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9540-01-412-1747
Structural Angle
9540014121747 014121747 AMS-T-9046 CVC10001-365GA MIL-T-9046
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
Managed by United States
NSN Created on 12 Apr 1995
Data Last Changed
January 2023
January 2023
NATO Update Count
9
9
NATO Data Quality
Marketplace 9540-01-412-1747
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Related Documents 9540-01-412-1747 5+ Documents (More...)
AMS-T-9046 CVC10001-365GA MIL-T-9046 A structural shape fabricated from a ferrous or nonferrous material
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Restrictions 9540-01-412-1747
9540-01-412-1747 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 9540-01-412-1747
- US Air Force (FNN5)
- Effective Date:
- 1 May 2003
- Former MOE Rule:
- FGKZ
- Brazil (YA01)
- Effective Date:
- 1 Jul 2001
Approved Sources 9540-01-412-1747
- Part Number
- Manufacturer
- Status
- AMS-T-9046
- Manufacturer
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- CVC10001-365GA
- 80378 - Triumph Aerostructures, Llc (Active)
- Primary Buy
- Primary Buy
- MIL-T-9046
- 81349 - Military Specifications (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-T-9046
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 9540-01-412-1747
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Base Flange Thickness [AJGP]
- 0.120 Inches Nominal
- Base Flange Width [AJGQ]
- 1.450 Inches Nominal
- Basic Shape Style [AGTA]
- Angle
- Fabrication Method [AARN]
- Extruded
- First Tip Style [CMZY]
- Square End
- Heat Treatment [HEAT]
- Annealed
- Material [MATT]
- Titanium, Mil-T-9046, Ab-1, Cda
- Nondefinitive Spec/Std Data [ZZZT]
- Composition Ab-1 And Condition A
- Left Inside Angle [CQHP]
- 90.0 Degrees Nominal
- Left Side Flange Height [ADXJ]
- 1.020 Inches Nominal
- Left Side Flange Thickness [ADXL]
- 0.120 Inches Nominal
- Length [ABRY]
- 12.000 Feet Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 1.170 Inches Nominal
- Overall Width [ABMK]
- 1.600 Inches Nominal
Management Data 9540-01-412-1747
- 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
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Freight Information 9540-01-412-1747
9540-01-412-1747 has freight characteristics.. 9540-01-412-1747 has a variance between NMFC and UFC when transported by rail and the description should be consulted.
Packaging Data 9540-01-412-1747
- Responsible Activity
- Packaging Data Source
- Primary Inventory Control Activity (PICA)
- Packaging Data does not meet current MIL-STD-2073-1E
Item Pack Level (Unpackaged)
- Item Size
- Item Weight
- Characteristics
- Weight/Dimensions Category
- Fragility
- Item Preservation
- Item Weight
- --
- --
- --
- --
- --
- --
Unit Pack Level (Packaged)
- Quantity per Pack
- Unit Size
- Unit Weight
- Unit Cube
- Preservation Method
- Cleaning/Drying
- Unit Size
- 1
- --
- --
- --
- --
- No Requirements
- --
- Preservation Material
- Wrapping Material
- Cushioning/Dunnage
- Cushioning Thickness
- Container
- Special Marking
- Wrapping Material
- No Requirement
- No Requirement
- No Requirement
- Not Applicable
- No Requirement
- --
- No Requirement
Intermediate Pack Level
- Quantity of Unit Packs
- Container
- --
- No Requirement