Product Details | AIRCRAFT FRAME

1560-01-333-2588 A principal transverse structural member of the fuselage, hull, nacelle, pod, and the like. It follows the periphery and provides shape and support by attachment to the longitudinal members or skin.

Part Alternates: 1560-01-333-2588, 01-333-2588, 1560013332588, 013332588

Aircraft and Airframe Structural Components | Airframe Structural Components

Supply Group (FSG) NSN Assign. NIIN
15 01-333-2588

Cross Reference | NSN 1560-01-333-2588

Part Number Cage Code Manufacturer
16K0522-47 81755 LOCKHEED MARTIN CORPORATION DBA LOCKHEED MARTIN AERONAUTICS
16K0522-53 81755 LOCKHEED MARTIN CORPORATION DBA LOCKHEED MARTIN AERONAUTICS

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Technical Data | NSN 1560-01-333-2588

Characteristic Specifications
MATERIAL ALUMINUM ALLOY 2024
MATERIAL DOCUMENT AND CLASSIFICATION QQ-A-250/4-T62 FED SPEC SINGLE MATERIAL RESPONSE
AIRCRAFT LOCATION CANOPY
SIDE FOR WHICH DESIGNED LEFT SIDE
AIRCRAFT MISSION DESIGN SERIES F-16C
OVERALL LENGTH 13.000 INCHES NOMINAL
OVERALL WIDTH 13.000 INCHES NOMINAL
MATERIAL THICKNESS 0.100 INCHES NOMINAL
MANUFACTURERS CODE 81755
DESIGN CONTROL REFERENCE 16K0522-47

Restrictions/Controls & Freight Information | NSN 1560-01-333-2588

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