Product Details | AIRCRAFT STRUCTURAL PANEL

1560-01-334-8075 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: 1560-01-334-8075, 01-334-8075, 1560013348075, 013348075

Aircraft and Airframe Structural Components | Airframe Structural Components

Supply Group (FSG) NSN Assign. NIIN
15 01-334-8075

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Technical Data | NSN 1560-01-334-8075

Characteristic Specifications
MATERIAL GLASS FIBER AND PLASTIC ARAMID
AIRCRAFT LOCATION LOWER OUTBOARD MAIN LANDING GEAR POD AFT SECT.
AIRCRAFT MISSION DESIGN SERIES C-141
OVERALL LENGTH 65.000 INCHES NOMINAL
OVERALL WIDTH 44.000 INCHES NOMINAL
MANUFACTURERS CODE 98752
DESIGN CONTROL REFERENCE 9032838-10

Restrictions/Controls & Freight Information | NSN 1560-01-334-8075

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