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9540-01-437-4996
Structural Angle
9540014374996 014374996 AMS-QQ-A-200/15 CVC10001-526CJ 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 9540-01-437-4996 5+ Documents (More...)
Quotation AMS-QQ-A-200/15 https/ 6 EA NS Request Quotation AMS-QQ-A-200/15 https//www.nsnlookup.com /
AMS-QQ-A-200/15 https/ 6 EA NS Request AMS-QQ-A-200/15 BEAM,STRUCTURAL 41 41 EA NS Request QQ-A-200
Structural Angle 9540014374996 014374996 9540-01-437-4996 9540014374996 014374996 is a structural
Structural Angle 9540014374996 014374996 9540-01-437-4996 9540014374996 014374996 is a structural
Structural Angle 9540014374996 014374996 9540-01-437-4996 9540014374996 014374996 is a structural
Structural Angle 9540014374996 014374996 9540-01-437-4996 9540014374996 014374996 is a structural
Restrictions 9540-01-437-4996
9540-01-437-4996 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 9540-01-437-4996
- US Air Force (FNN5)
- Effective Date:
- 1 Jul 2003
- Former MOE Rule:
- FGKZ
Approved Sources 9540-01-437-4996
- Part Number
- Manufacturer
- Status
- AMS-QQ-A-200/15
- Manufacturer
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- CVC10001-526CJ
- 80378 - Triumph Aerostructures, Llc (Active)
- Primary Buy
- Primary Buy
- QQ-A-200/15
- 81348 - Federal Specifications (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQ-A-200/15
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 9540-01-437-4996
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Base Flange Thickness [AJGP]
- 0.125 Inches Nominal
- Basic Shape Style [AGTA]
- Angle
- Fabrication Method [AARN]
- Extruded
- Fillet Radius Where Left Flange Joins Base Flange [AJGL]
- 0.156 Inches Nominal
- First Tip Radius [AJJB]
- 0.125 Inches Nominal
- First Tip Style [CMZY]
- Right Quarter Radius
- Heat Treatment [HEAT]
- T-76511 Solution Heat Treated
- Material [MATT]
- Aluminum Alloy, Qq-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]
- 0.125 Inches Nominal
- Length [ABRY]
- 12.000 Feet Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Not Identical
- Second Tip Radius [CMZZ]
- 0.125 Inches Nominal
- Second Tip Style [CNQK]
- Upper Radius
- Overall Height [ABKW]
- 1.000 Inches Nominal
- Overall Width [ABMK]
- 1.750 Inches Nominal
Management Data 9540-01-437-4996
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Oct 2006
- Department of the Air Force (DF)
- FT
- Subscribe
- 1
- FT
Air Force
- Budget:
- S
- 57X3010 - Aircraft Replenishment Spares
- Aggregation Code:
- BQ
- B-2 TSSP, NORTHROP GRUMMAN
- Price Validation Code:
- E
- The current standard price is an estimated price.
Estimated Price challenges are allowed but follow procedures in para 60.b. (3) of section L of this manual.
This code will be changed to a P code upon notification of a contract price or this code will be changed to an updated code upon determination of a valid price.
- Expendability
Recoverability
Repairability: - N
- Expendable. Condemn at User. Stock Fund (except Munitions).
NATO Stock Numbers Related to 9540-01-437-4996
Freight Information 9540-01-437-4996
9540-01-437-4996 has freight characteristics.. 9540-01-437-4996 has a variance between NMFC and UFC when transported by rail and the description should be consulted.