BR725

Technical data

• The BR725 features a 50-inch diameter swept fan with 24 blades driven by a three-stage low-pressure turbine, for improved flow, increased efficiency, reduced noise and lower emissions.
• Ten-stage high-pressure compressor incorporates the latest aerodynamic improvements and stages of blisks for improved performance and optimized weight.
• New combustor design provides significantly lower emissions.
• The two-stage shrouded high-pressure turbine uses advanced aerodynamic design and latest material for high efficiency, enhanced performance retention and longer life.
• New high-efficiency thrust reverser system for increased reverse thrust and lower drag.
• All new composite nacelle for higher flow.

Engine	EIS	Power	Applications	Seats	Range (nm)*
BR725	2012	15-17,000 lb	Gulfstream G650	14-19	7,000
BR710 A1-10	1997	14.750lb66 kN	Gulfstream V	19	6,500
BR710 C4-11	2004	15,385lb	Gulfstream G500	19	5,800
BR710 C4-11	2004	15,385lb	Gulfstream G550	19	6,750
BR710 A2-20	1999	14,750lb	Bombardier Global Express XRS	19	6,150
BR710 A2-20	2004	14,750lb	Bombardier Global 5000	17	5,200
BR715	1999	18,500lb to21,000lb	Boeing 717	117	2,060
*Aircraft Manufacturer's Data