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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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DTR
6.6
3.0
1.0
0.5
F20_PDF
8.2  FUSELAGE SSI INFORMATION D6-82669 Original


N9674f7
F-22 - FUSELAGE BULKHEAD BS 227.8
Original D6-82669 8.2  FUSELAGE SSI INFORMATION

F-22  INSPECTION INSTRUCTIONS  REFERENCES  ACCESS MANHOURS 
MPD  CPCP  OTHERS  INSP  MHRS  ELPSD 
TITLE:  FUSELAGE BULKHEAD BS 227.8  S53-14-A  C53-100-01 C53-101-01 C53-202-01  I.(1)  3  1.5 

I. INSPECTION OPTIONS - DTR CHECK FORM F-22A
From 5 inches (12.7 cm) below to 5 inches (12.7 cm) above WL 207.5 at BS 227.8, on both sides of the airplane.
(1) Inner Chord and Web
(Internal) From Direction 1, using visual inspection methods.

Access:  Below floor - forward access door 1103 and displace insulation blankets as required. Above floor - remove equipment, lining and insulation blankets from control cabin sidewall.
Zone(s):  101, 102, 202.
(2) Inner Chord
(Internal) From Direction 2, at specified locations, using HFEC (Ref. NDT Manual D6-37239, Part 6, 53-10-05). 1.0 elapsed hour and 1.0 manhour are required to accomplish this inspection.
Access:  Same as I. (1).
Zone(s):  202.
II.  INSPECTION OPTIONS - DTR CHECK FORM F-22B From LBBL 18 to RBBL 18 at BS 227.8
(1) Outer Chord and Doubler
(External) From Direction 3, at specified locations, using LFEC (Ref. NDT Manual D6-37239, Part 6, 53-10-04). 2.0 elapsed hours and 2.0 manhours are required to accomplish this inspection.
Access:  None required.
Zone(s):  200.
8.2  FUSELAGE SSI INFORMATION D6-82669  Original


Original D6-82669 8.2  FUSELAGE SSI INFORMATION


8.2  FUSELAGE SSI INFORMATION D6-82669 Original


N96610
F-23 - FUSELAGE BULKHEAD BS 259.5
Original D6-82669 8.2  FUSELAGE SSI INFORMATION

F-23  INSPECTION INSTRUCTIONS  REFERENCES  ACCESS MANHOURS 
MPD  CPCP  OTHERS  INSP  MHRS  ELPSD 
TITLE:  FUSELAGE BULKHEAD BS 259.5  S53-31-A  C53-100-01 C53-202-01  (1)  0.5  0.5 

I.  INSPECTION OPTIONS - DTR CHECK FORM F-23 At WL 192.5 from LBBL 18 to RBBL 18 at BS 259.5.
(1)
Lower Chord, Fail-Safe Chord and Webs
(Internal) From Direction 1, including fastener locations, using visual inspection methods.


Access: Access panel in cockpit floor.
Zone(s): 202.


(2)
Lower Chord and Fail-Safe Chord


(Internal) From Direction 2, at specified locations, using HFEC (Ref. NDT Manual D6-37239, Part 6, 53-10-07). 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
 
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