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9540-00-448-8414
Structural Angle
9540004488414 004488414 60-4663 MMS158 253142 1M2633 QQA200-11 AMS-QQA200-11
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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Restrictions 9540-00-448-8414
9540-00-448-8414 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 9540-00-448-8414
- Germany (ZG01)
- Effective Date:
- 1 Apr 1991
Approved Sources 9540-00-448-8414
- Part Number
- Manufacturer
- Status
- 60-4663
- Manufacturer
- 29321 - Transtar Metals Corp (Active)
- Incomplete Reference
- Incomplete Reference
- AMS-QQA200-11
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- MMS158
- 76301 - The Boeing Company (Active)
- Incomplete Reference
- Incomplete Reference
- 253142
- 01634 - Aluminum Co Of America (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- 1M2633
- 76301 - The Boeing Company (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- QQA200-11
- 81348 - Federal Specifications Promulgated (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQA200-11
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 9540-00-448-8414
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- Angle
- Base Flange Thickness [AJGP]
- 0.100 Inches Nominal
- Fabrication Method [AARN]
- Extruded
- Fillet Radius Where Left Flange Joins Base Flange [AJGL]
- 0.060 Inches Nominal
- First Tip Style [CMZY]
- Square End
- Heat Treatment [HEAT]
- T-73510 Solution Heat Treated
- Material Document And Classification [MDCL]
- Qq-A-200/11 Fed Spec 1St Material Response
- Material [MATT]
- Aluminum Alloy 7075
- Nondefinitive Spec/Std Data [ZZZT]
- T73510 Temper
- Left Inside Angle [CQHP]
- 135.0 Degrees Nominal
- Left Side Flange Thickness [ADXL]
- 0.100 Inches Nominal
- Length [ABRY]
- 10.000 Feet Minimum And 12.000 Feet Maximum
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 0.500 Inches Nominal
- Overall Width [ABMK]
- 0.820 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 0.156 Pounds Per Linear Foot
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Freight Information 9540-00-448-8414
9540-00-448-8414 has freight characteristics managed by the Southwestern Power Administration.It has a National Motor Freight Classification (NMFC) of 013140. A Sub NMFC of X. It has a NMFC Description of ALUMINUM ANGLES. 9540-00-448-8414 is rated as class 60 when transported by Less-Than Truckload (LTL) freight. 9540-00-448-8414 is rated as class 60 when transported by Less-Than Carload (LCL) rail or ocean freight. It has a Uniform Freight Classification (UFC) number of 05390 which rates the freight between FCL and LCL. 9540-00-448-8414 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. 9540-00-448-8414 is not classified as a special type of cargo when transported by water. 9540-00-448-8414 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.