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9540-00-528-8803

Structural Beam

9540005288803 005288803 AMS-QQA200-11 61127 QQA277TEMPERT6 1M5165 DIE61127 QQA200-11

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

9540-00-528-8803 BEAM,STRUCTURAL 9540005288803 005288803

Managed by United States
NSN Created on 1 Jan 1963
Data Last Changed
January 2023
NATO Update Count
11
NATO Data Quality
AGTA Style J4 for 9540-00-528-8803 1/2
NSN 9540-00-528-8803 (Identification) 1/2
CMZY Style 1 for 9540-00-528-8803 2/2
NSN 9540-00-528-8803 (Identification) 2/2

9540-00-528-8803 Stock and Availability Marketplace 9540-00-528-8803

9540-00-528-8803 Related Documents Related Documents 9540-00-528-8803 5+ Documents (More...)

AMS-QQA200-11 61127 QQA277TEMPERT6 1M5165 DIE61127 QQA200-11 A structural shape fabricated from a ferrous
PA22211 AMS-QQA200 - 11 PA22211 AMS-QQA200 https// AMS-QQA200 - 11 44939 AMS-QQA200 - 11 44939 22877
AMS-QQA200 - 11 44939 22877 QQA200 PA22211 44939 AMS-QQA200- 11 PA22211 AMS-QQA200- 11 PA22211 AMS-QQA200
instructions how to enable JavaScript in your web browser . 3020-01-090-2205Pinion3020010902205 010902205 1M5165
https//www.nsnlookup.com /fsg-30/fsc-3020/us 3020-01-090-2205 Pinion 3020010902205 010902205,1M5165 1M5165
by United States NSN Created on 14 Feb 1980 Data https//www.nsnlookup.com /fsg-95/fsc-9540/us 9540-00-528-8803
AMS-QQA200 - 11 - 11 44939 22877 QQA200-11 PA22211 44939 A AMS-QQA200- 11 PA22211 - 11 https/ AMS-QQA200
https/ AMS-QQA200 - 11 44939 22877 QQA200 PA22211 44939 AMS-QQA200- 11 PA22211 AMS-QQA200- 11 PA22211
AMS-QQA200- 11 https // - A structural AMS-QQA200- 11 PA22211 AMS-QQA200- 11 https /fsg-95 PA22211 AMS-QQA200
PA22211 44939 AMS-QQA200 AMS-QQA200- 11 https AMS-QQA200- 11 44939 PA22211 AMS-QQA200 AMS-QQA200
PA22211 44939 AMS-QQA200 - 11 PA22211 PA22211 AMS-QQA200- 11 44939 44939 AMS-QQA200- 11 PA22211
PA22211 44939 AMS-QQA200- 11 PA22211 PA22211 AMS-QQA200- 11 44939 44939 AMS-QQA200- 11 PA22211
PA22211 44939 AMS-QQA200- 11 PA22211 PA22211 AMS-QQA200- 11 44939 44939 AMS-QQA200- 11 PA22211 AMS-QQA200
- 11 PA22211 AMS-QQA200- 11 https - 11 PA22211 AMS-QQA200- 11 PA22211 44939 A AMS-QQA200 - 11 PA22211
PA22211 AMS-QQA200- 11 44939 22877 QQA200- PA22211 AMS-QQA200 - 11 https/ AMS-QQA200- 11 44939 22877

9540-00-528-8803 Demil Restrictions 9540-00-528-8803

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

9540-00-528-8803 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. The precious metals content of this item is unknown.

9540-00-528-8803 End Users End Users 9540-00-528-8803

Germany (ZG)
Germany (ZG01)
Effective Date:
1 Apr 1991
Turkey (ZW)
Turkey (ZW01)
Effective Date:
1 Nov 2005

9540-00-528-8803 Manufacturers Approved Sources 9540-00-528-8803

9540-00-528-8803 Technical Data Datasheet 9540-00-528-8803

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-1 Solution Heat Treated And Artifically Aged
Material [MATT]
Aluminum Alloy,Qq-A-200/11,Allot 7075
Nondefinitive Spec/Std Data [ZZZT]
T6 Temper
Left Side Top Flange Distance To Center Of Both Flanges [BPXD]
1.190 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]
10.000 Feet Minimum And 12.000 Feet Maximum
Right Side Top Flange Distance To Center Of Both Flanges [BPXG]
1.190 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]
1.250 Inches Nominal
Top Flange Width [BQJG]
2.380 Inches Nominal
Weight Per Unit Measure [BRFD]
0.280 Pounds Per Linear Foot
Third Tip Relationship To Preceding Tips [CNQL]
Identical W/First Tip

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9540-00-528-8803 Freight Data Freight Information 9540-00-528-8803

9540-00-528-8803 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 013760. A Sub NMFC of X. It has a NMFC Description of ALUM TEES. 9540-00-528-8803 is rated as class 60 when transported by Less-Than Truckload (LTL) freight. 9540-00-528-8803 is rated as class 60 when transported by Less-Than Carload (LCL) rail or ocean freight. It has a Uniform Freight Classification (UFC) number of 05830 which rates the freight between FCL and LCL. 9540-00-528-8803 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. 9540-00-528-8803 is not classified as a special type of cargo when transported by water. 9540-00-528-8803 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.