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National Stock Number:
1560-01-469-6113
Federal Supply Class:
1560
National Item Identification Number:
014696113
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:
| 17P2A6010-146 | 88277 | THE BOEING COMPANY |
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Techincal Specification:
| MATERIAL DOCUMENT AND CLASSIFICATION | DMS2288 MFR REF 1ST MATERIAL RESPONSE AND DMS1974 MFR REF 2ND MATERIAL RESPONSE | | III MATERIAL | PLASTIC EPOXY AND PLASTIC POLYAMIDE | | PROPRIETARY CHARACTERISTICS | NPAC | | OVERALL LENGTH | 78.000 INCHES NOMINAL | | OVERALL WIDTH | 44.000 INCHES NOMINAL | | SPECIAL FEATURES | MANUFACTURER SUGGESTED NAME-PANEL ASSEMBLY-FILLET,LWR Y=833.500-Y=910.500;NHA 17P2A6010-2/-502/-504/-506;LISTED DIMENTIONS ARE STOCK SIZE | | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-P-23377 MIL SPEC SINGLE TREATMENT RESPONSE | | SURFACE TREATMENT | PRIMER EPOXY | | AIRCRAFT LOCATION | CENTER FUSELAGE | | AIRCRAFT MISSION DESIGN SERIES | C-17A |
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