9520-14-320-1837

Structural Angle

9520143201837 143201837 2AT0336DET8

A structural shape fabricated from a ferrous or nonferrous material and resembling the letter L in cross-sectional form. The edges may have a bulb, be rounded, and the inside corner may have a fillet. View more Structural Angle

9520-14-320-1837 ANGLE,STRUCTURAL 9520143201837 143201837

Managed by France
NSN Created on 1 Jan 1975
Data Last Changed
July 2023
NATO Update Count
1
NATO Data Quality
9520-14-320-1837 ANGLE,STRUCTURAL 9520143201837 143201837 1/1
NSN 9520-14-320-1837 (Generic Image) 1/1

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9520-14-320-1837 Related Documents Related Documents 9520-14-320-1837 5+ Documents (More...)

Documents 9520-14-364-3554 2+ Documents ( More... ) https//www.nsnlookup.com /fsg-95/fsc-9520/fr 9520-14-320-1837
Structural Angle 9520143201837 143201837 axis in flight. https//www.nsnlookup.com /fsg-95/fsc-9520
Nov 1983 9620-14-253-7979 https//www.nsnlookup.com /cage Ceca Sa (CAGE Code F3757) Jan 1974 9520-14-320-1837
482-6224 https//www.nsnlookup.com /fsg-95/fsc-9520 Structural Shapes from France (FR) Aug 1980 9520-14-320-1837
1989 4460-14-310-2627 Plaque Haute Tensio 2AT0336REP10RNCC: 3 | RNVC: 2 | DAC: 2 1 Jan 1974 9520-14-320-1837
1560-00-902-9565 1560009029565 009029565 is a fixed horizontal airfoil, forming a part of the main directional control surfaces, parallel or approximately parallel to the lateral axis of an aircraft, guided missile or rocket. the functional purpose of the horizontal stabilizer is to maintain uniformity of motion in relation to the lateral axis in flight.

9520-14-320-1837 Demil Restrictions 9520-14-320-1837

DEMIL: | DEMILI: | CRITICALITY: | HMIC: | PMIC: | EDC: | ADPEC:

9520-14-320-1837 is a Structural Angle

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