Manufacturer Model Application Takeoff Thrust [lbf] Takeoff Thrust [N] Thrust (Cruise) [lbf] Thrust (Cruise) [N] SFC (h=0,M=0) [lb/lbf hr] SFC (h=0,M=0) [kg/s.N] SFC (Cruise) [lb/lbf hr] SFC (Cruise) [kg/s.N] OPR_ Sea lvl Cruise Altitude (h) [ft] Cruise Altitude (h) [Km] Cruise Temperature [K] Mach Number C_a [Kg/N.m] C_b [Kg/N.s] BPR Entry into service Dry Mass [lb] Dry Mass [kg] Number of spools Fan Diameter [in] Fan Diameter [m] Length [in] Length [m] Width/Diameter [in] Width/Diameter [m] Engine Volume [m^3]
Allison (RollsRoyce) AE3007A ERJ135ER, ERJ145ER 7580 33717.5076 NA NA 0.360 1.0115E-05 0.650 1.8266E-05 24.00 NA NA NA 0.80 NA NA 5.30 1991 1586 719.3969 2 38.5 0.9779 106.50 2.7051 43.5 1.1049 2.5937
Allison (Rolls-Royce) AE3007A1 ERJ-135ER, ERJ-145ER 7580 33717.5076 NA NA 0.360 1.0115E-05 0.650 1.8266E-05 24.00 NA NA NA 0.80 NA NA 5.30 1991 1586 719.3969 2 38.5 0.9779 106.50 2.7051 43.5 1.1049 2.5937
Allison (Rolls-Royce) AE3007A1/1 ERJ-135ER/LR, ERJ-145LR 7580 33717.5076 NA NA 0.390 1.0958E-05 0.650 1.8266E-05 NA NA NA NA 0.80 NA NA 5.30 1991 1586 719.3969 2 38.5 0.9779 106.50 2.7051 43.5 1.1049 2.5937
Allison (Rolls-Royce) AE3007A1/3 ERJ-135LR, ERJ-140, Legacy Corporate Shuttle 7200 32027.1840 NA NA 0.390 1.0958E-05 0.650 1.8266E-05 NA NA NA NA 0.80 NA NA 5.30 1991 1586 719.3969 2 38.5 0.9779 106.50 2.7051 43.5 1.1049 2.5937
Allison (Rolls-Royce) AE3007A1E ERJ-145XR 8110 36075.0642 NA NA 0.390 1.0958E-05 0.650 1.8266E-05 NA NA NA NA 0.80 NA NA 5.30 1991 1586 719.3969 2 38.5 0.9779 106.50 2.7051 43.5 1.1049 2.5937
Allison (Rolls-Royce) AE3007A1P ERJ-145LR, Legacy Executive  7580 33717.5076 NA NA 0.390 1.0958E-05 0.650 1.8266E-05 NA NA NA NA 0.80 NA NA 5.30 1991 1586 719.3969 2 38.5 0.9779 106.50 2.7051 43.5 1.1049 2.5937
Allison (Rolls-Royce) AE3007A3 ERJ-135 7000 31137.5400 NA NA 0.390 1.0958E-05 0.650 1.8266E-05 NA NA NA NA 0.80 NA NA 5.30 1991 1586 719.3969 2 38.5 0.9779 106.50 2.7051 43.5 1.1049 2.5937
Allison (Rolls-Royce) AE3007C Citation X 6442 28655.4332 NA NA 0.390 1.0958E-05 0.650 1.8266E-05 NA NA NA NA 0.80 NA NA 5.30 1991 1586 719.3969 2 38.5 0.9779 106.50 2.7051 43.5 1.1049 2.5937
Allison (Rolls-Royce) AE3007C1 Citation X  6764 30087.7601 NA NA 0.390 1.0958E-05 0.650 1.8266E-05 NA NA NA NA 0.80 NA NA 5.30 1991 1586 719.3969 2 38.5 0.9779 106.50 2.7051 43.5 1.1049 2.5937
Ivchenko (Klimov) AI-25 Yak-40 3300 14679.1260 976 4341.463 0.570 1.6015E-05 0.795 2.2340E-05 8.00 20000 6.096 248.536 0.50 4.7253E-08 1.4874E-05 2.10 1966 705 319.7824 2 NA NA 78.50 1.9939 35.3 0.8966 1.2590
Ivchenko (Klimov) AI-25A Yak-40A 3850 17125.6470 NA NA NA NA NA NA NA NA NA NA NA NA NA 2.10 NA NA NA 2 NA NA NA NA NA NA NA
Avco Lycoming ALF301  Technology demonstrator 2730 12143.6406 NA NA 0.440 1.2363E-05 NA NA 9.00 NA NA NA NA NA NA 5.60 NA NA NA 2 NA NA NA NA NA NA NA
