Product Details | AIRCRAFT STRUCTURAL PANEL

1560-01-326-9098 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: 3P21677137, 3P21677-137, 1560-01-326-9098, 01-326-9098, 1560013269098, 013269098

Aircraft and Airframe Structural Components | Airframe Structural Components

Supply Group (FSG) NSN Assign. NIIN
15 01-326-9098

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Technical Data | NSN 1560-01-326-9098

Characteristic Specifications
MATERIAL ALUMINUM ALLOY 2024
MATERIAL DOCUMENT AND CLASSIFICATION QQ-A-362 FED SPEC SINGLE MATERIAL RESPONSE
AIRCRAFT LOCATION AFT COWL-NO. 1 VANE SPLITTER
AIRCRAFT MISSION DESIGN SERIES C-141
OVERALL LENGTH 17.000 INCHES NOMINAL
OVERALL WIDTH 11.000 INCHES NOMINAL
THICKNESS 0.080 INCHES NOMINAL
MANUFACTURERS CODE 98897
DESIGN CONTROL REFERENCE 3P21677-137

Restrictions/Controls & Freight Information | NSN 1560-01-326-9098

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