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2840-01-433-6670
Aircraft Gas Turbine Engine Turbine Rotor Blade
2840014336670 014336670 3002616-2
An item mounted on a DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It is designed to create the flow of air in the turbine section of an ENGINE, GAS TURBINE, AIRCRAFT. View more Aircraft Gas Turbine Engine Turbine Rotor Blade
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014336670,3002616-2 3002616-2 An item mounted on a DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
Restrictions 2840-01-433-6670
2840-01-433-6670 is a Aircraft Gas Turbine Engine Turbine Rotor Blade 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.
Import and Export 2840-01-433-6670
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-433-6670
- US Coast Guard (C057)
- Effective Date:
- 1 Jul 1996
Approved Sources 2840-01-433-6670
- Part Number
- Manufacturer
- Status
- 3002616-2
- Manufacturer
- 99193 - Honeywell International Inc. (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-433-6670
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- Blade Attachment Method [BGLW]
- Slot
- Design Type [APGF]
- Compressor
- Engine Section Location [CZBJ]
- Compressor
- Material Thickness [ABPX]
- 0.150 Inches Nominal
- Material [MATT]
- Steel Overall
- Overall Height [ABKW]
- 4.965 Inches Nominal
- Overall Length [ABHP]
- 1.170 Inches Nominal
- Overall Width [ABMK]
- 0.590 Inches Nominal
- Stage Number [CZCJ]
- 2
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Freight Information 2840-01-433-6670
2840-01-433-6670 has freight characteristics.. 2840-01-433-6670 has a variance between NMFC and UFC when transported by rail and the description should be consulted.