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9540-01-471-8215

Structural Beam

9540014718215 014718215 CVC10011-75CJ

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

9540-01-471-8215 BEAM,STRUCTURAL 9540014718215 014718215

Managed by United States
NSN Created on 16 Feb 2000
Data Last Changed
May 2023
NATO Update Count
4
NATO Data Quality
AGTA Style J4 for 9540-01-471-8215 1/2
NSN 9540-01-471-8215 (Identification) 1/2
CMZY Style 7 for 9540-01-471-8215 2/2
NSN 9540-01-471-8215 (Identification) 2/2

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9540-01-471-8215 Demil Restrictions 9540-01-471-8215

DEMIL: A | DEMILI: 1 | CRITICALITY: X | HMIC: N | PMIC: U | EDC: A | ADPEC: 0

9540-01-471-8215 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. The precious metals content of this item is unknown.

9540-01-471-8215 End Users End Users 9540-01-471-8215

US Air Force (FNN5)
Effective Date:
1 Jun 2003
Former MOE Rule:
FGKZ

9540-01-471-8215 Manufacturers Approved Sources 9540-01-471-8215

9540-01-471-8215 Technical Data Datasheet 9540-01-471-8215

Characteristic
Specifications
FIIG
A13100
Basic Shape Style [AGTA]
T Shape
Fabrication Method [AARN]
Extruded
Fillet Radius Where Top Left Flange Joins Web Flange/Leg [BPXJ]
0.120 Inches Nominal
Fillet Radius Where Top Right Flange Joins Web Flange/Leg [BPXL]
0.125 Inches Nominal
First Tip Inner Radius [CNBD]
0.032 Inches Nominal
First Tip Outer Radius [CNBJ]
0.032 Inches Nominal
First Tip Style [CMZY]
Square W/ Inner And Outer Corner Radii
Heat Treatment [HEAT]
T-76511 Solution Heat Treated
Material [MATT]
Aluminum Alloy 7075
Left Side Top Flange Distance To Center Of Both Flanges [BPXD]
1.248 Inches Nominal
Left Side Top Flange Thickness [ADXR]
0.210 Inches Nominal
Left Top Inside Angle [CSMZ]
90.0 Degrees Nominal
Leg Thickness [AJJP]
0.156 Inches Nominal
Length [ABRY]
13.000 Feet Nominal
Right Side Top Flange Distance To Center Of Both Flanges [BPXG]
1.562 Inches Nominal
Right Side Top Flange Thickness [ADXS]
0.210 Inches Nominal
Right Top Inside Angle [CRZC]
90.0 Degrees Nominal
Second Tip Relationship To First Tip [CNQJ]
Identical
Overall Height [ABKW]
1.600 Inches Nominal
Special Features [FEAT]
Ws Is Aircraft,B-2 Bomber (Atb)
Top Flange Width [BQJG]
2.810 Inches Nominal
Weight Per Unit Measure [BRFD]
0.974 Pounds Per Linear Foot
Third Tip Relationship To Preceding Tips [CNQL]
Identical W/First Tip

9540-01-471-8215 Stock, Inventory and Procurement DLA Procurement Analysis 9540-01-471-8215

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9540-01-471-8215 Management Data Management Data 9540-01-471-8215

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Oct 2022
Defense Logistics Agency (DS)
FT
Subscribe
Oct 2021
Department of the Air Force (DF)
FT
Subscribe
Oct 2020
Department of the Air Force (DF)
FT
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Oct 2019
Department of the Air Force (DF)
FT
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9540-01-471-8215 Freight Data Freight Information 9540-01-471-8215

9540-01-471-8215 has freight characteristics.. 9540-01-471-8215 has a variance between NMFC and UFC when transported by rail and the description should be consulted.

9540-01-471-8215 Contracting Technical Data File (CTDF) Contracting Technical Data File (CTDF) 9540-01-471-8215 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: