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9540-00-145-8429
Structural Angle
9540001458429 001458429 QQ-A-200/3 AND10134-0701 1114111
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 9540-00-145-8429
9540-00-145-8429 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 9540-00-145-8429
- Brazil (YA01)
- Effective Date:
- 1 Jan 2011
- Germany (ZG01)
- Effective Date:
- 1 Apr 1991
Approved Sources 9540-00-145-8429
- Part Number
- Manufacturer
- Status
- 1114111
- Manufacturer
- 88277 - The Boeing Company (Active)
- Incomplete Reference
- Incomplete Reference
- QQ-A-200/3
- 81348 - Federal Specifications (Active)
- Incomplete Standard
- Incomplete Standard
- AND10134-0701
- 99237 - Airforce-Navy Aeronautical Design (Active)
- Incomplete Standard
- Incomplete Standard
- 1114111
- 18355 - The Boeing Company (Active)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 9540-00-145-8429
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- Angleangle
- Base Flange Thickness [AJGP]
- 0.063 Inches Nominal0.063 Inches Nominal
- Fabrication Method [AARN]
- Extrudedextruded
- Fillet Radius Where Left Flange Joins Base Flange [AJGL]
- 0.125 Inches Nominal0.125 Inches Nominal
- First Tip Radius [AJJB]
- 0.063 Inches Nominal0.063 Inches Nominal
- First Tip Style [CMZY]
- Right Quarter Radiusright Quarter Radius
- Heat Treatment [HEAT]
- T-4 Solution Heat Treatedt-4 Solution Heat Treated
- Material Document And Classification [MDCL]
- Qq-A-200/3 Fed Spec 1St Material Responseqq-A-200/3 Fed Spec 1St Material Response
- Material [MATT]
- Aluminum Alloy 2024Aluminum Alloy 2024
- Nondefinitive Spec/Std Data [ZZZT]
- T4 Tempert4 Temper
- Left Inside Angle [CQHP]
- 90.0 Degrees Nominal90.0 Degrees Nominal
- Left Side Flange Thickness [ADXL]
- 0.063 Inches Nominal0.063 Inches Nominal
- Length [ABRY]
- 10.000 Feet Minimum And 10.000 Feet Minimum And 12.000 Feet Maximum12.000 Feet Maximum
- Second Tip Radius [CMZZ]
- 0.063 Inches Nominal0.063 Inches Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Not Identicalnot Identical
- Second Tip Style [CNQK]
- Upper Radiusupper Radius
- Overall Height [ABKW]
- 0.625 Inches Nominal0.625 Inches Nominal
- Overall Width [ABMK]
- 0.875 Inches Nominal0.875 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 0.110 Pounds Per Linear Foot0.110 Pounds Per Linear Foot
NATO Stock Numbers Related to 9540-00-145-8429
Freight Information 9540-00-145-8429
9540-00-145-8429 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. 9540-00-145-8429 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. 9540-00-145-8429 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. 9540-00-145-8429 is not classified as a special type of cargo when transported by water. 9540-00-145-8429 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.