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9540-01-435-5245
Structural Beam
9540014355245 014355245 MIL-T-81556 CVC10010-1025GA CVC10010-1025GAX144
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
Managed by United States
NSN Created on 27 Aug 1996
Data Last Changed
May 2023
May 2023
NATO Update Count
6
6
NATO Data Quality
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Restrictions 9540-01-435-5245
9540-01-435-5245 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 9540-01-435-5245
- US Air Force (FNN5)
- Effective Date:
- 1 Jun 2003
- Former MOE Rule:
- FGKZ
Approved Sources 9540-01-435-5245
- Part Number
- Manufacturer
- Status
- CVC10010-1025GA
- Manufacturer
- 80378 - Triumph Aerostructures, Llc (Active)
- Primary Buy
- Primary Buy
- MIL-T-81556
- 81349 - Military Specifications (Active)
- Incomplete Standard
- Incomplete Standard
- CVC10010-1025GAX144
- 14153 - Defense Logistics Agency (Active)
- Secondary Buy
- Secondary Buy
Datasheet 9540-01-435-5245
- 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]
- 0.250 Inches Nominal
- Fillet Radius Where Top Right Flange Joins Web Flange/Leg [BPXL]
- 0.250 Inches Nominal
- First Tip Inner Radius [CNBD]
- 0.125 Inches Nominal
- First Tip Outer Radius [CNBJ]
- 0.125 Inches Nominal
- First Tip Style [CMZY]
- Square W/ Inner And Outer Corner Radii
- Heat Treatment [HEAT]
- Annealed
- Material [MATT]
- Titanium Alloy, Mil-T-81556, Comp Ab-1
- Nondefinitive Spec/Std Data [ZZZT]
- Composition Ab-1 And Condition Annealed
- Left Side Top Flange Distance To Center Of Both Flanges [BPXD]
- 6.000 Inches Nominal
- Left Side Top Flange Thickness [ADXR]
- 2.320 Inches Nominal
- Left Top Inside Angle [CSMZ]
- 90.0 Degrees Nominal
- Leg Thickness [AJJP]
- 1.000 Inches Nominal
- Length [ABRY]
- 12.000 Feet Nominal
- Right Side Top Flange Distance To Center Of Both Flanges [BPXG]
- 6.000 Inches Nominal
- Right Side Top Flange Thickness [ADXS]
- 2.320 Inches Nominal
- Right Top Inside Angle [CRZC]
- 90.0 Degrees Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 5.600 Inches Nominal
- Top Flange Width [BQJG]
- 12.000 Inches Nominal
- Third Tip Relationship To Preceding Tips [CNQL]
- Identical W/First Tip
DLA Procurement Analysis 9540-01-435-5245
Management Data 9540-01-435-5245
Air Force
- Fund:
- SF
- Stock fund applicable to items managed for the Air Force by the respective Inventory Control Point
- Budget:
- 9
- 57X4921.070 - General Support DIV - Air Force decentralized managed expense items (ERRC XB3, XF3) with a unit cost of less than $250,000 that are requisitioned/procured at base (retail) level from DLA, GSA, Army, Navy, Depot Maintenance Service, Air Force Industrial Fund (AFMC), local manufacture and commercial vendors
- Price Validation Code:
- E
- The current standard price is an estimated price.
Estimated Price challenges are allowed but follow procedures in para 60.b. (3) of section L of this manual.
This code will be changed to a P code upon notification of a contract price or this code will be changed to an updated code upon determination of a valid price.
- Expendability
Recoverability
Repairability: - N
- Expendable. Condemn at User. Stock Fund (except Munitions).
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Freight Information 9540-01-435-5245
9540-01-435-5245 has freight characteristics.. 9540-01-435-5245 has a variance between NMFC and UFC when transported by rail and the description should be consulted.
Contracting Technical Data File (CTDF) 9540-01-435-5245 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:
- Y
- Special Packaging Instruction Number (SPIN):
- Special Packaging Instruction Number Revision:
- Special Packaging Instruction Number Date:
- Pallet Reference Number Required: