Military Turbofan/Turbojet Specifications
 Civil Turbofan/Turbojet Specifications
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 Civil Turboshaft/Turboprop Specifications
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Civil Turbojet/Turbofan Specifications
Civil Turbojet/Turbofan Specifications
(sorted by engine manufacturer)
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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