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9540-00-243-9306
Structural Beam
9540002439306 002439306 AMS-QQ-A-200/11 LS4469 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
November 2023
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BEAM 200 AMS-QQ-A-200/ / 11 - - AMS-QQ-A-200 /11 /11 // // AMS-QQ-A AMS-QQ-A-200 11 - - AMS-QQ-A
// AMS-QQ-A -200 /11 / 9540013482848013482848AMS-QQ-A -200 / /11 - - AMS-QQ-A-200/11 /11 AMS-QQ-A
-200/ 11 - - AMS-QQ-A -200 /11 BEAM 200 AMS-QQ-A -200 / /11 11 A https - - AMS-QQ-A - - -200 /11 BEAM
Restrictions 9540-00-243-9306
9540-00-243-9306 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.
Import and Export 9540-00-243-9306
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 9540-00-243-9306
- US Air Force (FGGI)
- Effective Date:
- 1 Mar 2006
- Former MOE Rule:
- FGKZ
- US Navy (N9BZ)
- Effective Date:
- 1 Jan 2014
- Supplementary Collaborators:
- GG
- Brazil (YA01)
- Effective Date:
- 1 Jan 2011
- Australia (ZA01)
- Effective Date:
- 1 Apr 1991
- New Zealand (ZE01)
- Effective Date:
- 1 Jan 1998
- Republic of Korea (ZH01)
- Effective Date:
- 1 Jul 2004
Approved Sources 9540-00-243-9306
- Part Number
- Manufacturer
- Status
- LS4469
- Manufacturer
- 98897 - Lockheed Martin Corp (Active)
- Primary Buy
- Primary Buy
- AMS-QQ-A-200/11
- 0U583 - Sae International (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- 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 9540-00-243-9306
- 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]
- 0.109 Inches Minimum And 0.141 Inches Maximum
- Fillet Radius Where Top Right Flange Joins Web Flange/Leg [BPXL]
- 0.109 Inches Minimum And 0.141 Inches Maximum
- First Tip Inner Radius [CNBD]
- 0.016 Inches Minimum And 0.048 Inches Maximum
- First Tip Outer Radius [CNBJ]
- 0.016 Inches Minimum And 0.048 Inches Maximum
- First Tip Style [CMZY]
- Square W/ Inner And Outer Corner Radii
- Heat Treatment [HEAT]
- T-6511 Solution Heat Treated And Stress Relieved By Stretching
- Material [MATT]
- Aluminum Alloy Ams-Qq-A-200/11, Alloy 7075
- Nondefinitive Spec/Std Data [ZZZT]
- 7075 Composition And T6511 Temper
- Left Side Top Flange Distance To Center Of Both Flanges [BPXD]
- 1.106 Inches Minimum And 1.138 Inches Maximum
- Left Side Top Flange Thickness [ADXR]
- 0.149 Inches Minimum And 0.163 Inches Maximum
- Left Top Inside Angle [CSMZ]
- 98.0 Degrees Nominal
- Leg Thickness [AJJP]
- 0.149 Inches Minimum And 0.163 Inches Maximum
- Length [ABRY]
- 10.000 Feet Minimum And 12.000 Feet Maximum
- Right Side Top Flange Distance To Center Of Both Flanges [BPXG]
- 1.772 Inches Minimum And 1.804 Inches Maximum
- Right Side Top Flange Thickness [ADXS]
- 0.149 Inches Minimum And 0.163 Inches Maximum
- Right Top Inside Angle [CRZC]
- 82.0 Degrees Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 2.226 Inches Minimum And 2.274 Inches Maximum
- Weight Per Unit Measure [BRFD]
- 0.956 Pounds Per Linear Foot
- Third Tip Relationship To Preceding Tips [CNQL]
- Identical W/First Tip
- Top Flange Width [BQJG]
- 2.886 Inches Minimum And 2.934 Inches Maximum
Weapon Systems (WSDC) 9540-00-243-9306
DLA Procurement Analysis 9540-00-243-9306
- Last Stock Position:
- 87 In Stock
- DLA Administrative Lead Time:
- Subscribe
- DLA Production Lead Time:
- Subscribe
Management Data 9540-00-243-9306
Navy
- Cognizance:
- 9B
- Navy-owned stocks of DLA material
Naval Inventory Control Point, Mechanicsburg
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Freight Information 9540-00-243-9306
9540-00-243-9306 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. 9540-00-243-9306 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. 9540-00-243-9306 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. 9540-00-243-9306 is not classified as a special type of cargo when transported by water. 9540-00-243-9306 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 9540-00-243-9306
- 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
- No special marking
- --
Intermediate Pack Level
- Quantity of Unit Packs
- Container
- --
- No Requirement
Procurement History 9540-00-243-9306 1 Records
Contracting Technical Data File (CTDF) 9540-00-243-9306 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):
- F
Packaging Requirements
- Packaging Determination Table:
- Packaging Review Code:
- N
- Special Packaging Instruction Number (SPIN):
- Special Packaging Instruction Number Revision:
- Special Packaging Instruction Number Date:
- Pallet Reference Number Required: