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9540-01-086-1811
Structural Beam
9540010861811 010861811 10138-0403 50358 AND10138-0403 AMS-QQ-A-200/3 K50A4O MS14389E009 QQ-A-200/3 9540PL1013478
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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Structural Beam 9540010861811 010861811 AMS-QQ-A-200/3 K50A4O MS14389E009 QQ-A-200/3 9540PL1013478
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https - AMS-QQ-A -200/3 https AND10137-1604 AND10137 A structural - AMS-QQ-A-200/3 https AND10137
Restrictions 9540-01-086-1811
9540-01-086-1811 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 9540-01-086-1811
- US Air Force (FGGI)
- Effective Date:
- 1 Mar 2006
- Former MOE Rule:
- FGKZ
- Poland (WP01)
- Effective Date:
- 1 Apr 2011
- Brazil (YA01)
- Effective Date:
- 1 Oct 2000
- Singapore (YJ01)
- Effective Date:
- 1 Apr 1991
- Greece (ZU01)
- Effective Date:
- 1 Jan 2007
Approved Sources 9540-01-086-1811
- Part Number
- Manufacturer
- Status
- MS14389E009
- Manufacturer
- 96906 - Military Standards (Active)
- Definitive Standard
- Definitive Standard
- 10138-0403
- 29321 - Transtar Metals Corp (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- 50358
- 55088 - Pimalco Inc. (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- AND10138-0403
- 99237 - Airforce-Navy Aeronautical Design (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- AMS-QQ-A-200/3
- 0U583 - Sae International (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- K50A4O
- 81755 - Lockheed Martin Corporation (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- AMS-QQ-A-200/3
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- QQ-A-200/3
- 81348 - Federal Specifications Promulgated (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- 9540PL1013478
- 9009H - Jednolity Indeks Materialowy - (Active)
- NATO Reference
- NATO Reference
Datasheet 9540-01-086-1811
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- Z Shape
- Bottom Flange Width [BQJH]
- 0.750 Inches Nominal
- Fabrication Method [AARN]
- Extruded
- Fillet Radius Where Bottom Right Flange Joins Web Flange/Leg [BPXM]
- 0.094 Inches Nominal
- Fillet Radius Where Top Left Flange Joins Web Flange/Leg [BPXJ]
- 0.094 Inches Nominal
- First Tip Radius [AJJB]
- 0.050 Inches Nominal
- First Tip Style [CMZY]
- Lower Radius
- Heat Treatment [HEAT]
- O-Annealed
- Material [MATT]
- Aluminum Alloy Ams-Qq-A-200/3, Alloy 2024
- Nondefinitive Spec/Std Data [ZZZT]
- O Temper
- Left Side Top Flange Thickness [ADXR]
- 0.050 Inches Nominal
- Left Top Inside Angle [CSMZ]
- 90.0 Degrees Nominal
- Length [ABRY]
- 10.000 Feet Minimum And 12.000 Feet Maximum
- Right Bottom Inside Angle [CWKK]
- 90.0 Degrees Nominal
- Right Side Bottom Flange Thickness [BMPQ]
- 0.050 Inches Nominal
- Second Tip Radius [CMZZ]
- 0.050 Inches Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Not Identical
- Second Tip Style [CNQK]
- Upper Radius
- Overall Height [ABKW]
- 0.500 Inches Nominal
- Top Flange Width [BQJG]
- 0.750 Inches Nominal
- Web Flange Thickness [BPXN]
- 0.050 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 0.118 Pounds Per Linear Foot
DLA Procurement Analysis 9540-01-086-1811
Management Data 9540-01-086-1811
Similar Supply Items to 9540-01-086-1811
Freight Information 9540-01-086-1811
9540-01-086-1811 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. 9540-01-086-1811 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. 9540-01-086-1811 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. 9540-01-086-1811 is not classified as a special type of cargo when transported by water. 9540-01-086-1811 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 9540-01-086-1811
- 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) 9540-01-086-1811 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:
- N
- Special Packaging Instruction Number (SPIN):
- Special Packaging Instruction Number Revision:
- Special Packaging Instruction Number Date:
- Pallet Reference Number Required: