Product Details | AIRCRAFT SPAR

1560-01-183-2036 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: 32-15004-56, 1560-01-183-2036, 01-183-2036, 1560011832036, 321500456, 011832036

Aircraft and Airframe Structural Components | Airframe Structural Components

Supply Group (FSG) NSN Assign. NIIN
15 01-183-2036

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Technical Data | NSN 1560-01-183-2036

Characteristic Specifications
MATERIAL ALUMINUM ALLOY 7075
MATERIAL DOCUMENT AND CLASSIFICATION QQ-A-250/13 FED SPEC SINGLE MATERIAL RESPONSE
AIRCRAFT LOCATION TRAILING EDGE ASSEMBLY,OUTER WING
AIRCRAFT MISSION DESIGN SERIES F-4
OVERALL LENGTH 5.600 INCHES NOMINAL
OVERALL WIDTH 4.000 INCHES NOMINAL
MATERIAL THICKNESS 0.040 INCHES NOMINAL
MANUFACTURERS CODE 76301
DESIGN CONTROL REFERENCE 32-15004-56

Restrictions/Controls & Freight Information | NSN 1560-01-183-2036

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