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9540-01-261-6223
Structural Angle
9540012616223 012616223 AND10134-1003 AND10134-1003-7075T7
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
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6223Structural Angle9540012616223 012616223 AND10134 AND10134-1003 ANGLE,STRUCTURAL 10 EA NS Request
Updated Every Day 9540-01-261-6223 RQST NE AND10134-1003 ANGLE,STRUCTURAL 10 EA NS Request Quotation
/QQ-A-200/3-T3511 AND10134-1003 AMS10134-1003 LS10134-1003 QQ-A-200/3 9540PL0900340 9540PL1823575
Updated Every Day 9540-01-261-6223 RQST NE AND10134-1003 ANGLE,STRUCTURAL 10 EA NS Request Quotation
/QQ-A-200/3-T3511 AND10134-1003 AMS10134-1003 LS10134-1003 QQ-A-200/3 9540PL0900340 9540PL1823575
Structural Angle 9540012616223 012616223 AND10134-1003 /QQ-A-200/3-T3511 AND10134-1003 AMS10134
AMS10134-1003 LS10134-1003 QQ-A-200/3 9540PL0900340 9540PL1823575 https//www.nsnlookup.com AND10134-1003
/QQ-A-200/3-T3511 AND10134-1003 AMS10134-1003 LS10134-1003 QQ-A-200/3 9540PL0900340 AMS-QQ-A-200
Structural Angle 9540012616223 012616223 006894223 Account Upgrade 9540-00-689-4223Structural Angle9540006894223
Restrictions 9540-01-261-6223
9540-01-261-6223 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 9540-01-261-6223
- Brazil (YA01)
- Effective Date:
- 1 Jul 2001
Approved Sources 9540-01-261-6223
- Part Number
- Manufacturer
- Status
- AND10134-1003
- Manufacturer
- 99237 - Airforce-Navy Aeronautical Design (Active)
- Incomplete Standard
- Incomplete Standard
- AND10134-1003-7075T7
- 99237 - Airforce-Navy Aeronautical Design (Active)
- Incomplete Standard
- Incomplete Standard
Datasheet 9540-01-261-6223
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Base Flange Thickness [AJGP]
- 0.063 Inches Nominal
- Basic Shape Style [AGTA]
- Angle
- Fabrication Method [AARN]
- Extruded
- Fillet Radius Where Left Flange Joins Base Flange [AJGL]
- 0.125 Inches Nominal
- First Tip Style [CMZY]
- Right Quarter Radius
- Material Document And Classification [MDCL]
- Qq-A-200/11 Fed Spec 1St Material Response
- Material [MATT]
- Aluminum Alloy 7075
- Left Inside Angle [CQHP]
- 90.0 Degrees Nominal
- Left Side Flange Thickness [ADXL]
- 0.063 Inches Nominal
- Length [ABRY]
- 10.000 Feet Minimum And 12.000 Feet Maximum
- Second Tip Relationship To First Tip [CNQJ]
- Not Identical
- Second Tip Style [CNQK]
- Left Quarter Radius
- Overall Height [ABKW]
- 0.250 Inches Nominal
- Overall Width [ABMK]
- 1.000 Inches Nominal
NATO Stock Numbers Related to 9540-01-261-6223
Freight Information 9540-01-261-6223
9540-01-261-6223 has freight characteristics managed by the United Kingdom (UK).. 9540-01-261-6223 has a variance between NMFC and UFC when transported by rail and the description should be consulted.