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9540-00-119-9030
Structural Angle
9540001199030 001199030 734-6 1M263 BAC1503-4363 QQA200-3 AMS-QQA200-3
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 9540-00-119-9030
9540-00-119-9030 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 9540-00-119-9030
- Brazil (YA01)
- Effective Date:
- 1 Aug 2000
- New Zealand (ZE01)
- Effective Date:
- 1 Apr 1991
- Turkey (ZW01)
- Effective Date:
- 1 Nov 2005
Approved Sources 9540-00-119-9030
- Part Number
- Manufacturer
- Status
- 734-6
- Manufacturer
- 01634 - Aluminum Co Of America (Active)
- Incomplete Reference
- Incomplete Reference
- AMS-QQA200-3
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- 1M263
- 76301 - The Boeing Company (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- BAC1503-4363
- 81205 - The Boeing Company (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- QQA200-3
- 81348 - Federal Specifications (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQA200-3
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 9540-00-119-9030
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- Angle
- Base Flange Thickness [AJGP]
- 0.125 Inches Nominal
- Fabrication Method [AARN]
- Extruded
- Fillet Radius Where Left Flange Joins Base Flange [AJGL]
- 0.188 Inches Nominal
- First Tip Radius [AJJB]
- 0.094 Inches Nominal
- First Tip Style [CMZY]
- Right Quarter Radius
- Heat Treatment [HEAT]
- T-4 Solution Heat Treated And Natural Aged
- Material [MATT]
- Aluminum Alloy
- Nondefinitive Spec/Std Data [ZZZT]
- T-4 Temper
- Left Inside Angle [CQHP]
- 90.0 Degrees Nominal
- Left Side Flange Thickness [ADXL]
- 0.125 Inches Nominal
- Length [ABRY]
- 10.000 Feet Minimum And 12.000 Feet Maximum
- Second Tip Radius [CMZZ]
- 0.094 Inches Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Not Identical
- Second Tip Style [CNQK]
- Upper Radius
- Overall Height [ABKW]
- 1.250 Inches Nominal
- Overall Width [ABMK]
- 2.500 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 0.548 Pounds Per Linear Foot
NATO Stock Numbers Related to 9540-00-119-9030
Freight Information 9540-00-119-9030
9540-00-119-9030 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. 9540-00-119-9030 is rated as class 60 when transported by Less-Than Truckload (LTL) freight. 9540-00-119-9030 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. 9540-00-119-9030 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. 9540-00-119-9030 is not classified as a special type of cargo when transported by water. 9540-00-119-9030 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.