Technical data

• Two-shaft, high-bypass-ratio engines
• Both BR700 engine family members incorporate the BR700 core engine, with a ten-stage HP compressor, a single low emissions annular combustor with 20 burners and a two-stage shrouded HP turbine
• Different thrust levels of the two engines are realised by adapting the LP systems
• In the case of the BR710 the 48-inch diameter fan is driven by a two-stage LP turbine
• The BR715 features a 58-inch diameter fan and a two-stage booster driven by a three-stage LP turbine

Engine	EIS	Power	Applications	Seats	Range (nm)*
BR710	1997	15,000lb 66 kN	Gulfstream V	3-19	6500
BR710	2004	15,000lb 66 kN	Gulfstream G500	14-19	5800
BR710	2004	15,000lb 66 kN	Gulfstream G550	14-19	6750
BR710	1999	14,690lb 66 kN	Bombardier Global Express	8	6500
BR710	2001	15,500lb 69kN	BAE SYSTEMS Nimrod MRA4
BR710	2003	16, 000lb 71 kN	Tupolev Tu-334	-	120
BR715	1999	18,500 lb to 22,000 lb 82 kN to 98 kN	Boeing 717	106	2000
*Aircraft Manufacturer's Data