Model: 109R556G23
Turbine Engine AfterburnerSpecial Features:
Components include 1 nozzle, 1 duct, 4 acuators, 4 blankets, 2 manifolds, 3 shafts, 5 tubes, 1 spacer
Properties:
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 109R556G23 NSN 2840-00-133-5089
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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