8.2  FUSELAGE SSI INFORMATION D6-82669 BLANK

N98946
F-49 - FUSELAGE NOSE GEAR WHEEL WELL
Original D6-82669 8.2  FUSELAGE SSI INFORMATION

F-49  INSPECTION INSTRUCTIONS  REFERENCES  ACCESS MANHOURS 
MPD  CPCP  OTHERS  INSP  MHRS  ELPSD 
TITLE:  FUSELAGE NOSE GEAR WHEEL WELL  S53-31-A  C53-100-01 C53-202-01  I.(2)  1  1 

I.  INSPECTION OPTIONS - DTR CHECK FORM F-49A At BS 268.25 from WL 160 to WL 180.
(1)
Web
(External) From Direction 1, including fastener locations, using visual inspection methods.

Access: Open nose gear doors 3101, 3102.
Zone(s): 203

(2)
Stiffener
(Internal) From Direction 2, including fastener locations, using visual inspection methods.

Access: Remove nose wheel well panels 3105, 3106 and insulation.
Zone(s): 202.

(3)
Stiffener

(Internal) From Direction 3, at specified locations, using HFEC (Ref. NDT Manual D6-37239, Part 6, 53-10-34). 1.0 elapsed hour and 1.0 manhour are required to accomplish this inspection.
Access: Same as I. (2).
Zone(s): Same as I. (2).
8.2   FUSELAGE SSI INFORMATION D6-82669 Original

(4) Doubler (External) From Direction 1, at specified locations, using LFEC (Ref. NDT Manual D6-37239, Part 6,
53-10-46 or 53-10-47). 2.0 elapsed hours and 2.0 manhours are required to accomplish these inspections.
Access: Same as I. (1).
Zone(s): Same as I. (1).
II.  INSPECTION OPTIONS - DTR CHECK FORM F-49B At intersections of WL 185 and WL 169.1 with BS 251.6 and BS 259.5.
(1) Stiffener
(External) From Direction 1, at specified locations, using LFEC (Ref. NDT Manual D6-37239, Part 6, 53-10-46 or 53-10-47). 1.0 elapsed hour and 1.0 manhour are required to accomplish these inspections.
Access: Same as I. (1).
Zone(s): Same as I. (1).
III.  INSPECTION OPTIONS - DTR CHECK FORM F-49C At WL 185 and WL 169.1 BS 251.6 to BS 259.5.
(1) Stiffener
(External) From Direction 1, at specified locations, using LFEC (Ref. NDT Manual D6-37239, Part 6, 53-10-46 or 53-10-47). 1.0 elapsed hour and 1.0 manhour are required to accomplish these inspections.
Access: Same as I. (1).
Zone(s): Same as I. (1).
(2) Stiffener
(Internal) From Direction 2, including fastener locations, using visual inspection methods.

Access: Same as I. (2).
Zone(s): Same as I. (2).

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

N99086
F-55 -BODY SKIN AT WING PLUS CHORD SPLICE
Original D6-82669 8.2  FUSELAGE SSI INFORMATION
　
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