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National Stock Number:
1560-01-370-3138
Federal Supply Class:
1560
National Item Identification Number:
013703138
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:
| 17P2A6014-3 | 88277 | THE BOEING COMPANY |
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Techincal Specification:
| AIRCRAFT LOCATION | FILLET,AFT | | AIRCRAFT MISSION DESIGN SERIES | C-17 | | AIRCRAFT STATION NUMBER | Y1088 TO Y1184.797 | | FABRICATION METHOD | COMPOSITE AND HONEYCOMB AND SANDWICH | | MATERIAL DOCUMENT AND CLASSIFICATION | DMS2288,TYPE 4,CLASS 5,GRADE H MFR REF 1ST MATERIAL RESPONSE AND DMS1974,TYPE 2,CLASS 2,GRADE A,DENSITY 3PCF MFR REF 2ND MATERIAL RESPONSE | | III MATERIAL | PLASTIC ARAMID AND PLASTIC POLYAMIDE | | PROPRIETARY CHARACTERISTICS | NPAC | | SIDE FOR WHICH DESIGNED | LEFT SIDE | | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-P-23377 MIL SPEC SINGLE TREATMENT RESPONSE | | SURFACE TREATMENT | PRIMER EPOXY |
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