1650-00-715-5633
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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.
1650-00-715-5633, mounting gland assy
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