Avco Lycoming ALF501 Technology demonstrator 5800 25799.6760 NA NA 0.400 1.1239E-05 NA NA 9.30 NA NA NA NA NA NA 6.00 NA NA NA 2 NA NA NA NA NA NA NA
Avco Lycoming ALF502L Challenger 600 7500 33361.6500 2150 9563.673 0.428 1.2026E-05 0.730 2.0514E-05 13.60 30000 9.144 228.724 0.75 4.3099E-08 1.0714E-05 5.20 1980 1311 594.6591 2 NA NA 65.60 1.6662 50.0 1.2700 2.1107
Avco Lycoming ALF502L-2 Challenger 600 7500 33361.6500 7500 33361.650 0.428 1.2026E-05 0.730 2.0514E-05 13.60 30000 9.144 228.724 0.75 4.3099E-08 1.0714E-05 5.70 1980 1311 594.6591 2 NA NA 65.60 1.6662 50.0 1.2700 2.1107
Avco Lycoming ALF502L-2A Challenger 600 7500 33361.6500 7500 33361.650 0.414 1.1632E-05 0.730 2.0514E-05 13.80 30000 9.144 228.724 0.75 4.4640E-08 1.0363E-05 5.00 1980 1311 594.6591 2 NA NA 65.60 1.6662 50.0 1.2700 2.1107
Avco Lycoming ALF502L-2C Challenger 600 7500 33361.6500 7500 33361.650 0.414 1.1632E-05 0.730 2.0514E-05 13.80 30000 9.144 228.724 0.75 4.4640E-08 1.0363E-05 5.00 1980 1311 594.6591 2 NA NA 65.60 1.6662 50.0 1.2700 2.1107
Avco Lycoming ALF502L-3 Challenger 600 7800 34696.1160 7500 33361.650 0.415 1.1660E-05 0.730 2.0514E-05 13.80 30000 9.144 228.724 0.75 4.4530E-08 1.0388E-05 5.00 1980 1311 594.6591 2 NA NA 65.60 1.6662 50.0 1.2700 2.1107
Avco Lycoming ALF502R-1  NA NA NA 2250 10008.495 0.411 1.1548E-05 0.720 2.0233E-05 NA 25000 7.620 238.630 0.70 4.4859E-08 1.0509E-05 5.71 1980 1336 605.9989 2 NA NA 63.80 1.6205 50.0 1.2700 2.0528
Avco Lycoming ALF502R-2 NA NA NA 2250 10008.495 0.411 1.1548E-05 0.720 2.0233E-05 NA 25000 7.620 238.630 0.70 4.4859E-08 1.0509E-05 5.71 1980 1336 605.9989 2 NA NA 63.80 1.6205 50.0 1.2700 2.0528
Avco Lycoming ALF502R-3 BAe 146-100  6700 29803.0740 2250 10008.495 0.411 1.1548E-05 0.720 2.0233E-05 11.60 25000 7.620 238.630 0.70 4.4859E-08 1.0509E-05 5.71 1980 1336 605.9989 2 NA NA 63.80 1.6205 50.0 1.2700 2.0528
Avco Lycoming ALF502R-3A BAe 146-100 6970 31004.0934 2250 10008.495 0.408 1.1464E-05 0.720 2.0233E-05 11.60 25000 7.620 238.630 0.70 4.5213E-08 1.0432E-05 5.71 1980 1336 605.9989 2 NA NA 63.80 1.6205 50.0 1.2700 2.0528
Avco Lycoming ALF502R-4 NA 6970 31004.0934 2250 10008.495 0.408 1.1464E-05 0.720 2.0233E-05 NA 25000 7.620 238.630 0.70 4.5213E-08 1.0432E-05 5.60 1980 1336 605.9989 2 NA NA 63.80 1.6205 50.0 1.2700 2.0528
Avco Lycoming ALF502R-5  BAe 146-100/-200/-200ER/-300 6970 31004.0934 2250 10008.495 0.408 1.1464E-05 0.720 2.0233E-05 12.20 25000 7.620 238.630 0.70 4.5213E-08 1.0432E-05 5.60 1982 1336 605.9989 2 NA NA 63.80 1.6205 50.0 1.2700 2.0528
Avco Lycoming ALF502R-6 BAe 146-200/-200ER/-300 7500 33361.6500 2250 10008.495 0.415 1.1660E-05 0.720 2.0233E-05 13.80 25000 7.620 238.630 0.70 4.4387E-08 1.0611E-05 5.60 1980 1375 623.6890 2 NA NA 65.60 1.6662 50.0 1.2700 2.1107
AlliedSignal (Honeywell) AS905 Falcon 7X (candidate engine) NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 2005 NA NA NA NA NA NA NA NA NA NA
