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9540-01-459-2579
Structural Beam
9540014592579 014592579 26847 1M5261
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 9540-01-459-2579
9540-01-459-2579 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 9540-01-459-2579
- Germany (ZG01)
- Effective Date:
- 1 Sep 1998
Approved Sources 9540-01-459-2579
- Part Number
- Manufacturer
- Status
- 26847
- Manufacturer
- 01634 - Aluminum Co Of America (Active)
- Primary Buy
- Primary Buy
- 1M5261
- 76301 - The Boeing Company (Active)
- Secondary Buy
- Secondary Buy
Datasheet 9540-01-459-2579
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- End Item Identification [AGAV]
- Used On Ch-53G Helicopter
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Freight Information 9540-01-459-2579
9540-01-459-2579 has freight characteristics.. 9540-01-459-2579 has a variance between NMFC and UFC when transported by rail and the description should be consulted.