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9540-00-146-0726
Structural Angle
9540001460726 001460726 AMS-QQ-A-200/3 BAC1503-1061 14594 QQ-A-200/3 S122
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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Restrictions 9540-00-146-0726
9540-00-146-0726 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. This item does not contain a precious metal.
End Users 9540-00-146-0726
- Brazil (YA01)
- Effective Date:
- 1 Aug 2000
- Portugal (ZP01)
- Effective Date:
- 1 Apr 1991
- Greece (ZU01)
- Effective Date:
- 1 Apr 1991
Approved Sources 9540-00-146-0726
- Part Number
- Manufacturer
- Status
- AMS-QQ-A-200/3
- Manufacturer
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- BAC1503-1061
- 82918 - The Boeing Company (Active)
- Incomplete Reference
- Incomplete Reference
- S122
- 7EK50 - Textron Aviation Inc (Active)
- Incomplete Reference
- Incomplete Reference
- 14594
- 01634 - Aluminum Co Of America (Active)
- Incomplete Reference
- Incomplete Reference
- QQ-A-200/3
- 81348 - Federal Specifications (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- S122
- 71379 - Cessna Aircraft Company (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQ-A-200/3
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 9540-00-146-0726
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- Angle
- Base Flange Thickness [AJGP]
- 0.062 Inches Nominal
- Fabrication Method [AARN]
- Extruded
- Fillet Radius Where Left Flange Joins Base Flange [AJGL]
- 0.031 Inches Nominal
- First Tip Style [CMZY]
- Square End
- Heat Treatment [HEAT]
- T-3511 Solution Heat Treated
- Material Document And Classification [MDCL]
- Qq-A-200/3 Fed Spec 1St Material Response
- Material [MATT]
- Aluminum Alloy 2024
- Nondefinitive Spec/Std Data [ZZZT]
- T3511 Temper
- Left Inside Angle [CQHP]
- 90.0 Degrees Nominal
- Left Side Flange Thickness [ADXL]
- 0.062 Inches Nominal
- Length [ABRY]
- 10.000 Feet Minimum And 12.000 Feet Maximum
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 0.625 Inches Nominal
- Overall Width [ABMK]
- 1.000 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 0.120 Pounds Per Linear Foot
NATO Stock Numbers Related to 9540-00-146-0726
Freight Information 9540-00-146-0726
9540-00-146-0726 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 013140. A Sub NMFC of X. It has a NMFC Description of ALUMINUM ANGLES. 9540-00-146-0726 is rated as class 60 when transported by Less-Than Truckload (LTL) freight. It has a Uniform Freight Classification (UFC) number of 05390 which rates the freight between FCL and LCL. 9540-00-146-0726 has a variance between NMFC and UFC when transported by rail and the description should be consulted. It has a Water Commodity Code (WCC) of 576 for ocean manifesting and military sealift. 9540-00-146-0726 is not classified as a special type of cargo when transported by water. 9540-00-146-0726 is not a consolidation and does not exceed 84" in any dimension. It should be compatible with a standard 72" Aircraft Cargo Door when transported by air.