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9540-00-540-6025
Structural Beam
9540005406025 005406025 60-4493 AMS-QQA200-11 22899 BAC1505-26360 1M558 QQA200-11 E711111 14784
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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Updated Every Day Related Documents 9540-00-540-6025 5+ Documents (More...)
60-4493 1M558 BAC1505-26360 E711111 PA6108 QQ-A-200/11 A structural shape fabricated from a ferrous
Structural Beam 9540005406025 005406025 AMS-QQA200-11 22899BAC1505-263601M558 QQA200-11 E711111
14784 DIE22899 60-309 BAC1505-26360 1M558 E711111 AMS-QQ-A-200/3 QQ-A-200/3 A structural shape fabricated
Structural Beam 9540005406025 005406025 AMS-QQA200-11 22899 BAC1505-263601M558 QQA200-11 E71111114784
Structural Beam 9540005406025 005406025 9540-00-540-6025 9540005406025 005406025 is a structural
Structural Beam 9540005406025 005406025 9540-00-540-6025 9540005406025 005406025 is a structural
Structural Beam 9540005406025 005406025 9540-00-540-6025 9540005406025 005406025 is a structural
Restrictions 9540-00-540-6025
9540-00-540-6025 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. The precious metals content of this item is unknown.
End Users 9540-00-540-6025
- Germany (ZG01)
- Effective Date:
- 1 Apr 1991
Approved Sources 9540-00-540-6025
- Part Number
- Manufacturer
- Status
- 60-4493
- Manufacturer
- 29321 - Transtar Metals Corp (Active)
- Incomplete Reference
- Incomplete Reference
- AMS-QQA200-11
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- 22899
- 01634 - Aluminum Co Of America (Active)
- Incomplete Reference
- Incomplete Reference
- BAC1505-26360
- 81205 - The Boeing Company (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- 1M558
- 76301 - The Boeing Company (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- QQA200-11
- 81348 - Federal Specifications (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- E711111
- 14170 - Hughes Missile Systems Co San Diego (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- E711111
- 7B709 - Tracor Flight Systems Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQA200-11
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- 14784
- 27610 - International Light Metals Corp Sub (Obsolete)
- Canceled/Obsolete
- Canceled/Obsolete
- E711111
- 0WLU1 - General Dynamics Corp (Obsolete)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 9540-00-540-6025
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- T Shape
- Fabrication Method [AARN]
- Extruded
- Fillet Radius Where Top Left Flange Joins Web Flange/Leg [BPXJ]
- 0.094 Inches Nominal
- Fillet Radius Where Top Right Flange Joins Web Flange/Leg [BPXL]
- 0.094 Inches Nominal
- First Tip Style [CMZY]
- Square End
- Heat Treatment [HEAT]
- O-Annealed
- Material Document And Classification [MDCL]
- Qq-A-200/11 Fed Spec 1St Material Response
- Material [MATT]
- Aluminum Alloy 7075
- Nondefinitive Spec/Std Data [ZZZT]
- O Temper
- Left Side Top Flange Distance To Center Of Both Flanges [BPXD]
- 0.937 Inches Nominal
- Left Side Top Flange Thickness [ADXR]
- 0.050 Inches Nominal
- Left Top Inside Angle [CSMZ]
- 90.0 Degrees Nominal
- Leg Thickness [AJJP]
- 0.050 Inches Nominal
- Length [ABRY]
- 10.000 Feet Minimum And 12.000 Feet Maximum
- Right Side Top Flange Distance To Center Of Both Flanges [BPXG]
- 0.938 Inches Nominal
- Right Side Top Flange Thickness [ADXS]
- 0.050 Inches Nominal
- Right Top Inside Angle [CRZC]
- 90.0 Degrees Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 1.000 Inches Nominal
- Top Flange Width [BQJG]
- 1.875 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 0.170 Pounds Per Linear Foot
- Third Tip Relationship To Preceding Tips [CNQL]
- Identical W/First Tip
NATO Stock Numbers Related to 9540-00-540-6025
Freight Information 9540-00-540-6025
9540-00-540-6025 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 013760. A Sub NMFC of X. It has a NMFC Description of ALUM TEES. 9540-00-540-6025 is rated as class 60 when transported by Less-Than Truckload (LTL) freight. 9540-00-540-6025 is rated as class 60 when transported by Less-Than Carload (LCL) rail or ocean freight. It has a Uniform Freight Classification (UFC) number of 05830 which rates the freight between FCL and LCL. 9540-00-540-6025 has a variance between NMFC and UFC when transported by rail and the description should be consulted. It has a Water Commodity Code (WCC) of 576 for ocean manifesting and military sealift. 9540-00-540-6025 is not classified as a special type of cargo when transported by water. 9540-00-540-6025 is not a consolidation and does not exceed 84" in any dimension. It should be compatible with a standard 72" Aircraft Cargo Door when transported by air.