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9540-01-233-9410
Structural Angle
9540012339410 012339410 65209-02056-101
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
November 2023
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Related Documents 9540-01-233-9410 5+ Documents (More...)
Structural Angle 9540012339410 012339410 Metal from United States (US) 2000 9540-01-233-9410 https
from https//www.nsnlookup.com /nato/nato-stock-numbers/inc Structural Angle (INC 37017) 1992 9540-01-233-9410
Structural Angle 9540012339410 012339410 /fsc-9540/us 9540-01-597-5789 Structural Channel 9540015975789
015975789 /fsg-95/fsc-9540/us 9540-01-470-9889 Structural Beam 9540014709889014709889 Structural Angle 9540012339410
Structural Angle 9540012339410 012339410 Structural Angle (INC 37017) 1992 9540-01-233-9410 https
Channel 9540015975789015975789 /fsg-95/fsc-9540/us 9540-01-470-9889 Structural Beam Structural Angle 9540012339410
Structural Angle 9540012339410 012339410 nato-stock-numbers/inc Structural Angle (INC 37017) 1E90RNCC
Restrictions 9540-01-233-9410
9540-01-233-9410 is a Structural Angle that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. 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. The precious metals content of this item is unknown.
End Users 9540-01-233-9410
- Germany (ZG01)
- Effective Date:
- 1 Apr 1991
Approved Sources 9540-01-233-9410
- Part Number
- Manufacturer
- Status
- 65209-02056-101
- Manufacturer
- 78286 - Sikorsky Aircraft Corporation (Active)
- Primary Buy
- Primary Buy
Datasheet 9540-01-233-9410
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Base Flange Thickness [AJGP]
- 0.094 Inches Nominal
- Basic Shape Style [AGTA]
- Angle
- Fabrication Method [AARN]
- Extruded
- Fillet Radius Where Left Flange Joins Base Flange [AJGL]
- 0.094 Inches Nominal
- First Tip Style [CMZY]
- Square End
- Material Document And Classification [MDCL]
- Qq-A-200/8 Fed Spec 1St Material Response
- Material [MATT]
- Aluminum Alloy 6061 Or Aluminum Alloy 6062
- Outer Radius Where Left Flange Joins Base Flange [AJGM]
- 0.188 Inches Nominal
- Left Inside Angle [CQHP]
- 90.0 Degrees Nominal
- Left Side Flange Thickness [ADXL]
- 0.094 Inches Nominal
- Length [ABRY]
- 8.000 Feet Minimum
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 2.156 Inches Nominal
NATO Stock Numbers Related to 9540-01-233-9410
Freight Information 9540-01-233-9410
9540-01-233-9410 has freight characteristics managed by Germany.. 9540-01-233-9410 has a variance between NMFC and UFC when transported by rail and the description should be consulted.