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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:  FUSELAGE CIRCUMFERENTIAL SPLICES  S53-27-A S53-27-B S53-27-D S53-27-E S53-27-F S53-27-G S53-27-H  C53-107-01 C53-701-01  II.(1) III.(1) IV.(1) V.(1) VI.(1) VII.(1)  16 16 22 72 16 16  8 8 11 24 8 8 

I.  INSPECTION OPTIONS - DTR CHECK FORM F-38A At Body Station 360 from stringer S-10L to stringer S-10R (upper lobe).
(1) Splice Plate and Splice Channel (Internal) From Direction 1, including fastener locations, using visual inspection methods.
Access: Remove ceiling panels S1072 and displace insulation blankets. Zone(s): 107.
II.  INSPECTION OPTIONS - DTR CHECK FORM F-38B At Body Station 540 from stringer S-10L to stringer S-10R (upper lobe).
(1) Frame (Skin Flange) and Splice Stringer (Internal) From Direction 1, including fastener locations, using visual inspection methods.
Access: Same as I. (1).
Zone(s): Same as I. (1).

III.  INSPECTION OPTIONS - DTR CHECK FORM F-38C At Body Station 727 from stringer S-10L to stringer S-10R (upper lobe).
(1) Frame (Skin Flange) and Splice Stringer (Internal) From Direction 1, including fastener locations, using visual inspection methods.
Access: Remove ceiling panels S1082 and displace insulation blankets. Zone(s): 108.
Original  D6-82669 8.2  FUSELAGE SSI INFORMATION

IV.  INSPECTION OPTIONS - DTR CHECK FORM F-38D At Body Station 907 from stringer S-10L to stringer S-10R (upper lobe).
(1) Splice Plate and Splice Channel (Internal) From Direction 1, including fastener locations, using visual inspection methods.
Access: Same as III. (1).
Zone(s): Same as III. (1).

V.  INSPECTION OPTIONS - DTR CHECK FORM F-38E Forward of Body Station 1016 from stringer S-10L to stringer S-10R (upper lobe).
(1) Forward Frame Outer Chord and Stringer Attachment Fitting (Internal) From Direction 1, including fastener locations, using visual inspection methods.
Access: Remove galley and lavatory ceiling panels S1092, and displace insulation blankets. Zone(s): Same as III. (1).
VI.  INSPECTION OPTIONS - DTR CHECK FORM F-38F Aft of BS 1016 from stringer S-10L to stringer S-10R (upper lobe).
(1) Aft Frame Outer Chord and Stringer Attachment Fitting (External) From Direction 2, including fastener locations, using visual inspection methods.
Access: Stabilizer trim access door 3701.
Zone(s): 701.

VII. INSPECTION OPTIONS - DTR CHECK FORM F-38G At Body Station 500C (737-400 A/C only) from stringer S-10L to stringer S-10R (upper lobe).
(1) Splice Plate and Splice Channel (Internal) From Direction 1, including fastener locations, using visual inspection methods.
Access: Same as I. (1).
Zone(s): Same as I. (1).

8.2   FUSELAGE SSI INFORMATION D6-82669 Original

VIII.INSPECTION OPTIONS - DTR CHECK FORM F-38H At Body Station 727G (737-400 A/C only) from stringer S-10L to stringer S-10R (upper lobe).
(1) Splice Plate and Splice Channel (Internal) From Direction 1, including fastener locations, using visual inspection methods.
 
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