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9540-01-428-4059
Structural Angle
9540014284059 014284059 AMS-QQ-A-200/15 CVC10001-138CJ QQ-A-200/15
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 9540-01-428-4059 5+ Documents (More...)
QQ-A-200/15 ANGLE,STRUCTURAL 6 FT NS Request Quotation AMS-QQ-A-200/15 ANGLE,STRUCTURAL 41 FT NS Request
ANGLE,STRUCTURAL 6 FT NS Request Quotation AMS-QQ-A-200/15 ANGLE,STRUCTURAL 41 FT NS Request ANGLE
ANGLE,STRUCTURAL 6 FT NS Request Quotation AMS-QQ-A-200/15 ANGLE,STRUCTURAL 41 FT NS Request ANGLE
/fsg-95/fsc-9540/us 9540-01-428-4059 Structural Angle 9540014284059 014284059 QQ-A-200/15 ANGLE,STRUCTURAL
Angle 9540014374996014374996 A AMS-QQ-A-200/15 A A A AMS-QQ-A 95/fsc-9540/us 9540-01 A A AMS-QQ-A
Structural Angle 9540014284059 014284059 QQ-A-200/15 ANGLE,STRUCTURAL 6 FT NS Request Quotation
BEAM,STRUCTURAL 6 EA NS Request Quotation AMS-QQ-A-200/15 BEAM,STRUCTURAL 41 EA NS Request ANGLE,
ANGLE,STRUCTURAL 6 FT NS Request Quotation AMS-QQ-A-200/15 ANGLE,STRUCTURAL 41 FT NS Request ANGLE
Structural Angle 9540014284059 014284059 CVC10001-138CJ QQ-A-200/15 A structural shape fabricated
from a ferrous or nonferrous material and QQ-A-200/15 ANGLE,STRUCTURAL 6 FT NS Request Quotation AMS-QQ-A
Restrictions 9540-01-428-4059
9540-01-428-4059 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 9540-01-428-4059
- US Air Force (FNN5)
- Effective Date:
- 1 Jun 2003
- Former MOE Rule:
- FGKZ
Approved Sources 9540-01-428-4059
- Part Number
- Manufacturer
- Status
- AMS-QQ-A-200/15
- Manufacturer
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- CVC10001-138CJ
- 80378 - Triumph Aerostructures, Llc (Active)
- Primary Buy
- Primary Buy
- AMS-QQ-A-200/15
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- QQ-A-200/15
- 81348 - Federal Specifications Promulgated (Active)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 9540-01-428-4059
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Base Flange Thickness [AJGP]
- 0.050 Inches Nominal
- Basic Shape Style [AGTA]
- Angle
- Fabrication Method [AARN]
- Extruded
- Fillet Radius Where Left Flange Joins Base Flange [AJGL]
- 0.060 Inches Nominal
- First Tip Style [CMZY]
- Square End
- Heat Treatment [HEAT]
- T-76511 Solution Heat Treated
- End Item Identification [AGAV]
- B-2 Bomber
- Material [MATT]
- Aluminum Alloy, Q-A-200/15, Alloy 7075
- Nondefinitive Spec/Std Data [ZZZT]
- Alloy 7075 And Temper T76511
- Left Inside Angle [CQHP]
- 90.0 Degrees Nominal
- Left Side Flange Thickness [ADXL]
- 0.050 Inches Nominal
- Length [ABRY]
- 12.000 Feet Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 0.600 Inches Nominal
- Overall Width [ABMK]
- 0.800 Inches Nominal
Management Data 9540-01-428-4059
- 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 9540-01-428-4059
9540-01-428-4059 has freight characteristics.. 9540-01-428-4059 has a variance between NMFC and UFC when transported by rail and the description should be consulted.