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9540-01-437-4998
Structural Beam
9540014374998 014374998 MIL-T-81556 CVC10030-17GA
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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MIL-T-81556 BEAM,STRUCTURAL 9 FT NS Request Quotation Updated Every Day 9540-01-437-4998 RQST NE Updated
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Beam9540014374998 014374998 MIL-T-81556 MIL-T-81556 BEAM,STRUCTURAL 9 FT NS Request Quotation Updated
Structural Beam 9540014374998 014374998 MIL-T-81556 BEAM,STRUCTURAL 9 FT NS Request Quotation Updated
Every Day 9540-01-437-4998 RQST NE Updated STRUCTURAL SECTION,SPECIAL SHAPED 9 FT NS Request Quotation
Structural Beam 9540014374998 014374998 for $1 a day Upgrade your Account Upgrade 9540-01-437-4998Structural
Beam9540014374998 014374998 MIL-T-81556 MIL-T-81556 BEAM,STRUCTURAL 9 FT NS Request Quotation Updated
Restrictions 9540-01-437-4998
9540-01-437-4998 is a Structural Beam 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. This item does not contain a precious metal.
End Users 9540-01-437-4998
- US Air Force (FNN5)
- Effective Date:
- 1 Jun 2003
- Former MOE Rule:
- FGKZ
Approved Sources 9540-01-437-4998
- Part Number
- Manufacturer
- Status
- CVC10030-17GA
- Manufacturer
- 80378 - Triumph Aerostructures, Llc (Active)
- Primary Buy
- Primary Buy
- MIL-T-81556
- 81349 - Military Specifications (Active)
- Incomplete Standard
- Incomplete Standard
Datasheet 9540-01-437-4998
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- Z Shape
- Bottom Flange Width [BQJH]
- 0.750 Inches Nominal
- Fabrication Method [AARN]
- Extruded
- Fillet Radius Where Bottom Right Flange Joins Web Flange/Leg [BPXM]
- 0.090 Inches Nominal
- Fillet Radius Where Top Left Flange Joins Web Flange/Leg [BPXJ]
- 0.090 Inches Nominal
- First Tip Style [CMZY]
- Square End
- Heat Treatment [HEAT]
- Annealed
- Material [MATT]
- Titanium Alloy, Mil-T-81556, Comp Ab-1
- Nondefinitive Spec/Std Data [ZZZT]
- Composition Ab-1 And Condition Annealed
- Left Side Top Flange Thickness [ADXR]
- 0.070 Inches Nominal
- Left Top Inside Angle [CSMZ]
- 90.0 Degrees Nominal
- Length [ABRY]
- 12.000 Feet Nominal
- Right Side Bottom Flange Thickness [BMPQ]
- 0.080 Inches Nominal
- Right Bottom Inside Angle [CWKK]
- 90.0 Degrees Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 0.700 Inches Nominal
- Top Flange Width [BQJG]
- 0.600 Inches Nominal
- Web Flange Thickness [BPXN]
- 0.045 Inches Nominal
Management Data 9540-01-437-4998
- 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 9540-01-437-4998
9540-01-437-4998 has freight characteristics.. 9540-01-437-4998 has a variance between NMFC and UFC when transported by rail and the description should be consulted.