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National Stock Number: 1560-01-282-3575
Federal Supply Class: 1560
National Item Identification Number: 012823575
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:
835012-2 | 17772 | AERO ENGINEERING & MANUFACTURING COMPANY OF CALIFORNIA, LLC | 835012-2 | 98897 | LOCKHEED MARTIN CORP |
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Techincal Specification:
MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-362 FED SPEC SINGLE MATERIAL RESPONSE | III MATERIAL | ALUMINUM ALLOY | PROPRIETARY CHARACTERISTICS | PACS | OVERALL LENGTH | 13.800 INCHES NOMINAL | OVERALL WIDTH | 13.530 INCHES NOMINAL | SPECIAL FEATURES | CONSISTSOF ONE SKIN P/N 835012-3 ALUMINUM ALLOY QQ-A-362 2024T-3 CLAD 0.050 IN. THK; ONE DOUBLE P/N 835012-6,ALUMINUM ALLOY QQ-A-362 2024-T42 CLAD 0.040 IN. THK; SEVEN HOLES 0.190 IN.MIN AND 0.198 IN. MAX DIA CSK FOR NAS517-3 SCREW;ONE CUTOUT 8.840 IN. DIA | THICKNESS | 0.050 INCHES NOMINAL |
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