Model: 109R556G21
Turbine Engine AfterburnerProperties:
A chamber in which additional fuel is injected into, the exhaust gases, and reheating the gases to develop increased thrust. It consists of combustion area, flame holders, injection nozzles and an exhaust ejector.
Part 109R556G21 NSN 2840-00-656-0167
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: 8411997050
- SITC: 71499
- End Use: Engines and turbines for military aircraft
- NAICS: 336412
- USDA: 1
Freight Class: Parts of gas turbine aircraft engines, other than for use in civil aircraft
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