Product Details | AIRCRAFT FORMER

1560-01-162-1009 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: 35-8220-508, 1560-01-162-1009, 01-162-1009, 1560011621009, 358220508, 011621009

Aircraft and Airframe Structural Components | Airframe Structural Components

Supply Group (FSG) NSN Assign. NIIN
15 01-162-1009

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Technical Data | NSN 1560-01-162-1009

Characteristic Specifications
MATERIAL ALUMINUM ALLOY
MATERIAL DOCUMENT AND CLASSIFICATION MIL-S-25043 MIL STD SINGLE MATERIAL RESPONSE
AIRCRAFT LOCATION USED AS ANGLE UPPER OUTER ON FRAME-CANTED,BODY COWL PANEL
AIRCRAFT MISSION DESIGN SERIES B-52 AIRCRAFT
OVERALL LENGTH 13.600 INCHES NOMINAL
OVERALL WIDTH 2.000 INCHES NOMINAL
MATERIAL THICKNESS 0.032 INCHES NOMINAL
SPECIAL FEATURES OPP 35-8220-507
MANUFACTURERS CODE 81205
DESIGN CONTROL REFERENCE 35-8220-508

Restrictions/Controls & Freight Information | NSN 1560-01-162-1009

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