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9540-00-512-6532
Structural Beam
9540005126532 005126532 AMS-QQ-A-200/11 1MA160D05-10189 PA18353 QQ-A-200/11 10164558
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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May 2023
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Related Documents 9540-00-512-6532 5+ Documents (More...)
- - AMS-QQ-A-200/11 - - -200 - - AMS-QQ-A-200/11 - - AMS-QQ-A-200/11 - - https//www.nsnlookup.com /fsg
Beam 9540005126532005126532 - - AMS-QQ-A-200/11 - - AMS-QQ-A-200 /11 - - AMS-QQ-A -200/11 - - - - AMS-QQ-A
/fsg-95/fsc-9540/us 9540-00-512-6532 Structural Beam 9540005126532 005126532 - - -200 - - AMS-QQ-A-200
AMS-QQ-A-200/11 - - -200 - - AMS-QQ-A-200/11 - - AMS-QQ-A-200/11 - - BEAM 200 AMS-QQ-A -200/ / 11 - -
- - 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 - -
- - AMS-QQ-A-200/11 - // AMS-QQ-A AMS-QQ-A-200 / /11 - - AMS-QQ-A A https AMS-QQ-A-200 /11 BEAM
200 AMS-QQ-A-200 / /11 - - AMS-QQ-A-200/11 - // AMS-QQ-A -200 /11 A https AMS-QQ-A-200 /11 BEAM 200 AMS-QQ-A
- - AMS-QQ-A-200/11 /11 AMS-QQ-A -200/ 11 - - AMS-QQ-A -200 /11 /fsg-95 /11 AMS-QQ-A -200/11 - - AMS-QQ-A
BEAM 200 AMS-QQ-A-200/ / 11 - - AMS-QQ-A-200 /11 /11 // // AMS-QQ-A AMS-QQ-A-200 11 - - AMS-QQ-A
Restrictions 9540-00-512-6532
9540-00-512-6532 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 9540-00-512-6532
- US Air Force (FGGI)
- Effective Date:
- 1 Mar 2006
- US Navy (N9BZ)
- Effective Date:
- 1 Mar 2006
- Supplementary Collaborators:
- KE
- Finland (WF)
- Finland (WF01)
- Effective Date:
- 1 Jul 2009
- Spain (YB)
- Spain (YB01)
- Effective Date:
- 1 Apr 1991
- Canada (ZC)
- Canada (ZC01)
- Effective Date:
- 1 Apr 1991
- United States of America (ZZ)
Approved Sources 9540-00-512-6532
- Part Number
- Manufacturer
- Status
- AMS-QQ-A-200/11
- Manufacturer
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- 1MA160D05-10189
- 76301 - The Boeing Company (Active)
- Incomplete Reference
- Incomplete Reference
- PA18353
- 06012 - Transtar Metals Corp (Obsolete)
- Canceled/Obsolete
- Canceled/Obsolete
- QQ-A-200/11
- 81348 - Federal Specifications Promulgated (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQ-A-200/11
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- 10164558
- A486G - Nimikkeistokeskus Ncb Finland (Active)
- NATO Reference
- NATO Reference
Datasheet 9540-00-512-6532
- 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]
- 0.050 Inches Nominal
- First Tip Style [CMZY]
- Lower Radius
- Heat Treatment [HEAT]
- T-73511 Solution Heat Treated
- Material [MATT]
- Aluminum Alloy Ams-Qq-A-200/11, Alloy 7075
- Nondefinitive Spec/Std Data [ZZZT]
- T73511 Temper
- Left Side Top Flange Distance To Center Of Both Flanges [BPXD]
- 1.025 Inches Nominal
- Left Side Top Flange Thickness [ADXR]
- 0.050 Inches Nominal
- Left Top Inside Angle [CSMZ]
- 90.0 Degrees Nominal
- Leg Thickness [AJJP]
- 0.050 Inches Nominal
- Length [ABRY]
- 10.000 Feet Minimum And 12.000 Feet Maximum
- Right Side Top Flange Distance To Center Of Both Flanges [BPXG]
- 1.025 Inches Nominal
- Right Side Top Flange Thickness [ADXS]
- 0.050 Inches Nominal
- Right Top Inside Angle [CRZC]
- 90.0 Degrees Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 0.750 Inches Nominal
- Top Flange Width [BQJG]
- 2.050 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 0.166 Pounds Per Linear Foot
- Third Tip Style [CNQM]
- Square End
- Third Tip Relationship To Preceding Tips [CNQL]
- Not Identical
Weapon Systems (WSDC) 9540-00-512-6532
DLA Procurement Analysis 9540-00-512-6532
Management Data 9540-00-512-6532
Navy
- Cognizance:
- 9B
- Navy-owned stocks of DLA material
Naval Inventory Control Point, Mechanicsburg
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Freight Information 9540-00-512-6532
9540-00-512-6532 has freight characteristics managed by the Southwestern Power Administration.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. 9540-00-512-6532 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. 9540-00-512-6532 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. 9540-00-512-6532 is not classified as a special type of cargo when transported by water. 9540-00-512-6532 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.
Contracting Technical Data File (CTDF) 9540-00-512-6532 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):
- T
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: