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9540-01-471-8194
Structural Beam
9540014718194 014718194 CVC10030-15CJ
A structural shape fabricated from a ferrous or nonferrous material and resembles the following cross-sectional forms: For the letter H, both flanges of the H section are equal or longer than the width measured along the axis of the web; for the letter I, a 16 2/3 percent slope on the inside face of the ferrous type flange, either one or both of the nonferrous type flanges are shorter than the length measured along the axis of the web; for the letters T and Z, on nonferrous type, the web is usually at right angles to the flanges. Letter H section may have a maximum of 5 percent slope on the inside face of the flanges. View more Structural Beam
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Restrictions 9540-01-471-8194
9540-01-471-8194 is a Structural Beam that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. 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 9540-01-471-8194
- US Air Force (FNN5)
- Effective Date:
- 1 Jun 2003
- Former MOE Rule:
- FGKZ
Approved Sources 9540-01-471-8194
- Part Number
- Manufacturer
- Status
- CVC10030-15CJ
- Manufacturer
- 80378 - Triumph Aerostructures, Llc (Active)
- Primary Buy
- Primary Buy
Datasheet 9540-01-471-8194
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- H Shape
- Fabrication Method [AARN]
- Extruded
- Fillet Radius Where Bottom Left Flange Joins Web Flange/Leg [BPXK]
- 0.125 Inches Nominal
- Fillet Radius Where Bottom Right Flange Joins Web Flange/Leg [BPXM]
- 0.125 Inches Nominal
- Fillet Radius Where Top Left Flange Joins Web Flange/Leg [BPXJ]
- 0.125 Inches Nominal
- Fillet Radius Where Top Right Flange Joins Web Flange/Leg [BPXL]
- 0.125 Inches Nominal
- First Tip Inner Radius [CNBD]
- 0.032 Inches Nominal
- First Tip Outer Radius [CNBJ]
- 0.032 Inches Nominal
- First Tip Style [CMZY]
- Square W/ Inner And Outer Corner Radii
- Fourth Tip Relationship To Preceding Tips [CNQN]
- Identical W/First Tip
- Heat Treatment [HEAT]
- T-76511 Solution Heat Treated
- Material [MATT]
- Aluminum Alloy 7075
- Left Side Bottom Flange Distance To Center Of Both Flanges [BPXF]
- 0.750 Inches Nominal
- Left Side Flange Height [ADXJ]
- 1.500 Inches Nominal
- Left Bottom Inside Angle [CTBR]
- 90.0 Degrees Nominal
- Left Side Flange Thickness [ADXL]
- 0.136 Inches Nominal
- Left Side Top Flange Distance To Center Of Both Flanges [BPXD]
- 0.750 Inches Nominal
- Left Top Inside Angle [CSMZ]
- 90.0 Degrees Nominal
- Length [ABRY]
- 14.000 Feet Nominal
- Right Side Bottom Flange Distance To Center Of Both Flanges [BPXH]
- 2.150 Inches Nominal
- Right Side Flange Height [ADXK]
- 4.300 Inches Nominal
- Right Side Flange Thickness [ADXM]
- 0.210 Inches Nominal
- Right Side Top Flange Distance To Center Of Both Flanges [BPXG]
- 2.150 Inches Nominal
- Right Top Inside Angle [CRZC]
- 90.0 Degrees Nominal
- Right Bottom Inside Angle [CWKK]
- 90.0 Degrees Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Width [ABMK]
- 3.750 Inches Nominal
- Special Features [FEAT]
- Ws Is Aircraft,B-2 Bomber (Atb)
- Web Flange Thickness [BPXN]
- 0.156 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 19.968 Pounds Per Linear Foot
- Third Tip Relationship To Preceding Tips [CNQL]
- Identical W/First Tip
Management Data 9540-01-471-8194
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Apr 2009
- Department of the Air Force (DF)
- FT
- Subscribe
- FT
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Freight Information 9540-01-471-8194
9540-01-471-8194 has freight characteristics.. 9540-01-471-8194 has a variance between NMFC and UFC when transported by rail and the description should be consulted.