IAE V2500
Specifications

IAE V2500

Section Title: Specifications
Table Section Text: None

Type	Production start	Thrust (kN)	Thrust (lbf)	Weight (kg)	Thrust / Weight	Bypass ratio	Compression ratio	Fan diameter	Total length	Aircraft type

V2500-A1	1989	110.31	25,000	2,327	4.83	5.4:1	35.8:1	62.5in (1.587m)	126in (3.2m)	Airbus A320-231

V2527-A5	1993	118.32	26,600	2,359	5.11	4.8:1	32.8:1	63.5in (1.613m)	Airbus A319-133, A320-232, A320-233

V2530-A5	130.55	29,350	5.64	4.6:1	36.2:1	Airbus A321-131, A321-232

V2525-D5	1995	111.21	25,000	2,484	4.57	4.8:1	34.5:1	McDonnell Douglas MD-90

V2528-D5	124.55	28,000	5.11	4.7:1	35.2:1

V2522-A5	1997	102.49	23,000	2,359	4.43	4.9:1	32.8:1	Airbus A319-131

V2524-A5	108.89	24,800	4.71	Airbus A319-132

V2533-A5	150	33,000	5.75	4.5:1	35.2:1	Airbus A321-231

V2531-E5	2014	139.4	31,330	2,484	5.72	4.6:1	36.2:1	Embraer KC-390

Sentence(s)

The V2500 engine was installed on the Airbus A320.

final_sentence: The V2500 engine was installed on the Airbus A320.