Product Details | AIRCRAFT STRINGER

1560-01-032-1220 An auxiliary longitudinal member of the structural framework of a fuselage, nacelle, empennage, wing, and the like. It is designed to stiffen and/or support the skin by attachment of bulkheads, formers, frames, ribs, and the like.

Part Alternates: 3232081259, 32-32081-259, 1560-01-032-1220, 01-032-1220, 1560010321220, 010321220

Aircraft and Airframe Structural Components | Airframe Structural Components

Supply Group (FSG) NSN Assign. NIIN
15 01-032-1220

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Technical Data | NSN 1560-01-032-1220

Characteristic Specifications
MATERIAL ALUMINUM ALLOY
AIRCRAFT MISSION DESIGN SERIES F-4
OVERALL LENGTH 24.980 INCHES NOMINAL
OVERALL WIDTH 3.600 INCHES NOMINAL
MATERIAL THICKNESS 0.040 INCHES NOMINAL

Restrictions/Controls & Freight Information | NSN 1560-01-032-1220

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