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National Stock Number:
1560-01-371-1356
Federal Supply Class:
1560
National Item Identification Number:
013711356
Description:
PANEL,STRUCTURAL,AIRCRAFT
Detail:
A preformed item of various shapes, and contours, which may have a sandwich or honeycomb core bonded to a metallic or nonmetallic facing material. It is used to enclose integral portions of the fuselage or to form partitions or sections within a wing, empennage, fuselage, nacelle or crew compartment. It may have mounting provisions such as predrilled holes to facilitate installation, but will have no items attached to it except bracket (s) or other securing devices to accommodate its own mounting or support. It may be mounted by means of fasteners, bonding or welding. Excludes PANEL, INTERIOR LINING, AIRCRAFT; COVER ACCESS; COVER, ACCESS, AIRCRAFT; FLOOR (1), AIRCRAFT; CORE MATERIAL, CELLULAR, STRUCTURAL.
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Manufacturer Information:
| 17P2A6005-48 | 88277 | THE BOEING COMPANY |
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Techincal Specification:
| AIRCRAFT LOCATION | FWD FUSELAGE FILLET | | AIRCRAFT STATION NUMBER | FS 536.000 TO 609.500 | | AIRCRAFT MISSION DESIGN SERIES | C-17A | | FABRICATION METHOD | LAMINATED AND COMPOSITE | | MATERIAL DOCUMENT AND CLASSIFICATION | DMS1974 MFR REF 1ST MATERIAL RESPONSE AND DMS2288 MFR REF 2ND MATERIAL RESPONSE | | III MATERIAL | PLASTIC POLYAMIDE AND PLASTIC EPOXY | | PROPRIETARY CHARACTERISTICS | NPAC | | SIDE FOR WHICH DESIGNED | RIGHT SIDE | | SPECIAL FEATURES | NHA 17P2A6005-502 | | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-P-23377 MIL SPEC SINGLE TREATMENT RESPONSE | | SURFACE TREATMENT | PRIMER EPOXY |
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