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9540-01-468-1246
Structural Beam
9540014681246 014681246 AMS-QQ-A-200/11 10138-2404 AND10138-2404/QQ-A-200/11-T6511 AND10138-2404 AMS10138-2404
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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June 2023
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Related Documents 9540-01-468-1246 5+ Documents (More...)
AMS-QQ-A -200/11 A AMS-QQ-A -200 /11 A AMS-QQ-A AMS-QQ-A AMS-QQ-A -200/11 A AMS-QQ-A -200 /11 https A
AMS-QQ-A -200/11 A AMS-QQ-A -200 /11 A AMS-QQ-A A AMS-QQ-A -200/11 A AMS-QQ-A -200 /11 A AMS-QQ-A AMS-QQ-A
A AMS-QQ-A -200/11 A AMS-QQ-A -200 /11 A AMS-QQ-A AMS-QQ-A - -200/ / 11 - - AMS-QQ-A-200 /11 - /11 -
- - - AMS-QQ-A A AMS-QQ-A -200/11 A AMS-QQ-A -200/11 A AMS-QQ-A / AMS-QQ-A A AMS-QQ-A -200/11 A AMS-QQ-A
200 AMS-QQ-A -200/ 11 / / AMS-QQ-A - AMS-QQ-A-200/11 200 AMS-QQ-A -200/ 11 / / AMS-QQ-A 01-363
/ - AMS-QQ-A -200/11 HA18106 - - AMS-QQ-A -200 / 11 /11 AMS-QQ-A-200/11 - - HA18106 A AMS-QQ-A
- - AMS-QQ-A -200/11 BEAM AMS-QQ-A-200/11 /11 AMS-QQ-A -200/11 - - AMS-QQ-A https/ BEAM - - AMS-QQ-A
BEAM - - AMS-QQ-A-200/11 - // AMS-QQ-A - -200/11 - - AMS-QQ-A /11 - - AMS-QQ-A -200/11 - -
HA18106 A AMS-QQ-A -200/11 A AMS-QQ-A -200 /11 A AMS-QQ-A -200 /11 https A AMS-QQ-A -200/11
HA18106 - - AMS-QQ-A -200 /11 - - AMS-QQ-A-200/11 / /11 AMS-QQ-A-200 200 AMS-QQ-A -200 / /11 - - AMS-QQ-A
Restrictions 9540-01-468-1246
9540-01-468-1246 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 9540-01-468-1246
- US Air Force (FGGI)
- Effective Date:
- 1 Mar 2006
- Former MOE Rule:
- FGKZ
- US Navy (N9BZ)
- Effective Date:
- 1 Jan 2014
- Supplementary Collaborators:
- GG
Approved Sources 9540-01-468-1246
- Part Number
- Manufacturer
- Status
- AMS-QQ-A-200/11
- Manufacturer
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- AMS10138-2404
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- 10138-2404
- 29321 - Transtar Metals Corp (Active)
- Primary Buy
- Primary Buy
- AND10138-2404/QQ-A-200/11-T6511
- 14153 - Defense Logistics Agency (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- AND10138-2404
- 99237 - Airforce-Navy Aeronautical Design (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS10138-2404
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQ-A-200/11
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 9540-01-468-1246
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- Z Shape
- Bottom Flange Width [BQJH]
- 1.000 Inches Nominal
- Fabrication Method [AARN]
- Extruded
- Fillet Radius Where Bottom Right Flange Joins Web Flange/Leg [BPXM]
- 0.125 Inches Nominal
- Fillet Radius Where Top Left Flange Joins Web Flange/Leg [BPXJ]
- 0.125 Inches Nominal
- First Tip Radius [AJJB]
- 0.094 Inches Nominal
- First Tip Style [CMZY]
- Lower Radius
- Heat Treatment [HEAT]
- T-6511 Solution Heat Treated
- End Item Identification [AGAV]
- Acft Cen Sec
- Material [MATT]
- Aluminum Alloy, Ams-Qq-A-200/11, Alloy 7075
- Nondefinitive Spec/Std Data [ZZZT]
- Allou 7075 And Temper T6511
- Left Side Top Flange Thickness [ADXR]
- 0.094 Inches Nominal
- Left Top Inside Angle [CSMZ]
- 90.0 Degrees Nominal
- Length [ABRY]
- 10.000 Feet Minimum And 12.000 Feet Maximum
- Right Side Bottom Flange Thickness [BMPQ]
- 0.094 Inches Nominal
- Right Bottom Inside Angle [CWKK]
- 90.0 Degrees Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Not Identical
- Second Tip Radius [CMZZ]
- 0.094 Inches Nominal
- Second Tip Style [CNQK]
- Upper Radius
- Overall Height [ABKW]
- 2.500 Inches Nominal
- Top Flange Width [BQJG]
- 1.000 Inches Nominal
- Web Flange Thickness [BPXN]
- 0.094 Inches Nominal
- Specification/Standard Data [ZZZK]
- 99237-And10138 Government Standard
Weapon Systems (WSDC) 9540-01-468-1246
DLA Procurement Analysis 9540-01-468-1246
Management Data 9540-01-468-1246
Navy
- Cognizance:
- 9B
- Navy-owned stocks of DLA material
Naval Inventory Control Point, Mechanicsburg
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Freight Information 9540-01-468-1246
9540-01-468-1246 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 104420. A Sub NMFC of X. It has a NMFC Description of BEAMS NOI I/S. 9540-01-468-1246 is rated as class 50 when transported by Less-Than Truckload (LTL) freight. It has a Uniform Freight Classification (UFC) number of 53800 which rates the freight between FCL and LCL. 9540-01-468-1246 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. 9540-01-468-1246 is not classified as a special type of cargo when transported by water. 9540-01-468-1246 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.
Packaging Data 9540-01-468-1246
- Responsible Activity
- Packaging Data Source
- Primary Inventory Control Activity (PICA)
- --
Item Pack Level (Unpackaged)
- Item Size
- Item Weight
- Characteristics
- Weight/Dimensions Category
- Fragility
- Item Preservation
- Item Weight
- --
- --
- Plated/Coated Item
- Over 10lb
- Less than 85G
- Special Requirement
- --
Unit Pack Level (Packaged)
- Quantity per Pack
- Unit Size
- Unit Weight
- Unit Cube
- Preservation Method
- Cleaning/Drying
- Unit Size
- 1
- --
- --
- --
- --
- --
- --
- Preservation Material
- Wrapping Material
- Cushioning/Dunnage
- Cushioning Thickness
- Container
- Special Marking
- Wrapping Material
- --
- --
- --
- --
- No Requirement
- Special requirements
- --
Intermediate Pack Level
- Quantity of Unit Packs
- Container
- --
- No Requirement
Contracting Technical Data File (CTDF) 9540-01-468-1246 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):
- J
Packaging Requirements
- Packaging Determination Table:
- Packaging Review Code:
- Special Packaging Instruction Number (SPIN):
- Special Packaging Instruction Number Revision:
- Special Packaging Instruction Number Date:
- Pallet Reference Number Required: