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9540-01-475-0908
Structural Beam
9540014750908 014750908 CVC10031-19CA
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
January 2023
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Restrictions 9540-01-475-0908
9540-01-475-0908 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. This item does not contain a precious metal.
End Users 9540-01-475-0908
- US Air Force (FNN5)
- Effective Date:
- 1 Jun 2003
- Former MOE Rule:
- FGKZ
Approved Sources 9540-01-475-0908
- Part Number
- Manufacturer
- Status
- CVC10031-19CA
- Manufacturer
- 80378 - Triumph Aerostructures, Llc (Active)
- Primary Buy
- Primary Buy
Datasheet 9540-01-475-0908
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- H Shape
- Fabrication Method [AARN]
- Any Acceptable
- First Tip Style [CMZY]
- Square End
- End Item Identification [AGAV]
- Intermediate; Aircraft, B-2 Bomber (Atb)
- Material Document And Classification [MDCL]
- Qq-A-430, Alloy 7075 Fed Spec 1St Material Response
- Material [MATT]
- Aluminum Alloy 7075
- Left Side Bottom Flange Distance To Center Of Both Flanges [BPXF]
- 0.900 Inches Nominal
- Left Side Flange Height [ADXJ]
- 1.800 Inches Nominal
- Left Bottom Inside Angle [CTBR]
- 90.0 Degrees Nominal
- Left Side Flange Thickness [ADXL]
- 0.188 Inches Nominal
- Left Side Top Flange Distance To Center Of Both Flanges [BPXD]
- 0.900 Inches Nominal
- Left Top Inside Angle [CSMZ]
- 90.0 Degrees Nominal
- Length [ABRY]
- 10.000 Feet Minimum And 12.000 Feet Maximum
- Right Side Bottom Flange Distance To Center Of Both Flanges [BPXH]
- 0.900 Inches Nominal
- Right Side Flange Height [ADXK]
- 1.800 Inches Nominal
- Right Side Flange Thickness [ADXM]
- 0.125 Inches Nominal
- Right Side Top Flange Distance To Center Of Both Flanges [BPXG]
- 0.900 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]
- 1.000 Inches Nominal
- Web Flange Thickness [BPXN]
- 0.125 Inches Nominal
Management Data 9540-01-475-0908
- 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 9540-01-475-0908
9540-01-475-0908 has freight characteristics.. 9540-01-475-0908 has a variance between NMFC and UFC when transported by rail and the description should be consulted.