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9540-01-189-8617
Structural Beam
9540011898617 011898617 51066 AMS-QQ-A-200/11 16102 1MA160D05-10322 60-339 89615-2350 PA1382 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
May 2023
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/11 A structural shape AMS-QQ-A-200/ / 11 - - /11 AMS-QQ-A-200/11 - - AMS-QQ-A -200 /11 BEAM 200 AMS-QQ-A
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Structural Beam 9540011898617 011898617,51066 Upgrade 9540-01-189-8617Structural Beam9540011898617
011898617 51066 16102 1MA160D05-10322 60-339 89615 Plain Stud 5307015313479 015313479,89615 Textile
- - 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
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- - 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 9540-01-189-8617
9540-01-189-8617 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 9540-01-189-8617
- US Navy (N9BZ)
- Effective Date:
- 1 Mar 2006
- Former MOE Rule:
- N9ZD
- Supplementary Collaborators:
- KE
- Canada (ZC01)
- Effective Date:
- 1 Apr 1991
Approved Sources 9540-01-189-8617
- Part Number
- Manufacturer
- Status
- 51066
- Manufacturer
- 26510 - Sterling Tool Inc (Obsolete)
- Incomplete Reference
- Incomplete Reference
- AMS-QQ-A-200/11
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- 16102
- 77783 - Alcoa/Reynolds Metals Company (Active)
- Incomplete Reference
- Incomplete Reference
- 1MA160D05-10322
- 76301 - The Boeing Company (Active)
- Incomplete Reference
- Incomplete Reference
- 60-339
- 29321 - Transtar Metals Corp (Active)
- Incomplete Reference
- Incomplete Reference
- 89615-2350
- 50200 - Litton Industries Inc Reed Rolled (Obsolete)
- Canceled/Obsolete
- Canceled/Obsolete
- PA1382
- 06012 - Transtar Metals Corp (Obsolete)
- Canceled/Obsolete
- Canceled/Obsolete
- 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 9540-01-189-8617
- 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]
- 0.188 Inches Nominal
- Fillet Radius Where Top Right Flange Joins Web Flange/Leg [BPXL]
- 0.188 Inches Nominal
- First Tip Inner Radius [CNBD]
- 0.031 Inches Nominal
- First Tip Outer Radius [CNBJ]
- 0.031 Inches Nominal
- First Tip Style [CMZY]
- Square W/ Inner And Outer Corner Radii
- 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]
- 1.734 Inches Nominal
- Left Side Top Flange Thickness [ADXR]
- 0.125 Inches Nominal
- Left Top Inside Angle [CSMZ]
- 90.0 Degrees Nominal
- Leg Thickness [AJJP]
- 0.125 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]
- 1.734 Inches Nominal
- Right Side Top Flange Thickness [ADXS]
- 0.125 Inches Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 1.750 Inches Nominal
- Top Flange Width [BQJG]
- 3.625 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 0.804 Pounds Per Linear Foot
- Third Tip Relationship To Preceding Tips [CNQL]
- Identical W/First Tip
DLA Procurement Analysis 9540-01-189-8617
Management Data 9540-01-189-8617
Navy
- Cognizance:
- 9B
- Navy-owned stocks of DLA material
Naval Inventory Control Point, Mechanicsburg
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Freight Information 9540-01-189-8617
9540-01-189-8617 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. 9540-01-189-8617 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. 9540-01-189-8617 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. 9540-01-189-8617 is not classified as a special type of cargo when transported by water. 9540-01-189-8617 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 9540-01-189-8617
- 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
Contracting Technical Data File (CTDF) 9540-01-189-8617 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):
- 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: