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9540-00-492-3291
Structural Angle
9540004923291 004923291 1MA100D01-10270 QQ-A-200/11 10164545
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 9540-00-492-3291 5+ Documents (More...)
QQ-A-200/11 A metallic product of ferrous or nonferrous material.
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44132 QQ-A-200/11 A structural shape fabricated from a ferrous or nonferrous material and resembling
AMS-QQ-A-200/11 HA18106-7075T6511 Managed by United States NSN Created on 3 Apr 1979 Data Last Changed
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STRUCTURAL ALLOY 7075 TMPR 120078 AMS-STD-184 AMS-QQ-A-200/11 PA12597 QQ-A-200/11 A structural shape
Restrictions 9540-00-492-3291
9540-00-492-3291 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 9540-00-492-3291
- Finland (WF01)
- Effective Date:
- 1 Jul 2009
- Spain (YB01)
- Effective Date:
- 1 Apr 1991
- Canada (ZC01)
- Effective Date:
- 1 Apr 1991
Approved Sources 9540-00-492-3291
- Part Number
- Manufacturer
- Status
- 1MA100D01-10270
- Manufacturer
- 76301 - The Boeing Company (Active)
- Incomplete Reference
- Incomplete Reference
- QQ-A-200/11
- 81348 - Federal Specifications (Active)
- Incomplete Standard
- Incomplete Standard
- 10164545
- A486G - Nimikkeistokeskus Ncb Finland (Active)
- NATO Reference
- NATO Reference
Datasheet 9540-00-492-3291
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- Angle
- Base Flange Thickness [AJGP]
- 0.040 Inches Nominal
- Fabrication Method [AARN]
- Extruded
- Fillet Radius Where Left Flange Joins Base Flange [AJGL]
- 0.094 Inches Nominal
- First Tip Style [CMZY]
- Square End
- Heat Treatment [HEAT]
- O-Annealed
- Material Document And Classification [MDCL]
- Qq-A-200/11 Fed Spec 1St Material Response
- Material [MATT]
- Aluminum Alloy 7075
- Nondefinitive Spec/Std Data [ZZZT]
- O Temper
- Left Inside Angle [CQHP]
- 90.0 Degrees Nominal
- Left Side Flange Thickness [ADXL]
- 0.040 Inches Nominal
- Length [ABRY]
- 10.000 Feet Minimum And 12.000 Feet Maximum
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 1.200 Inches Nominal
- Overall Width [ABMK]
- 1.800 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 0.142 Pounds Per Linear Foot
NATO Stock Numbers Related to 9540-00-492-3291
Freight Information 9540-00-492-3291
9540-00-492-3291 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. 9540-00-492-3291 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. 9540-00-492-3291 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. 9540-00-492-3291 is not classified as a special type of cargo when transported by water. 9540-00-492-3291 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.