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9540-01-435-5250
Structural Angle
9540014355250 014355250 MIL-T-81556 CVC10001-1019GA CVC10001-1019GAX144
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 9540-01-435-5250 5+ Documents (More...)
MIL-T-81556 ANGLE,STRUCTURAL 9 FT NS Request Quotation Updated Every Day 9540-01-435-5250 RQST NE Updated
Every Day 9540-01-435-5250 RQST Updated Every Day 9540-01-435-5250 RQST NE Related Documents 9540-01
MIL-T-81556 STRUCTURAL SECTION,SPECIAL SHAPED 9 FT NS Request Quotation Updated Every Day 9540-01-437
MIL-T-81556 ANGLE,STRUCTURAL 9 FT NS Request Quotation Updated Every Day 9540-01-438-7991 RQST
MIL-T-81556 BEAM,STRUCTURAL 9 FT NS Request Quotation FedMall Updated Every 15 Minutes 9540-01-
Structural Angle 9540014355250 014355250 STRUCTURAL SECTION,SPECIAL SHAPED 9 FT NS Request Quotation
Structural Angle 9540014355250 014355250 STRUCTURAL SECTION,SPECIAL SHAPED 9 FT NS Request Quotation
MIL-T-81556 BEAM,STRUCTURAL 9 FT NS Request Quotation Updated Every Day 9540-01-463-0453 RQST NE
STRUCTURAL SECTION,SPECIAL SHAPED 9 FT NS Request Quotation Updated Every Day 9540-01-437 MIL-T-81556
MIL-T-81556 ANGLE,STRUCTURAL 9 FT NS Request Quotation Updated Every Day 9540-01-435-5249 RQST
Restrictions 9540-01-435-5250
9540-01-435-5250 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 9540-01-435-5250
- US Air Force (FNN5)
- Effective Date:
- 1 Jun 2003
- Former MOE Rule:
- FGKZ
Approved Sources 9540-01-435-5250
- Part Number
- Manufacturer
- Status
- CVC10001-1019GA
- Manufacturer
- 80378 - Triumph Aerostructures, Llc (Active)
- Primary Buy
- Primary Buy
- MIL-T-81556
- 81349 - Military Specifications (Active)
- Incomplete Standard
- Incomplete Standard
- CVC10001-1019GAX144
- 14153 - Defense Logistics Agency (Active)
- Secondary Buy
- Secondary Buy
Datasheet 9540-01-435-5250
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Base Flange Thickness [AJGP]
- 0.500 Inches Nominal
- Basic Shape Style [AGTA]
- Angle
- Fabrication Method [AARN]
- Extruded
- Fillet Radius Where Left Flange Joins Base Flange [AJGL]
- 0.380 Inches Nominal
- First Tip Inner Radius [CNBD]
- 0.062 Inches Nominal
- First Tip Outer Radius [CNBJ]
- 0.062 Inches Nominal
- First Tip Style [CMZY]
- Square W/ Inner And Outer Corner Radii
- Heat Treatment [HEAT]
- Annealed
- Material [MATT]
- Titanium Alloy, Mil-T-81556, Comp Ab-1
- Nondefinitive Spec/Std Data [ZZZT]
- Composition Ab-1 And Condition Annealed
- Left Inside Angle [CQHP]
- 105.0 Degrees Nominal
- Left Side Flange Thickness [ADXL]
- 0.450 Inches Nominal
- Length [ABRY]
- 12.000 Feet Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 2.000 Inches Nominal
- Overall Width [ABMK]
- 2.100 Inches Nominal
Management Data 9540-01-435-5250
- 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 9540-01-435-5250
9540-01-435-5250 has freight characteristics.. 9540-01-435-5250 has a variance between NMFC and UFC when transported by rail and the description should be consulted.