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9540-01-428-9031
Structural Angle
9540014289031 014289031 AMS-QQ-A-200/11 CVC10001-307CA QQ-A-200/11
A structural shape fabricated from a ferrous or nonferrous material and resembling the letter L in cross-sectional form. The edges may have a bulb, be rounded, and the inside corner may have a fillet. View more Structural Angle
January 2023
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Related Documents 9540-01-428-9031 5+ Documents (More...)
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-200 / /11 - - AMS-QQ-A-200/11 /11 AMS-QQ-A -200/ 11 - - AMS-QQ-A -200 /11 BEAM 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
- - 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 - // 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-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
Restrictions 9540-01-428-9031
9540-01-428-9031 is a Structural Angle 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 9540-01-428-9031
- US Air Force (FNN5)
- Effective Date:
- 1 Jun 2003
- Former MOE Rule:
- FGKZ
Approved Sources 9540-01-428-9031
- Part Number
- Manufacturer
- Status
- AMS-QQ-A-200/11
- Manufacturer
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- CVC10001-307CA
- 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 9540-01-428-9031
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Base Flange Thickness [AJGP]
- 0.113 Inches Nominal
- Basic Shape Style [AGTA]
- Angle
- Fabrication Method [AARN]
- Extruded
- Fillet Radius Where Left Flange Joins Base Flange [AJGL]
- 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 Inside Angle [CQHP]
- 88.0 Degrees Nominal
- Left Side Flange Thickness [ADXL]
- 0.163 Inches Nominal
- Length [ABRY]
- 12.000 Feet Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 1.190 Inches Nominal
- Overall Width [ABMK]
- 3.000 Inches Nominal
Management Data 9540-01-428-9031
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- May 2009
- Department of the Air Force (DF)
- FT
- Subscribe
- FT
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Freight Information 9540-01-428-9031
9540-01-428-9031 has freight characteristics.. 9540-01-428-9031 has a variance between NMFC and UFC when transported by rail and the description should be consulted.