Product Details | AIRCRAFT FRAME

1560-01-021-1667 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: 3232008137, 32-32008-137, 1560-01-021-1667, 01-021-1667, 1560010211667, 010211667

Aircraft and Airframe Structural Components | Airframe Structural Components

Supply Group (FSG) NSN Assign. NIIN
15 10 MAY 1976 01-021-1667

Cross Reference | NSN 1560-01-021-1667

Part Number Cage Code Manufacturer
32-32008-137 76301 BOEING COMPANY, THE DBA BOEING

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Technical Data | NSN 1560-01-021-1667

Characteristic Specifications
MATERIAL ALUMINUM ALLOY 7178
MATERIAL DOCUMENT AND CLASSIFICATION QQ-A-250/15 FED SPEC SINGLE MATERIAL RESPONSE
AIRCRAFT LOCATION AIRFRAME
AIRCRAFT MISSION DESIGN SERIES F-4
OVERALL LENGTH 14.000 INCHES NOMINAL
OVERALL WIDTH 7.500 INCHES NOMINAL
MATERIAL THICKNESS 0.040 INCHES NOMINAL
MANUFACTURERS CODE 76301
DESIGN CONTROL REFERENCE 32-32008-137

Restrictions/Controls & Freight Information | NSN 1560-01-021-1667

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
Demilitarization Code:BMunitions List Item - Mutilation (MUT) to the point of scrap required. (Formerly: Demilitarization not required. Trade Security Controls (TSCs) required at disposition.)
Precious Metals Indicator Code:UPrecious metal type is unknown
Criticality Code:X The item does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application.
Category Code Description
No Freight Information