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9540-01-118-2584
Structural Beam
9540011182584 011182584 AMS-QQ-A-200/15 10136-2406 AND10136-2406/QQ-A-200/15-T76511 CVC10010-552CJ 1MA160D06-10113 QQ-A-200/15
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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Related Documents 9540-01-118-2584 5+ Documents (More...)
AMS-QQ-A-200/15 BEAM,STRUCTURAL 41 FT NS Request Quotation QQ-A-200/15 BEAM,STRUCTURAL 6 FT NS Request
Quotation QQ-A-200/15 BEAM,STRUCTURAL 6 FT NS Request BEAM AMS-QQ-A -200 /fsc- AMS-QQ-A - /fsc- AMS-QQ-A
QQ-A- 200/15 BEAM,STRUCTURAL 6 FT NS Request BEAM AMS-QQ-A -200/ 15 BEAM AMS-QQ-A https//www.nsnlookup.com
/fsg-95/fsc-9540/us 9540-01-118-2584 Structural Beam 9540011182584 011182584 AMS-QQ-A-200/15 BEAM,STRUCTURAL
ANGLE,STRUCTURAL 6 FT NS Request Quotation AMS-QQ-A-200/15 ANGLE,STRUCTURAL 41 FT NS Request ANGLE
6 FT NS Request Quotation AMS-QQ-A-200/15 ANGLE,STRUCTURAL 41 FT NS Request ANGLE,STRUCTURAL 6 FT NS
ANGLE,STRUCTURAL 6 EA NS Request Quotation AMS-QQ-A-200/15 ANGLE,STRUCTURAL 41 EA NS Request ANGLE
,STRUCTURAL 6 EA NS Request Quotation AMS-QQ-A-200/15 ANGLE,STRUCTURAL 41 EA NS Request ANGLE https//
BEAM,STRUCTURAL 6 EA NS Request Quotation AMS-QQ-A-200/15 BEAM,STRUCTURAL 41 EA NS Request ANGLE,
6 EA NS Request Quotation AMS-QQ-A-200/15 ANGLE,STRUCTURAL 41 EA NS Request ANGLE,STRUCTURAL 6 EA NS
Restrictions 9540-01-118-2584
9540-01-118-2584 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 9540-01-118-2584
- US Air Force (FNN5)
- Effective Date:
- 1 May 2003
- Former MOE Rule:
- FGKZ
Approved Sources 9540-01-118-2584
- Part Number
- Manufacturer
- Status
- AMS-QQ-A-200/15
- Manufacturer
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- 10136-2406
- 29321 - Transtar Metals Corp (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- AND10136-2406/QQ-A-200/15-T76511
- 14153 - Defense Logistics Agency (Active)
- Secondary Buy
- Secondary Buy
- CVC10010-552CJ
- 80378 - Triumph Aerostructures, Llc (Active)
- Secondary Buy
- Secondary Buy
- 1MA160D06-10113
- 76301 - The Boeing Company (Active)
- Secondary Buy
- Secondary Buy
- AMS-QQ-A-200/15
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- QQ-A-200/15
- 81348 - Federal Specifications Promulgated (Active)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 9540-01-118-2584
- 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]
- 0.125 Inches Nominal
- Fillet Radius Where Top Right Flange Joins Web Flange/Leg [BPXL]
- 0.125 Inches Nominal
- First Tip Radius [AJJB]
- 0.156 Inches Nominal
- First Tip Style [CMZY]
- Lower Radius
- Heat Treatment [HEAT]
- T-76511 Solution Heat Treated
- Material [MATT]
- Aluminum Alloy Ams-Qq-A-200/15, Alloy 7075
- Nondefinitive Spec/Std Data [ZZZT]
- T6511 Temper
- Left Side Top Flange Distance To Center Of Both Flanges [BPXD]
- 1.250 Inches Nominal
- Left Side Top Flange Thickness [ADXR]
- 0.156 Inches Nominal
- Left Top Inside Angle [CSMZ]
- 90.0 Degrees Nominal
- Leg Thickness [AJJP]
- 0.156 Inches Nominal
- Length [ABRY]
- 10.000 Feet Minimum And 12.000 Feet Maximum
- Right Top Inside Angle [CRZC]
- 90.0 Degrees Nominal
- Right Side Top Flange Distance To Center Of Both Flanges [BPXG]
- 1.250 Inches Nominal
- Right Side Top Flange Thickness [ADXS]
- 0.156 Inches Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 1.625 Inches Nominal
- Top Flange Width [BQJG]
- 2.500 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 0.743 Pounds Per Linear Foot
- Specification/Standard Data [ZZZK]
- 76301-1Ma160 Manufacturers Standard
- Third Tip Radius [CNBB]
- 0.078 Inches Nominal
- Third Tip Relationship To Preceding Tips [CNQL]
- Not Identical
- Third Tip Style [CNQM]
- Full Radius
DLA Procurement Analysis 9540-01-118-2584
Management Data 9540-01-118-2584
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:
- E
- The current standard price is an estimated price.
Estimated Price challenges are allowed but follow procedures in para 60.b. (3) of section L of this manual.
This code will be changed to a P code upon notification of a contract price or this code will be changed to an updated code upon determination of a valid price.
- Expendability
Recoverability
Repairability: - N
- Expendable. Condemn at User. Stock Fund (except Munitions).
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Freight Information 9540-01-118-2584
9540-01-118-2584 has freight characteristics managed by the Southwestern Power Administration.. 9540-01-118-2584 has a variance between NMFC and UFC when transported by rail and the description should be consulted.
Packaging Data 9540-01-118-2584
- 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) 9540-01-118-2584 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: