Technical data

• The V2500-A5 is a two-shaft high-bypass-ratio engine
• Fan diameter 63.5 inches (1.61m)
• Four-stage LP compressor
• Ten-stage HP compressor
• Single annular combustor with 20 fuel injectors
• Two-stage HP turbine and five-stage LP turbine

Engine	EIS	Power	Applications	Seats*	Range (nm)*
Baseline engine:
V2500-A1	1989	25,000lb 111kN	Airbus A320	150	2700
V2500-A5 for Airbus:
V2500-A5	1997	22,000lb 98 kN	Airbus A319	124	1900
V2500-A5	1997	24,000lb 107 kN	Airbus A319	124	3000
V2500-A5	1993	26,500lb 118 kN	Airbus A320	150	2900
V2500-A5	1994	31,400lb 140 kN	Airbus A321	185	2250
V2500-A5	1997	33,000lb 147 kN	Airbus A321	185	2700
V2500-D5 for Boeing:
V2525-D5	1996	25,000lb 111 kN	Boeing MD-90-30	153	2045
V2528-D5	1995	28,000lb 124 kN	Boeing MD-90-30	153	2045
*Aircraft Manufacturer's Data