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9540-01-437-3884

Structural Beam

9540014373884 014373884 AMS-QQ-A-200/11 CVC10011-56CA QQ-A-200/11

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

Managed by United States

NSN Created on 11 Oct 1996

Data Last Changed
May 2023

NATO Update Count
10

NATO Data Quality

AGTA Style J4 for 9540-01-437-3884 1/2 — NSN 9540-01-437-3884 (Identification) 1/2

CMZY Style 7 for 9540-01-437-3884 2/2 — NSN 9540-01-437-3884 (Identification) 2/2

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QQ-A-20011 BEAM,STRUCTURAL 12 FT NS

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Related Documents 9540-01-437-3884 5+ Documents (More...)

https//www.nsnlookup.com
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9540-01-437-3884 Structural Beam 9540014373884 014373884

AMS-QQ-A-200/11 CVC10011-56CA QQ-A-200/11 A structural shape fabricated from a ferrous or nonferrous
11 - - AMS-QQ-A -200/11 - - AMS-QQ-A-200/11 BEAM 200 AMS-QQ-A -200/ 11 // AMS-QQ-A -200 /11 https//
- - AMS-QQ-A-200/11 BEAM - - AMS-QQ-A -200 /11 BEAM 200 AMS-QQ-A-200/ / 11 - - AMS-QQ-A-200/11 - /11

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6650-99-444-9387 Magnifier 6650994449387 994449387,56CA

6650-99-444-9387 https//www.nsnlookup.com https https//www.nsnlookup.com /fsg-95/fsc-9540/us 9540-01-437-3884
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Beam9540014373884 014373884 CVC10011-56CA AMS-QQ-A-200/ / 11 - - AMS-QQ-A-200/11 - /11 - https//www.nsnlookup.com

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9530-01-337-5563 Metal Bar 9530013375563 013375563

AMS-QQ-A-200/ / 11 - - AMS-QQ-A - - AMS-QQ-A -200/11 - AMS-QQ-A -200 /11 - /11 - 200 - AMS-QQ-A -200
9530013375563013375563 - - AMS-QQ-A-200 /11 013795683AMS-QQ-A BEAM 200 AMS-QQ-A -200/ / 11 - - AMS-QQ-A
013795683AMS-QQ-A BEAM 200 AMS-QQ-A-200/ / 11 - - AMS-QQ-A-200 11 - - AMS-QQ-A BEAM 200 AMS-QQ-A

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9540-01-378-8212 Structural Angle 9540013788212 013788212

BEAM - - AMS-QQ-A-200/11 - // AMS-QQ-A - -200/11 - - AMS-QQ-A /11 - - AMS-QQ-A -200/11 - -
- - AMS-QQ-A -200/11 BEAM AMS-QQ-A-200/11 /11 AMS-QQ-A -200/11 - - AMS-QQ-A https/ BEAM - - AMS-QQ-A
BEAM - - AMS-QQ-A-200/11 - // AMS-QQ-A - -200/11 - - AMS-QQ-A /11 - - AMS-QQ-A -200/11 - -

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9540-00-492-3625 Structural Channel 9540004923625 004923625

- - AMS-QQ-A-200/11 - // AMS-QQ-A 200 AMS-QQ-A-200 / /11 - - AMS-QQ-A-200/ 11 - // AMS-QQ-A -200
- - AMS-QQ-A-200/11 - // AMS-QQ-A AMS-QQ-A-200 / /11 - - AMS-QQ-A A https AMS-QQ-A-200 /11 BEAM
200 AMS-QQ-A-200 / /11 - - AMS-QQ-A-200/11 - // AMS-QQ-A -200 /11 A https AMS-QQ-A-200 /11 BEAM 200

Restrictions 9540-01-437-3884

9540-01-437-3884 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 9540-01-437-3884

US Air Force (FNN5)
Effective Date:: 1 Jun 2003
Former MOE Rule:: FGKZ; AMC 0 AMSC 0 IMC B

Approved Sources 9540-01-437-3884

Part Number
Manufacturer
Status
AMS-QQ-A-200/11: 0U583 - Sae International (Active); Incomplete Reference; RNCC 3 RNVC 1 DAC E
CVC10011-56CA: 80378 - Triumph Aerostructures, Llc (Active); Primary Buy; RNCC 3 RNVC 2 DAC E
AMS-QQ-A-200/11: 81343 - Society Of Automotive Engineers Inc (Replaced); Canceled/Obsolete; RNCC 5 RNVC 9 DAC E
QQ-A-200/11: 81348 - Federal Specifications Promulgated (Active); Canceled/Obsolete; RNCC 5 RNVC 9 DAC E

Datasheet 9540-01-437-3884

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]: 0.090 Inches Nominal
Fillet Radius Where Top Right Flange Joins Web Flange/Leg [BPXL]: 0.090 Inches Nominal
First Tip Inner Radius [CNBD]: 0.030 Inches Nominal
First Tip Outer Radius [CNBJ]: 0.030 Inches Nominal
First Tip Style [CMZY]: Square W/ Inner And Outer Corner Radii
Heat Treatment [HEAT]: O-Annealed
Material [MATT]: Aluminum Alloy, Qq-A-200/11, Alloy 7075
Nondefinitive Spec/Std Data [ZZZT]: Alloy 7075 And Temper 0
Left Side Top Flange Distance To Center Of Both Flanges [BPXD]: 1.420 Inches Nominal
Left Side Top Flange Thickness [ADXR]: 0.125 Inches Nominal
Left Top Inside Angle [CSMZ]: 90.0 Degrees Nominal
Leg Thickness [AJJP]: 0.156 Inches Nominal
Length [ABRY]: 12.000 Feet Nominal
Right Side Top Flange Distance To Center Of Both Flanges [BPXG]: 1.420 Inches Nominal
Right Side Top Flange Thickness [ADXS]: 0.125 Inches Nominal
Right Top Inside Angle [CRZC]: 90.0 Degrees Nominal
Second Tip Relationship To First Tip [CNQJ]: Identical
Overall Height [ABKW]: 2.280 Inches Nominal
Top Flange Width [BQJG]: 2.840 Inches Nominal
Third Tip Relationship To Preceding Tips [CNQL]: Identical W/First Tip

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Management Data 9540-01-437-3884

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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; Subscribe
Oct 2019: Department of the Air Force (DF); FT; Subscribe

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Freight Information 9540-01-437-3884

9540-01-437-3884 has freight characteristics.. 9540-01-437-3884 has a variance between NMFC and UFC when transported by rail and the description should be consulted.

Contracting Technical Data File (CTDF) 9540-01-437-3884 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:

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