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9540-01-578-3552

Structural Angle

9540015783552 015783552 60-8245 TMS60-8245

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

9540-01-578-3552 ANGLE,STRUCTURAL 9540015783552 015783552

Managed by United States
NSN Created on 2 Oct 2009
Data Last Changed
November 2023
NATO Update Count
5
NATO Data Quality
9540-01-578-3552 ANGLE,STRUCTURAL 9540015783552 015783552 1/1
NSN 9540-01-578-3552 (Generic Image) 1/1

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9540-01-578-3552 Related Documents Related Documents 9540-01-578-3552 5+ Documents (More...)

https//www.nsnlookup.com /nato/nato-stock-numbers/inc Structural Angle (INC 37017) 14 Feb 1979 9540-01-578-3552
/fsg-95/fsc-9540 Structural Shapes, Nonferrous Base Metal from United States (US) 4 Feb 2012 9540-01-578-3552
Shapes, Nonferrous Base Metal from United States https//www.nsnlookup.com /fsg-95/fsc-9540/us 9540-01-578-3552
Structural Angle 9540015783552 015783552 Metal from United States (US) Structural Channel 3003125RNCC
Feb 1972 9540-01-071-7380 Structural Angle K10A67T8511RNCC: 5 | RNVC: 1 | DAC: 1 14 Feb 1979 9540-01-578-3552
Structural Channel 3003125RNCC: 3 | RNVC: 2 | DAC: D 12 Mar 2013 9540-01-602-7598 4 Feb 2012 9540-01-578-3552

9540-01-578-3552 Demil Restrictions 9540-01-578-3552

DEMIL: D | DEMILI: 1 | CRITICALITY: X | HMIC: N | PMIC: A | EDC: A | ADPEC: 0

9540-01-578-3552 is a Structural Angle that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. This item is a US Munitions List or Commerce Control List Item which must be destroyed to prevent restoration or repair. Only authorized parties may possess this item. This item is not suspected to be hazardous. This item does not contain a precious metal.

9540-01-578-3552 End Users End Users 9540-01-578-3552

Australia (ZA01)
Effective Date:
1 Oct 2009

9540-01-578-3552 Manufacturers Approved Sources 9540-01-578-3552

9540-01-578-3552 Technical Data Datasheet 9540-01-578-3552

Characteristic
Specifications
Base Flange Thickness [AJGP]
0.050 Inches Nominal
Basic Shape Style [AGTA]
Angle
Fabrication Method [AARN]
Extruded And Hot Finish
First Tip Inner Radius [CNBD]
0.050 Inches Nominal
First Tip Outer Radius [CNBJ]
0.016 Inches Nominal
First Tip Style [CMZY]
Square W/ Inner And Outer Corner Radii
End Item Identification [AGAV]
Airbus;F-35 Joint Strike Fighter
Material [MATT]
Aluminum Alloy
Part Name Assigned By Controlling Agency [CXCY]
Structural Beam Section
Left Inside Angle [CQHP]
93.0 Degrees Nominal
Left Side Flange Thickness [ADXL]
0.050 Inches Nominal
Second Tip Relationship To First Tip [CNQJ]
Identical
Overall Height [ABKW]
0.750 Inches Nominal
Overall Width [ABMK]
0.937 Inches Nominal
Special Features [FEAT]
Obtuse Angle,Unequal Legs;Aircraft Aluminum;Aircraft Spares

9540-01-578-3552 Related Items NATO Stock Numbers Related to 9540-01-578-3552

9540-01-578-3552 Freight Data Freight Information 9540-01-578-3552

9540-01-578-3552 has freight characteristics managed by Australia.. 9540-01-578-3552 has a variance between NMFC and UFC when transported by rail and the description should be consulted.