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9540-01-478-9727

Structural Beam

9540014789727 014789727 HS1006AA41B0027

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

9540-01-478-9727 BEAM,STRUCTURAL 9540014789727 014789727

Managed by United States
NSN Created on 4 Oct 2000
Data Last Changed
January 2023
NATO Update Count
3
NATO Data Quality
AGTA Style J4 for 9540-01-478-9727 1/2
NSN 9540-01-478-9727 (Identification) 1/2
CMZY Style 1 for 9540-01-478-9727 2/2
NSN 9540-01-478-9727 (Identification) 2/2

9540-01-478-9727 Stock and Availability Marketplace 9540-01-478-9727

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9540-01-478-9727 Demil Restrictions 9540-01-478-9727

DEMIL: B | DEMILI: 3 | CRITICALITY: X | HMIC: N | PMIC: A | EDC: A | ADPEC: 0

9540-01-478-9727 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.

9540-01-478-9727 HTS and ScheduleB Import and Export 9540-01-478-9727

9540-01-478-9727 End Users End Users 9540-01-478-9727

United Kingdom (ZK01)
Effective Date:
1 Oct 2000

9540-01-478-9727 Manufacturers Approved Sources 9540-01-478-9727

9540-01-478-9727 Technical Data Datasheet 9540-01-478-9727

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]
0.125 Inches Nominal
Fillet Radius Where Top Right Flange Joins Web Flange/Leg [BPXL]
0.125 Inches Nominal
First Tip Style [CMZY]
Square End
Heat Treatment [HEAT]
T-6 Solution Heat Treated Or T-6511 Solution Heat Treated
End Item Identification [AGAV]
Apache Helicopter
Material Document And Classification [MDCL]
Qq-A-200/11 Fed Spec 1St Material Response
Material [MATT]
Aluminum Alloy 7075
Part Name Assigned By Controlling Agency [CXCY]
Extrusion, Tee, Aluminum Alloy
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]
0.844 Inches 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
Right Top Inside Angle [CRZC]
90.0 Degrees Nominal
Second Tip Relationship To First Tip [CNQJ]
Identical
Overall Height [ABKW]
2.500 Inches Nominal
Top Flange Width [BQJG]
1.500 Inches Nominal
Third Tip Relationship To Preceding Tips [CNQL]
Identical W/First Tip

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9540-01-478-9727 Freight Data Freight Information 9540-01-478-9727

9540-01-478-9727 has freight characteristics managed by the Bureau of Engraving and Printing.. 9540-01-478-9727 has a variance between NMFC and UFC when transported by rail and the description should be consulted.