Product Details | AIRCRAFT SPAR

1560-01-185-6404 A principal spanwise member of the structural framework of a wing, stabilizer, other airfoil, and the like. It is designed to absorb bending loads applied to the airfoil.

Part Alternates: 53-46501-75, 1560-01-185-6404, 01-185-6404, 1560011856404, 534650175, 011856404

Aircraft and Airframe Structural Components | Airframe Structural Components

Supply Group (FSG) NSN Assign. NIIN
15 01-185-6404

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Technical Data | NSN 1560-01-185-6404

Characteristic Specifications
MATERIAL ALUMINUM ALLOY 7178
MATERIAL DOCUMENT AND CLASSIFICATION QQ-A-250 FED SPEC SINGLE MATERIAL RESPONSE
AIRCRAFT MISSION DESIGN SERIES F-4
OVERALL LENGTH 17.400 INCHES NOMINAL
OVERALL WIDTH 2.700 INCHES NOMINAL
MATERIAL THICKNESS 0.040 INCHES NOMINAL
MANUFACTURERS CODE 76301
DESIGN CONTROL REFERENCE 53-46501-75

Restrictions/Controls & Freight Information | NSN 1560-01-185-6404

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