BMW Rolls-Royce BR715

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© Kenneth W Shanaberger 2000 - 2010

The Engine

Specifications

First flown in 1997, the BR715 is designed for the high-frequency, short-haul market.

	High-bypass turbofan
	Fan: 1-stage
	Compressor: 3-stage LP and 10-stage HP
	Turbines: 3-stage LP and 2-stage HP

Models

Used by

	BR715-A1-30: 18,500 lb (82 kN) thrust
	BR715-C1-30: 21,000 lb (93 kN) thrust

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page updated 26 February 2003