Military Turbofan/Turbojet Specifications
 Civil Turbofan/Turbojet Specifications
 Military Turboshaft/Turboprop Specifications
 Civil Turboshaft/Turboprop Specifications
Home



Civil Turbojet/Turbofan Specifications
Civil Turbojet/Turbofan Specifications
(sorted by engine manufacturer)
1 2 3 4 5 6 7 8 9 10 11 12
Manufacturer Model Application(s) Thrust Thrust SFC SFC Airflow OPR FPR BPR Thrust SFC Cruise Cruise TIT Number Fan LPC HPC HPT IPT LPT Fan Length Width/ Dry Notes Refs
(dry) (wet) (dry) (wet) (static) (static) (static) (static) (cruise) (cruise) Speed Altitude Spools Stgs Stgs Stgs Stgs Stgs Stgs Diameter Diameter Weight 1 2 3 4 5 6 7 8 9 10 11 12
[lbf] [lbf] [lb/lbf hr] [lb/lbf hr] [lb/s] [lbf] [lb/lbf hr] [M] [ft] [K] [in] [in] [in] [lb]
Agilis Engines TF1000 S-26 Safire (candidate engine) 1,000 - 0.400 - 270 0.640 0.60 30,000 56.0 23.0 285 1 1 1 1 1
Agilis Engines TF1200 1,288 - 0.410 - 400 0.660 0.60 30,000 56.0 23.0 285 1 1 1 1 1
Agilis Engines TF1400 1,400 - 0.410 - 400 0.660 0.60 30,000 56.0 23.0 300 1 1 1 1 1
Agilis Engines TF1500 1,500 - 0.410 - 397 0.680 0.60 30,000 56.0 23.0 300 1 1 1 1 1
Agilis Engines TJ60 60 - 1.240 - 30 1.500 0.90 20,000 13.5 5.0 9 1 1 1 1 1
Agilis Engines TJ75 75 - 1.240 - 48 1.500 0.90 20,000 13.5 7.0 10 1 1 1 1 1
Agilis Engines TJ80 72 - 1.240 - 48 1.500 0.90 20,000 13.5 5.0 9 1 1 1 1 1
Agilis Engines TJ400 403 - 0.900 - 30.0 15.0 136 1 1 1 1 1
AlliedSignal (Honeywell) AS905 Falcon 7X (candidate engine) - -
AlliedSignal (Honeywell) AS907 Challenger 300 6,500 - 0.420 - 21.0 4.50 2 1 4B 1C 2 - 3 34.2 92.4 46.3 1,364
AlliedSignal (Honeywell) AS977-1A RJX-70/-85/-100/-115, SL-100 (not produced) 7,100 - 0.416 - 23.0 4.50 2 1 4B 1C 2 - 3 34.2 92.4 49.9 1,364 Notes
Allison (Rolls-Royce) AE3007A ERJ-135ER, ERJ-145ER 7,580 - 0.360 - 294 24.0 5.30 2 1 - 14 3 - 2 38.5 106.5 43.5 1,586 Notes 2
Allison (Rolls-Royce) AE3007A1 ERJ-135ER, ERJ-145ER 7,580 - 0.360 - 294 24.0 5.30 2 1 - 14 3 - 2 38.5 106.5 43.5 1,586 Notes 2
Allison (Rolls-Royce) AE3007A1P ERJ-145LR, Legacy Executive 7,580 - - 5.30 2 1 - 14 3 - 2 38.5 106.5 43.5 2
Allison (Rolls-Royce) AE3007A1/1 ERJ-135ER/LR, ERJ-145LR 7,580 - - 5.30 2 1 - 14 3 - 2 38.5 106.5 43.5 2
Allison (Rolls-Royce) AE3007A1/3 ERJ-135LR, ERJ-140, Legacy Corporate Shuttle 7,200 - - 5.30 2 1 - 14 3 - 2 38.5 106.5 43.5 2
Allison (Rolls-Royce) AE3007A1E ERJ-145XR 8,110 - - 2 1 - 14 3 - 2 38.5 106.5 43.5 2
Allison (Rolls-Royce) AE3007A3 ERJ-135 7,000 - - 5.30 2 1 - 14 3 - 2 38.5 106.5 43.5 2
Allison (Rolls-Royce) AE3007C Citation X 6,442 - - 5.30 2 1 - 14 3 - 2 38.5 106.5 43.5 1,586 2
Allison (Rolls-Royce) AE3007C1 Citation X 6,764 - - 5.30 2 1 - 14 3 - 2 38.5 106.5 43.5 2
Avco Lycoming ALF301 Technology demonstrator 2,730 - 0.440 - 100 9.0 5.60 2 1 - 5 + 1C 2 - 2
Avco Lycoming ALF501 Technology demonstrator 5,800 - 0.400 - 221 9.3 6.00 2 1 - 7 + 1C 2 - 2
Avco Lycoming ALF502L Challenger 600 7,500 - 0.428 - 256 13.6 5.20 2,150 0.730 0.75 30,000 2 1 2B 7 + 1C 2 - 2 65.6 50.0 1,311 Notes 2 2 1 1 1 2 2 2
Avco Lycoming ALF502L-2 Challenger 600 7,500 - 0.428 - 13.6 2 1 2B 7 + 1C 2 - 2 65.6 50.0 1,311 2 2 2 2 2 2
Avco Lycoming ALF502L-2A Challenger 600 7,500 - 0.414 - 13.8 2 1 2B 7 + 1C 2 - 2 65.6 50.0 1,311 2 2 2 2 2
Avco Lycoming ALF502L-2C Challenger 600 7,500 - 0.414 - 13.8 2 1 2B 7 + 1C 2 - 2 65.6 50.0 1,311 2 2 2 2 2
Avco Lycoming ALF502L-3 Challenger 600 7,800 - 0.415 - 13.8 5.00 2 1 2B 7 + 1C 2 - 2 65.6 50.0 1,311 2 2 2 2 2 2
Avco Lycoming ALF502R-1 2 1 1B 7 + 1C 2 - 2 63.8 50.0 1,336 2 2 2 2 2 2 2
Avco Lycoming ALF502R-2 2 1 1B 7 + 1C 2 - 2 63.8 50.0 1,336 2 2 2 2 2 2 2
Avco Lycoming ALF502R-3 BAe 146-100 6,700 - 0.411 - 11.6 5.71 2 1 1B 7 + 1C 2 - 2 63.8 50.0 1,336 2 2 2 2 2 2 2
Avco Lycoming ALF502R-3A BAe 146-100 6,970 - 0.408 - 11.6 5.71 2 1 2B 7 + 1C 2 - 2 63.8 50.0 1,336 2 2 2 2 2 2 2
Avco Lycoming ALF502R-4 2 1 1B 7 + 1C 2 - 2 63.8 50.0 1,336 2 2 2 2 2 2 2
Avco Lycoming ALF502R-5 BAe 146-100/-200/-200ER/-300 6,970 - 0.408 - 12.2 5.60 2,250 0.720 0.70 25,000 2 1 2B 7 + 1C 2 - 2 63.8 50.0 1,336 2 2 2 2 1 2 2 2
Avco Lycoming ALF502R-6 BAe 146-200/-200ER/-300 7,500 - 0.415 - 192 13.8 5.60 2 1 2B 7 + 1C 2 - 2 65.6 50.0 1,375 2 2 2 2 2 2
Avco Lycoming (Textron Lycoming) LF507-1F RJ-70/-85/-100/-115 7,000 - 0.406 - 192 13.8 5.70 2 3 7B 1C 2 - 2 40.0 58.6 41.7 1,385 Notes
Avco Lycoming (Textron Lycoming) LF507-1H RJ-70/-85/-100/-115 7,000 - - 13.8 5.70 2 3 7B 1C 2 - 2 40.0 58.6 41.7 1,375 Notes
Avco Lycoming (Textron Lycoming) LF507-1N Yak-40TL 7,000 - - 2 3 7B 1C 2 - 2 40.0 58.6 41.7 1,375
Bristol Siddeley (Rolls-Royce) Viper Mk.520 DH 125-1 3,100 - - - - 1 - - 7 1 - - - - - -
Bristol Siddeley (Rolls-Royce) Viper Mk.521 DH 125-1A/-1B/-2 3,100 - 0.990 - 53 5.6 - - 1 - - 8 1 - - - - - -
Bristol Siddeley (Rolls-Royce) Viper Mk.522 HS 125-3/-3A/-3B/-400B/-403B/-600 3,360 - 1.000 - 5.6 - - 1 - - 8 1 - - - 92.9 28.9 760 - - -
Bristol Siddeley (Rolls-Royce) Viper Mk.526 PD-808 - - - - 1 - - 8 1 - - - - - -
CFE CFE738-1-1B Falcon 2000 5,725 - 0.372 - 210 23.0 1.70 5.30 1,464 0.645 0.80 40,000 2 1 - 5 + 1C 2 - 3 35.5 99.0 48.0 1,325 Notes 1 1 2 1 2 1 1 1 1 1 1
CFM CFM56-2A2 (see military turbofan specifications) - -
CFM CFM56-2A3 (see military turbofan specifications) - -
CFM CFM56-2B1 (see military turbofan specifications) - -
CFM CFM56-2C1 DC-8-71F/-72/-72F/-73F, DC-8-71/-73 (option) 22,000 - 0.350 - 788 24.7 6.00 4,980 0.671 0.80 35,000 2 1 3B 9 1 - 4 68.3 95.7 72.0 4,635 Notes 1 1 1 1 1 1 1 1 1 1
CFM CFM56-2C2 Trident 24,000 - 0.360 - 26.5 2 1 3B 9 1 - 4 68.3 95.7 72.0 1 1 1 1 1 1
CFM CFM56-2C3 DC-8-71/-71F/-72/-72F/-73/-73F (option) - - 2 1 3B 9 1 - 4 68.3 95.7 72.0 4,635
CFM CFM56-2C5 DC-8-72, DC-8-71/-71F/-72F/-73/-73F (option) - - 2 1 3B 9 1 - 4 68.3 95.7 72.0 4,635
CFM CFM56-2C6 DC-8-71/-71F/-72/-72F/-73/-73F (option) - - 2 1 3B 9 1 - 4 68.3 95.7 72.0 4,635
CFM CFM56-3B1 737-300/-300(QC)/-500, 737-400 (option) 20,000 - 0.380 - 655 22.6 6.00 4,650 0.667 0.80 35,000 2 1 3B 9 1 - 4 60.0 93.1 63.0 4,276 Notes 1 1 1 1 1 1 1 1 1 1
CFM CFM56-3B2 737-300/-300(QC)/-300F/-400 22,000 - 0.390 - 683 24.3 5.90 5,040 0.667 0.80 35,000 2 1 3B 9 1 - 4 60.0 93.1 63.0 4,301 1 1 1 1 1 1 1 1 1 1
CFM CFM56-3C1 737-300/-300(QC)/-300F/-400/-500 23,500 - 0.330 - 710 25.7 6.00 5,370 0.667 0.80 35,000 2 1 3B 9 1 - 4 60.0 93.1 63.0 4,301 1 1 1 1 1 1 1 1 1 1
CFM CFM56-3C3 737-300, 737-300(QC)/-300F/-400/-500 (option) - - 2 1 3B 9 1 - 4 60.0 93.1 63.0
CFM CFM56-5A1 A320-211/-311 25,000 - 0.330 - 852 26.5 6.00 5,000 0.596 0.80 35,000 2 1 3B 9 1 - 4 68.3 95.4 72.0 4,995 Notes 1 1 1 1 1 1 1 1 1 1
CFM CFM56-5A3 A320-212 26,500 - 0.330 - 876 27.8 6.00 5,000 0.596 0.80 35,000 2 1 3B 9 1 - 4 68.3 95.4 72.0 4,995 1 1 1 1 1 1 1 1 1 1
CFM CFM56-5A4 A319-113 22,000 - 0.320 - 816 24.1 6.20 5,000 0.80 35,000 2 1 3B 9 1 - 4 68.3 95.4 72.0 4,975 1 1 1 1 1 1 1 1 1 1
CFM CFM56-5A5 A319-114 23,500 - 0.320 - 842 25.4 6.20 5,000 0.80 35,000 2 1 3B 9 1 - 4 68.3 95.4 72.0 4,975 1 1 1 1 1 1 1 1 1 1
CFM CFM56-5B1 A321-111 30,000 - 0.350 - 943 32.0 5.50 5,840 0.596 0.80 35,000 2 1 4B 9 1 - 4 68.3 102.4 72.0 5,250 1 1 1 1 1 1 1 1 1 1
CFM CFM56-5B1/P A321-111 30,000 - 0.350 - 943 32.0 5.50 2 1 4B 9 1 - 4 68.3 102.4 72.0 5,250 1 1 1 1 1 1 1 1 1
CFM CFM56-5B1/2 A321-111 30,000 - 0.350 - 943 32.0 5.50 2 1 4B 9 1 - 4 68.3 102.4 72.0 5,250 1 1 1 1 1 1 1 1 1
CFM CFM56-5B1/2P - - 2 1 4B 9 1 - 4 68.3 102.4 72.0 5,250
CFM CFM56-5B2 A321-112 31,000 - 0.350 - 956 32.9 5.50 5,840 0.545 0.80 35,000 2 1 4B 9 1 - 4 68.3 102.4 72.0 5,250 1 1 1 1 1 1 1 1 1 1
CFM CFM56-5B2/P A321-112 31,000 - 0.350 - 956 32.9 5.50 2 1 4B 9 1 - 4 68.3 102.4 72.0 5,250 1 1 1 1 1 1 1 1 1 1
CFM CFM56-5B2/2 - - 2 1 4B 9 1 - 4 68.3 102.4 72.0 5,250
CFM CFM56-5B2/2P - - 2 1 4B 9 1 - 4 68.3 102.4 72.0 5,250
CFM CFM56-5B3 A321-211 32,000 - 0.360 - 956 33.7 5.40 5,840 0.80 35,000 2 1 4B 9 1 - 4 68.3 102.4 72.0 5,250 1 1 1 1 1 1 1 1 1 1
CFM CFM56-5B3/P A321-211 32,000 - 0.360 - 956 33.7 5.40 2 1 4B 9 1 - 4 68.3 102.4 72.0 5,250 1 1 1 1 1 1 1 1 1 1
CFM CFM56-5B3/2P A321-211 32,000 - 0.360 - 33.7 2 1 4B 9 1 - 4 68.3 102.4 72.0 5,250 1 1 1 1 1 1 1
CFM CFM56-5B4 A320-214 27,000 - 0.340 - 897 29.1 5.70 5,000 0.545 0.80 35,000 2 1 4B 9 1 - 4 68.3 102.4 72.0 5,250 1 1 1 1 1 1 1 1 1 1
CFM CFM56-5B4/P A320-214 27,000 - 0.340 - 897 29.1 5.70 2 1 4B 9 1 - 4 68.3 102.4 72.0 5,250 1 1 1 1 1 1 1 1 1
CFM CFM56-5B4/2 A320-214 27,000 - 0.340 - 897 29.1 5.70 2 1 4B 9 1 - 4 68.3 102.4 72.0 5,250 1 1 1 1 1 1 1 1 1
CFM CFM56-5B4/2P A320-214 27,000 - 0.340 - 897 29.1 5.70 2 1 4B 9 1 - 4 68.3 102.4 72.0 5,250 1 1 1 1 1 1 1 1 1
CFM CFM56-5B5 A319-111 22,000 - 0.320 - 818 24.4 6.00 2 1 4B 9 1 - 4 68.3 102.4 72.0 5,250 1 1 1 1 1 1 1 1 1
CFM CFM56-5B5/P A319-111 22,000 - 0.320 - 818 24.4 6.00 2 1 4B 9 1 - 4 68.3 102.4 72.0 5,250 1 1 1 1 1 1 1 1 1
CFM CFM56-5B6 A319-112 23,500 - 0.330 - 844 25.8 5.90 2 1 4B 9 1 - 4 68.3 102.4 72.0 5,250 1 1 1 1 1 1 1 1 1
CFM CFM56-5B6/P A319-112 23,500 - 0.330 - 844 25.8 5.90 2 1 4B 9 1 - 4 68.3 102.4 72.0 5,250 1 1 1 1 1 1 1 1 1
CFM CFM56-5B6/2 A319-112 23,500 - 0.330 - 844 25.8 5.90 2 1 4B 9 1 - 4 68.3 102.4 72.0 5,250 1 1 1 1 1 1 1 1 1
CFM CFM56-5B6/2P A319-112 23,500 - 0.330 - 844 25.8 5.90 2 1 4B 9 1 - 4 68.3 102.4 72.0 5,250 1 1 1 1 1 1 1 1 1
CFM CFM56-5B7 - - 2 1 4B 9 1 - 4 68.3 102.4 72.0 5,250
CFM CFM56-5B7/P A319-115/-115CJ/-115XCJ 27,000 - 0.340 - 29.1 2 1 4B 9 1 - 4 68.3 102.4 72.0 5,250 1 1 1 1 1 1
CFM CFM56-5B8/P A318-111 29,000 - - 2 1 4B 9 1 - 4 68.3 102.4 72.0 5,250 1 1 1 1
CFM CFM56-5B9/P A318-112 29,000 - - 2 1 4B 9 1 - 4 68.3 102.4 72.0 5,250 1 1 1 1 1
CFM CFM56-5C2 A340-211/-311 31,200 - 0.320 - 1027 31.5 6.60 6,915 0.545 0.80 35,000 2 1 4B 9 1 - 5 72.3 103.0 76.6 5,700 Notes 1 1 1 1 1 1 1 1 1 1
CFM CFM56-5C2/4 - - 2 1 4B 9 1 - 5 72.3 103.0 76.6
CFM CFM56-5C2/F - - 2 1 4B 9 1 - 5 72.3 103.0 76.6
CFM CFM56-5C2/F4 - - 2 1 4B 9 1 - 5 72.3 103.0 76.6
CFM CFM56-5C2/G - - 2 1 4B 9 1 - 5 72.3 103.0 76.6
CFM CFM56-5C2/G4 - - 2 1 4B 9 1 - 5 72.3 103.0 76.6
CFM CFM56-5C3 A340-212/-312 32,500 - 0.320 - 1045 32.6 6.50 6,910 0.545 0.80 35,000 2 1 4B 9 1 - 5 72.3 103.0 76.6 5,700 1 1 1 1 1 1 1 1 1 1
CFM CFM56-5C3/F A340-312 32,500 - 0.320 - 1045 32.6 6.50 2 1 4B 9 1 - 5 72.3 103.0 76.6 5,700 1 1 1 1 1 1 1 1 1
CFM CFM56-5C3/F4 - - 2 1 4B 9 1 - 5 72.3 103.0 76.6
CFM CFM56-5C3/G - - 2 1 4B 9 1 - 5 72.3 103.0 76.6
CFM CFM56-5C3/G4 - - 2 1 4B 9 1 - 5 72.3 103.0 76.6
CFM CFM56-5C4 A340-213/-213X/-313/-313X 34,000 - 0.330 - 1065 33.9 6.40 7,100 0.545 0.80 35,000 2 1 4B 9 1 - 5 72.3 103.0 76.6 5,700 1 1 1 1 1 1 1 1 1 1
CFM CFM56-5C4/1 - - 2 1 4B 9 1 - 5 72.3 103.0 76.6
CFM CFM56-7B18 737-600 (option) 18,500 - 0.350 - 667 21.7 5.60 5,420 0.80 35,000 2 1 3B 9 1 - 4 61.0 98.9 65.0 5,216 1 1 1 1 1 1 1 1 1 1
CFM CFM56-7B20 737-600/-700 20,600 - 0.360 - 686 22.7 5.60 5,450 0.633 0.80 35,000 2 1 3B 9 1 - 4 61.0 98.9 65.0 5,216 1 1 1 1 1 1 1 1 1 1
CFM CFM56-7B20/2 - - 2 1 3B 9 1 - 4 61.0 98.9 65.0 5,216 1 1 1 1 1 1 1 1 1 1
CFM CFM56-7B22 737-600/-700/-700BBJ/-800/-800BBJ2 22,000 - - 726 24.6 5.40 5,450 0.80 35,000 2 1 3B 9 1 - 4 61.0 98.9 65.0 5,216 1 1 1 1 1 1 1 1 1 1
CFM CFM56-7B22/2 - - 2 1 3B 9 1 - 4 61.0 98.9 65.0 5,216 1 1 1 1 1 1 1 1 1 1
CFM CFM56-7B22/B1 - - 2 1 3B 9 1 - 4 61.0 98.9 65.0 5,216 1 1 1 1 1 1 1 1 1 1
CFM CFM56-7B24 737-700/-800/-900, 737-700BBJ/-800BBJ2 (option) 24,000 - 0.370 - 754 26.0 5.30 5,480 0.627 0.80 35,000 2 1 3B 9 1 - 4 61.0 98.9 65.0 5,216 1 1 1 1 1 1 1 1 1 1
CFM CFM56-7B24/2 - - 2 1 3B 9 1 - 4 61.0 98.9 65.0 5,216 1 1 1 1 1 1 1 1 1 1
CFM CFM56-7B24/B1 - - 2 1 3B 9 1 - 4 61.0 98.9 65.0 5,216 1 1 1 1 1 1 1 1 1 1
CFM CFM56-7B26 737-700/-700BBJ/-800/-800BBJ2/-900 26,400 - 0.380 - 783 27.9 5.10 5,480 0.80 35,000 2 1 3B 9 1 - 4 61.0 98.9 65.0 5,216 1 1 1 1 1 1 1 1 1 1
CFM CFM56-7B26/2 - - 2 1 3B 9 1 - 4 61.0 98.9 65.0 5,216 1 1 1 1 1 1 1 1 1 1
CFM CFM56-7B26/B1 - - 2 1 3B 9 1 - 4 61.0 98.9 65.0 5,216 1 1 1 1 1 1 1 1 1 1
CFM CFM56-7B27 737-600/-800, 737-700/-900 (option) 27,300 - 0.380 - 28.9 2 1 3B 9 1 - 4 61.0 98.9 65.0 5,216 1 1 1 1 1 1 1
CFM CFM56-7B27/2 - - 2 1 3B 9 1 - 4 61.0 98.9 65.0 5,216 1 1 1 1 1 1 1 1 1 1
CFM CFM56-7B27/B1 - - 2 1 3B 9 1 - 4 61.0 98.9 65.0 5,216 1 1 1 1 1 1 1 1 1 1
CFM CFM56-7B27/B3 - - 2 1 3B 9 1 - 4 61.0 98.9 65.0 5,216 1 1 1 1 1 1 1 1 1 1
CFM CFM56-9 A316/A317 (A31X), BRJ-X, AE-100, N-2130 (not produced) 20,000 - 0.380 - 23.2 2 1 2B 9 1 - 3 91.7 56.0 4,252 1 1 1 1 1 1
de Havilland Ghost 50 Mk.1 Comet 1 5,000 - -
de Havilland Ghost 50 Mk.2 Comet 1A 5,020 - -
Engine Alliance GP7168 747-500X/-600X (not produced) 68,000 - - 2000 42.3 7.00 2 1 3B 9 2 - 4 169.0 99.0 11,500 Notes 1 1 1 1 1 1 1
Engine Alliance GP7172 767-400ERX, (not produced) 71,000 - - 2 1 3B 9 2 - 4 1 1
Engine Alliance GP7268 (cancelled) 68,000 - - 46.0 8.00 2 1 5B 9 2 - 6 1 1 1 1
Engine Alliance GP7270 A380-861 70,000 - - 45.6 8.70 12,633 0.85 35,000 2 1 5B 9 2 - 6 116.0 187.1 124.0 1 1 1 1 1 1
Engine Alliance GP7277 A380-863F 77,000 - - 2600 45.6 8.70 13,700 0.85 35,000 2 1 5B 9 2 - 6 116.0 187.1 124.0 13,300 1 1 1 1 1 1 1
Garrett ATF3 Sabreliner 60, HFB 330 4,050 - 0.440 - 140 17.0 3.00 3 1 5 1C 1 3 2 Notes
Garrett ATF3-6A Falcon 200 5,200 - - 162 21.3 2.80 3 1 5 1C 1 3 2 102.0 33.6 1,125
Garrett TFE731-2 Falcon 10, Learjet 31/31A, SA-28T 3,500 - 0.504 - 113 13.0 1.54 2.66 755 0.815 0.80 40,000 2 1G 1C 4 1 - 3 28.2 49.7 39.4 743 Notes 1 1 1 1 1 1 2 1 1 1 1
Garrett TFE731-2-2B Learjet 35/36 3,500 - 0.504 - 113 13.0 1.54 2.66 2 1G 1C 4 1 - 3 28.2 49.7 39.4 743 Notes 1 1 1 1 1 1 1 1 1 1
Garrett TFE731-2-2N IA 63 NGA - - 2 1G 1C 4 1 - 3 28.2 49.7 39.4
Garrett TFE731-2A-2A K-8E - - 2 1G 1C 4 1 - 3 28.2 49.7 39.4
Garrett TFE731-2C - - 2 1G 1C 4 1 - 3 28.2 49.7 39.4
Garrett TFE731-3 JetStar II 3,700 - 0.511 - 118 14.6 2.80 2.80 817 0.819 0.80 40,000 2 1G 1C 4 1 - 3 28.2 49.7 39.4 754 1 1 1 1 1 1 1 1 1 1 1
Garrett TFE731-3-1D Sabreliner 65 3,700 - - 118 14.6 2.80 2.80 2 1G 1C 4 1 - 3 28.2 49.7 39.4 754 1 1 1 1 1 1 1 1 1
Garrett TFE731-3-1G 1124 Westwind 3,700 - - 118 14.6 2.80 2.80 2 1G 1C 4 1 - 3 28.2 49.7 39.4 754 1 1 1 1 1 1 1 1 1
Garrett TFE731-3-1H BAe HS 125-600F/-700B 3,700 - - 118 14.6 2.80 2.80 2 1G 1C 4 1 - 3 28.2 49.7 39.4 754 1 1 1 1 1 1 1 1 1
Garrett TFE731-3-100S Citation III 3,650 - - 118 14.6 2.80 2.80 2 1G 1C 4 1 - 3 28.2 49.7 39.4 769 1 1 1 1 1 1 1 1 1
Garrett TFE731-3A-2B Learjet 55B/55C/55C-LR 3,650 - 0.515 - 118 14.6 2.80 2.80 838 0.823 0.80 40,000 2 1G 1C 4 1 - 3 28.2 49.7 39.4 775 1 1 1 1 1 1 2 1 1 1 1
Garrett TFE731-3A-300G Astra, Astra SP 3,650 - - 118 14.6 2.80 2.80 2 1G 1C 4 1 - 3 28.2 49.7 39.4 775 1 1 1 1 1 1 1 1 1
Garrett TFE731-3AR - - 2 1G 1C 4 1 - 3 28.2 49.7 39.4
Garrett TFE731-3B-100 Citation VI 3,650 - 0.507 - 118 14.4 2.80 2.80 844 0.816 0.80 40,000 2 1G 1C 4 1 - 3 28.2 49.7 39.4 750 1 1 1 1 1 1 2 1 1 1 1
Garrett TFE731-3BR - - 2 1G 1C 4 1 - 3 28.2 49.7 39.4
Garrett TFE731-3C - - 2 1G 1C 4 1 - 3 28.2 49.7 39.4
Garrett TFE731-3CR - - 2 1G 1C 4 1 - 3 28.2 49.7 39.4
Garrett TFE731-3D - - 2 1G 1C 4 1 - 3 28.2 49.7 39.4
Garrett TFE731-3DR - - 2 1G 1C 4 1 - 3 28.2 49.7 39.4
Garrett TFE731-3R - - 2 1G 1C 4 1 - 3 28.2 49.7 39.4
Garrett TFE731-4 Citation VII, Citation IV (not produced) 4,080 - 0.517 - 14.8 2.40 929 0.796 0.80 40,000 2 1G 1C 4 1 - 3 28.2 51.0 39.4 822 1 1 1 1 2 1 1 1 1
Garrett TFE731-5 BAe HS 125-800, Sabreliner 85 4,304 - 0.484 - 143 14.4 3.48 3.65 955 0.802 0.80 40,000 2 1G 1C 4 1 - 3 29.7 54.7 40.5 852 1 1 1 1 1 1 1 1 1 1 1
Garrett TFE731-5A - - 2 1G 1C 4 1 - 3
Garrett TFE731-5AR Falcon 900, Falcon 20RE 4,500 - 0.469 - 143 14.6 3.48 3.65 986 0.771 0.80 40,000 2 1G 1C 4 1 - 3 29.7 80.8 40.5 884 1 1 1 1 1 1 1 1 1 1 1
Garrett TFE731-5B - - 2 1G 1C 4 1 - 3
Garrett (Allied-Signal) TFE731-5BR Falcon 900B, Falcon 20RE, Hawker 800XP 4,750 - 0.470 - 143 15.1 3.48 3.50 1,052 0.756 0.80 40,000 2 1G 1C 4 1 - 3 29.7 80.8 40.5 899 1 1 1 1 1 1 2 1 1 1 1
Garrett (Honeywell) TFE731-5BR-1C Falcon 900C 4,750 - - 2 1G 1C 4 1 - 3 29.7 80.8 40.5 899 1 1 1 1 1
Garrett TFE731-5R - - 2 1G 1C 4 1 - 3
Garrett (AlliedSignal) TFE731-20 Learjet 45 3,500 - 0.441 - 123 21.0 3.70 3.10 876 0.728 0.80 40,000 2 1G 1C 4 1 - 3 28.2 51.0 39.4 885 1 1 1 1 1 1 2 1 1 1 1
Garrett (Honeywell) TFE731-20AR Learjet 40 3,500 - - 2 1G 1C 4 1 - 3 28.2 51.0 39.4 1 1 1 1
Garrett (Honeywell) TFE731-20BR Learjet 40XR/45XR 3,500 - - 2 1G 1C 4 1 - 3 28.2 51.0 39.4 1 1 1 1
Garrett (AlliedSignal) TFE731-20R - - 2 1G 1C 4 1 - 3 28.2 51.0 39.4
Garrett (AlliedSignal) TFE731-40 Falcon 50EX, Hawker 450 4,250 - 0.457 - 145 22.0 2.90 2 1G 1C 4 1 - 3 28.2 51.0 39.4 885 1 1 1 1 1 1 1 1 1
Garrett (AlliedSignal) TFE731-40R G100 (Astra SP), G150 (Astra SPX), IA 63 NGB 4,250 - - 2 1G 1C 4 1 - 3 28.2 51.0 39.4 1 1 1 1
Garrett (Honeywell) TFE731-40AR-200G G150 4,420 - - 2 1G 1C 4 1 - 3 28.2 51.0 39.4 1 1 1 1
Garrett (AlliedSignal) TFE731-60 Falcon 900EX 5,000 - 0.405 - 187 22.0 3.90 2 1G 1C 4 1 - 3 30.7 72.0 42.4 988 1 1 1 1 1 1 1 1 1
GE CF6-6 DC-10-10 (option) 40,000 - - 1343 26.6 1.64 6.20 2 1 1B 16 2 - 5 172.5 92.0 7,350 Notes 1 1 1 1 1 1 1 1
GE CF6-6D DC-10-10/-10F/-10F(CF) 40,000 - 0.354 - 1303 24.3 5.72 9,080 0.646 0.80 35,000 2 1 1B 16 2 - 5 86.4 188.0** 105.0 7,896 Notes 1 1 1 1 1 1 1 1 1 1
GE CF6-6D1 DC-10-10/-10F/-10F(AF) 41,500 - 0.350 - 1328 25.2 5.76 9,220 0.646 0.80 35,000 2 1 1B 16 2 - 5 86.4 188.0** 105.0 7,896 1 1 1 1 1 1 1 1 1 1
GE CF6-6D1A DC-10-10/-10F/-10F(AF) 41,500 - 0.350 - 1328 25.2 5.76 9,220 0.646 0.80 35,000 2 1 1B 16 2 - 5 86.4 188.0** 105.0 7,896 1 1 1 1 1 1 1 1 1 1
GE CF6-6E DC-10-10/-10F (option) 40,600 - - 2 1 1B 16 2 - 5 86.4 1 1
GE CF6-6F DC-10-10/-10F (option) 42,000 - - 2 1 1B 16 2 - 5 86.4 1 1
GE CF6-6K DC-10-10/-10F 41,500 - 0.346 - 25.0 2 1 1B 16 2 - 5 86.4 188.0** 105.0 8,176 1 1 1 1 1 1 1
GE CF6-6K2 DC-10-10/-10F (option) 41,500 - 0.346 - 25.0 2 1 1B 16 2 - 5 86.4 188.0** 105.0 8,176 1 1 1 1 1 1 1
GE CF6-45A 747-100SR/-100SR(SF) 46,500 - - 1393 26.3 4.64 11,250 0.630 0.80 35,000 2 1 3B 14 2 - 4 86.4 188.0** 105.0 8,768 1 1 1 1 1 1 1 1 1
GE CF6-45A2 747-100SR/-100SR(SF) 46,500 - - 1393 26.3 4.64 11,250 0.630 0.80 35,000 2 1 3B 14 2 - 4 86.4 188.0** 105.0 8,768 1 1 1 1 1 1 1 1 1
GE CF6-45B 747-100SR/-100SR(SF) 46,500 - - 1393 26.3 4.64 11,250 0.630 0.80 35,000 2 1 3B 14 2 - 4 86.4 188.0** 105.0 8,768 1 1 1 1 1 1 1 1 1
GE CF6-45B2 747-100SR/-100SR(SF), A300B10 (A310) (candidate engine) 46,500 - - 1393 26.3 4.64 11,250 0.630 0.80 35,000 2 1 3B 14 2 - 4 86.4 188.0** 105.0 8,768 1 1 1 1 1 1 1 1 1
GE CF6-50 DC-10-30/-30F 49,000 - - 0.645 0.80 35,000 2 1 3B 14 2 - 4 92.0 8,100 1 1 1 1 1
GE CF6-50A DC-10-30/-30F, A300B1, A300B2-1A 49,000 - 0.389 - 1444 28.6 1.69 4.40 0.654 0.80 35,000 2 1 3B 14 2 - 4 86.4 183.0** 92.0 8,201 Notes 1 1 1 1 1 1 1 1 1 1 1
GE CF6-50B 49,000 - 0.389 - 1444 28.6 1.69 4.40 0.654 0.80 35,000 2 1 3B 14 2 - 4 86.4 183.0** 92.0 8,201 1 1 1 1 1 1 1 1 1 1 1
GE CF6-50C A300B1, A300B2-1C/-101, A300B4-2C/-203, DC-10-30/-30CF/-30F 51,000 - 0.394 - 1451 29.3 4.26 11,100 0.657 0.80 35,000 2 1 3B 14 2 - 4 86.4 183.0** 105.0 8,721 1 1 1 1 1 1 1 1 1 1
GE CF6-50C1 DC-10-30, A300B2-202, A300B4-102 52,500 - 0.371 - 1470 30.1 4.24 11,555 0.657 0.80 35,000 2 1 3B 14 2 - 4 86.4 183.0** 105.0 8,721 1 1 1 1 1 1 1 1 1 1
GE CF6-50C2 A300B2-203, A300B4-103/-103F/-2C/-203/-203F, A300C4-203, A300F4-203, DC-10-30/-30F/-30F(CF), A300B1 (option) 52,500 - 0.371 - 1476 30.4 4.31 11,555 0.630 0.80 35,000 2 1 3B 14 2 - 4 86.4 183.0** 105.0 8,731 Notes 1 1 1 1 1 1 1 1 1 1
GE CF6-50C2B DC-10-30/-30ER 54,000 - 0.385 - 1504 31.1 4.25 11,555 0.630 0.80 35,000 2 1 3B 14 2 - 4 86.4 183.0** 105.0 8,731 1 1 1 1 1 1 1 1 1 1
GE CF6-50C2F DC-10-15 46,500 - - 1393 26.3 4.64 11,555 0.630 0.80 35,000 2 1 3B 14 2 - 4 86.4 183.0** 105.0 8,731 1 1 1 1 1 1
GE CF6-50C2R A300B2-1C/-101, A300B2K-3C, A300B4-2C, DC-10-30 51,500 - 0.368 - 29.2 2 1 3B 14 2 - 4 86.4 183.0** 105.0 8,731 1 1 1 1 1 1 1 1 1
GE CF6-50D DC-10-10 51,000 2 1 3B 14 2 - 4 86.4 183.0** 105.0 8,325 1 1 1 1
GE CF6-50D1 (see military turbofan specifications)
GE CF6-50E 747-200B 52,500 - 0.376 - 1470 30.1 4.24 11,555 0.657 0.80 35,000 2 1 3B 14 2 - 4 86.4 183.0** 105.0 8,490 1 1 1 1 1 1 1 1 1 1
GE CF6-50E1 747-200B 52,500 - 0.371 - 1470 30.1 4.24 11,555 0.657 0.80 35,000 2 1 3B 14 2 - 4 86.4 183.0** 105.0 8,490 1 1 1 1 1 1 1 1 1 1
GE CF6-50E2 747-200B/-200B(M)/-200B(SF)/-200C(M)/-200F/-300/-300(M)/-300(SF) 52,500 - 0.371 - 1476 30.4 4.31 11,555 0.630 0.80 35,000 2 1 3B 14 2 - 4 86.4 183.0** 105.0 8,768 1 1 1 1 1 1 1 1 1 1
GE CF6-50E2B 747-200/-300 (option) 54,000 - 0.375 - 1504 30.9 4.24 11,730 0.630 0.80 35,000 2 1 3B 14 2 - 4 86.4 183.0** 105.0 8,768 1 1 1 1 1 1 1 1 1 1
GE CF6-80A 767-200/-200ER/-200PC 48,000 - 0.344 - 1435 27.3 4.66 11,045 0.623 0.80 35,000 2 1 3B 14 2 - 4 86.4 157.4 98.0 8,496 Notes 1 1 1 1 1 1 1 1 1 1
GE CF6-80A1 767-200/-200ER (option) 48,000 - 0.344 - 1435 27.3 4.66 11,045 0.623 0.80 35,000 2 1 3B 14 2 - 4 86.4 157.4 98.0 8,420 1 1 1 1 1 1 1 1 1 1
GE CF6-80A2 767-200/-200ER/-300 50,000 - 0.349 - 1460 28.4 1.70 4.59 11,045 0.623 0.80 35,000 2 1 3B 14 2 - 4 86.4 157.4 98.0 8,496 1 1 1 1 1 1 1 1 1 1 1
GE CF6-80A3 A310-203/-203F 50,000 - 0.357 - 1460 28.4 1.70 4.59 11,045 0.623 0.80 35,000 2 1 3B 14 2 - 4 86.4 157.4 98.0 8,420 1 1 1 1 1 1 1 1 1 1 1
GE CF6-80C2 767-200ER/-300 (option) 52,500 - 0.329 - 1769 30.4 5.20 11,330 0.85 35,000 2 1 4B 14 2 - 5 93.0 160.9 9,135 Notes 1 1 1 1 1 2 1 1 1 1
GE CF6-80C2A1 A300B4-601 59,000 - 0.334 - 1754 30.4 5.15 11,810 0.576 0.80 35,000 2 1 4B 14 2 - 5 93.0 160.9 106.0 9,360 1 1 1 1 1 1 1 1 1 1
GE CF6-80C2A2 A310-204/-304/-304ET/-304F 52,460 - 0.317 - 1769 30.4 1.66 5.05 11,330 0.578 0.80 35,000 2 1 4B 14 2 - 5 93.0 160.9 106.0 9,360 1 1 1 1 1 1 1 1 1 1 1
GE CF6-80C2A3 A300B4-603, MD-11 (option) 58,950 - 0.329 - 1769 30.4 1.73 5.05 11,340 0.576 0.80 35,000 2 1 4B 14 2 - 5 93.0 160.9 106.0 9,360 1 1 1 1 1 1 1 1 1 1 1
GE CF6-80C2A5 A300B4-605R, A300C4-605R, A300F4-605R 60,100 - 0.340 - 31.5 5.05 2 1 4B 14 2 - 5 93.0 160.9 106.0 9,389 1 1 1 1 1 1 1 1
GE CF6-80C2A5F A300B4-605R, A300C4-605R, A300F4-605R 60,100 - 0.340 - 31.5 5.05 2 1 4B 14 2 - 5 93.0 160.9 106.0 9,389 1 1 1 1 1 1 1 1
GE CF6-80C2A6 64,000 - - 2 1 4B 14 2 - 5 1 1
GE CF6-80C2A6F 63,000 - - 2 1 4B 14 2 - 5 1 1
GE CF6-80C2A7 A310-308, A310-308ET (option) 59,000 - - 2 1 4B 14 2 - 5 93.0 160.9 106.0 9,389 1 1 1 1 1 1 1 1 1
GE CF6-80C2A8 A300B4-608ST, A310-308/-308ET 59,000 - 0.344 - 1769 30.4 5.05 2 1 4B 14 2 - 5 93.0 160.9 106.0 9,389 1 1 1 1 1 1 1 1 1
GE CF6-80C2B1 747-300/-300(M) 56,700 - 0.323 - 1710 30.4 5.19 12,820 0.576 0.80 35,000 2 1 4B 14 2 - 5 93.0 160.9 106.0 9,388 1 1 1 1 1 1 1 1 1 1
GE CF6-80C2B1F 747-400/-400D/-400ER/-400(M)/-400F 57,160 - 0.316 - 1764 30.4 5.15 12,820 0.564 0.80 35,000 2 1 4B 14 2 - 5 93.0 160.9 106.0 9,499 1 1 1 1 1 1 1 1 1 1
GE CF6-80C2B1F2 747-400/-400D/-400ER/-400(M)/-400F 57,900 - - 2 1 4B 14 2 - 5 93.0 160.9 106.0 9,499 1 1 1 1 1
GE CF6-80C2B2 767-200ER/-300/-300ER, 737-200 (option) 51,590 - 0.318 - 1650 30.4 5.31 12,000 0.576 0.80 35,000 2 1 4B 14 2 - 5 93.0 160.9 106.0 9,388 1 1 1 1 1 1 1 1 1 1
GE CF6-80C2B2F 767-200/-200ER/-300, 767-300ER (option) 52,010 - - 2 1 4B 14 2 - 5 93.0 160.9 106.0 9,499 1 1 1 1 1
GE CF6-80C2B2F2 767-200/-200ER/-300, 767-300ER (option) - - 2 1 4B 14 2 - 5 93.0 160.9 106.0 9,499 1 1 1 1 1
GE CF6-80C2B3 747-300/-400 (option) 52,010 - - 2 1 4B 14 2 - 5 93.0 160.9 106.0 9,388 1 1 1 1
GE CF6-80C2B3F 747-300/-400 (option) 52,010 - - 2 1 4B 14 2 - 5 93.0 160.9 106.0 9,499 1 1 1 1 1
GE CF6-80C2B4 767-200ER/-300/-300ER 57,180 - 0.326 - 29.9 5.15 2 1 4B 14 2 - 5 93.0 160.9 106.0 9,399 1 1 1 1 1 1 1 1
GE CF6-80C2B4F 767-200ER/-300/-300ER 57,280 - 0.317 - 29.9 5.14 2 1 4B 14 2 - 5 93.0 160.9 106.0 9,760 1 1 1 1 1 1 1 1
GE CF6-80C2B5F 747-400/-400ER/-400F/-400FER 62,100 - 0.323 - 31.4 2 1 4B 14 2 - 5 93.0 160.9 106.0 9,760 1 1 1 1 1 1 1
GE CF6-80C2B6 767-300/-300ER, 767-200ER (option), An-218-200/-300 (proposed) 60,070 - 0.334 - 31.1 5.06 2 1 4B 14 2 - 5 93.0 160.9 106.0 9,670 1 1 1 1 1 1 1 1
GE CF6-80C2B6F 767-300ER, 767-200ER (option) 60,030 - 0.323 - 31.4 5.06 2 1 4B 14 2 - 5 93.0 160.9 106.0 9,760 1 1 1 1 1 1 1 1
GE CF6-80C2B6FA 767-200ER 60,030 - 0.323 - 31.4 2 1 4B 14 2 - 5 93.0 160.9 106.0 9,760 1 1 1 1 1 1 1
GE CF6-80C2B7F 767-300ER/-300F, 767-200ER (option) 62,100 - 0.323 - 31.4 2 1 4B 14 2 - 5 93.0 160.9 106.0 9,760 1 1 1 1 1 1 1
GE CF6-80C2B8F 767-400ER/-400FER 63,500 - - 31.4 2 1 4B 14 2 - 5 93.0 160.9 106.0 9,970 1 1 1 1 1 1
GE CF6-80C2B9F 747-400XQLR/-XQLRF 63,300 - - 31.4 2 1 4B 14 2 - 5 93.0 160.9 106.0 1 1 1 1 1
GE CF6-80C2B10F 747-XQLRF - - 31.4 2 1 4B 14 2 - 5 93.0 160.9 106.0 1 1 1 1 1
GE CF6-80C2D1F MD-11/-11F/-11F(AF)/-11F(C) 60,690 - 0.322 - 31.8 5.03 2 1 4B 14 2 - 5 93.0 160.9 106.0 9,850 1 1 1 1 1 1
GE CF6-80C2G2 767-400ERX, 747-400X (not produced) - - 2 1 4B 14 2 - 5 93.0 160.9 106.0 Notes 1 1 1
GE CF6-80C2L1F (see military turbofan specifications)
GE CF6-80E1 A330-200/-300 (option) 65,500 - 0.329 - 1913 32.0 5.30 2 1 4B 14 2 - 4 164.3 114.0 11,162 Notes 1 1 1 1 1 1 1 1 1
GE CF6-80E1A1 A330-200/-300 (option) 65,500 - 0.329 - 1913 32.0 5.30 2 1 4B 14 2 - 5 164.3 114.0 11,162 1 1 1 1 1 1 1 1 1
GE CF6-80E1A2 A330-201 67,500 - 0.332 - 1926 32.6 5.30 2 1 4B 14 2 - 5 164.3 114.0 11,162 1 1 1 1 1 1 1 1 1
GE CF6-80E1A3 A330-203 68,240 - - 33.7 5.00 2 1 4B 14 2 - 5 171.0 114.0 10,726 Notes 1 1 1 1 1 1 1
GE CF6-80E1A4 A330-202 66,870 - 0.338 - 33.7 5.00 2 1 4B 14 2 - 5 171.0 114.0 10,726 1 1 1 1 1 1 1 1
GE CF34-1A Challenger 601-1A 8,650 - 0.360 - 6.20 2 1 - 14 2 - 4 44.0 103.0 49.0 1,625 1 1 1 1 1 1 1
GE CF34-3A Challenger 601-3A 9,220 - 0.357 - 332 21.0 6.30 2 1 - 14 2 - 4 44.0 103.0 49.0 1,625 Notes 1 1 1 1 1 1 1 1 1 1
GE CF34-3A1 CRJ100/200 9,220 - 0.357 - 332 21.0 6.30 2 1 - 14 2 - 4 44.0 103.0 49.0 1,655 Notes 1 1 1 1 1 1 1 1 1 1
GE CF34-3B CRJ100/200, Challenger 604, Challenger 800 9,220 - 0.346 - 21.0 6.30 2 1 - 14 2 - 4 44.0 103.0 49.0 1,670 1 1 1 1 1 1 1 1
GE CF34-3B1 CRJ100/200/200ER/200LR, Challenger 604, Challenger 800 9,220 - 0.346 - 21.0 6.30 2 1 - 14 2 - 4 44.0 103.0 49.0 1,670 1 1 1 1 1 1 1 1
GE CF34-8C1 CRJ700-701/-701ER 13,790 - 0.370 - 27.0 4.90 2 1 - 10 2 - 4 46.2 128.0 52.0 2,350 Notes 1 1 1 1 1 1
GE CF34-8C5 CRJ700-705/-705ER, CRJ900/900ER 14,500 - 0.390 - 4.90 2 1 - 10 2 - 4 46.2 128.0 52.0 2,470 Notes 1 1 1 1 1 1
GE CF34-8C5A1 - - 2 1 - 10 2 - 4 46.2 128.0 52.0 2,470 1 1 1 1 1 1
GE CF34-8C5A2 - - 2 1 - 10 2 - 4 46.2 128.0 52.0 2,470 1 1 1 1 1 1
GE CF34-8C5A3 - - 2 1 - 10 2 - 4 46.2 128.0 52.0 2,470 1 1 1 1 1 1
GE CF34-8C5B1 CRJ700-705LR 14,255 - - 2 1 - 10 2 - 4 46.2 128.0 52.0 2,470 4 1 1 1 1 1
GE CF34-8D?? SL-200/-300 (not produced) - - 2 1 - 10 2 - 4 46.2 128.0 52.0 2,470 1 1 1 1 1
GE CF34-8D1 728-100, 528-100 (not produced) 12,500 - 0.390 - 2 1 - 10 2 - 4 46.2 128.0 52.0 2,470 1 1 1 1 1
GE CF34-8D3 728-200 (not produced) 12,875 - 0.390 - 27.0 4.90 2 1 - 10 2 - 4 46.2 128.0 52.0 2,470 Notes 1 1 1 1 1
GE CF34-8D5 - - 2 1 - 10 2 - 4 46.2 128.0 52.0 2,470 1 1 1 1 1
GE CF34-8D6 Envoy 7 (not produced) 13,050 - 0.390 - 2 1 - 10 2 - 4 46.2 128.0 52.0 2,470 1 1 1 1 1
GE CF34-8E2 ERJ-170, ERJ-170LR (option) 14,000 - 0.390 - 2 1 - 10 2 - 4 46.2 128.0 52.0 2,470 1 1 1 1 1
GE CF34-8E2A1 - - 2 1 - 10 2 - 4 46.2 128.0 52.0 1 1 1 1
GE CF34-8E5 ERJ-170LR, ERJ-170 (option) - - 2 1 - 10 2 - 4 46.2 128.0 52.0 1 1 1 1
GE CF34-8E5A1 ERJ-170/-170LR (option) - - 2 1 - 10 2 - 4 46.2 128.0 52.0 1 1 1 1
GE CF34-8E5A2 - - 2 1 - 10 2 - 4 46.2 128.0 52.0 1 1 1 1
GE CF34-8E6 - - 2 1 - 10 2 - 4 46.2 128.0 52.0 1 1 1 1
GE CF34-8E6A1 - - 2 1 - 10 2 - 4 46.2 128.0 52.0 1 1 1 1
GE CF34-8E?? Il-214, RRJ (candidate engine) - - 2 1 - 10 2 - 4 46.0 128.0 52.0 1 1 1 1
GE CF34-10A ARJ21 18,000 - - 2 1 3B 9 1 - 4
GE CF34-10D5 928-100 (not produced) 17,355 - 0.380 - 29.0 5.00 2 1 3B 9 1 - 4 90.0 57.0 3,800 Notes 1 1 1 1 1
GE CF34-10D6 928-200 (not produced) 18,750 - 0.380 - 29.0 5.00 2 1 3B 9 1 - 4 90.0 57.0 3,800 Notes 1 1 1 1 1
GE CF34-10E5 ERJ-190/-190AR, ERJ-195/-195AR 18,500 - 0.380 - 2 1 3B 9 1 - 4 90.0 57.0 3,800 1 1 1 1 1
GE CF700-2B Falcon 20 - - 84 1.90 2 1 aft - 8 2 - 1 53.6 33.2
GE CF700-2C Falcon 20C 4,125 - 0.652 - 84 6.9 1.90 2 1 aft - 8 2 - 1 53.6 33.2 725 Notes 2 2 2 2 2 2 2
GE CF700-2D Mystere 20, Falcon 20D 4,250 - 0.652 - 84 6.2 1.90 2 1 aft - 8 2 - 1 53.6 33.2 737 2 2 2 2 2 2 2
GE CF700-2D2 Falcon 20E/F, Sabreliner 75A/80A 4,315 - 0.643 - 84 6.9 1.90 2 1 aft - 8 2 - 1 53.6 37.0 767
GE CJ610-1 Learjet 23, HFB 320, 1121A Commdore 2,850 - 0.990 - 44 - - 1 - - 8 2 - - - 51.1 17.7 399 Notes 2 2 2 - - 2 - 2 2
GE CJ610-4 Learjet 23/24 2,850 - 0.990 - 44 - - 1 - - 8 2 - - - 45.4 17.7 389 2 2 2 - - 2 - 2 2
GE CJ610-5 HFB 320, 1121B/1122 Commodore 2,950 - 0.980 - 44 6.8 - - 1 - - 8 2 - - - 51.1 17.7 402 2 2 2 - - 2 - 2 2
GE CJ610-6 Learjet 24B/D, Learjet 24C (not produced) 2,950 - 0.980 - 44 6.8 - - 1 - - 8 2 - - - 45.4 17.7 392 2 2 2 - - 2 - 2 2
GE CJ610-8 HFB 320 2,950 - - 44 - - 1 - - 8 2 - - - 45.4 17.7 407 2 2 - - 2 - 2 2
GE CJ610-8A Learjet 24E/F/25B/25C/25D/28/29 2,950 - - 44 - - 1 - - 8 2 - - - 45.4 17.7 407 2 2 - - 2 - 2 2
GE CJ610-9 HFB 320, 1123 Commodore 3,100 - 1.000 - 44 6.8 - - 1 - - 8 2 - - - 51.1 17.7 417 Notes 2 2 - - 2 - 2 2
GE CJ805-3 Convair CV-880 11,200 - - 2 1 aft - 17 3 - 1 Notes
GE CJ805-3A Convair CV-880 11,200 - - 2 1 aft - 17 3 - 1 Notes
GE CJ805-3B Convair CV-880 11,650 - - 2 1 aft - 17 3 - 1
GE CJ805-23B Convair CV-990/-990A 16,100 - 0.530 - 171 13.0 2 1 aft - 17 3 - 1 Notes
GE CJ805-23C Caravelle 7/10A 16,100 - - 2 1 aft - 17 3 - 1
GE GE1 Technology demonstrator 5,000 - 0.700 - 77 11.0 - - 1 - - 14 2 - - - - - -
GE GE4/J5P B-2707-200/-300 (not produced) 51,500 68,600 1.040 1.86 646 12.5 - - 1 - - 9 2 - - - 308.0 89.5 11,300 Notes 2 - - - 2 2
GE GE39 Technology demonstrator 2 2 UDF - - - Notes
GE GE90-76B 777-200 76,400 - - 3037 39.3 1.65 8.40 17,500 0.545 0.83 35,000 2 1 3B 10 2 - 6 123.0 192.8 134.0 15,596 Notes 1 1 1 1 1 1 1 1 1 1
GE GE90-85B 777-200/-200ER 84,700 - 0.324 - 3037 39.3 1.65 8.40 17,500 0.520 0.83 35,000 2 1 3B 10 2 - 6 123.0 192.8 134.0 15,596 1 1 1 1 1 1 1 1 1 1 1
GE GE90-90B 777-200ER, 777-200 (option) 90,000 - - 3195 40.0 1.65 8.40 2 1 3B 14 2 - 6 123.0 192.8 134.0 15,596
GE GE90-92B 777-200ER, 777-200 (option) 92,000 - - 3221 40.0 1.65 8.30 2 1 3B 14 2 - 6 123.0 192.8 134.0 15,596
GE GE90-94B 777-200/-200ER/-300 93,700 - - 40.0 1.65 2 1 3B 14 2 - 6 123.0 192.8 134.0 16,644 1 1 1 1 1 1 1
GE GE90-110B1 777-200LR, 777-300ER (option), 777-200F (proposed) 110,000 - - 2 1 ?? ?? ?? - ?? 123.0 192.8 134.0
GE GE90-113B - - 2 1 ?? ?? ?? - ?? 123.0 192.8 134.0
GE GE90-115B 777-300ER, 777-200LR (option) 115,000 - - 42.0 2 1 4B 9 2 - 6 123.0 192.8 134.0 18,260 1 1 1 1 1 1
GE GEnx 72A1 787-3/-8/-9, A350-800/-900 53,000 - -
Instytut Lotnictwa D-18A 3,968 - 0.740 - 8.0 2.07 0.70 2 2 - 5 1 - 1 76.4 35.4 838 2 2 2 2 2 2 2 2
Instytut Lotnictwa K-15 I-22 3,307 - 1.006 - 52 5.3 - - 1 - - 6 1 - - - 61.4 35.1 705 2 2 2 2 - - 2 - 2 2
International Aero Engines V2500-A1 A320-231 25,000 - 0.350 - 783 29.4 1.65 5.40 2 1 3B 10 2 - 5 63.5 126.0** 67.5 5,074 Notes 1 1 1 1 1 1 1 1 1 1
International Aero Engines V2522-A5 A319-131 22,000 - 0.340 - 738 25.2 4.90 2 1 4B 10 2 - 5 63.5 126.0** 67.5 5,230 1 1 1 1 1 1 1 1 1
International Aero Engines V2522-D5 MD-90-10 (not produced) 22,000 - 0.340 - 848 25.2 4.90 2 1 4B 10 2 - 5 63.5 126.0** 67.5 1 1 1 1 1 1 1 1 1
International Aero Engines V2524-A5 A319-132/-132CJ 23,500 - 0.360 - 772 27.1 4.90 2 1 4B 10 2 - 5 63.5 126.0** 67.5 5,139 1 1 1 1 1 1 1 1 1
International Aero Engines V2525-D5 MD-90-30 25,000 - 0.350 - 784 27.7 4.80 2 1 4B 10 2 - 5 63.5 126.0** 67.5 5,252 1 1 1 1 1 1 1 1 1
International Aero Engines V2527-A5 A319-133CJ/-133XCJ, A320-232 26,500 - 0.360 - 784 27.7 4.80 2 1 4B 10 2 - 5 63.5 126.0** 67.5 5,139 1 1 1 1 1 1 1 1 1
International Aero Engines V2527E-A5 A320-233 - - 2 1 4B 10 2 - 5 63.5 126.0** 67.5
International Aero Engines V2527M-A5 A319-133CJ/-133XCJ - - 2 1 4B 10 2 - 5 63.5 126.0** 67.5
International Aero Engines V2528-D5 MD-90-30/-30ER 28,000 - 0.350 - 825 30.4 4.70 2 1 4B 10 2 - 5 63.5 126.0** 67.5 5,252 1 1 1 1 1 1 1 1 1
International Aero Engines V2530-A5 A321-131/-232 31,400 - 0.360 - 849 31.6 4.60 2 1 4B 10 2 - 5 63.5 126.0** 67.5 5,139 1 1 1 1 1 1 1 1 1
International Aero Engines V2530-D5 MD-90-50 (not produced) 30,000 - 0.360 - 31.6 4.60 2 1 4B 10 2 - 5 63.5 126.0** 67.5 1 1 1 1 1 1 1
International Aero Engines V2533-A5 A321-231 33,000 - 0.370 - 872 35.2 1.79 4.50 2 1 4B 10 2 - 5 63.5 126.0** 67.5 5,139 1 1 1 1 1 1 1 1 1 1
Ivchenko (Klimov) AI-25 Yak-40 3,300 - 0.570 - 33 8.0 1.70 2.10 976 0.795 0.50 20,000 2 3 - 8 1 - 2 78.5 35.3 705.0 2 2 2 2 2 2 2 2 2
Ivchenko (Klimov) AI-25A Yak-40A 3,850 - - 1.70 2.10 2 3 - 8 1 - 2
Kuznetsov NK-8-2 Tu-154 20,944 - 0.579 - 462 21.5 2.15 1.00 2 2 2B 6 1 - 2 187.5 56.8 4,629 Notes 2 2 2 2 2 2 2
Kuznetsov NK-8-2U Tu-154A/B 23,150 - 0.569 - 503 23.2 2.15 1.05 2 2 2B 6 1 - 2 187.5 56.8 4,629 Notes
Kuznetsov NK-8-3 Il-62 20,950 - - 2 2 2B 6 1 - 2
Kuznetsov NK-8-4 Il-62 23,150 - 0.588 - 489 23.2 2.15 1.02 2 2 2B 6 1 - 2 201.0 56.8 4,629 Notes 2 2 2 2 2 2 2
Kuznetsov NK-8-6 (see NK-86)
Kuznetsov NK-44
Kuznetsov NK-44K
Kuznetsov NK-86 Il-86 28,660 - - 644 13.4 1.15 2 2 2B 6 1 - 2 143.0 63.0 5,401 Notes
Kuznetsov NK-93 Il-96M, Tu-204-230, Tu-330 (proposed) 39,683 - 0.235 - 2205 37.0 1.00 16.60 3 2 DPF 7 8 1 1 3 114.2 235.1 8,047 Notes 2 2 2 2 2 2 2 2 2 2
Kuznetsov NK-144 Tu-144/-144D/-144LL 28,660 38,580 551 14.2 0.60 2 2 3B 11 1 - 2 Notes
Kuznetsov NK-144A Tu-144S (not produced) 33,070 40,000 17.0 0.53 2 2 3B 11 1 - 2 Notes
Kuznetsov NK-321 Tu-144 30,843 55,077 805 28.4 1.40 3 3 5 7 1 1 2 236.0 57.5 7,588 Notes 2 2 2 2 2 2 2
Lotarev (Motor Sich) D-18T An-124-100 'Condor', An-225 'Mriya' 51,660 - 0.360 - 1687 25.0 5.60 10,716 0.570 0.75 36,100 3 1 7 7 1 1 4 91.7 212.6 115.6 9,039 2 2 2 2 2 2 2 2 2 2
Lotarev (Motor Sich) D-18T-1 An-218-100 48,148 - - 5.60 11,596 0.615 0.80 36,100 3 1 7 7 1 1 4 91.7 212.6 115.6 9,039 2 2 2 2 2 2
Lotarev (Motor Sich) D-18T-3 An-124-100M (proposed) 51,660 - - 3 1 7 7 1 1 4 91.7 212.6 115.6 9,039 2 2 2 2 2 2 2 2 2 2
Lotarev (Progress) D-18TM An-218 (proposed) 55,777 - - 1698 5.50 3 1 7 7 1 1 3 224.5 117.6 10,472 2 2 2 2 2
Lotarev (Progress) D-18TR An-218-200/-300 (proposed) 60,627 - - 3 1 7 7 1 1 3 224.5 117.6 10,472 2 2
Lyulka (Saturn) AL-5 Tu-110 12,125 - - 10.0 1.00 2 2 2B 6 1 - 2
Maverick MC-750 MC-2400 Legend 750 - - - - 1 - - 10 2 - -
Microturbo TRS 18-1 Microjet 200 293 - -
Mikulin RD-3 Tu-104 14,881 - -
Mikulin RD-3M Tu-104A/D/V 19,180 - -
Mikulin RD-3M-500 Tu-104B 21,385 - -
Perm Aviadvigatel D-21A1 S-21 11,750 - - 20.2 2.99 0.83 2 5 - 10 2 - 2 4,630 2 2 2 2 2 2
Perm Aviadvigatel D-100 42,000 - - 35.0 8.00 2 1 2B 13 2 - 4
Perm Aviadvigatel D-110 44,090 - - 31.0 1.00 3.00 2 2G 2B 13 2 - 4
Perm Aviadvigatel D-120 - - 1.00 5.00 2 2 2B 13 2 - 4
Pratt Whitney JT3C-1 Prototype - - 2 - 9 7 1 - 2 Notes
Pratt Whitney JT3C-2 DC-8-11/-12 11,200 13,750 0.950 2 - 9 7 1 - 2 38.8 138.6 38.9 3,870 Notes 2 2 2 2 2
Pratt Whitney JT3C-4 707-120, 720 11,200 2 - 9 7 1 - 2 38.8 138.6 38.9 2 2 2 2 2
Pratt Whitney JT3C-6 707-120, DC-8-11/-12 11,200 13,500 0.775 2 - 9 7 1 - 2 38.8 138.6 38.9 4,234 2 2 2 2 2
Pratt Whitney JT3C-7 720, 720F 12,000 - 0.785 - 187 13.0 2 - 9 7 1 - 2 38.8 138.6 38.9 3,495 2 2 2 2 2
Pratt Whitney JT3C-10 DC-8-12 2 - 9 7 1 - 2 38.8 138.6 38.9 2 2 2 2 2
Pratt Whitney JT3C-12 720, 720F, 707-120 (option) 12,000 - 0.775 - 187 13.8 2 - 9 7 1 - 2 38.8 138.6 3,550 Notes
Pratt Whitney JT3D-1 707-120B/-120BF, 720B, 720BF, DC-8-51/52 17,000 - 0.520 - 450 12.5 1.40 2 2 6B 7 1 - 3 53.1 136.3 53.0 4,145 Notes 1 1 1 1 1 1 1 1 1
Pratt Whitney JT3D-1 (HK) 707-120B 17,000 - 0.520 - 450 12.5 1.40 2 2 6B 7 1 - 3 53.1 136.3 53.0 1 1 1 1 1 1 1
Pratt Whitney JT3D-1 (HK3) 707-120B 17,000 - 0.520 - 450 12.5 1.40 2 2 6B 7 1 - 3 53.1 136.3 53.0 1 1 1 1 1 1 1
Pratt Whitney JT3D-1 (Q) 707-120B 17,000 - 0.520 - 450 12.5 1.40 2 2 6B 7 1 - 3 53.1 136.3 53.0 1 1 1 1 1 1 1
Pratt Whitney JT3D-2 (see military turbofan specifications TF33-P-3)
Pratt Whitney JT3D-3 707-120B/-320B/-320C, 720B, DC-8-51/-51F/-52/-52F/-53/-53F/-54/-54F/-55/-55F/-61/-61F/-62/-62F (option) 18,000 - 0.535 - 2 2 6B 7 1 - 3 53.0 Notes 2 2 2 2 2
Pratt Whitney JT3D-3A 2 2 6B 7 1 - 3
Pratt Whitney JT3D-3B 707-120B/-320B/-320BH/-320C/-320CH, 720B, 720BF, DC-8-53F/-55/-62/-62F 18,000 - 0.510 - 450 13.0 1.66 1.40 2 2 6B 7 1 - 3 53.1 145.5 53.0 4,340 Notes 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT3D-3B (HK) 707-120B/-320B/-320BH/-320C/-320CH, 720B, 720BF, DC-8-51F/-53F/-54/-55/-62F(AF) 18,000 - 0.510 - 450 13.0 1.66 1.40 2 2 6B 7 1 - 3 53.1 53.0 1 1 1 1 1 1 1 1
Pratt Whitney JT3D-3B (HK2) 707-320B/-320C, DC-8-51F/-52F/-54F/-55F/-61F/-62F(CF) 18,000 - 0.510 - 450 13.0 1.66 1.40 2 2 6B 7 1 - 3 53.1 53.0 1 1 1 1 1 1 1 1
Pratt Whitney JT3D-3B (HK3) 707-320B, DC-8-51F/-54F/-55F/-61/-61F/-62/-62F/-62F(AF)/-62F(CF) 18,000 - 0.510 - 450 13.0 1.66 1.40 2 2 6B 7 1 - 3 53.1 53.0 1 1 1 1 1 1 1 1
Pratt Whitney JT3D-3B (Q) 707-120B, DC-8-51/-51F/-52/-52F/-54/-55/-55F/-61/-61F(AF)/-62/-62F(CF) 18,000 - 0.510 - 450 13.0 1.66 1.40 2 2 6B 7 1 - 3 53.1 53.0 1 1 1 1 1 1 1 1
Pratt Whitney JT3D-3C 18,000 - 0.510 - 450 13.0 1.66 1.40 2 2 6B 7 1 - 3 53.1 145.5 53.0 4,340 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT3D-5 (see military turbofan specifications TF33-P-7)
Pratt Whitney JT3D-7 707-320B/-320C, DC-8-62/-62F/-63/-63F 19,000 - 0.520 - 472 13.5 1.82 1.43 2 2 7B 7 1 - 3 53.1 145.5 53.0 4,340 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT3D-7 (HK) 707-320B/-320C 19,000 - 0.520 - 472 13.5 1.82 1.43 2 2 7B 7 1 - 3 53.1 53.0 1 1 1 1 1 1 1 1
Pratt Whitney JT3D-7 (HK2) 707-320B/-320C 19,000 - 0.520 - 472 13.5 1.82 1.43 2 2 7B 7 1 - 3 53.1 53.0 1 1 1 1 1 1 1 1
Pratt Whitney JT3D-7 (HK3) 707-320B/-320C, DC-8-62/-62F/-62F(AF)/-62F(CF)/-63/-63F/-63F(CF) 19,000 - 0.520 - 472 13.5 1.82 1.43 2 2 7B 7 1 - 3 53.1 53.0 1 1 1 1 1 1 1 1
Pratt Whitney JT3D-7 (Q) DC-8-62F/-63F/-63F(AF) 19,000 - 0.520 - 472 13.5 1.82 1.43 2 2 7B 7 1 - 3 53.1 53.0 1 1 1 1 1 1 1 1
Pratt Whitney JT3D-7A 19,000 - 0.520 - 472 13.5 1.82 1.43 2 2 7B 7 1 - 3 53.1 145.5 53.0 4,340 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT4A-3 707-220, DC-8-21/-21F (option) 15,800 - 0.770 - - - 2 - 8 7 1 - 2 42.5 144.1 5,020 - -
Pratt Whitney JT4A-5 707-220 (option) 15,800 - 0.770 - - - 2 - 8 7 1 - 2 42.5 144.1 4,815 - -
Pratt Whitney JT4A-7 707-320 (option) 15,800 - 0.770 - - - 2 - 8 7 1 - 2 - -
Pratt Whitney JT4A-9 DC-8-21/-21F/-33F/-33F(AF) 16,800 - 0.810 - - - 2 - 8 7 1 - 2 42.5 144.1 43.0 5,050 2 2 - - 2 2 2
Pratt Whitney JT4A-10 707-320 (option) 16,800 - 0.810 - - - 2 - 8 7 1 - 2 42.5 144.1 43.0 5,100 2 2 - - 2 2 2
Pratt Whitney JT4A-11 DC-8-33F/-33F(AF), 707-320 (option) 17,500 - 0.840 - 256 12.5 - - 2 - 8 7 1 - 2 42.5 144.1 5,100 - -
Pratt Whitney JT4A-12 707-320/-320F 17,500 - 0.840 - 256 12.5 - - 2 - 8 7 1 - 2 42.5 144.1 4,895 - -
Pratt Whitney JT8D-1 Caravelle 10B1R/10B3, DC-9-15 14,000 - 0.585 - 315 15.4 1.90 1.06 2 2 4B 7 1 - 3 42.5 123.5 42.5 3,096 Notes 2 2 2 2 2
Pratt Whitney JT8D-1A 14,000 - 0.585 - 315 15.4 1.90 1.06 2 2 4B 7 1 - 3 42.5 123.5 42.5 3,096 2 2 - - 2 2 2
Pratt Whitney JT8D-1B 14,000 - 0.585 - 315 15.4 1.90 1.06 2 2 4B 7 1 - 3 42.5 123.5 42.5 3,096 2 2 - - 2 2 2
Pratt Whitney JT8D-3 (see military turbofan specifications TF33-P-102)
Pratt Whitney JT8D-5 DC-9-11 12,250 - 0.565 - 2 2 4B 7 1 - 3 42.5 123.5 42.5 3,096 2 2 2 2 2
Pratt Whitney JT8D-7 727-100/-100C/-100QC/-100F/-200/-200F, 737-100/-200A/-200CA, DC-9-15/-15F(RC)/-31, Caravelle 10B1R/10B3/11R 14,000 - 0.585 - 315 15.8 1.93 1.07 4,270 0.796 0.80 30,000 2 2 4B 7 1 - 3 42.5 123.5 42.5 3,096 1 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT8D-7 (HK3) 727-100/-100C, DC-9-15/-15F(RC) 14,000 - 0.585 - 315 15.8 1.93 1.07 4,270 0.796 0.80 30,000 2 2 4B 7 1 - 3 42.5 42.5 1 1 1 1 1 1 1 1 1
Pratt Whitney JT8D-7A 727-100/-100C/-100QC/-100F/-200, 737-100/-200, DC-9-14/-15/-15F(MC)/-31/-31 14,000 - 0.585 - 315 15.8 1.93 1.07 4,270 0.796 0.80 30,000 2 2 4B 7 1 - 3 42.5 123.5 42.5 3,096 1 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT8D-7A (HK3) 727-100/-100C, DC-9-15/-15F(RC)/-32 14,000 - 0.585 - 315 15.8 1.93 1.07 4,270 0.796 0.80 30,000 2 2 4B 7 1 - 3 42.5 42.5 1 1 1 1 1 1 1 1 1
Pratt Whitney JT8D-7B 727-100/-100C/-100F/-200/-200A/-200F, 737-100/-200, DC-9-14/-15/-15F(MC)/-15F(RC)/-31/-31F/-32 14,000 - 0.585 - 315 15.8 1.93 1.07 4,270 0.796 0.80 30,000 2 2 4B 7 1 - 3 42.5 123.5 42.5 3,096 1 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT8D-7B (HK) 727-200F 14,000 - 0.585 - 315 15.8 1.93 1.07 4,270 0.796 0.80 30,000 2 2 4B 7 1 - 3 42.5 42.5 1 1 1 1 1 1 1 1 1
Pratt Whitney JT8D-7B (HK3) 727-100/-100C/-100F/-200/-200A/-200AF/-200F, 737-200, DC-9-14/-15/-15F(MC)/-15F(RC)/-31/-32/-32F 14,000 - 0.585 - 315 15.8 1.93 1.07 4,270 0.796 0.80 30,000 2 2 4B 7 1 - 3 42.5 42.5 1 1 1 1 1 1 1 1 1
Pratt Whitney JT8D-7B (Q) 727-100/-100F 14,000 - 0.585 - 315 15.8 1.93 1.07 4,270 0.796 0.80 30,000 2 2 4B 7 1 - 3 42.5 42.5 1 1 1 1 1 1 1 1 1
Pratt Whitney JT8D-9 727-100/-100C/-200/-200A, 737-200/-200A/-200C/-200CA, DC-9-32/-32F/-33F/-33F(RC), Caravelle 10B3/12 14,500 - 0.565 - 319 15.9 1.91 1.03 4,540 0.800 0.80 30,000 2 2 4B 7 1 - 3 42.5 123.5 42.5 3,196 1 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT8D-9 (HK3) 727-200F, DC-9-31/-32/-32F/-33F 14,500 - 0.565 - 319 15.9 1.91 1.03 4,540 0.800 0.80 30,000 2 2 4B 7 1 - 3 42.5 42.5 1 1 1 1 1 1 1 1 1
Pratt Whitney JT8D-9A 727-100/-100C/-100F/-200/-200A/-200AF/-200F, 737-100/-200/-200A/-200C/-200CA/-200AF, DC-9-31/-32/-32F/-33F(RC) 14,500 - 0.565 - 319 15.9 1.91 1.03 4,540 0.800 0.80 30,000 2 2 4B 7 1 - 3 42.5 123.5 42.5 3,196 1 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT8D-9A (HK3) 727-100/-200/-200A/-200AF/-200F, 737-200/-200A/-200C/-200CA, DC-9-31/-32/-33F(CF)/-33F(RC) 14,500 - 0.565 - 319 15.9 1.91 1.03 4,540 0.800 0.80 30,000 2 2 4B 7 1 - 3 42.5 42.5 1 1 1 1 1 1 1 1 1
Pratt Whitney JT8D-11 DC-9-21/-32/-41 15,000 - 0.620 - 327 16.2 1.05 4,750 0.806 0.80 30,000 2 2 6B 7 1 - 3 42.5 123.5 42.5 3,310 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT8D-11 (HK) DC-9-21 15,000 - 0.620 - 327 16.2 1.05 4,750 0.806 0.80 30,000 2 2 6B 7 1 - 3 42.5 42.5 1 1 1 1 1 1 1 1 1
Pratt Whitney JT8D-11 (HK3) DC-9-21/-32/-33F/-41 15,000 - 0.620 - 327 16.2 1.05 4,750 0.806 0.80 30,000 2 2 6B 7 1 - 3 42.5 42.5 1 1 1 1 1 1 1 1 1
Pratt Whitney JT8D-15 727-200/-200A/-200F/-200AF, 737-200A/-200CA, DC-9-33/-34/-41, Mercure-100 15,500 - 0.630 - 322 16.5 1.03 4,920 0.810 0.80 30,000 2 2 6B 7 1 - 3 42.5 123.5 42.5 3,414 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT8D-15 (HK) 727-200A, 737-200/-200A 15,500 - 0.630 - 322 16.5 1.03 4,920 0.810 0.80 30,000 2 2 6B 7 1 - 3 42.5 42.5 1 1 1 1 1 1 1 1
Pratt Whitney JT8D-15 (HK3) 727-200A/-200AF, 737-200/-200A/-200C/-200CA, DC-9-31/-32/-41 15,500 - 0.630 - 322 16.5 1.03 4,920 0.810 0.80 30,000 2 2 6B 7 1 - 3 42.5 42.5 1 1 1 1 1 1 1 1
Pratt Whitney JT8D-15A 727-200A, 737-200A/-200CA, DC-9-30/-40/-50 (option) 15,500 - 0.590 - 327 16.6 1.04 4,920 0.810 0.80 30,000 2 2 6B 7 1 - 3 42.5 123.5 42.5 3,474 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT8D-15A (HK3) 727-200A/-200AF, 737-200A/-200CA 15,500 - 0.590 - 327 16.6 1.04 4,920 0.810 0.80 30,000 2 2 6B 7 1 - 3 42.5 42.5 1 1 1 1 1 1 1 1
Pratt Whitney JT8D-17 727-200A/-200AF, 737-200/-200A/-200CA/-200F/-200AF, DC-9-31/-32/-34/-34F(CF)/-51 16,000 - 0.600 - 324 16.9 1.01 5,140 0.814 0.80 30,000 2 2 6B 7 1 - 3 42.5 123.5 42.5 3,430 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT8D-17 (HK3) 727-200A/-200AF, 737-200A/-200CA, DC-9-51 16,000 - 0.600 - 324 16.9 1.01 5,140 0.814 0.80 30,000 2 2 6B 7 1 - 3 42.5 42.5 1 1 1 1 1 1 1 1
Pratt Whitney JT8D-17A 727-200A, 737-200A/-200CA/-200AF, DC-9-41/-51 16,000 - 0.600 - 328 17.1 1.02 5,140 0.773 0.80 30,000 2 2 6B 7 1 - 3 42.5 123.5 42.5 3,475 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT8D-17A (HK3) 727-200A/-200AF, 737-200A/-200CA, DC-9-41/-51 16,000 - 0.600 - 328 17.1 1.02 5,140 0.773 0.80 30,000 2 2 6B 7 1 - 3 42.5 42.5 1 1 1 1 1 1 1 1
Pratt Whitney JT8D-17AR 727-200A, 737-200 16,400 - 0.610 - 326 17.3 2.16 1.00 5,140 0.780 0.80 30,000 2 2 6B 7 1 - 3 42.5 123.5 42.5 3,495 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT8D-17R 727-200/-200A/-200AF 17,400 - - 331 17.5 1.00 5,140 0.820 0.80 30,000 2 2 6B 7 1 - 3 42.5 123.5 42.5 3,495 1 1 1 1 1 1 1 1 1
Pratt Whitney JT8D-17R (HK3) 727-200A/-200AF 17,400 - - 331 17.5 1.00 5,140 0.820 0.80 30,000 2 2 6B 7 1 - 3 42.5 42.5 1 1 1 1 1 1 1
Pratt Whitney JT8D-209 MD-81 18,500 - 0.510 - 471 17.4 1.82 4,945 0.724 0.80 35,000 2 1 6B 7 1 - 3 49.2 154.2 4,410 Notes 1 1 1 1 1 2 1 1 1 1
Pratt Whitney JT8D-216 MD-95-30 (not produced) - - 2 1 6B 7 1 - 3 49.2 154.2
Pratt Whitney JT8D-217 MD-81/-82 20,000 - 0.530 - 486 18.6 1.77 5,240 0.753 0.80 35,000 2 1 6B 7 1 - 3 49.2 154.2 4,430 Notes 1 1 1 1 1 2 1 1 1 1
Pratt Whitney JT8D-217A MD-81/-82/-82(SA) 20,000 - 0.530 - 486 18.6 1.77 5,240 0.753 0.80 35,000 2 1 6B 7 1 - 3 49.2 154.2 4,430 1 1 1 1 1 2 1 1 1 1
Pratt Whitney JT8D-217C 727-100(RE)/-200A(RE)/-200AF(RE), MD-81/-82/-87/-88 20,000 - 0.500 - 497 20.1 1.72 5,240 0.736 0.80 35,000 2 1 6B 7 1 - 3 49.2 154.2 4,500 1 1 1 1 1 2 1 1 1 1
Pratt Whitney JT8D-218 MD-95-30 (not produced) - - 2 1 6B 7 1 - 3 49.2 154.2
Pratt Whitney JT8D-219 MD-82/-83/-87/-88, 707-330C(RE), 727-200AF(RE) 21,000 - 0.519 - 497 20.1 1.91 1.72 5,250 0.737 0.80 35,000 2 1 6B 7 1 - 3 49.2 154.2 4,500 1 1 1 1 1 2 1 1 1 1
Pratt Whitney JT9D-1 747-100 (option) 42,000 1484 21.5 1.60 5.00 2 1 3B 11 2 - 4 95.6 154.2 Notes 1 1 1 1 1 1 1 1 1
Pratt Whitney JT9D-3 747-100 (option) 43,500 0.346 22.0 1.51 5.20 2 1 3B 11 2 - 4 95.6 154.2 8,430 Notes 1 1 1 1 1 1 1 1 1
Pratt Whitney JT9D-3A 747-100 44,250 45,800 0.346 1509 21.5 1.51 5.20 10,200 0.624 0.85 35,000 2 1 3B 11 2 - 4 95.6 154.2 8,608 Notes 1 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT9D-7 747-100/-200B 46,300 47,900 0.355 1521 22.3 5.20 10,200 0.620 0.85 35,000 2 1 3B 11 2 - 4 95.6 154.2 8,850 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT9D-7A 747-SF/-SP/-100/-100A/-100(SF)/-100F/-100SR/-100SRB/-100SR(SF)/-200/-200B/-200C 46,950 48,570 0.364 1534 22.5 5.10 10,830 0.625 0.85 35,000 2 1 3B 11 2 - 4 95.6 154.2 8,850 Notes 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT9D-7AH 747-SP/-100/-100(SF)/-100F/-200B 2 1 3B 11 2 - 4 95.6 154.2 8,850
Pratt Whitney JT9D-7ASP 747-SP (option) 46,950 48,570 0.364 1534 22.5 5.10 10,680 0.630 0.85 35,000 2 1 3B 11 2 - 4 95.6 154.2 8,780 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT9D-7AW 747-200B/-200(SF)/-100SR/-200F, 747-100/-100B (option) 2 1 3B 11 2 - 4 95.6 154.2 8,850 1 1 1 1
Pratt Whitney JT9D-7F 747-SP/-100B/-200/-200B/-200B(M)/-200(SF)/-200F 48,000 50,000 0.367 1565 22.8 5.10 11,050 0.631 0.85 35,000 2 1 3B 11 2 - 4 95.6 154.2 8,850 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT9D-7FW 747-SP/-200B(SF)/-200C(M) 48,000 50,000 2 1 3B 11 2 - 4 95.6 154.2 8,850 1 1 1 1 1
Pratt Whitney JT9D-7H 2 1 3B 11 2 - 4 95.6 154.2 8,850 1 1 1 1
Pratt Whitney JT9D-7J 747-100F/-200B/-200B(M)/-200B(SF)/-200C/-200F 50,000 - - 1590 23.5 5.10 11,050 0.631 0.85 35,000 2 1 3B 11 2 - 4 95.6 154.2 8,850 1 1 1 1 1 1 1 1 1
Pratt Whitney JT9D-7Q 747-200B/-200B(M)/-200B(SF)/-200F 53,000 - - 1640 24.5 4.90 11,950 0.631 0.85 35,000 2 1 3B 11 2 - 4 93.6 153.6 9,295 1 1 1 1 1 1 1 1 1
Pratt Whitney JT9D-7Q3 747-200B/-200B(M)/-200B(SF) 53,000 - - 1640 24.5 4.90 11,950 0.631 0.85 35,000 2 1 3B 11 2 - 4 93.6 153.6 9,295 1 1 1 1 1 1 1 1 1
Pratt Whitney JT9D-7R 767-200/-200ER/-200ET/-200PC/-300 48,000 - - 1585 23.4 4.90 11,200 0.615 0.85 35,000 2 1 4B 11 2 - 4 93.4 153.6 8,905 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT9D-7R4D 767-200/-200ER/-200ET/-200PC/-300 48,000 - 0.343 - 1585 23.4 4.90 11,200 0.615 0.85 35,000 2 1 4B 11 2 - 4 93.4 153.6 8,905 Notes 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT9D-7R4D1 A310-221 (option) 48,000 - 0.343 - 1585 23.4 4.90 11,200 0.615 0.85 35,000 2 1 4B 11 2 - 4 93.4 153.6 8,905 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT9D-7R4E 767-200ER 50,000 - 0.343 - 1615 24.2 4.90 11,700 0.620 0.85 35,000 2 1 4B 11 2 - 4 93.4 153.6 8,905 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT9D-7R4E1 A310-222/-222F/-322 50,000 - 0.343 - 1615 24.2 4.90 11,700 0.620 0.85 35,000 2 1 4B 11 2 - 4 93.4 153.6 8,905 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT9D-7R4E3 767-200ER (option) 50,000 - 0.343 - 1615 24.2 4.90 11,700 0.620 0.85 35,000 2 1 4B 11 2 - 4 93.4 153.6 9,100 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT9D-7R4E4 767-200ER 50,000 - 0.343 - 1615 24.2 4.90 11,700 0.620 0.85 35,000 2 1 4B 11 2 - 4 93.4 153.6 9,100 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT9D-7R4G2 747-200B/-200B(SF)/-200F/-300/-300(M)/-300(SF) 54,750 - 0.360 - 1695 26.3 4.80 12,250 0.639 0.85 35,000 2 1 4B 11 2 - 4 93.4 153.6 9,135 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT9D-7R4H1 A300B4-620 56,000 - 0.364 - 1695 26.7 4.80 12,250 0.628 0.85 35,000 2 1 4B 11 2 - 4 93.4 153.6 8,885 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT9D-7W 747-200B 4.90 2 1 3B 11 2 - 4 95.6 154.2 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT9D-9 A300B2/B4 53,000 - - 2 1 3B 11 2 - 4 95.6 154.2 1 1 1 1 1
Pratt Whitney JT9D-15 DC-10-20/-40 (option), MD-11 (proposed) 45,500 47,000 0.355 2 1 3B 11 2 - 4 95.6
Pratt Whitney JT9D-20 DC-10-40, MD-11 (proposed) 46,300 49,400 0.370 1521 21.1 5.20 10,680 0.624 0.85 35,000 2 1 3B 11 2 - 4 95.6 153.6 8,450 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT9D-20J DC-10-40, MD-11 (proposed) 46,300 49,400 0.370 1521 21.1 5.20 10,680 0.624 0.85 35,000 2 1 3B 11 2 - 4 95.6 153.6 8,450 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT9D-25 DC-10-20 (option), MD-11 (proposed) 47,000 50,000 5.20 2 1 3B 11 2 - 4 95.6 153.6 1 1 1 1 1
Pratt Whitney JT9D-59 A300B4-120/-220/-220F/-220FF (option) 53,000 - 0.375 - 1639 24.5 4.90 11,950 0.631 0.85 35,000 2 1 4B 11 2 - 4 95.6 153.6 9,140 Notes 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT9D-59A A300B4-120/-220/-220F/-220FF, DC-10-40(D)/-40(I)/-40F, A300B4-320 (option) 53,000 - 0.375 - 1639 24.5 4.90 11,950 0.631 0.85 35,000 2 1 4B 11 2 - 4 95.6 153.6 9,140 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT9D-59B 54,500 - - 1660 25.2 4.80 12,200 0.631 0.85 35,000 2 1 4B 11 2 - 4 95.6 153.6 9,160 1 1 1 1 1 1 1 1 1
Pratt Whitney JT9D-70A 747-200B/-200B(M)/-200B(SF)/-200F 53,000 - 0.375 - 1639 24.5 4.90 11,950 0.631 0.85 35,000 2 1 4B 11 2 - 4 95.6 153.6 9,155 1 1 1 1 1 1 1 1 1 1
Pratt Whitney JT9D-70B 54,500 - - 1660 25.2 4.80 12,200 0.631 0.85 35,000 2 1 4B 11 2 - 4 95.6 153.6 9,175 1 1 1 1 1 1 1 1 1
Pratt Whitney JT10D-132 (see PW2037)
Pratt Whitney JT11D-20 (see military turbofan specifications J58-P-4)
Pratt Whitney JT12A-3 (see military turbofan specifications)
Pratt Whitney JT12A-5 (see military turbofan specifications)
Pratt Whitney JT12A-6 Sabreliner 40/50 3,000 - 0.960 - - - 1 - - 9 2 - - - 21.9 453 2 2 - - 2 - 2 2
Pratt Whitney JT12A-6A Sabreliner 40/50, JetStar I 3,000 - 0.960 - - - 1 - - 9 2 - - - 21.9 453 Notes 2 2 - - 2 - 2 2
Pratt Whitney JT12A-8 Sabreliner 60, JetStar I 3,300 - 0.995 - 51 6.7 - - 1 - - 9 2 - - - 21.9 468 2 2 - - 2 - 2 2
Pratt Whitney JT12A-8A Sabreliner 60, JetStar I 3,300 - 0.995 - 51 6.7 - - 1 - - 9 2 - - - 21.9 468 2 2 - - 2 - 2 2
Pratt Whitney JTF14 Technology demonstrator - -
Pratt Whitney JTF17A-21 L-2000-7B (not produced), B-2707-200/-300 (candidate engine) 38,300 61,000 0.750 1.78 675 2 2 - 6 1 - 2
Pratt Whitney PW2037 757-200/-200ET 36,600 - 0.335 - 1210 27.9 1.63 5.80 6,500 0.582 0.85 35,000 2 1 4B 12 2 - 5 78.5 141.4 84.8 7,185 Notes 1 1 1 1 1 1 1 1 1 1 1
Pratt Whitney PW2040 757-200/-200ET/-200F 40,100 - 0.330 - 1255 27.6 1.66 5.90 6,500 0.582 0.85 35,000 2 1 4B 12 2 - 5 78.5 141.4 84.8 7,185 1 1 1 1 1 1 1 1 1 1 1
Pratt Whitney PW2043 757-300, 757-200/-200ET/-200F (option) 42,600 - 0.350 - 31.2 6.00 2 1 4B 12 2 - 5 78.5 141.4 84.8 7,161 1 1 1 1 1 1 1 1
Pratt Whitney PW2143 A340-521, A340-621 (proposed) 42,600 - 0.350 - 31.2 6.00 2 1 4B 12 2 - 5 78.5 141.4 84.8 7,161 1 1 1 1 1 1 1 1
Pratt Whitney PW2237 Tu-204-140/-140C (proposed) 36,600 - 0.335 - 1210 27.9 1.63 5.80 6,500 0.582 0.85 35,000 2 1 4B 12 2 - 5 78.5 141.4 84.8 7,185 1 1 1 1 1 1 1 1 1 1 1
Pratt Whitney PW2240 Tu-204-240/-240C, Tu-330 (Tu-204-330) (proposed) 40,100 - 0.330 - 1255 27.6 1.66 5.90 6,500 0.582 0.85 35,000 2 1 4B 12 2 - 5 78.5 141.4 84.8 7,185 1 1 1 1 1 1 1 1 1 1 1
Pratt Whitney PW2337 Il-96M/T 36,600 - 0.335 - 1210 27.9 1.63 5.80 6,500 0.582 0.85 35,000 2 1 4B 12 2 - 5 78.5 141.4 84.8 7,185 1 1 1 1 1 1 1 1 1 1 1
Pratt Whitney PW2643 42,600 - 0.350 - 31.2 6.00 2 1 4B 12 2 - 5 78.5 141.4 84.8 7,161 1 1 1 1 1 1 1 1
Pratt Whitney PW4052 767-200ER/-300ER 52,200 - 0.312 - 1705 27.5 1.70 4.85 2 1 4B 11 2 - 4 93.6 132.2 97.0 9,213 Notes 1 1 1 1 1 1 1 1 1 1
Pratt Whitney PW4056 747-400/-400(M)/-400F, 767-200ER/-300/-300ER 56,750 - 0.320 - 1705 30.2 1.70 4.85 2 1 4B 11 2 - 4 93.6 132.2 97.0 9,213 1 1 1 1 1 1 1 1 1 1
Pratt Whitney PW4060 767-300/-300ER, An-218-200/-300 (proposed) 60,000 - 0.330 - 1705 31.5 4.85 2 1 4B 11 2 - 4 93.6 132.2 97.0 9,213 1 1 1 1 1 1 1 1 1
Pratt Whitney PW4060A 767-200ER 60,000 - 0.330 - 1705 31.5 4.85 2 1 4B 11 2 - 4 93.6 132.2 97.0 9,213 1 1 1 1 1 1 1 1 1
Pratt Whitney PW4062 767-300ER, 747-400/-400ER/-400F/-400FER, 767-200ER/-200FER/-300F/-400ER (option) 63,300 - - 32.3 1.80 4.85 2 1 4B 11 2 - 4 93.6 132.2 97.0 9,213 1 1 1 1 1 1 1 1
Pratt Whitney PW4074 777-200 74,500 - - 2550 30.3 6.00 2 1 6B 11 2 - 7 112.0 191.7 118.5 14,545 1 1 1 1 1 1 1 1
Pratt Whitney PW4077 777-200 77,000 - - 2550 31.5 6.20 2 1 6B 11 2 - 7 112.0 191.7 118.5 14,545 1 1 1 1 1 1 1 1
Pratt Whitney PW4077D - - 2 1 6B 11 2 - 7 112.0 191.7 118.5 14,545 1 1 1 1 1 1 1 1
Pratt Whitney PW4084 777-200 84,000 - - 2550 34.2 1.68 6.41 2 1 6B 11 2 - 7 112.0 191.7 118.5 14,545 Notes 1 1 1 1 1 1 1 1 1
Pratt Whitney PW4084D - - 2 1 6B 11 2 - 7 112.0 191.7 118.5 14,545 1 1 1 1 1 1 1 1
Pratt Whitney PW4090 777-200ER/-300 90,200 - - 2712 38.6 1.70 6.30 2 1 6B 11 2 - 7 112.0 191.7 118.5 15,584 1 1 1 1 1 1 1 1 1
Pratt Whitney PW4090D - - 2 1 6B 11 2 - 7 112.0 191.7 118.5 15,584 1 1 1 1 1 1 1 1
Pratt Whitney PW4090-3 - - 2 1 6B 11 2 - 7 112.0 191.7 118.5 15,584 1 1 1 1 1 1 1 1
Pratt Whitney PW4098 777-300 98,000 - - 2800 42.8 1.75 5.80 14,000 0.581 0.83 35,000 2 1 7B 11 2 - 7 112.0 194.7 119.5 16,500 1 1 1 1 1 1 1 1 1 1
Pratt Whitney PW4152 A310-324/-324ET/-324F 52,200 - 0.312 - 1705 27.5 1.70 4.85 2 1 4B 11 2 - 4 93.6 132.2 97.0 9,213 1 1 1 1 1 1 1 1 1 1
Pratt Whitney PW4156 A310-325ET 56,750 - 0.320 - 1705 30.2 1.70 4.85 2 1 4B 11 2 - 4 93.6 132.2 97.0 9,213 1 1 1 1 1 1 1 1 1 1
Pratt Whitney PW4156A A310-325ET 56,750 - 0.320 - 1705 30.2 1.70 4.85 2 1 4B 11 2 - 4 93.6 132.2 97.0 9,213 1 1 1 1 1 1 1 1 1 1
Pratt Whitney PW4158 A300B4-622/-622R/-622RF, A300F4-622R 58,000 - 0.323 - 1705 30.6 4.75 2 1 4B 11 2 - 4 93.6 132.2 97.0 9,213 1 1 1 1 1 1 1 1 1
Pratt Whitney PW4164 A330-321, A330-221 (option) 64,000 - - 1934 32.0 1.75 5.10 2 1 5B 11 2 - 5 99.8 163.1 106.9 12,400 1 1 1 1 1 1 1 1 1
Pratt Whitney PW4168 A330-222/-322 68,600 - - 1934 32.0 1.75 5.10 2 1 5B 11 2 - 5 99.8 163.1 106.9 12,400 1 1 1 1 1 1 1 1 1
Pratt Whitney PW4168A A330-223/-323X 68,600 - - 1934 32.0 1.75 5.10 2 1 5B 11 2 - 5 99.8 163.1 106.9 12,400 1 1 1 1 1 1 1 1 1
Pratt Whitney PW4460 MD-11/-11F/-11F(AF) 60,000 - 0.330 - 1705 31.5 4.85 2 1 4B 11 2 - 4 93.6 132.2 97.0 9,213 1 1 1 1 1 1 1 1 1
Pratt Whitney PW4462 MD-11/-11F/-11F(CF) 63,300 - - 32.3 1.80 4.85 2 1 4B 11 2 - 4 93.6 132.2 97.0 9,213 1 1 1 1 1 1 1 1
Pratt Whitney PW6122 A318-121, Il-214 (candidate engine), A316/A317 (A31X) (not produced) 22,000 - 0.360 - 27.2 2 1 4B 5 1 - 3 56.5 92.0 60.0 4,115 Notes 1 1 1 1 1 1 1
Pratt Whitney PW6162 A318-122 24,000 - 0.370 - 29.6 4.90 2 1 4B 5 1 - 3 56.5 92.0 60.0 4,115 1 1 1 1 1 1 1 1
Pratt Whitney PW8160 A340-521, A340-621 (proposed) 65,000 - - 2 1G 3B 5 1 - 3 3 3
Pratt Whitney Canada JT15D-1 Citation, SN.600 prototype 2,200 - 0.540 - 75 3.30 2 1 - 1C 1 - 2 27.3 59.3 27.2 514 Notes 2 2 2 2 2
Pratt Whitney Canada JT15D-1A Citation I/ISP 2,200 - 0.540 - 75 3.30 2 1 - 1C 1 - 2 27.3 59.3 27.2 519 2 2 2 2 2
Pratt Whitney Canada JT15D-1B Citation I/ISP 2,200 - 0.540 - 75 10.0 1.50 3.30 2 1 - 1C 1 - 2 27.3 59.3 27.2 519 2 2 2 2 2 2 2 2 2
Pratt Whitney Canada JT15D-4 Citation II/IISP, SN.601 Corvette, Diamond I 2,500 - 0.562 - 2.60 2 1 1B 1C 1 - 2 20.8 63.0 27.0 557 2 2 2 2 2
Pratt Whitney Canada JT15D-4B Citation S/II 2,500 - 0.562 - 2.60 2 1 1B 1C 1 - 2 20.8 63.0 27.0 568 2 2 2 2 2
Pratt Whitney Canada JT15D-4C S211 2,500 - 0.562 - 2.60 2 1 1B 1C 1 - 2 20.8 63.0 27.0 575 2 2 2 2 2
Pratt Whitney Canada JT15D-4D Diamond IA 2,500 - 0.562 - 2.60 2 1 1B 1C 1 - 2 20.8 63.0 27.0 560 2 2 2 2 2
Pratt Whitney Canada JT15D-5 Beechjet 400 (Diamond II), Beechjet 400A/400T 2,900 - 0.551 - 93 12.6 2.00 2 1 1B 1C 1 - 2 20.5 63.0 27.0 632 2 2 2 2 2
Pratt Whitney Canada JT15D-5A Citation V 2,900 - 0.551 - 2.00 2 1 1B 1C 1 - 2 20.5 63.0 27.0 632 2 2 2 2 2
Pratt Whitney Canada JT15D-5B (see military turbofan specifications)
Pratt Whitney Canada JT15D-5C S211A 3,190 - 0.551 - 2.00 2 1 1B 1C 1 - 2 20.5 63.0 27.0 665 2 2 2 2 2
Pratt Whitney Canada JT15D-5D Citation V Ultra, VisionAire Vantage 3,045 - 0.550 - 13.1 2.00 2 1 1B 1C 1 - 2 20.5 63.0 27.0 627 2 2 2 2 2
Pratt Whitney Canada PW305A Learjet 60 4,679 - 0.388 - 15.5 1.50 4.30 2 1 - 4 + 1C 2 - 3 30.7 81.5 36.5 993 Notes 1 1 1 1 1 1 1 1 1
Pratt Whitney Canada PW305B BAe (Hawker) 1000 5,258 - 0.391 - 180 15.5 4.30 2 1 - 4 + 1C 2 - 3 30.7 81.5 36.5 993 1 1 1 1 1 1 1 1
Pratt Whitney Canada PW306A G200 (Galaxy) 6,040 - 0.394 - 18.3 1.57 4.50 2 1 - 4 + 1C 2 - 3 31.7 75.6 1,043 1 1 1 1 1 1 1 1 1
Pratt Whitney Canada PW306B 328JET, Envoy 3 6,050 - - 4.50 2 1 - 4 + 1C 2 - 3 31.7 75.6 1,043 1 1 1 1 1
Pratt Whitney Canada PW306C Citation Sovereign 5,686 - - 4.50 2 1 - 4 + 1C 2 - 3 31.7 75.6 1,043 1 1 1 1 1
Pratt Whitney Canada PW307A Falcon 7X 6,100 - - 2 1 - 4 + 1C 2 - 3 31.7 75.6 1 1 1
Pratt Whitney Canada PW308A Hawker Horizon 6,575 - - 4.10 2 1 - 4 + 1C 2 - 3 31.7 75.6 1 1 1
Pratt Whitney Canada PW308B 428JET (not produced) 8,089 - - 4.10 2 1 - 4 + 1C 2 - 3 31.7 75.6 1 1 1
Pratt Whitney Canada PW308C Falcon 2000EX 7,000 - - 4.10 2 1 - 4 + 1C 2 - 3 31.7 75.6 1 1 1
Pratt Whitney Canada PW530A Citation Bravo 2,748 - - 13.3 1.62 3.70 2 1 - 2 + 1C 1 - 2 22.8 60.0 616 Notes 1 1 1 1 1 1 1
Pratt Whitney Canada PW535A Citation Encore 3,621 - - 2.60 2 1 1B 2 + 1C 1 - 3 1 1
Pratt Whitney Canada PW545A Citation Excel 3,784 - - 15.7 1.59 4.12 2 1 1B 2 + 1C 1 - 3 27.2 68.0 32.0 815 1 1 1 1 1 1 1 1
Pratt Whitney Canada PW610F Eclipse 500 1,112 - -
Pratt Whitney Canada PW615F Citation Mustang, Eclipse 500, ProJet (candidate engine) 1,350 - -
Pratt Whitney Canada PW625F Technology demonstrator 2,500 - -
Pratt Whitney Canada PW645 Citation CJ3 (candidate engine) - -
Pratt Whitney Canada PW800 (AFTI) Technology demonstrator 12,500 - - 7.80 2 1G - 4 + 1C 2 - 3 Notes
Pratt Whitney Canada PW800?? Il-214, RRJ (candidate engine) - - 2 1G - 4 + 1C 2 - 3
Progress AI-22 Tu-324 - -
Progress D-36-1 An-74 14,330 - 0.360 - 562 18.7 6.30 3,527 0.650 0.75 26,250 3 1 6 7 1 1 3 136.6 54.1 2,445 Notes 2 2 2 2 2 2 2 2 2
Progress D-36-1A An-74 - - 6.30 3 1 6 7 1 1 3 136.6 54.1 2,445
Progress D-36-2A An-74, An-74D-200 - - 6.30 3 1 6 7 1 1 3 136.6 54.1 2,445
Progress D-36-3A An-74-200, An-74T-100/-200A, An-74TK-100/200, An-74D-200, An-74VIP - - 6.30 3 1 6 7 1 1 3 136.6 54.1 2,445
Progress D-36-4A AN-74T-300, An-74TK-300 14,330 - - 6.30 3 1 6 7 1 1 3 136.6 54.1 2,445
Progress D-36-5A An-148 (proposed engine) - - 6.30 3 1 6 7 1 1 3 136.6 54.1 2,445
Progress D-436-148 An-148 - -
Progress D-436K (see military turbofan specifications)
Progress D-436T1 Tu-334-100 16,865 - - 25.2 4.95 3 1 + 1 6 7 1 1 3 54.1 3,197 2 2 2 2 2 2
Progress D-436T1-134 Tu-134M (proposed) - - 3 1 6 7 1 1 3 54.1 2 2 2 2 2 2
Progress D-436T2 Tu-334-100D, Tu-354 (Tu-334-200) 18,078 - - 584 26.2 4.90 3 1 + 1 6 7 1 1 3 54.1 3,197 2 2 2 2 2 2
Progress D-436TM Yak-42-200 (Yak-42M) (proposed) 16,865 - - 25.2 4.95 3 1 + 1 6 7 1 1 3 3,197
Progress D-436TP Be-200 16,500 - -
Progress D-436?? Il-214, RRJ (candidate engine) - - 3 1 6 7 1 1 3
Rolls-Royce Avon RA.7 Mk.117 Comet 2R 7,350 - - - - 1 - - ?? 3 - - - - - -
Rolls-Royce Avon RA.25 Mk.502 Comet 2 6,500 - - - - 1 - - ?? 3 - - - - - -
Rolls-Royce Avon RA.25 Mk.503 Comet 2 6,500 - - - - 1 - - ?? 3 - - - - - -
Rolls-Royce Avon RA.25 Mk.504 Comet 2E 6,500 - - - - 1 - - ?? 3 - - - - - -
Rolls-Royce Avon RA.26 Mk.522 Comet 4 10,000 - - - - 1 - - ?? 3 - - - - - -
Rolls-Royce Avon RA.29 Mk.522 Caravelle 1 10,500 - - - - 1 - - ?? 3 - - - - - -
Rolls-Royce Avon RA.29 Mk.523 Comet 3 10,500 - - - - 1 - - ?? 3 - - - - - -
Rolls-Royce Avon RA.29/1 Mk.524 Comet 2E/4 10,250 - 0.786 - 170 8.8 - - 1 - - 16 3 - - - 126.0 39.0 3,343 Notes 2 2 - - - 2 2
Rolls-Royce Avon RA.29/1 Mk.525B Comet 4B/4C 10,250 - - - - 1 - - 16 3 - - - 126.0 39.0 2 - - -
Rolls-Royce Avon RA.29/1 Mk.526 Caravelle 1A 10,250 - 0.786 - 170 8.8 - - 1 - - 16 3 - - - 126.0 39.0 3,343 Notes 2 - - -
Rolls-Royce Avon RA.29/3 Mk.527B Caravelle 3 11,400 - 0.853 - - - 1 - - 16 3 - - - 126.0 39.0 3,347 2 2 - - - 2 2
Rolls-Royce Avon RA.29/6 Mk.531B Caravelle 6N 12,200 - 0.802 - - - 1 - - 17 3 - - - 134.0 39.0 3,488 2 - - -
Rolls-Royce Avon RA.29/6 Mk.533R Caravelle 6R 12,600 - 0.785 - - - 1 17 3 - - - 134.0 39.0 2 - - -
Rolls-Royce Avon RA.29/6 Mk.535R Caravelle 6R 12,600 - 0.785 - 185 10.3 - - 1 - - 17 3 - - - 134.0 39.0 2 - - -
Rolls-Royce Conway RCo.12 Mk.508 707-420/-420F 17,500 - 0.726 - 280 14.1 0.30 4,625 0.822 0.83 36,000 2 7 - 9 1 - 2 132.4 42.0 4,544 Notes 2 2 2 2 2 2 2 2 2
Rolls-Royce Conway RCo.12 Mk.508A 707-420 18,000 - 0.735 - 285 14.0 0.30 4,625 0.822 0.83 36,000 2 7 - 9 1 - 2 132.4 42.0 4,544 2 2 2 2 2 2 2 2 2
Rolls-Royce Conway RCo.12 Mk.509 DC-8-41/-42/-43/-43F 17,500 - - 280 14.1 0.30 4,625 0.822 0.83 36,000 2 7 - 9 1 - 2 132.4 42.0 4,544 2 2 2 2 2 2 2 2
Rolls-Royce Conway RCo.12 Mk.509A DC-8-41/-42/-43/-43F 18,000 - 0.735 - 285 14.0 0.30 4,625 0.822 0.83 36,000 2 7 - 9 1 - 2 132.4 42.0 4,544 2 2 2 2 2 2 2 2 2
Rolls-Royce Conway RCo.42 Mk.540 VC.10 Type 1101/1102/1103/1109 20,370 - 0.656 - 367 14.8 0.60 5,250 0.840 0.83 36,000 2 4 3B 9 1 - 2 154.0 50.0 5,001 Notes 2 2 2 2 2 2 2 2 2
Rolls-Royce Conway RCo.43D Mk.550B Super VC.10 Type 1151/1154 21,800 - 0.590 - 375 15.8 0.60 5,345 0.819 0.83 36,000 2 4 4B 9 1 - 2 154.0 50.0 5,101 Notes 2 2 2 2 2 2 2 2 2
Rolls-Royce Derwent RB.37 5/17 C-102 Jetliner 3,600 - - - - 1 - - - - - - - -
Rolls-Royce Nene RB.41-1 F26 (not produced) 4,600 - 1.049 - 90 4.0 - - 1 - - 1C 1 - - - - - -
Rolls-Royce RB.141-3 HFB 314 (not produced) - -
Rolls-Royce RB.162-86 Trident 3B (booster) 5,250 - 1.120 - 86 4.3 - - 1 - - 6 1 - - - 97.7** 520 1 1 1 - - 1 - 1 1
Rolls-Royce RB.178 28,500 - -
Rolls-Royce RB.178-51 747-100 (proposed) - - 8.00
Rolls-Royce RB.202 Do 231C (lift engines, not produced) 13,100 - -
Rolls-Royce RB.207 A300, L1011-1-1 (candidate engine) 47,500 - 0.540 - 1660 27.0 2.00 5.00 3 1 7 6 1 1 3
Rolls-Royce RB.211-22-02 L1011-1 40,600 - - 1325 27.0 1.42 4.80 3 1 7 6 1 1 3 128.7 7,189 Notes
Rolls-Royce RB.211-22B-02 L1011-1/-1F/-50/-100/-150, L1011-400 (not produced) 42,000 - 0.373 - 1380 24.5 1.42 4.80 9,495 0.628 0.85 35,000 3 1 7 6 1 1 3 84.8 119.4** 9,195 Notes 1 1 1 1 1 1 1 1 1
Rolls-Royce RB.211-22C-02 L1011-1/-50/-100/-150 (option) 42,000 - - 3 1 7 6 1 1 3 Notes
Rolls-Royce RB.211-22CA-02 L1011-1/-50/-100/-150 (option) - - 3 1 7 6 1 1 3
Rolls-Royce RB.211-23 L1011-1/-50/-100/-150 (option) 38,380 - - 3 1 7 6 1 1 3
Rolls-Royce RB.211-24 (see RB.211-524), L1011-2 (not produced) 50,000 - - 3 1 7 6 1 1 4
Rolls-Royce RB.211-40 BAC 311 (not produced) 43,040 - - 3 1 7 6 1 1 3
Rolls-Royce RB.211-52 - - 3 1 7 6 1 1 4
Rolls-Royce RB.211-53 - - 3 1 7 6 1 1 4
Rolls-Royce RB.211-56 L1011-3, L1011-8.4 (not produced) 52,200 - - 1370 26.0 1.59 5.04 3 1 7 6 1 1 4
Rolls-Royce RB.211-61 BAC 311 (not produced) 50,000 - - 3 1 7 6 1 1 3
Rolls-Royce RB.211-524 L1011-100/-200, 747-SP (option), L-1011-300 (not produced) 48,000 - - 3 1 7 6 1 1 3 Notes
Rolls-Royce RB.211-524B-02 747-SP, L1011-200/-200F/-500/-500F, 747-100 (option), L-1011-600 (not produced) 50,000 - - 1513 28.4 4.50 3 1 7 6 1 1 3 84.8 119.4** 9,814 1 1 1 1 1 1 1 1
Rolls-Royce RB.211-524BD-02 L1011-200/-200F/-500, 747-100 (option) 50,000 - - 1513 28.4 4.50 3 1 7 6 1 1 3 84.8 119.4** 9,814 1 1 1 1 1 1 1 1
Rolls-Royce RB.211-524B2-02 L1011-200/-200F/-500, 747-SP/-100 (option) 50,000 - - 1513 28.4 4.50 3 1 7 6 1 1 3 84.8 119.4** 9,814 1 1 1 1 1 1 1 1
Rolls-Royce RB.211-524B3-02 - - 3 1 7 6 1 1 3
Rolls-Royce RB.211-524B4-02 L1011-200/-200F/-250/-500 50,000 - - 1500 29.0 4.40 11,000 0.606 0.85 35,000 3 1 7 6 1 1 3 85.8 122.3** 9,814 1 1 1 1 2 1 1 1 1
Rolls-Royce RB.211-524B4D-02 L1011-200/-500 50,000 - - 1512 28.6 4.40 3 1 7 6 1 1 3 85.8 122.3** 9,814 1 1 1 1 1 1 1 1
Rolls-Royce RB.211-524C 747-SP/-100B/-200B/-300 51,500 - - 1532 28.6 4.50 11,490 0.642 0.85 35,000 3 1 7 6 1 1 3 84.8 119.4** 9,859 1 1 1 1 1 1 1 1 1
Rolls-Royce RB.211-524C2 747-SP/-100B/-200B/-300 51,500 - - 1532 28.6 4.50 11,490 0.642 0.85 35,000 3 1 7 6 1 1 3 84.8 119.4** 9,859 1 1 1 1 1 1 1 1 1
Rolls-Royce RB.211-524C4 747-200B, 747-100B/-300 (option) - - 4.50 3 1 7 6 1 1 3 84.8 119.4** 9,859
Rolls-Royce RB.211-524D4 747-SP/-200B/-200B(M)/-200B(SF)/-200F/-300, L1011-500H&H (not produced) 53,000 - - 1548 29.3 4.40 11,230 0.617 0.85 35,000 3 1 7 6 1 1 3 85.8 122.3** 9,874 1 1 1 1 2 1 1 1 1
Rolls-Royce RB.211-524D4B 747-200/-200F/-300 (option) 53,000 - - 1548 29.6 4.40 11,230 0.601 0.85 35,000 3 1 7 6 1 1 3 85.8 122.3** 9,874 1 1 1 1 2 1 1 1 1
Rolls-Royce RB.211-524G 747-400/-400F, 767-300ER (option) 58,000 - - 1604 32.9 4.30 11,813 0.570 0.85 35,000 3 1 7 6 1 1 3 86.3 125.0** 9,671 1 1 1 1 2 1 1 1 1
Rolls-Royce RB.211-524G2 747-400/-400F (option) - - 4.10 3 1 7 6 1 1 3 86.3 125.0** 9,671
Rolls-Royce RB.211-524G3 767-300ER/-300FER (option) - - 4.10 3 1 7 6 1 1 3 86.3 125.0** 9,671
Rolls-Royce RB.211-524G-T 747-400/-400F, 767-300ER (option) 58,000 - - 1604 32.9 4.30 11,813 0.570 0.85 35,000 3 1 7 6 1 1 3 86.3 125.0** 9,470 1 1 1 1 2 1 1 1 1
Rolls-Royce RB.211-524G2-T 747-400ER (option) - - 4.10 3 1 7 6 1 1 3 86.3 125.0** 9,470
Rolls-Royce RB.211-524G3-T - - 4.10 3 1 7 6 1 1 3 86.3 125.0** 9,470
Rolls-Royce RB.211-524G4-T 767-300ER/-300FER (option) 56,400 - - 4.10 3 1 7 6 1 1 3 86.3 125.0** 9,671
Rolls-Royce RB.211-524G/H - - 4.30 11,813 0.570 0.85 35,000 3 1 7 6 1 1 3 86.3 125.0** 9,671 1 1 1 1 2 1 1 1 1
Rolls-Royce RB.211-524G/H-T - - 4.30 11,813 0.570 0.85 35,000 3 1 7 6 1 1 3 86.3 125.0** 9,671 1 1 1 1 2 1 1 1 1
Rolls-Royce RB.211-524H 747-400, 767-300ER, 767-300F/-300FER/-400F (option) 60,600 - - 1604 34.5 4.10 11,813 0.570 0.85 35,000 3 1 7 6 1 1 3 86.3 125.0** 9,671 1 1 1 1 2 1 1 1 1
Rolls-Royce RB.211-524H2 747-400/-400F - - 4.10 3 1 7 6 1 1 3 86.3 125.0** 9,671
Rolls-Royce RB.211-524H3 767-300ER, 767-300FER (option) - - 4.10 3 1 7 6 1 1 3 86.3 125.0** 9,671
Rolls-Royce RB.211-524H4 An-218-200/-300 (proposed) - - 4.10 3 1 7 6 1 1 3 86.3 125.0** 9,671
Rolls-Royce RB.211-524H-T 747-400/-400F, 767-300ER, An-124-210 (option) 60,600 - - 1604 34.5 4.10 11,813 0.570 0.85 35,000 3 1 7 6 1 1 3 86.3 125.0** 9,470
Rolls-Royce RB.211-524H2-T 747-400ER (option) 59,500 - - 4.10 3 1 7 6 1 1 3 86.3 125.0** 9,470
Rolls-Royce RB.211-535C-37 757-200/-200(SF)/-200F 37,400 - - 1142 21.1 4.40 8,453 0.646 0.80 35,000 3 1 6 6 1 1 3 73.2 118.5 7,294 Notes 1 1 1 1 2 1 1 1 1
Rolls-Royce RB.211-535E4-37 757-200/-200ER/-200ET/-200F, Tu-204-120/-120C/-220/-220C/-222, Tu-224 40,100 - 0.324 - 1151 25.8 4.30 8,700 0.598 0.80 35,000 3 1 6 6 1 1 3 74.1 117.9 7,264 Notes 1 1 1 1 2 1 1 1 1
Rolls-Royce RB.211-535E4B-37 757-200/-200ET/-300, 757-200ER/-200F (option), Tu-214, Tu-330 (Tu-204-330) (proposed) 43,100 - - 1151 25.8 4.30 3 1 6 6 1 1 3 74.1 117.9 7,264 1 1 1 1 1 1 1 1
Rolls-Royce RB.211-535E4C-37 757-300 - - 4.30 3 1 6 6 1 1 3 74.1 117.9 7,264
Rolls-Royce RB.211-535F5-37 Tu-204-220/-222 43,100 - - 3 1 6 6 1 1 3
Rolls-Royce RB.220 Do 231C (not produced) 24,000 - -
Rolls-Royce RB.432 F29 (not produced) 16,000 - -
Rolls-Royce Spey RSp.1 Mk.505-5 Trident 1/1C 12,550 - - 203 2.70 0.71 3,070 0.763 0.77 32,000 2 4 - 12 2 - 2 110.0** 37.0 2,200 Notes 2 2 2 2 2 2 2 2
Rolls-Royce Spey RSp.3 Mk.506-2 10,410 - - 2.70 0.71 3,070 0.764 0.77 32,000 2 4 - 12 2 - 2 110.0** 37.0 2 2 2 2 2
Rolls-Royce Spey RSp.3 Mk.506-14 BAC 111-200 10,410 - - 2.70 0.71 3,070 0.764 0.77 32,000 2 4 - 12 2 - 2 110.0** 37.0 2,257 2 2 2 2 2 2
Rolls-Royce Spey RSp.3 Mk.506-14A 10,410 - - 2.70 0.71 3,070 0.764 0.77 32,000 2 4 - 12 2 - 2 110.0** 37.0 2,257 2 2 2 2 2 2
Rolls-Royce Spey RSp.3W Mk.506-14AW BAC 111-200 10,410 - - 2.70 0.71 3,070 0.764 0.77 32,000 2 4 - 12 2 - 2 110.0** 37.0 2,288 2 2 2 2 2 2
Rolls-Royce Spey RSp.3 Mk.506-14D 10,410 - - 2.70 0.71 3,070 0.764 0.77 32,000 2 4 - 12 2 - 2 110.0** 37.0 2,257 2 2 2 2 2 2
Rolls-Royce Spey RSp.4 Mk.510-5 Trident 1D 11,000 - - 2.70 0.71 3,070 0.770 0.77 32,000 2 5 - 12 2 - 2 32.5 109.6 37.1 2,312 Notes 1 1 1 2 1 1 1 1
Rolls-Royce Spey RSp.4 Mk.510-14 BAC 111-300/-400 11,000 - 0.600 - 206 18.4 2.70 0.71 3,070 0.770 0.77 32,000 2 5 - 12 2 - 2 32.5 109.6 37.1 2,332 1 1 1 1 1 1 2 1 1 1 1
Rolls-Royce Spey RSp.4 Mk.510-14W BAC 111-300/-400 11,000 - 0.600 - 206 18.4 2.70 0.71 3,070 0.770 0.77 32,000 2 5 - 12 2 - 2 32.5 109.6 37.1 2,621 1 1 1 1 1 1 2 1 1 1 1
Rolls-Royce Spey RSp.4 Mk.511-5 Trident 1E/2 11,400 - 0.600 - 206 18.4 2.70 0.71 3,070 0.770 0.77 32,000 2 5 - 12 2 - 2 32.5 109.6 37.1 2,312 1 1 1 1 1 1 2 1 1 1 1
Rolls-Royce Spey RSp.4 Mk.511-5W Trident 1E/2 11,400 - 0.600 - 206 18.4 2.70 0.71 3,070 0.770 0.77 32,000 2 5 - 12 2 - 2 32.5 109.6 37.1 2,317 1 1 1 1 1 1 2 1 1 1 1
Rolls-Royce Spey RSp.4 Mk.511-8 Gulfstream II/II-B/III 11,400 - 0.600 - 197 18.4 2.70 0.64 3,070 0.770 0.77 32,000 2 5 - 12 2 - 2 32.5 109.6 37.1 2,483 1 1 1 1 1 1 2 1 1 1 1
Rolls-Royce Spey RSp.4 Mk.511-14 BAC 111-300/-400 11,400 - 0.600 - 206 18.4 2.70 0.71 3,070 0.770 0.77 32,000 2 5 - 12 2 - 2 32.5 109.6 37.1 2,483 1 1 1 1 1 1 2 1 1 1 1
Rolls-Royce Spey RSp.4 Mk.511-14W BAC 111-300/-400 11,400 - 0.600 - 206 18.4 2.70 0.71 3,070 0.770 0.77 32,000 2 5 - 12 2 - 2 32.5 109.6 37.1 2,621 1 1 1 1 1 1 2 1 1 1 1
Rolls-Royce Spey RSp.4 Mk.512-5W Trident 2E/3B 12,000 - 0.600 - 206 20.7 2.60 0.71 3,070 0.77 32,000 2 5 - 12 2 - 2 32.5 109.6 37.1 2,609 1 1 1 1 1 1 2 1 1 1 1
Rolls-Royce Spey RSp.4 Mk.512-14 BAC 111-475/-500, ROMBAC 111-560 12,550 - 0.600 - 206 20.7 2.60 0.71 3,070 0.77 32,000 2 5 - 12 2 - 2 32.5 109.6 37.1 2,609 1 1 1 1 1 1 2 1 1 1 1
Rolls-Royce Spey RSp.4 Mk.512-14DW BAC 111-475/-500, ROMBAC 111-560 12,550 - 0.600 - 206 20.7 2.60 0.71 3,070 0.77 32,000 2 5 - 12 2 - 2 32.5 109.6 37.1 2,609 1 1 1 1 1 1 2 1 1 1 1
Rolls-Royce Spey RSp.4 Mk.512-14DWE 12,550 - - 2.60 0.71 3,070 0.77 32,000 2 5 - 12 2 - 2 32.5 109.6 37.1 2,609 1 1 1 1 1 1 2 1 1 1 1
Rolls-Royce Spey RSp.4 Mk.512-25 BAC 111-475/-500, ROMBAC 111-560 12,550 - 0.600 - 206 20.7 2.60 0.71 3,070 0.77 32,000 2 5 - 12 2 - 2 32.5 109.6 37.1 2,609 1 1 1 1 1 1 2 1 1 1 1
Rolls-Royce Spey Jr. RB.183-2 Mk.555-15 F28 Mk.1000/Mk.1000C/Mk.2000 9,850 - 0.750 - 199 15.4 2.46 1.00 2 4 - 12 2 - 2 32.5 97.0 2,257 1 1 1 1 1 1 1 1 1 1
Rolls-Royce Spey Jr. RB.183-2 Mk.555-15H F28 Mk.6000, F28 Mk.5000/Mk.6600 (not produced) - - 199 15.4 2.46 1.00 2 4 - 12 2 - 2 32.5 97.0 2,257 1 1 1 1 1 1 1 1
Rolls-Royce Spey Jr. RB.183-2 Mk.555-15N - - 2 4 - 12 2 - 2 32.5 97.0 2,257 1 1 1 1 1 1 1 1
Rolls-Royce Spey Jr. RB.183-2 Mk.555-15P F28 Mk.3000/Mk.4000 9,900 - - 199 15.4 2.46 1.00 2 4 - 12 2 - 2 32.5 97.0 2,257 1 1 1 1 1 1 1 1 1
Rolls-Royce Tay RB.183-3 Mk.611-8 G300, G400 (Gulfstream IV/IV-SP) 13,850 - 0.430 - 410 15.8 3.04 0.710 0.80 43,000 2 1 3B 12 2 - 3 44.0 94.7 2,951 Notes 1 1 1 1 1 2 1 1 1 1
Rolls-Royce Tay RB.183-3 Mk.611-8C G350, G400 13,850 - 0.430 - 410 15.8 3.04 0.710 0.80 43,000 2 1 3B 12 2 - 3 44.0 94.7 2,951 1 1 1 1 1 2 1 1 1 1
Rolls-Royce Tay RB.183-3 Mk.620-15 Fokker 70 13,850 - - 410 15.8 3.04 0.690 0.73 30,000 2 1 3B 12 2 - 3 44.0 94.7 3,185 1 1 1 1 2 1 1 1 1
Rolls-Royce Tay RB.183-3 Mk.650-14 BAC 111-475/-500/-560 15,100 - - 418 16.2 3.06 0.690 0.73 30,000 2 1 3B 12 2 - 3 44.8 94.8 3,340 Notes 1 1 1 1 2 1 1 1 1
Rolls-Royce Tay RB.183-3 Mk.650-15 Fokker 100 15,100 - - 418 16.2 3.06 0.690 0.73 30,000 2 1 3B 12 2 - 3 44.8 94.8 3,340 1 1 1 1 2 1 1 1 1
Rolls-Royce Tay RB.183-3 Mk.651-54 727-100(QF)/-100C(QF) 15,400 - 0.450 - 426 16.6 3.07 0.690 0.78 35,000 2 1 3B 12 2 - 3 44.8 94.7 3,380 1 1 1 1 1 2 1 1 1 1
Rolls-Royce Tay RB.183-3 Mk.670 727-200RE, DC-9RE, 737-100RE/-200RE, MD-95 (proposed for re-engining) 18,000 - - 511 19.0 3.20 2 1 3B 12 2 - 3 50.0 112.0 3,750 Notes 1 1 1 1 1 1 1 1
Rolls-Royce Trent 553-61 A340-541, A340-641?? (option) 53,000 - - 1847 35.1 7.70 3 1 8 6 1 1 5 97.4 154.0 10,400 Notes
Rolls-Royce Trent 556-61 A340-642 56,000 - - 1892 36.7 7.60 3 1 8 6 1 1 5 97.4 154.0 10,400
Rolls-Royce Trent 556B-61 - - 3 1 8 6 1 1 5 97.4 154.0 10,400
Rolls-Royce Trent 560-61 - - 3 1 8 6 1 1 5 97.4 154.0 10,400
Rolls-Royce Trent 600 MD-11 (option) 68,000 - - 2032 4.30 3 1 8 6 1 1 4 97.4 154.0 102.0 10,400
Rolls-Royce Trent 672 767-400ERX 72,000 - - 43.2 3 1 8 6 1 1 4 97.4 154.0 102.0 11,400
Rolls-Royce Trent 6?? 747-XQLR (candidate engine), 747-500X/-600X (not produced) - - 3 1 8 6 1 1 4 97.4 154.0 102.0 11,400
Rolls-Royce Trent 758 A330-141 58,000 - - 3 1 8 6 1 1 4 97.4 154.0 Notes
Rolls-Royce Trent 764 MD-12 (not built) 64,000 - - 3 1 8 6 1 1 4 97.4 154.0
Rolls-Royce Trent 768-60 A330-341, A330-241 (option) 67,500 - - 1932 35.2 4.97 3 1 8 6 1 1 4 97.4 154.0 10,550 Notes 1 1 1 1 1 1 1 1
Rolls-Royce Trent 772-60 A330-242/-342 71,100 - - 1978 36.8 4.89 11,500 0.565 0.82 35,000 3 1 8 6 1 1 4 97.4 154.0 10,550 1 1 1 1 1 1 1 1
Rolls-Royce Trent 772B-60 A330-243/-343X 72,000 - - 1978 36.8 4.89 3 1 8 6 1 1 4 97.4 154.0 10,467 1 1 1 1 1 1 1 1
Rolls-Royce Trent 775-60 A330-244, A330-344 (option) 75,150 - - 2024 39.0 4.77 3 1 8 6 1 1 4 97.4 154.0 1 1 1 1 1 1 1
Rolls-Royce Trent 871-17 777-200 71,000 - - 3 1 8 6 1 1 5 110.0 172.0 13,100
Rolls-Royce Trent 875-17 777-200 77,900 - - 2482 35.9 6.21 3 1 8 6 1 1 5 110.0 172.0 13,100 1 1 1 1 1 1 1 1
Rolls-Royce Trent 877-17 777-200 80,720 - - 2578 37.0 6.15 3 1 8 6 1 1 5 110.0 172.0 13,100 1 1 1 1 1 1 1 1
Rolls-Royce Trent 882-17 777-200 (option) 84,700 - - 38.8 3 1 8 6 1 1 5 110.0 172.0 13,100 Notes
Rolls-Royce Trent 884-17 777-200/-200ER 86,910 - - 2661 39.8 5.95 3 1 8 6 1 1 5 110.0 172.0 13,100 1 1 1 1 1 1 1 1
Rolls-Royce Trent 884B-17 - - 3 1 8 6 1 1 5 110.0 172.0 13,100
Rolls-Royce Trent 890-17 777-200ER/-300, Tu-304 (proposed) 91,300 - - 2720 42.7 5.74 13,000 0.557 0.83 35,000 3 1 8 6 1 1 5 110.0 172.0 13,100 1 1 1 1 1 1 1 1
Rolls-Royce Trent 892-17 777-200ER/-300/-300ER 91,450 - - 2645 40.8 5.79 3 1 8 6 1 1 5 110.0 172.0 13,133
Rolls-Royce Trent 892B-17 - - 3 1 8 6 1 1 5 110.0 172.0 13,133
Rolls-Royce Trent 895-17 777-200ER, 777-300/-300ER (option) 95,000 - - 2664 41.6 1.81 5.79 3 1 8 6 1 1 5 110.0 172.0 13,186
Rolls-Royce Trent 895C-17 777-200ER, 777-300/-300ER (option) 95,000 - - 2664 41.6 1.81 5.79 3 1 8 6 1 1 5 110.0 172.0 13,186
Rolls-Royce Trent 8104 Technology demonstrator 104,000 - - 45.0 3 1 8 6 1 1 5 110.0 172.0 14,400
Rolls-Royce Trent 970-84 A380-841 75,150 - - 3 1 8 6 1 1 5 110.0 208.8** 155.2 13,825
Rolls-Royce Trent 970B-84 A380-841 78,300 - - 3 1 8 6 1 1 5 110.0 208.8** 155.2 13,825
Rolls-Royce Trent 975 747-500X/-600X (not produced) 75,000 - - 2481 35.8 7.80 3 1 8 6 1 1 5 110.0 208.8** 155.2 13,825 Notes
Rolls-Royce Trent 977-84 A380-843F 80,780 - - 3 1 8 6 1 1 5 110.0 208.8** 155.2 13,825
Rolls-Royce Trent 977B-84 A380-843F 83,835 - - 3 1 8 6 1 1 5 110.0 208.8** 155.2 13,825
Rolls-Royce Trent 980-84 A380-84?/-84?F (proposed future engine choice) 84,100 - - 3 1 8 6 1 1 5 110.0 208.8** 155.2 13,825
Rolls-Royce Trent 1000 787-3/-8/-9, A350-800/-900 (expected) 53,000 - - 2750 11.00 3 1 8 6 1 1 6 112.0 152.0 1 1 1 1 1 1
Rolls-Royce Viper Mk.600 3,750 - 0.950 - 58 5.8 - - 1 - - 8 2 - - - - - -
Rolls-Royce Viper Mk.601-22 HS 125-600B 3,750 - 0.950 - - - 1 - - 8 2 - - - 830 2 2 - - 2 - 2
BMW/Rolls-Royce (Rolls-Royce Deutschland) BR710A1-10 G500 (Gulfstream V), G550 (Gulfstream V-SP) 14,750 - 0.390 - 435 25.7 4.20 2 1 - 10 2 - 2 48.0 87.0 52.9 3,520 Notes 1 1 1 1 1 1 1 1 1
BMW/Rolls-Royce (Rolls-Royce Deutschland) BR710A2-20 Global Express, Global Express XRS, Global 5000 14,750 - 0.390 - 435 25.7 4.20 2 1 - 10 2 - 2 48.0 87.0 52.9 3,520 1 1 1 1 1 1 1 1 1
BMW/Rolls-Royce (Rolls-Royce Deutschland) BR710C4-11 G500 (Gulfstream V), G550 (Gulfstream V-SP) 14,750 - 0.390 - 435 25.7 4.20 2 1 - 10 2 - 2 48.0 87.0 52.9 3,520 1 1 1 1 1 1 1 1 1
BMW/Rolls-Royce (Rolls-Royce Deutschland) BR710-48 Tu-334-120 16,000 - - 2 1 - 10 2 - 2 48.0 Notes
BMW/Rolls-Royce (Rolls-Royce Deutschland) BR710-?? ARJ 21 - - 2 1 - 10 2 - 2
BMW/Rolls-Royce (Rolls-Royce Deutschland) BR710-?? SL-200/-300 (not produced) - - 2 1 - 10 2 - 2
BMW/Rolls-Royce (Rolls-Royce Deutschland) BR715A1-30 717-200 18,500 - 0.370 - 614 32.1 4.70 2 1 2B 10 2 - 3 56.0 93.0 60.2 4,597 1 1 1 1 1 1 1 1 1
BMW/Rolls-Royce (Rolls-Royce Deutschland) BR715B1-30 717-200 (option) 20,000 - - 2 1 2B 10 2 - 3 56.0
BMW/Rolls-Royce (Rolls-Royce Deutschland) BR715C1-30 717-200 HGW 21,000 - - 689 32.6 5.00 2 1 2B 10 2 - 3 56.0 93.0 60.2 4,597 1 1 1 1 1 1 1 1 1
BMW/Rolls-Royce (Rolls-Royce Deutschland) BR715-55 Tu-354 (Tu-334-200) (proposed) 20,000 - - 2 1 2B 10 2 - 3 56.0
BMW/Rolls-Royce (Rolls-Royce Deutschland) BR715-?? Il-214, RRJ, N-2130-100/-200 (candidate engine), A316/A317 (A31X) (not produced) - - 2 1 2B 10 2 - 3 56.0
BMW/Rolls-Royce (Rolls-Royce Deutschland) BR720 - - 2 1 3B 10 2 - 4
Rolls-Royce/Snecma M45F Technology demonstrator - - 2 1 5B 7 1 - 3
Rolls-Royce/Snecma M45H-C 8,800 - - 2 1 5B 7 1 - 3
Rolls-Royce/Snecma M45H-D Mk.501 VFW 614 (not produced) 7,760 - 0.451 - 233 18.8 1.60 2.85 2,745 0.725 0.65 20,000 2 1 5B 7 1 - 3 41.7 116.5 1,483 2 2 2 2 2 2 2 2 2 2 2
Rolls-Royce/Snecma M45H-E1 9,250 - - 2 1 6B 7 1 - 3
Rolls-Royce/Snecma M45H-E2 9,600 - - 2 2 6B 7 1 - 3
Rolls-Royce/Snecma Olympus 593 Mk.601 Concorde 32,600 - 0.700 - 410 15.5 2 - 7 7 1 - 1 138.2** 47.9 5,814 Notes
Rolls-Royce/Snecma Olympus 593 Mk.610 Concorde 38,150 - - 2 - 7 7 1 - 1 138.2** 47.9 5,814
Rolls-Royce/Snecma Olympus 593 Mk.611 Concorde 38,400 - 0.700 - 450 2 - 7 7 1 - 1 138.2** 47.9 5,814
Rolls-Royce/Snecma Olympus 593 Mk.621 Concorde 38,400 - 0.700 - 450 2 - 7 7 1 - 1 138.2** 47.9 5,814
PowerJet SaM146 RRJ, Il-214 (candidate engine) 15,000
Snecma/PWC SPW14 (cancelled) 14,000 - - 2 1G - 4 + 1C 2 - 3 Notes
Solovyev D-20 11,905 - - 2 3 - 8 1 - 2
Solovyev D-20P Tu-124K/K2/V 11,905 - 0.620 - 249 13.6 2.60 1.00 2 3 - 8 1 - 2 130.0 38.3 3,236
Solovyev D-30-1 Tu-134/-134K/-134LK 14,990 - 0.600 - 280 18.6 2.65 1.00 2 4 - 10 2 - 2 156.8 41.3 3,417
Solovyev D-30-2 Tu-134A/AK/AN/B/B-1 14,990 - - 2.65 1.00 2 4 - 10 2 - 2 Notes
Solovyev D-30-3 Tu-134A-3/B-3/BW 14,990 - 0.608 - 280 17.7 2.65 1.00 2 5 - 10 2 - 2 156.8 41.3 3,417
Solovyev D-30KP Il-76T 26,460 - 0.481 - 640 18.4 2.42 2 3 - 11 2 - 4 Notes
Solovyev D-30KP-2 Il-76TD/MDP/LL 26,460 - - 2.42 2 3 - 11 2 - 4
Solovyev D-30KPV A-40 26,460 - - 2 3 - 11 2 - 4
Solovyev (Perm Aviadvigatel) D-30KU Il-62M (Il-62-200) 24,250 - 0.495 - 593 17.4 2.35 2 3 - 11 2 - 2 224.0 61.4 5,882 Notes
Solovyev (Perm Aviadvigatel) D-30KU-2 Il-62M (Il-62-200) 23,850 - - 593 2.35 2 3 - 11 2 - 2
Solovyev (Perm Aviadvigatel) D-30KU-90 26,455 - - 2.44 2 3 - 11 2 - 2 224.4 61.4 5,291
Solovyev (Perm Aviadvigatel) D-30KU-154-2 Tu-154M - - 2 3 - 11 2 - 2
Solovyev (Perm Aviadvigatel) D-30U-154 Tu-154M 14,990 - 0.600 - 280 18.6 2.65 1.00 2 4 - 10 2 - 2 156.8 41.3 3,417
Solovyev PS-7 17,000 - - 3,417 0.620 0.80 36,000 47.6 2,976 1 1 1 1
Solovyev PS-9 Il-214-100, Il-214T (candidate engine) 22,000 - - 4,630 0.590 0.80 36,000 56.5 3,858 1 1 1 1
Solovyev PS-12 MS-21-100/-200/-300, MS-21K, MS-12KP (candidate engine) 29,762 - 1193 40.2 8.39 5,665 0.549 0.80 36,000 73.6 5,400 1 1 1 1 1 1 1
Solovyev PS-12M 32,740 - - 6,062 0.553 0.80 36,000 73.6 5,400 1 1 1 1
Solovyev (Perm Aviadvigatel) PS-90A Il-96-300, Tu-204-100/-100C/-200/-200C, Tu-214, Tu-330 (Tu-204-330), Tu-134D (proposed), Tu-154M2 (not produced) 35,250 - - 4.80 2 1 2B 13 2 - 4
Solovyev (Perm Aviadvigatel) PS-90A-154 Tu-154M-2 (proposed) - - 2 1 2B 13 2 - 4 2 2 2 2 2 2 2
Solovyev (Perm Aviadvigatel) PS-90A2 Il-96-300, Il-76TF, Tu-204-500/-600 (proposed) - - 2 1 2B 13 2 - 4
Solovyev (Perm Aviadvigatel) PS-90A10 20,283 - - 582 23.1 3.76 2 1 - 12 2 - 2 55.1 168.5 4,180 2 2 2 2 2 2 2
Solovyev (Perm Aviadvigatel) PS-90A12 Yak-242 26,455 - - 816 25.3 5.05 2 1 - 13 2 - 3 65.8 188.2 5,071 2 2 2 2 2 2 2
Solovyev (Perm Aviadvigatel) PS-90AN-76 Il-76TF 35,275 - - 1036 35.5 4.60 2 1 2B 13 2 - 4 74.8 195.4 6,503 2 2 2 2 2 2 2
Solovyev (Perm Aviadvigatel) PS-90AP Tu-234 - - 2 1 - ?? ?? - ??
Solovyev (Perm Aviadvigatel) PS-90A-?? Il-214, RRJ (candidate engine) - - 2 1 2B 13 2 - 4
Soyuz R123-300 3,100 - - 6.00 2 1 - 2 + 1C 1 - 1
Soyuz R126-300 Tu-324 8,818 - - 2 1 - 5 + 1C 2 - 3
Soyuz R127-300 1,985 - - 68 2 1 - 2C 2 - 2
Turbomeca Astafan 2 1,685 - 0.380 - 8.5 1.00 1 1 - 2 + 1C 3 - - Notes
Turbomeca Astafan 3 1,900 - - 1 1 - 2 + 1C 3 - - Notes
Turbomeca Astafan 4 2,414 - - 1 1 - 2 + 1C 4 - - Notes
Turbomeca Aubisque 1A Saab 105 1,635 - 0.600 - 48 6.9 1.50 2.00 1 1G - 1 + 1C 2 - -
Turbomeca Bastafan 1,765 - - 1 1G - 2 + 1C 3 - - Notes
Turbomeca Marbore 2 Saulnier Paris 1 882 - - - - 1 - - 1C 1 - - - - - -
Turbomeca Marbore 2A Noratlas N-2502 882 - - 1 - - 1C 1 - - - - - -
Turbomeca Marbore 6C Saulnier Paris 2, Saulnier Paris 3 1,060 - 1.110 - 21 3.8 - - 1 - - 1C 1 - - - - - -
Turbomeca Marbore 6F CM.191 (not produced) 1,058 - 1.110 - 21 3.8 - - 1 - - 1C 1 - - - - - -
Turbomeca/Snecma Larzac 49-01 Falcon 10, Corvette 2,300 - 0.610 - 57 9.0 2.00 1.40 2 2 - 4 1 - 1
Williams EJ22-1 Eclipse 500 (candidate engine) 700 - - 2 ?? - ?? ?? - ?? 41.0 14.5 85
Williams FJ22-1 (see EJ22-1)
Williams FJ33-1 Aerostar, Century Jet, FJ-100, Leopard Six 1,200 - - 2 ?? - ?? ?? - ?? 47.9 19.0 300
Williams FJ33-4 S-26 Safire, Javelin Mk.10, D-Jet 1,200 - - 2 ?? - ?? ?? - ?? 47.9 19.0 300
Williams FJ33-?? MC-2400 Legend, A700 1,100 - - 2 ?? - ?? ?? - ?? 47.9 19.0 300
Williams FJ33-?? Citation Mustang, ProJet (candidate engine) 1,350 - - 2 ?? - ?? ?? - ?? 47.9 19.0 300
Williams/Rolls-Royce FJ44-1A Citation CJ1, SigmaJet, MagnaJet 1,900 - 0.456 - 63 12.8 3.28 2 1 1B 1C 1 - 2 20.9 41.9 447
Williams/Rolls-Royce FJ44-1AP Citation CJ1+ 1,900 - - 2 1 1B 1C 1 - 2 20.7 41.4 460 4 1 1 1
Williams/Rolls-Royce FJ44-1C SK60 1,500 - 0.460 - 58 10.3 3.40 2 1 1B 1C 1 - 2 41.9 447
Williams/Rolls-Royce FJ44-2A Premier 1, SJ30-2, Citation Eagle II, NauticAir 450 2,300 - - 2 1 1B 2 + 1C 1 - 2 47.2
Williams/Rolls-Royce FJ44-2C Citation CJ2, Spirit Wing Learjet 25D 2,400 - - 2 1 1B 2 + 1C 1 - 2 47.2
Williams/Rolls-Royce FJ44-3A Citation CJ2+, CJ3 3,000 - - 1
Williams FJX-1 V-Jet II 540 - - 2 ?? - ?? ?? - ??
Williams FJX-2 V-Jet II, Eclipse 500 (candidate engine) 700 - - 2 ?? - ?? ?? - ?? 41.0 14.5 85
B - Booster stage(s)
C - Centrifugal compressor stage(s)
R - Radial turbine stage(s)
G - Geared (fan)
** - denotes length given from intake flange to turbine exhaust flange
grey - denotes optional engine selection or no nominal application for engine
(cancelled) - denotes that the engine program or derivative was cancelled
(not produced) - denotes the aircraft program or derivative was cancelled
Notes:
1. The technical information presented here is to the best of my knowledge.  Any comments, suggestions, questions or
    corrections will be greatly appreciated.
2. While the designation system used by Boeing for their aircraft consists of a 2-digit customer configuration code, only the
    major series have been indicated here. (eg. 747-4F6 -> 747-400)



To top of page


Last updated: 03 Apr 2005

Nathan Meier   nate@jet-engine.net
Copyright © 2000-2005 Nathan Meier