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9540-01-435-4800
Structural Angle
9540014354800 014354800 MIL-T-81556 CVC10001-1010GA CVC10001-1010GAX144
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
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Related Documents 9540-01-435-4800 5+ Documents (More...)
MIL-T-81556 ANGLE,STRUCTURAL 9 FT NS Request Quotation Updated Every Day 9540-01-435-4800 RQST NE Updated
Every Day 9540-01-435-4800 RQST Updated Every Day 9540-01-435-4800 RQST NE Related Documents 9540-01
MIL-T-81556 ANGLE,STRUCTURAL 9 FT NS Request Quotation Updated Every Day 9540-01-445-7878 RQST NE Updated
ANGLE,STRUCTURAL 9 FT NS Request Quotation Updated Every Day 9540-01-435-4800 RQST STRUCTURAL SECTION
Structural Angle 9540014354800 014354800 MIL-T-81556 ANGLE,STRUCTURAL 9 FT NS Request Quotation
Updated Every Day 9540-01-435-4800 RQST NE Updated Structural Angle 9540014355249014355249MIL-T-81556
Structural Angle 9540014354800 014354800 for $1 a day Upgrade your Account Upgrade 9540-01-435-
4800Structural Angle9540014354800 014354800 MIL-T-81556 MIL-T-81556 ANGLE,STRUCTURAL 9 FT NS Request
MIL-T-81556 ANGLE,STRUCTURAL 9 FT NS Request Quotation Updated Every Day 9540-01-440-6242 RQST
STRUCTURAL SECTION,SPECIAL SHAPED 9 FT NS Request Quotation Updated Every Day 9540-01-428 MIL-T-81556
Restrictions 9540-01-435-4800
9540-01-435-4800 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 9540-01-435-4800
- US Air Force (FNN5)
- Effective Date:
- 1 Jun 2003
- Former MOE Rule:
- FGKZ
Approved Sources 9540-01-435-4800
- Part Number
- Manufacturer
- Status
- CVC10001-1010GA
- Manufacturer
- 80378 - Triumph Aerostructures, Llc (Active)
- Primary Buy
- Primary Buy
- MIL-T-81556
- 81349 - Military Specifications (Active)
- Incomplete Standard
- Incomplete Standard
- CVC10001-1010GAX144
- 14153 - Defense Logistics Agency (Active)
- Secondary Buy
- Secondary Buy
Datasheet 9540-01-435-4800
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Base Flange Thickness [AJGP]
- 0.450 Inches Nominal
- Basic Shape Style [AGTA]
- Angle
- Fabrication Method [AARN]
- Extruded
- Fillet Radius Where Left Flange Joins Base Flange [AJGL]
- 0.250 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]
- Tatanium Alloy, Mil-T-81556, Comp Ab-1
- Nondefinitive Spec/Std Data [ZZZT]
- Composition Ab-1 And Condition Annealed
- Left Inside Angle [CQHP]
- 90.0 Degrees Nominal
- Left Side Flange Thickness [ADXL]
- 0.560 Inches Nominal
- Length [ABRY]
- 12.000 Feet Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 1.650 Inches Nominal
- Overall Width [ABMK]
- 2.000 Inches Nominal
Management Data 9540-01-435-4800
- 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 9540-01-435-4800
9540-01-435-4800 has freight characteristics.. 9540-01-435-4800 has a variance between NMFC and UFC when transported by rail and the description should be consulted.