dai rispettivi siti dei costruttori:
CFM (-5B5 per 319 320 321)
CFM56-5B1 -5B2 -5B3 -5B4 -5B5 -5B6 -5B7 -5B8 -5B9
TAKEOFF CONDITIONS (sea level)
- Max. takeoff (lb) 30,000 31,000 33,000 27,000 22,000 23,500 27,000 21,600 23,300
- Airflow (lb/sec) 943 956 968 897 818 844 897 811 841
- Bypass ratio 5.5 5.5 5.4 5.7 6.0 5.9 5.7 6.0 5.9
IN-FLIGHT PERFORMANCE (installed)
(35,000 ft-Mach=0.80-ISA)
- Max. climb thrust (lb) 6,420 6,420 6,420 5,630 5,630 5,630 6,420 5630 5630
- Overall pressure ratio at max. climb 35.4 35.4 35.5 32.6 32.6 32.6 35.5 32.6 32.6
- Max. cruise thrust (lb) 5,840 5,840 5,840 5,020 5,020 5,020 5,840 5020 5020
ENGINE CHARACTERISTICS
- Length (in) 102.4 102.4 102.4 102.4 102.4 102.4 102.4 102.4 102.4
- Fan diameter (in) 68.3 68.3 68.3 68.3 68.3 68.3 68.3 68.3 68.3
- Basic dry weight (lb) 5,250 5,250 5,250 5,250 5,250 5,250 5,250 5,250 5,250
APPLICATIONS A321 A321 A321 A320 A319 A319 A319
A319CJ A318 A318
IAE
Thrust range:
22,000 to 33,000lb thrust
Models:
V2500-A1, V2500-A5, V2500-D5
Applications:
Airbus A319, A320 and A321, Airbus Corporate Jetliner (ACJ), Boeing MD-90
Production Shares:
Pratt & Whitney
Diffuser-Combustor, High Pressure Turbine, Turbine Exhaust Case
Rolls-Royce
High Pressure Compressor & Gear Box
Japanese Aero Engines Corporation
Fan Case and Low-Pressure Compressor
MTU Aero Engines
Low-Pressure Turbine Module
Entered Into Service:
Model
Date
V2500-A1
May 1989
V2500-A5
Dec. 1993
V2500-D5
Apr. 1995
Total Order Book
(Firm and Option):
More Than 5,000 Engines
Total Engine Hours:
Over 36 Million
Total Number of Engines Delivered:
Over 2,600
By Engine
V2500-A5 - over 1,950
V2500-A1 - over 360
V2500-D5 - over 290
Number of customers:
103
le comparazioni economiche non sono facili da trovare..e anche i dati sul iae fanno schifo