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9540-01-469-3308
Structural Beam
9540014693308 014693308 CVC10010-161GA
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
June 2023
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Restrictions 9540-01-469-3308
9540-01-469-3308 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 has been confirmed as a Critical Munitions List Item or a Sensitive Commerce Control List Item and cannot be in the possession of any party anywhere in the World who is not an authorized NATO Government. Any other possessor of this item should mutilate it now as possession violates international and local laws. This item is a US Munitions List Item and must be mutilated to scrap. This item is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 9540-01-469-3308
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 9540-01-469-3308
- US Air Force (FNN5)
- Effective Date:
- 1 Jun 2003
- Former MOE Rule:
- FGKZ
Approved Sources 9540-01-469-3308
- Part Number
- Manufacturer
- Status
- CVC10010-161GA
- Manufacturer
- 80378 - Triumph Aerostructures, Llc (Active)
- Primary Buy
- Primary Buy
Datasheet 9540-01-469-3308
- 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]
- 0.110 Inches Minimum And 0.130 Inches Maximum
- Fillet Radius Where Top Right Flange Joins Web Flange/Leg [BPXL]
- 0.110 Inches Minimum And 0.130 Inches Maximum
- First Tip Style [CMZY]
- Right Taper Length
- First Tip Thickness [CNPS]
- 0.990 Inches Minimum And 1.010 Inches Maximum
- First Tip Taper Length [CNPD]
- 0.690 Inches Minimum And 0.710 Inches Maximum
- Heat Treatment [HEAT]
- Annealed
- Material [MATT]
- Titanium Alloy, Mil-T-81556, Comp Ab-1
- Left Side Top Flange Distance To Center Of Both Flanges [BPXD]
- 2.560 Inches Nominal
- Left Side Top Flange Thickness [ADXR]
- 0.115 Inches Minimum And 0.135 Inches Maximum
- Left Top Inside Angle [CSMZ]
- 90.0 Degrees Nominal
- Leg Thickness [AJJP]
- 0.115 Inches Minimum And 0.135 Inches Maximum
- Length [ABRY]
- 18.800 Inches Minimum And 18.820 Inches Maximum
- Right Side Top Flange Distance To Center Of Both Flanges [BPXG]
- 2.560 Inches Nominal
- Right Side Top Flange Thickness [ADXS]
- 0.115 Inches Minimum And 0.135 Inches Maximum
- Right Top Inside Angle [CRZC]
- 90.0 Degrees Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Not Identical
- Second Tip Style [CNQK]
- Left Taper Length
- Second Tip Taper Length [CNPF]
- 0.690 Inches Minimum And 0.710 Inches Maximum
- Second Tip Thickness [CNPT]
- 0.990 Inches Minimum And 1.010 Inches Maximum
- Overall Height [ABKW]
- 4.440 Inches Nominal
- Special Features [FEAT]
- Along Length Flanges On Both Sides Narrow From Normal Width From Center (At 4.04 In. From First Tip) To 1.01 In. From Center (At 6.73 In. From First Tip); Flanges Widen From 1.01 In. From Center (At 13.18 In. From First Tip) To Normal Width (At 15.88 In. From First Tip); Weapons System Is Aircraft, B-2 Bomber (Atb)
- Top Flange Width [BQJG]
- 5.120 Inches Nominal
DLA Procurement Analysis 9540-01-469-3308
Management Data 9540-01-469-3308
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Oct 2022
- Defense Logistics Agency (DS)
- FT
- Subscribe
- FT
- Oct 2021
- Department of the Air Force (DF)
- FT
- Subscribe
- FT
- Oct 2020
- Department of the Air Force (DF)
- FT
- Subscribe
- FT
- Aug 2020
- Department of the Navy (DN)
- FT
- Subscribe
- 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
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Freight Information 9540-01-469-3308
9540-01-469-3308 has freight characteristics.. 9540-01-469-3308 has a variance between NMFC and UFC when transported by rail and the description should be consulted.
Contracting Technical Data File (CTDF) 9540-01-469-3308 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: