Product Details | AIRCRAFT FORMER

1560-01-376-4521 A light, secondary structural member that does not completely partition various components such as the fuselage, boom, wing, and the like. It is designed to give cross-sectional shape and strength to the item of which it is a part.

Part Alternates: 1560-01-376-4521, 01-376-4521, 1560013764521, 013764521

Aircraft and Airframe Structural Components | Airframe Structural Components

Supply Group (FSG) NSN Assign. NIIN
15 01-376-4521

Cross Reference | NSN 1560-01-376-4521

Part Number Cage Code Manufacturer
68A336002-2002 76301 BOEING COMPANY, THE DBA BOEING
68A336002-2034 76301 BOEING COMPANY, THE DBA BOEING

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Technical Data | NSN 1560-01-376-4521

Characteristic Specifications
MATERIAL TITANIUM ALLOY
MATERIAL DOCUMENT AND CLASSIFICATION MIL-T-9046 TYPE 3,COMPOSITION EANNEALED,6AL-6V-2SN MIL SPEC SINGLE MATERIAL RESPONSE
AIRCRAFT MISSION DESIGN SERIES F-15
OVERALL LENGTH 50.000 INCHES NOMINAL
OVERALL WIDTH 16.000 INCHES NOMINAL
MATERIAL THICKNESS 0.050 INCHES NOMINAL
SPECIAL FEATURES FORMER-UPPER PANEL,FS 634.950
MANUFACTURERS CODE 76301
DESIGN CONTROL REFERENCE 68A336002-2002

Restrictions/Controls & Freight Information | NSN 1560-01-376-4521

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