AlliedSignal (Honeywell) AS907 Challenger 300  6500 28913.4300 NA NA 0.420 1.1801E-05 NA NA 21.00 NA NA NA 0.82 NA NA 4.50 2001 1364 618.6995 2 34.2 0.8687 92.40 2.3470 46.3 1.1760 2.5493
AlliedSignal (Honeywell) AS977-1A RJX-70/-85/-100/-115, SL-100 (not produced) 7100 31582.3620 NA NA 0.416 1.1688E-05 NA NA 23.00 NA NA NA NA NA NA 4.50 2001 1364 618.6995 2 34.2 0.8687 92.40 2.3470 49.9 1.2675 2.9612
Turbomeca Astafan 2 NA 1685 7495.2507 NA NA 0.380 1.0677E-05 NA NA 8.50 NA NA NA NA NA NA 1.00 NA NA NA 1 NA NA NA NA NA NA NA
Turbomeca Astafan 3 NA 1900 8451.6180 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 1 NA NA NA NA NA NA NA
Turbomeca Astafan 4 NA 2414 10738.0031 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 1 NA NA NA NA NA NA NA
Garrett ATF3 Sabreliner 60, HFB 330 4050 18015.2910 NA NA 0.440 1.2363E-05 NA NA 17.00 NA NA NA NA NA NA 3.00 NA NA NA 3 NA NA NA NA NA NA NA
Garrett ATF3-6 Falcon 10, Learjet 31/31A, SA-28T 5200 23130.7440 1099 4888.594 0.520 1.4611E-05 0.810 2.2762E-05 21.00 40026 12.200 216.650 0.80 4.2759E-08 1.2669E-05 2.90 1981 1124 509.8374 3 NA NA 102.00 2.5908 33.6 0.8534 1.4821
Turbomeca Aubisque 1A Saab 105 1635 7272.8397 NA NA 0.600 1.6858E-05 NA NA 6.90 NA NA NA NA NA NA 2.00 NA NA NA 1 NA NA NA NA NA NA NA
Rolls-Royce Avon RA.25 Mk.502 Comet 2 6500 28913.4300 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 1 NA NA NA NA NA NA NA
Rolls-Royce Avon RA.25 Mk.503 Comet 2 6500 28913.4300 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 1 NA NA NA NA NA NA NA
Rolls-Royce Avon RA.25 Mk.504 Comet 2E 6500 28913.4300 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 1 NA NA NA NA NA NA NA
Rolls-Royce Avon RA.26 Mk.522 Comet 4 10000 44482.2000 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 1 NA NA NA NA NA NA NA
Rolls-Royce Avon RA.29 Mk.522 Caravelle 1 10500 46706.3100 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 1 NA NA NA NA NA NA NA
Rolls-Royce Avon RA.29 Mk.523 Comet 3 10500 46706.3100 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 1 NA NA NA NA NA NA NA
Rolls-Royce Avon RA.29/1 Mk.524 Comet 2E/4 10250 45594.2550 NA NA 0.786 2.2085E-05 NA NA 8.80 NA NA NA NA NA NA NA NA 3340 1514.9973 1 NA NA 126.00 3.2004 39.0 0.9906 2.4666
Rolls-Royce Avon RA.29/1 Mk.525B Comet 4B/4C 10498 46697.4136 NA NA NA NA NA NA 8.80 NA NA NA NA NA NA NA NA 3340 1514.9973 1 NA NA 126.00 3.2004 39.0 0.9906 2.4666
Rolls-Royce Avon RA.29/1 Mk.526 Caravelle 1A 10250 45594.2550 NA NA 0.786 2.2085E-05 NA NA 8.80 NA NA NA NA NA NA NA NA 3340 1514.9973 1 NA NA 126.00 3.2004 39.0 0.9906 2.4666
Rolls-Royce Avon RA.29/3 Mk.527B Caravelle 3 11400 50709.7080 NA NA 0.853 2.3967E-05 NA NA NA NA NA NA NA NA NA NA NA 3350 1519.5332 1 NA NA 126.00 3.2004 39.0 0.9906 2.4666
Rolls-Royce Avon RA.29/6 Mk.531B Caravelle 6N 12200 54268.2840 NA NA 0.802 2.2534E-05 NA NA NA NA NA NA NA NA NA NA NA 3490 1583.0361 1 NA NA 134.00 3.4036 39.0 0.9906 2.6232
Rolls-Royce Avon RA.29/6 Mk.533R Caravelle 6R 12600 56047.5720 NA NA 0.785 2.2056E-05 NA NA NA NA NA NA NA NA NA NA NA NA NA 1 NA NA 134.00 3.4036 39.0 0.9906 2.6232
Rolls-Royce Avon RA.29/6 Mk.535R Caravelle 6R 12600 56047.5720 NA NA 0.785 2.2056E-05 NA NA 10.30 NA NA NA NA NA NA NA NA NA NA 1 NA NA 134.00 3.4036 39.0 0.9906 2.6232
Rolls-Royce Avon RA.7 Mk.117 Comet 2R 7350 32694.4170 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 1 NA NA NA NA NA NA NA
Turbomeca Bastafan NA 1765 7851.1083 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 1 NA NA NA NA NA NA NA
BMW/Rolls-Royce (Rolls-Royce Deutschland) BR710 Tu-334-120 14845 66033.8259 3480 15479.806 0.390 1.0958E-05 0.640 1.7985E-05 25.70 35000 10.668 218.818 0.80 3.5560E-08 9.5489E-06 4.00 1996 3520 1596.6438 2 48.0 1.2192 NA NA NA NA NA
BMW/Rolls-Royce (Rolls-Royce Deutschland) BR710A1-10 G500 (Gulfstream V), G550 (Gulfstream V-SP) 14750 65611.2450 3480 15479.806 0.390 1.0958E-05 0.640 1.7985E-05 25.70 35000 10.668 218.818 0.80 3.5560E-08 9.5489E-06 4.20 1996 3520 1596.6438 2 48.0 1.2192 87.00 2.2098 52.9 1.3437 3.1334
BMW/Rolls-Royce (Rolls-Royce Deutschland) BR710A2-20 Global Express, Global Express XRS, Global 5000 14750 65611.2450 3480 15479.806 0.390 1.0958E-05 0.640 1.7985E-05 25.70 35000 10.668 218.818 0.80 3.5560E-08 9.5489E-06 4.20 1996 3520 1596.6438 2 48.0 1.2192 87.00 2.2098 52.9 1.3437 3.1334
BMW/Rolls-Royce (Rolls-Royce Deutschland) BR710C4-11 G500 (Gulfstream V), G550 (Gulfstream V-SP) 14750 65611.2450 3480 15479.806 0.390 1.0958E-05 0.640 1.7985E-05 25.70 35000 10.668 218.818 0.80 3.5560E-08 9.5489E-06 4.20 1996 3520 1596.6438 2 48.0 1.2192 87.00 2.2098 52.9 1.3437 3.1334
BMW/Rolls-Royce (Rolls-Royce Deutschland) BR715-55 Tu-354 (Tu-334-200) (proposed) 19883 88443.9583 4380 19483.204 0.370 1.0396E-05 0.620 1.7423E-05 32.10 35000 10.668 218.818 0.80 3.5255E-08 9.0592E-06 4.70 1996 4546 2062.0292 2 56.0 1.4224 NA NA NA NA NA
BMW/Rolls-Royce (Rolls-Royce Deutschland) BR715A1-30 717-200 18500 82292.0700 4380 19483.204 0.370 1.0396E-05 0.620 1.7423E-05 32.10 35000 10.668 218.818 0.80 3.5255E-08 9.0592E-06 4.70 1998 4600 2086.5232 2 56.0 1.4224 93.00 2.3622 60.2 1.5291 4.3378
BMW/Rolls-Royce (Rolls-Royce Deutschland) BR715B1-30 717-200 (option) 20000 88964.4000 4380 19483.204 0.370 1.0396E-05 0.620 1.7423E-05 NA 35000 10.668 218.818 0.80 3.5255E-08 9.0592E-06 4.02 1998 4600 2086.5232 2 56.0 1.4224 NA NA NA NA NA
BMW/Rolls-Royce (Rolls-Royce Deutschland) BR715C1-30 717-200 HGW 21000 93412.6200 4380 19483.204 0.370 1.0396E-05 0.620 1.7423E-05 32.60 35000 10.668 218.818 0.80 3.5255E-08 9.0592E-06 5.00 1998 4600 2086.5232 2 56.0 1.4224 93.00 2.3622 60.2 1.5291 4.3378
BMW/Rolls-Royce (Rolls-Royce Deutschland) BR720 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 2 NA NA NA NA NA NA NA
