Product Details | AIRCRAFT STRUCTURAL PANEL

1560-01-302-2093 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: 1560-01-302-2093, 01-302-2093, 1560013022093, 013022093

Aircraft and Airframe Structural Components | Airframe Structural Components

Supply Group (FSG) NSN Assign. NIIN
15 01-302-2093

Cross Reference | NSN 1560-01-302-2093

Part Number Cage Code Manufacturer
68A332045-2043 76301 BOEING COMPANY, THE DBA BOEING
68A332045-2055 76301 BOEING COMPANY, THE DBA BOEING

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Technical Data | NSN 1560-01-302-2093

Characteristic Specifications
MATERIAL ALUMINUM ALLOY 6061
AIRCRAFT LOCATION CLOSURE-VERTICAL STABILIZER LEADING EDGE
AIRCRAFT MISSION DESIGN SERIES F-15
SPECIAL FEATURES AL ALLOY 6061-T6

Restrictions/Controls & Freight Information | NSN 1560-01-302-2093

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