSELAGE BEAMS OVER MAIN WHEEL WELL
Original D6-82669 8.2 FUSELAGE SSI INFORMATION
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