Model: 506959
Aircraft Gas Combustion Chamber16.135 inches overall length, acft engine j60 end item identification, agav criticality code justification, combustion chamber engine section location.
Properties:
The portion of an engine, gas turbine, aircraft in which fuel is burned. it may be an annular type in which the space between the circular inner and outer cylinders form the burning chamber or it may be the multi-arrangement can type in which separate can like burn cylinders are positioned in a circular arrangement within an inner and outer case.
Part 506959 NSN 2840-00-015-1682
Material Classification
Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicatorsPackaging & Shipping
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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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