9540-01-265-2006

Structural Beam

9540012652006 012652006 150010-1

A structural shape fabricated from a ferrous or nonferrous material and resembles the following cross-sectional forms: For the letter H, both flanges of the H section are equal or longer than the width measured along the axis of the web; for the letter I, a 16 2/3 percent slope on the inside face of the ferrous type flange, either one or both of the nonferrous type flanges are shorter than the length measured along the axis of the web; for the letters T and Z, on nonferrous type, the web is usually at right angles to the flanges. Letter H section may have a maximum of 5 percent slope on the inside face of the flanges. View more Structural Beam

9540-01-265-2006 BEAM,STRUCTURAL 9540012652006 012652006

Managed by United States
NSN Created on 10 Oct 1987
Data Last Changed
November 2023
NATO Update Count
5
NATO Data Quality
9540-01-265-2006 BEAM,STRUCTURAL 9540012652006 012652006 1/1
NSN 9540-01-265-2006 (Generic Image) 1/1

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https//www.nsnlookup.com /nato/nato-stock-numbers/inc Structural Beam (INC 37018) 20 Oct 1987 9540-01-265-2006
https//www.nsnlookup.com /cage Lockheed Martin Corporation (CAGE Code 80070) A 4 Apr 1983 9540-01-265-2006
Details... 53E150010-1 ADAPTER,TEST 1 EA NS Request Quotation Subscribe to View Vendor Details... 53E-150010-1
4920-00-905-1631 4920009051631 009051631 is a test set primarily designed for use in making examinations of a flight control system.

9540-01-265-2006 Demil Restrictions 9540-01-265-2006

DEMIL: A | DEMILI: | CRITICALITY: | HMIC: N | PMIC: A | EDC: | ADPEC: 0

9540-01-265-2006 is a Structural Beam This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. This item does not contain a precious metal.

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