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9540-00-261-5145
Structural Beam
9540002615145 002615145 AMS-QQ-A-200/3 AMS-STD-184 HT197 5779 AND10136-2006 FS50104-2012-2 40176 QQ-A-200/3
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
November 2023
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-40176/NCOP-40176 Managed by ,COP-40176/N ,COP-40176/ N ,COP-40176/NCOP -40176/NCOP-40176 Managed by
Restrictions 9540-00-261-5145
9540-00-261-5145 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.
Import and Export 9540-00-261-5145
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 9540-00-261-5145
- US Air Force (FGGI)
- Effective Date:
- 1 Mar 2006
- Former MOE Rule:
- FGKZ
- Brazil (YA01)
- Effective Date:
- 1 Aug 2000
- Republic of Korea (ZH01)
- Effective Date:
- 1 Apr 1991
Approved Sources 9540-00-261-5145
- Part Number
- Manufacturer
- Status
- AMS-QQ-A-200/3
- Manufacturer
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- AMS-STD-184
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- HT197
- 10383 - Kaiser Aluminum And Chemical Corp (Active)
- Incomplete Reference
- Incomplete Reference
- 5779
- 01484 - Reynolds Metals Co (Obsolete)
- Incomplete Reference
- Incomplete Reference
- AND10136-2006
- 99237 - Airforce-Navy Aeronautical Design (Active)
- Incomplete Standard
- Incomplete Standard
- FS50104-2012-2
- 89446 - Hiller Aircraft Corporation (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- AMS-QQ-A-200/3
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-STD-184
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- 40176
- 99267 - Bohn Aluminum And Brass Co Div Of (Obsolete)
- Canceled/Obsolete
- Canceled/Obsolete
- QQ-A-200/3
- 81348 - Federal Specifications Promulgated (Active)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 9540-00-261-5145
- 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]
- 0.125 Inches Nominal
- First Tip Style [CMZY]
- Lower Radius
- Heat Treatment [HEAT]
- T-3511 Solution Heat Treated
- Material [MATT]
- Aluminum Alloy Ams-Qq-A-200/3, Alloy 2024
- Nondefinitive Spec/Std Data [ZZZT]
- T3511 Temper
- Left Side Top Flange Distance To Center Of Both Flanges [BPXD]
- 1.000 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 Side Top Flange Distance To Center Of Both Flanges [BPXG]
- 1.000 Inches Nominal
- Right Side Top Flange Thickness [ADXS]
- 0.125 Inches Nominal
- Right Top Inside Angle [CRZC]
- 90.0 Degrees Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 1.250 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 0.470 Pounds Per Linear Foot
- Third Tip Relationship To Preceding Tips [CNQL]
- Not Identical
- Third Tip Style [CNQM]
- Full Radius
- Third Tip Radius [CNBB]
- 0.062 Inches Nominal
- Top Flange Width [BQJG]
- 2.000 Inches Nominal
Weapon Systems (WSDC) 9540-00-261-5145
DLA Procurement Analysis 9540-00-261-5145
- Last Stock Position:
- 124 In Stock
- DLA Administrative Lead Time:
- Subscribe
- DLA Production Lead Time:
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Management Data 9540-00-261-5145
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Freight Information 9540-00-261-5145
9540-00-261-5145 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. 9540-00-261-5145 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. 9540-00-261-5145 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. 9540-00-261-5145 is not classified as a special type of cargo when transported by water. 9540-00-261-5145 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 9540-00-261-5145
- 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) 9540-00-261-5145 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):
- L
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: