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9540-01-475-0870
Structural Beam
9540014750870 014750870 CVC10032-14CA
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 9540-01-475-0870
9540-01-475-0870 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 9540-01-475-0870
- US Air Force (FNN5)
- Effective Date:
- 1 Jun 2003
- Former MOE Rule:
- FGKZ
Approved Sources 9540-01-475-0870
- Part Number
- Manufacturer
- Status
- CVC10032-14CA
- Manufacturer
- 80378 - Triumph Aerostructures, Llc (Active)
- Primary Buy
- Primary Buy
Datasheet 9540-01-475-0870
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- T 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 Top Flange Distance To Center Of Both Flanges [BPXD]
- 1.140 Inches Nominal
- Left Side Top Flange Thickness [ADXR]
- 0.084 Inches Nominal
- Left Top Inside Angle [CSMZ]
- 45.0 Degrees Nominal
- Leg Thickness [AJJP]
- 0.150 Inches Nominal
- Length [ABRY]
- 10.000 Feet Minimum And 12.000 Feet Maximum
- Right Side Top Flange Distance To Center Of Both Flanges [BPXG]
- 1.220 Inches Nominal
- Right Side Top Flange Thickness [ADXS]
- 0.084 Inches Nominal
- Right Top Inside Angle [CRZC]
- 135.0 Degrees Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 1.747 Inches Nominal
- Top Flange Width [BQJG]
- 2.360 Inches Nominal
Management Data 9540-01-475-0870
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- May 2009
- Department of the Air Force (DF)
- FT
- Subscribe
- FT
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Freight Information 9540-01-475-0870
9540-01-475-0870 has freight characteristics.. 9540-01-475-0870 has a variance between NMFC and UFC when transported by rail and the description should be consulted.