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9540-01-428-9526
Structural Beam
9540014289526 014289526 AMS-QQ-A-200/11 CVC10012-207CA 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 3 Apr 1996
Data Last Changed
June 2023
June 2023
NATO Update Count
10
10
NATO Data Quality
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AMS-QQ-A200/11 BEAM,STRUCTURAL 45 FT NS
AMS-QQ-A-200/11 BEAM,STRUCTURAL 3 FT NS
QQA200-11 BEAM,STRUCTURAL 603 FT NS
QQ-A200/11 BEAM,STRUCTURAL 16 FT NS
QQ-A-200/11 BEAM,STRUCTURAL 4 FT NS
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Related Documents 9540-01-428-9526 5+ Documents (More...)
- - AMS-QQ-A -200 /11 - /11 - - AMS-QQ-A -200 /11 - - AMS-QQ-A-200 /11 BEAM BEAM 200 AMS-QQ-A-
- // 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 - - AMS-QQ-A-200/11 /11 AMS-QQ-A -200/ 11 - - AMS-QQ-A -200 /11 BEAM 200 AMS-QQ-A -200 / /
- // 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 - - AMS-QQ-A-200/11 /11 AMS-QQ-A -200/ 11 - - AMS-QQ-A -200 /11 BEAM 200 AMS-QQ-A -200 / /
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 - -
- - 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 - -
- // AMS-QQ-A -200 200 AMS-QQ-A-200 / /11 - - AMS-QQ-A-200/11 - // AMS-QQ-A A https - - AMS-QQ-A
- - 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 AMS-QQ-A
- - 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 AMS-QQ-A
- - AMS-QQ-A-200/11 /us 9540-00-409-5972 A https AMS-QQ-A-200 /11 BEAM 200 AMS-QQ-A -200 / /11
- - AMS-QQ-A-200/11 /11 AMS-QQ-A -200/ 11 - - AMS-QQ-A -200 /11 /fsg-95 /11 AMS-QQ-A -200/11 - - AMS-QQ-A
BEAM 200 AMS-QQ-A-200/ / 11 - - AMS-QQ-A-200 /11 /11 // // AMS-QQ-A AMS-QQ-A-200 11 - - AMS-QQ-A
- - AMS-QQ-A-200/11 /11 AMS-QQ-A -200/ 11 - - AMS-QQ-A -200 /11 /fsg-95 /11 AMS-QQ-A -200/11 - - AMS-QQ-A
BEAM 200 AMS-QQ-A-200/ / 11 - - AMS-QQ-A-200 /11 /11 // // AMS-QQ-A AMS-QQ-A-200 11 - - AMS-QQ-A
/11 AMS-QQ-A -200/11 - - AMS-QQ-A -200 /11 -200 /11 /11 AMS-QQ-A-200/11 200 AMS-QQ-A -200/ 11
// AMS-QQ-A -200 /11 / 9540013482848013482848AMS-QQ-A -200 / /11 - - AMS-QQ-A-200/11 /11 AMS-QQ-A
-200/ 11 - - AMS-QQ-A -200 /11 BEAM 200 AMS-QQ-A -200 / /11 11 A https - - AMS-QQ-A - - -200 /11 BEAM
// AMS-QQ-A -200 /11 / 9540013482848013482848AMS-QQ-A -200 / /11 - - AMS-QQ-A-200/11 /11 AMS-QQ-A
-200/ 11 - - AMS-QQ-A -200 /11 BEAM 200 AMS-QQ-A -200 / /11 11 A https - - AMS-QQ-A - - -200 /11 BEAM
Restrictions 9540-01-428-9526
9540-01-428-9526 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 9540-01-428-9526
- US Air Force (FNN5)
- Effective Date:
- 1 Jul 2003
- Former MOE Rule:
- FGKZ
Approved Sources 9540-01-428-9526
- Part Number
- Manufacturer
- Status
- AMS-QQ-A-200/11
- Manufacturer
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- CVC10012-207CA
- 80378 - Triumph Aerostructures, Llc (Active)
- Primary Buy
- Primary Buy
- QQ-A-200/11
- 81348 - Federal Specifications Promulgated (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQ-A-200/11
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 9540-01-428-9526
- 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]
- 0.120 Inches Nominal
- Fillet Radius Where Top Right Flange Joins Web Flange/Leg [BPXL]
- 0.120 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
- End Item Identification [AGAV]
- B-2 Bomber
- 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]
- 2.270 Inches Nominal
- Left Side Top Flange Thickness [ADXR]
- 0.174 Inches Nominal
- Left Top Inside Angle [CSMZ]
- 91.0 Degrees Nominal
- Leg Thickness [AJJP]
- 0.155 Inches Nominal
- Length [ABRY]
- 12.000 Feet Nominal
- Right Side Top Flange Distance To Center Of Both Flanges [BPXG]
- 5.330 Inches Nominal
- Right Side Top Flange Thickness [ADXS]
- 0.174 Inches Nominal
- Right Top Inside Angle [CRZC]
- 89.0 Degrees Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 3.000 Inches Nominal
- Top Flange Width [BQJG]
- 7.600 Inches Nominal
- Third Tip Relationship To Preceding Tips [CNQL]
- Identical W/First Tip
DLA Procurement Analysis 9540-01-428-9526
Management Data 9540-01-428-9526
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Jun 2023
- Defense Logistics Agency (DS)
- FT
- Subscribe
- 1
- FT
- May 2023
- Department of the Air Force (DF)
- FT
- Subscribe
- 1
- FT
- Feb 2023
- Defense Logistics Agency (DS)
- FT
- Subscribe
- 1
- FT
- Oct 2021
- Department of the Air Force (DF)
- FT
- Subscribe
- FT
- Oct 2020
- Department of the Air Force (DF)
- FT
- Subscribe
- FT
- Oct 2019
- Department of the Air Force (DF)
- FT
- Subscribe
- FT
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Freight Information 9540-01-428-9526
9540-01-428-9526 has freight characteristics.. 9540-01-428-9526 has a variance between NMFC and UFC when transported by rail and the description should be consulted.
Procurement History 9540-01-428-9526 2 Records
Contracting Technical Data File (CTDF) 9540-01-428-9526 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: