Model: T58-GE-402
Turbo-shaft Aircraft EngineSpecial Features:
10 compressor stages
Properties:
A continuous-combustion type engine, may be with or without container, designed to use superheated air to drive a turbine rotor which is connected to the rotorshaft of a helicopter by way of reduction gears.
Part T58-GE-402 NSN 2840-01-533-0397
Material Classification
Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicatorsPricing & Availability Check
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Schedule B and Export
- Schedule B: 8411814050
- SITC: 71489
- End Use: Engines and turbines for military aircraft
- NAICS: 336412
- USDA: 1
Freight Class: Aircraft turbines (engines), except for use in civil aircraft, of a power not exceeding 5000 kw
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