GE CF34-10A ARJ21 18000 80067.9600 15490 68902.928 0.380 1.0677E-05 0.650 1.8266E-05 NA 42265 12.882 216.650 0.82 3.7230E-08 9.2579E-06 5.10 NA 1526 692.1814 2 NA NA NA NA NA NA NA
GE CF34-10D5 928-100 (not produced) 17355 77198.8581 15490 68902.928 0.380 1.0677E-05 0.650 1.8266E-05 29.00 42265 12.882 216.650 0.82 3.7230E-08 9.2579E-06 5.00 NA 3800 1723.6496 2 NA NA 90.00 2.2860 57.0 1.4478 3.7634
GE CF34-10D6 928-200 (not produced) 18750 83404.1250 15490 68902.928 0.380 1.0677E-05 0.650 1.8266E-05 29.00 42265 12.882 216.650 0.82 3.7230E-08 9.2579E-06 5.00 NA 3800 1723.6496 2 NA NA 90.00 2.2860 57.0 1.4478 3.7634
GE CF34-10E5 ERJ-190/-190AR, ERJ-195/-195AR 18500 82292.0700 15490 68902.928 0.380 1.0677E-05 0.640 1.7985E-05 NA 42265 12.882 216.650 0.82 3.6068E-08 9.2579E-06 5.40 NA 3800 1723.6496 2 NA NA 90.00 2.2860 57.0 1.4478 3.7634
GE CF34-1A Challenger 601-1A 8650 38477.1030 NA NA 0.360 1.0115E-05 NA NA NA NA NA NA NA NA NA 6.02 NA 1630 739.3550 2 44.0 1.1176 103.00 2.6162 49.0 1.2446 3.1829
GE CF34-3A Challenger 601-3A 9220 41012.5884 NA NA 0.357 1.0031E-05 0.700 1.9671E-05 21.00 37000 11.278 216.650 0.70 5.3128E-08 8.6975E-06 6.20 1996 1630 739.3550 2 44.0 1.1176 103.00 2.6162 49.0 1.2446 3.1829
GE CF34-3A1 CRJ100/200 9220 41012.5884 NA NA 0.357 1.0031E-05 0.700 1.9671E-05 21.00 37000 11.278 216.650 0.70 5.3128E-08 8.6975E-06 6.30 1996 1660 752.9627 2 44.0 1.1176 103.00 2.6162 49.0 1.2446 3.1829
GE CF34-3B CRJ100/200, Challenger 604, Challenger 800 9220 41012.5884 NA NA 0.346 9.7217E-06 0.700 1.9671E-05 NA 39000 11.887 216.650 0.76 5.0128E-08 8.4295E-06 6.30 1996 1670 757.4986 2 44.0 1.1176 103.00 2.6162 49.0 1.2446 3.1829
GE CF34-3B1 CRJ100/200/200ER/200LR, Challenger 604, Challenger 800 9220 41012.5884 NA NA 0.346 9.7217E-06 0.700 1.9671E-05 21.00 39000 11.887 216.650 0.76 5.0128E-08 8.4295E-06 6.30 1996 1670 757.4986 2 44.0 1.1176 103.00 2.6162 49.0 1.2446 3.1829
GE CF34-8C1 CRJ700-701/-701ER 13790 61340.9538 NA NA 0.370 1.0396E-05 0.680 1.9109E-05 27.00 NA NA NA NA NA NA 4.90 NA 2350 1065.9412 2 46.2 1.1735 128.00 3.2512 52.0 1.3208 4.4546
GE CF34-8C5 CRJ700-705/-705ER, CRJ900/900ER 14500 64499.1900 NA NA 0.390 1.0958E-05 0.680 1.9109E-05 NA NA NA NA NA NA NA 4.90 NA 2470 1120.3722 2 46.2 1.1735 128.00 3.2512 52.0 1.3208 4.4546
GE CF34-8C5A1 NA NA NA NA NA NA NA 0.680 1.9109E-05 NA NA NA NA NA NA NA 4.90 NA 2470 1120.3722 2 46.2 1.1735 128.00 3.2512 52.0 1.3208 4.4546
GE CF34-8C5A2 NA NA NA NA NA NA NA 0.680 1.9109E-05 NA NA NA NA NA NA NA 4.90 NA 2470 1120.3722 2 46.2 1.1735 128.00 3.2512 52.0 1.3208 4.4546
GE CF34-8C5A3 NA NA NA NA NA NA NA 0.680 1.9109E-05 NA NA NA NA NA NA NA 4.90 NA 2470 1120.3722 2 46.2 1.1735 128.00 3.2512 52.0 1.3208 4.4546
GE CF34-8C5B1 CRJ700-705LR 14255 63409.3761 NA NA NA NA 0.680 1.9109E-05 NA NA NA NA NA NA NA 4.90 NA 2470 1120.3722 2 46.2 1.1735 128.00 3.2512 52.0 1.3208 4.4546
GE CF34-8D1 728-100, 528-100 (not produced) 12500 55602.7500 NA NA 0.390 1.0958E-05 NA NA NA NA NA NA NA NA NA NA NA 2470 1120.3722 2 46.2 1.1735 128.00 3.2512 52.0 1.3208 4.4546
GE CF34-8D3 728-200 (not produced) 12875 57270.8325 NA NA 0.390 1.0958E-05 NA NA 27.00 NA NA NA NA NA NA 4.90 NA 2470 1120.3722 2 46.2 1.1735 128.00 3.2512 52.0 1.3208 4.4546
GE CF34-8D5 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 2470 1120.3722 2 46.2 1.1735 128.00 3.2512 52.0 1.3208 4.4546
GE CF34-8D6 Envoy 7 (not produced) 13050 58049.2710 NA NA 0.390 1.0958E-05 NA NA NA NA NA NA NA NA NA NA NA 2470 1120.3722 2 46.2 1.1735 128.00 3.2512 52.0 1.3208 4.4546
GE CF34-8E2 ERJ-170, ERJ-170LR (option) 14000 62275.0800 NA NA 0.390 1.0958E-05 0.680 1.9109E-05 27.00 NA NA NA NA NA NA 5.10 NA 2470 1120.3722 2 46.2 1.1735 128.00 3.2512 52.0 1.3208 4.4546
GE CF34-8E2A1 NA NA NA NA NA NA NA 0.680 1.9109E-05 NA NA NA NA NA NA NA 4.64 NA NA NA 2 46.2 1.1735 128.00 3.2512 52.0 1.3208 4.4546
GE CF34-8E5 ERJ-170LR, ERJ-170 (option) NA NA NA NA NA NA 0.680 1.9109E-05 NA NA NA NA NA NA NA 5.10 NA NA NA 2 46.2 1.1735 128.00 3.2512 52.0 1.3208 4.4546
GE CF34-8E5A1 ERJ-170/-170LR (option) NA NA NA NA NA NA 0.680 1.9109E-05 NA NA NA NA NA NA NA 5.10 NA NA NA 2 46.2 1.1735 128.00 3.2512 52.0 1.3208 4.4546
GE CF34-8E5A2 NA NA NA NA NA NA NA 0.680 1.9109E-05 NA NA NA NA NA NA NA 5.10 NA NA NA 2 46.2 1.1735 128.00 3.2512 52.0 1.3208 4.4546
GE CF34-8E6 NA NA NA NA NA NA NA 0.680 1.9109E-05 NA NA NA NA NA NA NA 5.10 NA NA NA 2 46.2 1.1735 128.00 3.2512 52.0 1.3208 4.4546
GE CF34-8E6A1 NA NA NA NA NA NA NA 0.680 1.9109E-05 NA NA NA NA NA NA NA 5.10 NA NA NA 2 46.2 1.1735 128.00 3.2512 52.0 1.3208 4.4546
GE CF6-45A 747-100SR/-100SR(SF) 46500 206842.2300 11250 50042.475 0.350 9.8341E-06 0.630 1.7704E-05 26.30 35000 10.668 218.818 0.80 3.8503E-08 8.5695E-06 4.64 1976 8768 3977.0947 2 86.4 2.1946 188.00 4.7752 105.0 2.6670 26.6764
GE CF6-45A2 747-100SR/-100SR(SF) 46500 206842.2300 11250 50042.475 0.350 9.8341E-06 0.630 1.7704E-05 26.30 35000 10.668 218.818 0.80 3.8503E-08 8.5695E-06 4.64 1976 8768 3977.0947 2 86.4 2.1946 188.00 4.7752 105.0 2.6670 26.6764
GE CF6-45B 747-100SR/-100SR(SF) 46500 206842.2300 11250 50042.475 0.350 9.8341E-06 0.630 1.7704E-05 26.30 35000 10.668 218.818 0.80 3.8503E-08 8.5695E-06 4.64 1976 8768 3977.0947 2 86.4 2.1946 188.00 4.7752 105.0 2.6670 26.6764
GE CF6-45B2 747-100SR/-100SR(SF), A300B10 (A310) (candidate engine) 46500 206842.2300 11250 50042.475 0.350 9.8341E-06 0.630 1.7704E-05 26.30 35000 10.668 218.818 0.80 3.8503E-08 8.5695E-06 4.64 1976 8768 3977.0947 2 86.4 2.1946 188.00 4.7752 105.0 2.6670 26.6764
GE CF6-50 DC-10-30/-30F 49000 217962.7800 NA NA NA NA 0.645 1.8125E-05 NA 35000 10.668 218.818 0.80 NA NA 4.40 1970 8100 3674.0952 2 92.0 2.3368 183.00 4.6482 92.0 2.3368 19.9351
GE CF6-50A DC-10-30/-30F, A300B1, A300B2-1A 48334 215000.2655 11250 50042.475 0.389 1.0930E-05 0.654 1.8378E-05 28.60 35000 10.668 218.818 0.80 3.7321E-08 9.5244E-06 4.40 1970 8200 3719.4544 2 86.4 2.1946 183.00 4.6482 92.0 2.3368 19.9351
GE CF6-50B NA 49000 217962.7800 11250 50042.475 0.389 1.0930E-05 0.654 1.8378E-05 28.60 35000 10.668 218.818 0.80 3.7321E-08 9.5244E-06 4.40 1970 8200 3719.4544 2 86.4 2.1946 183.00 4.6482 92.0 2.3368 19.9351
GE CF6-50C A300B1, A300B2-1C/-101, A300B4-2C/-203, DC-10-30/-30CF/-30F 50357 223999.0145 11100 49375.242 0.394 1.1070E-05 0.657 1.8462E-05 29.30 35000 10.668 218.818 0.80 3.7161E-08 9.6469E-06 4.26 1972 8720 3955.3222 2 86.4 2.1946 183.00 4.6482 105.0 2.6670 25.9669
GE CF6-50C1 DC-10-30, A300B2-202, A300B4-102 51818 230497.8640 11555 51399.182 0.371 1.0424E-05 0.657 1.8462E-05 30.10 35000 10.668 218.818 0.80 3.9534E-08 9.0837E-06 4.24 1970 8720 3955.3222 2 86.4 2.1946 183.00 4.6482 105.0 2.6670 25.9669
GE CF6-50C2 A300B2-203, A300B4-103/-103F/-2C/-203/-203F, A300C4-203, A300F4-203, DC-10-30/-30F/-30F(CF), A300B1 (option) 51818 230497.8640 11555 51399.182 0.371 1.0424E-05 0.630 1.7704E-05 30.40 35000 10.668 218.818 0.80 3.6336E-08 9.0837E-06 4.31 1972 8730 3959.8582 2 86.4 2.1946 183.00 4.6482 105.0 2.6670 25.9669
GE CF6-50C2B DC-10-30/-30ER 54000 240203.8800 11555 51399.182 0.385 1.0817E-05 0.630 1.7704E-05 31.10 35000 10.668 218.818 0.80 3.4891E-08 9.4265E-06 4.25 1970 8730 3959.8582 2 86.4 2.1946 183.00 4.6482 105.0 2.6670 25.9669
GE CF6-50C2F DC-10-15 46500 206842.2300 11555 51399.182 0.370 1.0396E-05 0.630 1.7704E-05 26.30 35000 10.668 218.818 0.80 3.6439E-08 9.0592E-06 4.64 1970 8730 3959.8582 2 86.4 2.1946 183.00 4.6482 105.0 2.6670 25.9669
GE CF6-50C2R A300B2-1C/-101, A300B2K-3C, A300B4-2C, DC-10-30 50357 223999.0145 11555 51399.182 0.368 1.0340E-05 0.630 1.7704E-05 29.20 35000 10.668 218.818 0.80 3.6646E-08 9.0103E-06 4.31 NA 8730 3959.8582 2 86.4 2.1946 183.00 4.6482 105.0 2.6670 25.9669
GE CF6-50D DC-10-10 51000 226859.2200 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 8330 3778.4214 2 86.4 2.1946 183.00 4.6482 105.0 2.6670 25.9669
GE CF6-50D1 (see military turbofan specifications) 51000 226859.2200 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA
GE CF6-50E 747-200B 52500 233531.5500 11555 51399.182 0.376 1.0565E-05 0.657 1.8462E-05 30.10 35000 10.668 218.818 0.80 3.9018E-08 9.2061E-06 4.24 1971 8490 3850.9961 2 86.4 2.1946 183.00 4.6482 105.0 2.6670 25.9669
GE CF6-50E1 747-200B 52500 233531.5500 11555 51399.182 0.371 1.0424E-05 0.657 1.8462E-05 30.10 35000 10.668 218.818 0.80 3.9534E-08 9.0837E-06 4.24 1971 8490 3850.9961 2 86.4 2.1946 183.00 4.6482 105.0 2.6670 25.9669
GE CF6-50E2 747-200B/-200B(M)/-200B(SF)/-200C(M)/-200F/-300/-300(M)/-300(SF) 52500 233531.5500 11555 51399.182 0.371 1.0424E-05 0.630 1.7704E-05 30.40 35000 10.668 218.818 0.80 3.6336E-08 9.0837E-06 4.31 1971 8770 3978.0018 2 86.4 2.1946 183.00 4.6482 105.0 2.6670 25.9669
