1560-01-116-2220 PANEL,STRUCTURAL,AIRCRAFT Index 1560-01-116-2222 PANEL ASSEMBLY

National Stock Number:
1560-01-116-2221

Federal Supply Class:
1560

National Item Identification Number:
011162221

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.


Manufacturer Information:
4J50012-113B059S2AAR COMPONENT SERVICES - HOT SPRINGS, LLC.
4J50012-113B29183G. S. E. DYNAMICS, INC.
4J50012-113B29957NORDAM GROUP LLC, THE
4J50012-113B3ECN8LBZ, L.L.C
4J50012-113B419Y2TOP FLIGHT AEROSTRUCTURES, INC.
4J50012-113B4PFC1CASCADE COMPOSITES LLC
4J50012-113B59213AERO COMPONENTS, LLC
4J50012-113B7HU35HONEYCOMB AIRCRAFT REPAIR CENTER, LLC
4J50012-113B96670BEVLES COMPANY INCORPORATED
4J50012-113B98897LOCKHEED MARTIN CORP
4J50012-113B99115HONEYCOMB COMPANY OF AMERICA, INC.


Techincal Specification:
AIRCRAFT LOCATIONFIXED TRAILNG EDGE
AIRCRAFT MISSION DESIGN SERIESC-5A
OVERALL LENGTH37.000 INCHES NOMINAL
OVERALL WIDTH1.000 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-250 FED SPEC SINGLE MATERIAL RESPONSE
MATERIALALUMINUM ALLOY 2024
THICKNESS0.032 INCHES NOMINAL


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