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9540-01-428-2776
Structural Beam
9540014282776 014282776 AMS-QQ-A-200/11 60-10675 CVC10012-36CH ASTM B221 QQ-A-200/11
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 9540-01-428-2776
9540-01-428-2776 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 9540-01-428-2776
- US Air Force (FNN5)
- Effective Date:
- 1 Jun 2003
- Former MOE Rule:
- FGKZ
Approved Sources 9540-01-428-2776
- Part Number
- Manufacturer
- Status
- AMS-QQ-A-200/11
- Manufacturer
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- 60-10675
- 29321 - Transtar Metals Corp (Active)
- Primary Buy
- Primary Buy
- CVC10012-36CH
- 80378 - Triumph Aerostructures, Llc (Active)
- Primary Buy
- Primary Buy
- ASTM B221
- 81346 - American Society For Testing And (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQ-A-200/11
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- QQ-A-200/11
- 81348 - Federal Specifications Promulgated (Active)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 9540-01-428-2776
- 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]
- 0.190 Inches Nominal
- Fillet Radius Where Top Right Flange Joins Web Flange/Leg [BPXL]
- 0.190 Inches Nominal
- First Tip Style [CMZY]
- Square End
- Heat Treatment [HEAT]
- T-73511 Solution Heat Treated
- End Item Identification [AGAV]
- B-2 Bomber
- Material [MATT]
- Aluminum Alloy Ams-Qq-A-200/11, Alloy 7075
- Nondefinitive Spec/Std Data [ZZZT]
- Alloy 7075 And Temper T73511
- Left Side Top Flange Distance To Center Of Both Flanges [BPXD]
- 2.000 Inches Nominal
- Left Side Top Flange Thickness [ADXR]
- 0.140 Inches Nominal
- Left Top Inside Angle [CSMZ]
- 100.0 Degrees Nominal
- Leg Thickness [AJJP]
- 0.140 Inches Nominal
- Length [ABRY]
- 12.000 Feet Nominal
- Right Side Top Flange Distance To Center Of Both Flanges [BPXG]
- 2.000 Inches Nominal
- Right Side Top Flange Thickness [ADXS]
- 0.140 Inches Nominal
- Right Top Inside Angle [CRZC]
- 80.0 Degrees Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 5.500 Inches Nominal
- Top Flange Width [BQJG]
- 4.000 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 1.594 Pounds Per Square Foot
- Third Tip Relationship To Preceding Tips [CNQL]
- Identical W/First Tip
DLA Procurement Analysis 9540-01-428-2776
Management Data 9540-01-428-2776
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Freight Information 9540-01-428-2776
9540-01-428-2776 has freight characteristics.. 9540-01-428-2776 has a variance between NMFC and UFC when transported by rail and the description should be consulted.
Packaging Data 9540-01-428-2776
- Responsible Activity
- Packaging Data Source
- Primary Inventory Control Activity (PICA)
- Packaging Data does not meet current MIL-STD-2073-1E
Item Pack Level (Unpackaged)
- Item Size
- Item Weight
- Characteristics
- Weight/Dimensions Category
- Fragility
- Item Preservation
- Item Weight
- --
- --
- --
- --
- --
- --
Unit Pack Level (Packaged)
- Quantity per Pack
- Unit Size
- Unit Weight
- Unit Cube
- Preservation Method
- Cleaning/Drying
- Unit Size
- --
- --
- --
- --
- --
- --
- --
- Preservation Material
- Wrapping Material
- Cushioning/Dunnage
- Cushioning Thickness
- Container
- Special Marking
- Wrapping Material
- --
- --
- --
- --
- No Requirement
- --
- --
Intermediate Pack Level
- Quantity of Unit Packs
- Container
- --
- No Requirement
Contracting Technical Data File (CTDF) 9540-01-428-2776 October 2021
Criticality and Quality
- Critical Item Code:
- Flight Safety:
- Life Support:
- Certified Samples:
- Serialization:
- First Article Test (FAT):
- Certificate of Quality Compliance:
- Production Lot Testing:
- Special Testing:
- Qualified Products List (QPL):
Commercial Properties
- Government Furnished Material:
- Government Furnished Tooling:
- Government Furnished Property:
- Price Evaluation Code:
- Diminshing Manufacturing Sources:
- Warranty:
- Commerical Off The Shelf (COTS):
- End Item Application:
- Auctioning Candidate:
- Source of Procurement:
- Contract Option:
Restrictions
- Boeing Rights Guard:
- Export Controlled:
- Controlled Technical Data Package (TDP):
- Restricted Technical Data Package (TDP):
- Contains Classified Material
- Weapons System Indicator Code (WSIC):
- N
Packaging Requirements
- Packaging Determination Table:
- Packaging Review Code:
- Y
- Special Packaging Instruction Number (SPIN):
- Special Packaging Instruction Number Revision:
- Special Packaging Instruction Number Date:
- Pallet Reference Number Required: