Product Details | AIRCRAFT STRUCTURAL PANEL

1560-01-339-0434 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.

Part Alternates: 1560-01-339-0434, 01-339-0434, 1560013390434, 013390434

Aircraft and Airframe Structural Components | Airframe Structural Components

Supply Group (FSG) NSN Assign. NIIN
15 01-339-0434

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Technical Data | NSN 1560-01-339-0434

Characteristic Specifications
MATERIAL ALUMINUM ALLOY
MATERIAL DOCUMENT AND CLASSIFICATION P190-1B MFR REF SINGLE MATERIAL RESPONSE
SIDE FOR WHICH DESIGNED RIGHT SIDE
AIRCRAFT MISSION DESIGN SERIES F-16
OVERALL LENGTH 23.000 INCHES NOMINAL
OVERALL WIDTH 17.000 INCHES NOMINAL
THICKNESS 2.000 INCHES NOMINAL
SPECIAL FEATURES VENTRAL FIN CORE
MANUFACTURERS CODE 81755
DESIGN CONTROL REFERENCE 16B730-48

Restrictions/Controls & Freight Information | NSN 1560-01-339-0434

Category Code Description
Hazardous Material Indicator CodePThere is no information in the HMIS; however, the NSN is in an FSC in Table II of Federal Standard 313 and an MSDS may be required by the user. The requirement for an MSDS is dependent on a hazard determination of the supplier or the intended end use of the product
Category Code Description
No Freight Information