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National Stock Number: 1560-01-528-1016
Federal Supply Class: 1560
National Item Identification Number: 015281016
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:
71091 | 91145 | FLEET READINESS CENTER SOUTHWEST | 71091-13 | 91145 | FLEET READINESS CENTER SOUTHWEST |
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Techincal Specification:
AIRCRAFT LOCATION | WING CENTER SECTION TRAILING EDGE | AIRCRAFT MISSION DESIGN SERIES | C-2A | OVERALL LENGTH | 46.000 INCHES NOMINAL | OVERALL WIDTH | 6.000 INCHES NOMINAL | PART NAME ASSIGNED BY CONTROLLING AGENCY | INAVY:STRIP | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 ASSN STD SINGLE MATERIAL RESPONSE | MATERIAL | ALUMINUM ALLOY 2024 | SIDE FOR WHICH DESIGNED | BOTH SIDES | RELATIONSHIP TO SIMILAR EQUIPMENT | 71091-11 CAP STRIP REPAIR, FOR WING CENTER SECTION TRAILING EDGE | SPECIAL FEATURES | SURFACE TREATMENT SPECIFICATION ALSO INCLUDES LPS-409. | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-STD-130 MIL STD SINGLE TREATMENT RESPONSE | SURFACE TREATMENT | PRIMER EPOXY | THICKNESS | 0.250 INCHES NOMINAL |
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