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9540-00-118-0168
Structural Angle
9540001180168 001180168 AMS-QQ-A-200/3 36180 S74 QQ-A-200/3
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 9540-00-118-0168
9540-00-118-0168 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 9540-00-118-0168
- Brazil (YA01)
- Effective Date:
- 1 Aug 2000
- New Zealand (ZE01)
- Effective Date:
- 1 Apr 1991
- Greece (ZU01)
- Effective Date:
- 1 Jan 2007
Approved Sources 9540-00-118-0168
- Part Number
- Manufacturer
- Status
- AMS-QQ-A-200/3
- Manufacturer
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- 36180
- 27610 - International Light Metals Corp Sub (Obsolete)
- Incomplete Reference
- Incomplete Reference
- S74
- 7EK50 - Textron Aviation Inc (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- AMS-QQ-A-200/3
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- S74
- 71379 - Cessna Aircraft Company (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- QQ-A-200/3
- 81348 - Federal Specifications Promulgated (Active)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 9540-00-118-0168
- 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]
- 0.120 Inches Nominal
- First Tip Radius [AJJB]
- 0.060 Inches Nominal
- First Tip Style [CMZY]
- Right Quarter Radius
- 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 Radius [CMZZ]
- 0.060 Inches Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Not Identical
- Second Tip Style [CNQK]
- Upper Radius
- Overall Height [ABKW]
- 0.500 Inches Nominal
- Overall Width [ABMK]
- 0.875 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 0.100 Pounds Per Linear Foot
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Freight Information 9540-00-118-0168
9540-00-118-0168 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. 9540-00-118-0168 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. 9540-00-118-0168 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. 9540-00-118-0168 is not classified as a special type of cargo when transported by water. 9540-00-118-0168 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.