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9540-00-501-6128
Structural Angle
9540005016128 005016128 AND10133-1001 QQ-A-200/16
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
January 2023
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Related Documents 9540-00-501-6128 5+ Documents (More...)
AND10133-1001 ANGLE,STRUCTURAL 4 EA NS Request Quotation QQ-A-200/16 ANGLE,STRUCTURAL 8 EA NS Request
(Identification) 2/3 NSN 9540-00-501-6128 (Identification AND10133-1001 ANGLE,STRUCTURAL 4 EA NS
ANGLE,STRUCTURAL 8 EA NS Request AND10133-1001 https//www.nsnlookup.com /fsg-95/fsc-9540/us 9540-00
AND10133-1001 ANGLE,STRUCTURAL 4 EA NS Request Quotation QQ-A-200/16 ANGLE,STRUCTURAL 8 EA NS Request
ANGLE,STRUCTURAL 4 EA NS Request Quotation QQ-A-200/16 ANGLE,STRUCTURAL 8 EA NS Request Structural
ANGLE,STRUCTURAL 4 EA NS Request Quotation QQ-A-200/16 ANGLE,STRUCTURAL 8 EA NS Request AND10133
STRUCTURAL 8 FT NS Request Quotation AMS-QQ-A-200/9 ANGLE,STRUCTURAL 29 FT NS Request Quotation AND10133-1001
Structural Angle 9540005016128 005016128 $1 a day Upgrade your Account Upgrade 9540-00-501-6128Structural
AND10133-1001 ANGLE,STRUCTURAL 4 EA NS Request Quotation QQ-A-200/16 ANGLE,STRUCTURAL 8 EA NS Request
https//www.nsnlookup.com /fsg-95/fsc-9540/us 9540-00-501-6128 Structural Angle 9540005016128 005016128
Restrictions 9540-00-501-6128
9540-00-501-6128 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 9540-00-501-6128
- NASA (G860)
- Effective Date:
- 1 Apr 1991
- Turkey (ZW01)
- Effective Date:
- 1 Nov 2005
Approved Sources 9540-00-501-6128
- Part Number
- Manufacturer
- Status
- AND10133-1001
- Manufacturer
- 99237 - Airforce-Navy Aeronautical Design (Active)
- Incomplete Standard
- Incomplete Standard
- QQ-A-200/16
- 81348 - Federal Specifications Promulgated (Active)
- Incomplete Standard
- Incomplete Standard
- AND10133-1001
- 1JGN2 - Requirees (Active)
- Secondary Buy
- Secondary Buy
Datasheet 9540-00-501-6128
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- Angle
- Base Flange Thickness [AJGP]
- 0.063 Inches Nominal
- Fabrication Method [AARN]
- Extruded
- Fillet Radius Where Left Flange Joins Base Flange [AJGL]
- 0.188 Inches Nominal
- First Tip Radius [AJJB]
- 0.063 Inches Nominal
- First Tip Style [CMZY]
- Right Quarter Radius
- Heat Treatment [HEAT]
- T-6 Solution Heat Treated
- Material [MATT]
- Aluminum Alloy, Qq-A-200/16, Alloy 6061
- Nondefinitive Spec/Std Data [ZZZT]
- T6 Temper
- Left Inside Angle [CQHP]
- 90.0 Degrees Nominal
- Left Side Flange Thickness [ADXL]
- 0.063 Inches Nominal
- Second Tip Radius [CMZZ]
- 0.063 Inches Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Not Identical
- Second Tip Style [CNQK]
- Upper Radius
- Overall Height [ABKW]
- 1.000 Inches Nominal
- Overall Width [ABMK]
- 1.000 Inches Nominal
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Freight Information 9540-00-501-6128
9540-00-501-6128 has freight characteristics.. 9540-00-501-6128 has a variance between NMFC and UFC when transported by rail and the description should be consulted.