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9540-01-071-0123
Structural Beam
9540010710123 010710123 K40A12T3511 60-3129 5781 24826 AMS-QQ-A-200/3 MS14375E027 QQ-A-200/3 9540PL0900346
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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Restrictions 9540-01-071-0123
9540-01-071-0123 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 9540-01-071-0123
- US Air Force (FGGI)
- Effective Date:
- 1 Mar 2006
- Former MOE Rule:
- FGKZ
- US Navy (N9BZ)
- Effective Date:
- 1 Jan 2014
- Supplementary Collaborators:
- GG
- Poland (WP01)
- Effective Date:
- 1 Jan 2007
- Brazil (YA01)
- Effective Date:
- 1 Oct 2000
- Singapore (YJ01)
- Effective Date:
- 1 Oct 1993
- Italy (ZR01)
- Effective Date:
- 1 Dec 2007
- Greece (ZU01)
- Effective Date:
- 1 Jan 2007
Approved Sources 9540-01-071-0123
- Part Number
- Manufacturer
- Status
- MS14375E027
- Manufacturer
- 96906 - Military Standards (Active)
- Definitive Standard
- Definitive Standard
- K40A12T3511
- 81755 - Lockheed Martin Corporation (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- 60-3129
- 29321 - Transtar Metals Corp (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- 5781
- 77783 - Alcoa/Reynolds Metals Company (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- 24826
- 01634 - Aluminum Co Of America (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- AMS-QQ-A-200/3
- 0U583 - Sae International (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
- 9540PL0900346
- 9009H - Jednolity Indeks Materialowy - (Active)
- NATO Reference
- NATO Reference
Datasheet 9540-01-071-0123
- 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]
- 0.062 Inches Nominal
- Fillet Radius Where Top Right Flange Joins Web Flange/Leg [BPXL]
- 0.062 Inches Nominal
- First Tip Style [CMZY]
- Square End
- 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]
- 0.750 Inches Nominal
- Left Side Top Flange Thickness [ADXR]
- 0.062 Inches Nominal
- Left Top Inside Angle [CSMZ]
- 90.0 Degrees Nominal
- Leg Thickness [AJJP]
- 0.062 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]
- 0.750 Inches Nominal
- Right Side Top Flange Thickness [ADXS]
- 0.062 Inches Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 1.250 Inches Nominal
- Top Flange Width [BQJG]
- 1.500 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 0.205 Pounds Per Linear Foot
- Specification/Standard Data [ZZZK]
- 81755-K40 Manufacturers Standard
- Third Tip Relationship To Preceding Tips [CNQL]
- Identical W/First Tip
Weapon Systems (WSDC) 9540-01-071-0123
DLA Procurement Analysis 9540-01-071-0123
- Last Stock Position:
- 341 In Stock
- DLA Administrative Lead Time:
- Subscribe
- DLA Production Lead Time:
- Subscribe
Management Data 9540-01-071-0123
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Oct 2022
- Department of the Air Force (DF)
- FT
- Subscribe
- 1
- FT
- Jan 2022
- Department of the Air Force (DF)
- FT
- Subscribe
- 1
- FT
- Oct 2021
- Department of the Air Force (DF)
- FT
- Subscribe
- 1
- FT
- Oct 2020
- Department of the Air Force (DF)
- FT
- Subscribe
- 1
- FT
- Oct 2019
- Department of the Air Force (DF)
- FT
- Subscribe
- FT
Navy
- Cognizance:
- 9B
- Navy-owned stocks of DLA material
Naval Inventory Control Point, Mechanicsburg
Similar Supply Items to 9540-01-071-0123
Freight Information 9540-01-071-0123
9540-01-071-0123 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. 9540-01-071-0123 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. 9540-01-071-0123 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. 9540-01-071-0123 is not classified as a special type of cargo when transported by water. 9540-01-071-0123 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 9540-01-071-0123
- 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) 9540-01-071-0123 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: