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9540-00-241-2712
Structural Beam
9540002412712 002412712 AMS-QQ-A-200/11 H199 35302 AMS10134-3002 QQ-A-200/11 AND10140-4006 10081
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
May 2023
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BEAM,STRUCTURAL https A structural shape fabricated from a ferrous or nonferrous AMS-QQ-A-200/11
Quotation QQA200-11 BEAM,STRUCTURAL 603 EA NS Request Quotation AMS-QQ-A-200/11 BEAM,STRUCTURAL https
Quotation AMS-QQ-A-200/11 ANGLE,STRUCTURAL 3 EA NS Request Quotation QQA200-11 ANGLE,STRUCTURAL
BEAM,STRUCTURAL 3 EA NS Request Quotation AMS-QQ-A-200/11 ANGLE,STRUCTURAL 3 EA NS Request Quotation
BEAM,STRUCTURAL 3 EA NS Request Quotation AMS-QQ-A-200/11 ANGLE,STRUCTURAL 3 EA NS Request Quotation
Quotation AMS-QQ-A-200/11 ANGLE,STRUCTURAL 3 EA NS Request Quotation QQA200-11 ANGLE,STRUCTURAL
QQA200-11 ANGLE,STRUCTURAL BEAM,STRUCTURAL 3 EA NS Request Quotation AMS-QQ-A-200/11 ANGLE,STRUCTURAL
Quotation AMS-QQ-A-200/11 ANGLE,STRUCTURAL 3 EA NS Request Quotation QQA200-11 ANGLE,STRUCTURAL
QQA200-11 ANGLE,STRUCTURAL BEAM,STRUCTURAL 3 EA NS Request Quotation AMS-QQ-A-200/11 ANGLE,STRUCTURAL
Quotation AMS-QQ-A-200/11 ANGLE,STRUCTURAL 3 EA NS Request Quotation QQA200-11 ANGLE,STRUCTURAL
Restrictions 9540-00-241-2712
9540-00-241-2712 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 9540-00-241-2712
- US Air Force (FGGI)
- Effective Date:
- 1 Mar 2006
- Former MOE Rule:
- FGKZ
- US Navy (N9BZ)
- Effective Date:
- 1 Mar 2006
- Supplementary Collaborators:
- GTKE
Approved Sources 9540-00-241-2712
- Part Number
- Manufacturer
- Status
- AMS-QQ-A-200/11
- Manufacturer
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- H199
- 10383 - Kaiser Aluminum And Chemical Corp (Active)
- Incomplete Reference
- Incomplete Reference
- AMS10134-3002
- 0U583 - Sae International (Active)
- Primary Buy
- Primary Buy
- 35302
- 01634 - Aluminum Co Of America (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- QQ-A-200/11
- 81348 - Federal Specifications (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- AND10140-4006
- 99237 - Airforce-Navy Aeronautical Design (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- 10081
- 01484 - Reynolds Metals Co (Obsolete)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQ-A-200/11
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS10134-3002
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 9540-00-241-2712
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- I Shape
- Bottom Flange Width [BQJH]
- 3.500 Inches Nominal
- Fabrication Method [AARN]
- Extruded
- Fillet Radius Where Bottom Left Flange Joins Web Flange/Leg [BPXK]
- 0.188 Inches Nominal
- Fillet Radius Where Bottom Right Flange Joins Web Flange/Leg [BPXM]
- 0.188 Inches Nominal
- Fillet Radius Where Top Left Flange Joins Web Flange/Leg [BPXJ]
- 0.188 Inches Nominal
- Fillet Radius Where Top Right Flange Joins Web Flange/Leg [BPXL]
- 0.188 Inches Nominal
- First Tip Radius [AJJB]
- 0.250 Inches Nominal
- First Tip Style [CMZY]
- Lower Radius
- Fourth Tip Relationship To Preceding Tips [CNQN]
- Identical W/Third Tip
- Heat Treatment [HEAT]
- T-6 Solution Heat Treated
- Material [MATT]
- Aluminum Alloy Ams-Qq-A-200/11, Alloy 7075
- Nondefinitive Spec/Std Data [ZZZT]
- T-6 Temper
- Left Side Bottom Flange Distance To Center Of Both Flanges [BPXF]
- 1.750 Inches Nominal
- Left Side Bottom Flange Thickness [BMPR]
- 0.250 Inches Nominal
- Left Side Top Flange Distance To Center Of Both Flanges [BPXD]
- 1.750 Inches Nominal
- Left Side Top Flange Thickness [ADXR]
- 0.250 Inches Nominal
- Left Top Inside Angle [CSMZ]
- 90.0 Degrees Nominal
- Left Bottom Inside Angle [CTBR]
- 90.0 Degrees Nominal
- Length [ABRY]
- 10.000 Feet Minimum And 12.000 Feet Maximum
- Right Side Bottom Flange Distance To Center Of Both Flanges [BPXH]
- 1.750 Inches Nominal
- Right Side Bottom Flange Thickness [BMPQ]
- 0.250 Inches Nominal
- Right Side Top Flange Distance To Center Of Both Flanges [BPXG]
- 1.750 Inches Nominal
- Right Side Top Flange Thickness [ADXS]
- 0.250 Inches Nominal
- Right Top Inside Angle [CRZC]
- 90.0 Degrees Nominal
- Right Bottom Inside Angle [CWKK]
- 90.0 Degrees Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 4.000 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 3.120 Pounds Per Linear Foot
- Web Flange Thickness [BPXN]
- 0.250 Inches Nominal
- Third Tip Radius [CNBB]
- 0.250 Inches Nominal
- Third Tip Relationship To Preceding Tips [CNQL]
- Not Identical
- Third Tip Style [CNQM]
- Upper Radius
- Top Flange Width [BQJG]
- 3.500 Inches Nominal
DLA Procurement Analysis 9540-00-241-2712
Management Data 9540-00-241-2712
Air Force
- Fund:
- SF
- Stock fund applicable to items managed for the Air Force by the respective Inventory Control Point
- Budget:
- 9
- 57X4921.070 - General Support DIV - Air Force decentralized managed expense items (ERRC XB3, XF3) with a unit cost of less than $250,000 that are requisitioned/procured at base (retail) level from DLA, GSA, Army, Navy, Depot Maintenance Service, Air Force Industrial Fund (AFMC), local manufacture and commercial vendors
- Price Validation Code:
- V
- The current standard price has been validated.
The item has been analyzed in conjunction with the Zero Overpricing Program and is in the accepted price range.
The item was procured under open competition and under the competitive arena the price is considered fair and reasonable.
ZOP or Standard price challenges are permissible but must be supported by adequate justification.
- Expendability
Recoverability
Repairability: - N
- Expendable. Condemn at User. Stock Fund (except Munitions).
Navy
- Cognizance:
- 9B
- Navy-owned stocks of DLA material
Naval Inventory Control Point, Mechanicsburg
NATO Stock Numbers Related to 9540-00-241-2712
Freight Information 9540-00-241-2712
9540-00-241-2712 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. 9540-00-241-2712 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. 9540-00-241-2712 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. 9540-00-241-2712 is not classified as a special type of cargo when transported by water. 9540-00-241-2712 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 9540-00-241-2712
- 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 9540-00-241-2712 1 Records
Contracting Technical Data File (CTDF) 9540-00-241-2712 October 2021
Criticality and Quality
- Critical Item Code:
- X
- 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:
- N
- Special Packaging Instruction Number (SPIN):
- Special Packaging Instruction Number Revision:
- Special Packaging Instruction Number Date:
- Pallet Reference Number Required: