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9540-01-232-7034
Structural Beam
9540012327034 012327034 SS1513-4
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 9540-01-232-7034
9540-01-232-7034 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 9540-01-232-7034
- US Navy (N9BZ)
- Effective Date:
- 1 Mar 2006
- Former MOE Rule:
- N9ZD
- Supplementary Collaborators:
- KE
- Germany (ZG01)
- Effective Date:
- 1 Apr 1991
Approved Sources 9540-01-232-7034
- Part Number
- Manufacturer
- Status
- SS1513-4
- Manufacturer
- 78286 - Sikorsky Aircraft Corporation (Active)
- Primary Buy
- Primary Buy
Datasheet 9540-01-232-7034
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- Z Shape
- Bottom Flange Width [BQJH]
- 0.880 Inches Nominal
- Fabrication Method [AARN]
- Extruded
- Fillet Radius Where Bottom Right Flange Joins Web Flange/Leg [BPXM]
- 0.125 Inches Nominal
- Fillet Radius Where Top Left Flange Joins Web Flange/Leg [BPXJ]
- 0.125 Inches Nominal
- First Tip Style [CMZY]
- Square End
- Material [MATT]
- Aluminum Alloy, Ams-Qq-A-250/13, Alclad 7075
- Left Side Top Flange Thickness [ADXR]
- 0.063 Inches Nominal
- Left Top Inside Angle [CSMZ]
- 90.0 Degrees Nominal
- Right Side Bottom Flange Thickness [BMPQ]
- 0.063 Inches Nominal
- Right Bottom Inside Angle [CWKK]
- 90.0 Degrees Nominal
- Second Tip Inner Corner Radius [CNNP]
- 0.125 Inches Nominal
- Second Tip Flange Height [CNPZ]
- 0.250 Inches Nominal
- Second Tip Style [CNQK]
- Flange Right Upward With Square End And Inner And Outer Corner Radii
- Second Tip Relationship To First Tip [CNQJ]
- Not Identical
- Second Tip Thickness [CNPT]
- 0.063 Inches Nominal
- Overall Height [ABKW]
- 1.000 Inches Nominal
- Top Flange Width [BQJG]
- 0.750 Inches Nominal
- Web Flange Thickness [BPXN]
- 0.063 Inches Nominal
DLA Procurement Analysis 9540-01-232-7034
Management Data 9540-01-232-7034
Navy
- Cognizance:
- 9B
- Navy-owned stocks of DLA material
Naval Inventory Control Point, Mechanicsburg
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Freight Information 9540-01-232-7034
9540-01-232-7034 has freight characteristics managed by Germany.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. 9540-01-232-7034 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. 9540-01-232-7034 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. 9540-01-232-7034 is not classified as a special type of cargo when transported by water. 9540-01-232-7034 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 9540-01-232-7034
- 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
- Special requirements
- --
Intermediate Pack Level
- Quantity of Unit Packs
- Container
- --
- No Requirement
Contracting Technical Data File (CTDF) 9540-01-232-7034 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):
- F
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: