Model: 3013600
Turbo-prop Aircraft EngineSpecial Features:
Shaft horsepower at 2200 output rpm; grade jp4 or jp5 fuel
Properties:
A combustion type power unit, may be with or without container, designed to use superheated air to spin a turbine rotor attached to the propeller shaft through reduction gears.
Part 3013600 NSN 2840-00-855-6100
Material Classification
Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicatorsPackaging & Shipping
Freight Classification
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Schedule B and Export
- Schedule B: 8411214050
- SITC: 71481
- End Use: Engines and turbines for military aircraft
- NAICS: 336412
- USDA: 1
Freight Class: Turbopropeller aircraft turbines (engines) other than for civil aircraft, of a power not exceeding 1100 kw
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