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National Stock Number:
1560-01-478-0838
Federal Supply Class:
1560
National Item Identification Number:
014780838
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:
| 17P2A6519-3 | 88277 | THE BOEING COMPANY |
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Techincal Specification:
| AIRCRAFT LOCATION | WG TO FUS PANEL, FILLET-OUTBD, UPR, AFT | | AIRCRAFT MISSION DESIGN SERIES | C-17 | | MATERIAL DOCUMENT AND CLASSIFICATION | DMS 2288,TYPE 2,CLASS 2,GRADE D MFR REF 1ST MATERIAL RESPONSE AND DMS 1974,TYPE 2,CLASS 2,GRADE B,DENSITY-3 PCF MFR REF 2ND MATERIAL RESPONSE | | III MATERIAL | PLASTIC EPOXY AND PLASTIC POLYIMIDE | | PROPRIETARY CHARACTERISTICS | NPAC | | SPECIAL FEATURES | CONSISTS OF 1(-5) PANEL, 1(-7) CORE, 1(-9) CORE, 2 RETAINERS, 2 SEALS AND 44 RIVETS. PANEL MATERIAL GLASS FIBER WOVEN FABRIC AND CARBON FIBER WOVEN FABRIC; CORE MATERIAL HONECOMB POLYMIDE PAPER, OVEREXPANDED |
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