GE CF6-50E2B 747-200/-300 (option) 54000 240203.8800 11730 52177.621 0.375 1.0537E-05 0.630 1.7704E-05 30.90 35000 10.668 218.818 0.80 3.5923E-08 9.1817E-06 4.24 1971 8770 3978.0018 2 86.4 2.1946 183.00 4.6482 105.0 2.6670 25.9669
GE CF6-6 DC-10-10 (option) 40000 177928.8000 9080 40389.838 0.350 9.8341E-06 0.646 1.8153E-05 26.60 35000 10.668 218.818 0.80 4.0399E-08 8.5695E-06 6.20 1970 7350 3333.9012 2 NA NA 172.50 4.3815 92.0 2.3368 18.7913
GE CF6-6D DC-10-10/-10F/-10F(CF) 40000 177928.8000 9080 40389.838 0.354 9.9465E-06 0.646 1.8153E-05 24.30 35000 10.668 218.818 0.80 3.9986E-08 8.6675E-06 5.72 NA 7900 3583.3768 2 86.4 2.1946 188.00 4.7752 105.0 2.6670 26.6764
GE CF6-6D1 DC-10-10/-10F/-10F(AF) 41500 184601.1300 9220 41012.588 0.350 9.8341E-06 0.646 1.8153E-05 25.20 35000 10.668 218.818 0.80 4.0399E-08 8.5695E-06 5.76 1970 7900 3583.3768 2 86.4 2.1946 188.00 4.7752 105.0 2.6670 26.6764
GE CF6-6D1A DC-10-10/-10F/-10F(AF) 41500 184601.1300 9220 41012.588 0.350 9.8341E-06 0.646 1.8153E-05 25.20 35000 10.668 218.818 0.80 4.0399E-08 8.5695E-06 5.76 1970 7900 3583.3768 2 86.4 2.1946 188.00 4.7752 105.0 2.6670 26.6764
GE CF6-6E DC-10-10/-10F (option) 40600 180597.7320 NA NA 0.320 8.9911E-06 NA NA NA NA NA NA NA NA NA NA NA NA NA 2 86.4 2.1946 NA NA NA NA NA
GE CF6-6F DC-10-10/-10F (option) 42000 186825.2400 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 2 86.4 2.1946 NA NA NA NA NA
GE CF6-6K DC-10-10/-10F 41500 184601.1300 NA NA 0.346 9.7217E-06 NA NA 25.00 NA NA NA NA NA NA NA NA 8180 3710.3826 2 86.4 2.1946 188.00 4.7752 105.0 2.6670 26.6764
GE CF6-6K2 DC-10-10/-10F (option) 41500 184601.1300 NA NA 0.346 9.7217E-06 NA NA 25.00 NA NA NA NA NA NA NA NA 8180 3710.3826 2 86.4 2.1946 188.00 4.7752 105.0 2.6670 26.6764
GE CF6-80A 767-200/-200ER/-200PC 48000 213514.5600 11045 49130.590 0.344 9.6655E-06 0.623 1.7507E-05 27.30 35000 10.668 218.818 0.80 3.8294E-08 8.4226E-06 4.66 1981 8500 3855.5320 2 86.4 2.1946 157.40 3.9980 98.0 2.4892 19.4557
GE CF6-80A1 767-200/-200ER (option) 48000 213514.5600 11045 49130.590 0.344 9.6655E-06 0.623 1.7507E-05 27.30 35000 10.668 218.818 0.80 3.8294E-08 8.4226E-06 4.66 1981 8420 3819.2446 2 86.4 2.1946 157.40 3.9980 98.0 2.4892 19.4557
GE CF6-80A2 767-200/-200ER/-300 50000 222411.0000 11045 49130.590 0.349 9.8060E-06 0.623 1.7507E-05 28.40 35000 10.668 218.818 0.80 3.7777E-08 8.5451E-06 4.59 1981 8500 3855.5320 2 86.4 2.1946 157.40 3.9980 98.0 2.4892 19.4557
GE CF6-80A3 A310-203/-203F 48986 217900.5049 11045 49130.590 0.357 1.0031E-05 0.623 1.7507E-05 28.40 35000 10.668 218.818 0.80 3.6952E-08 8.7409E-06 4.59 1982 8420 3819.2446 2 86.4 2.1946 157.40 3.9980 98.0 2.4892 19.4557
GE CF6-80C2 767-200ER/-300 (option) 52500 233531.5500 11330 50398.333 0.329 9.2440E-06 0.564 1.5849E-05 30.40 35000 10.668 218.818 0.85 3.0920E-08 8.0554E-06 5.20 NA 9140 4145.8309 2 93.0 2.3622 160.90 4.0869 NA NA NA
GE CF6-80C2A1 A300B4-601 57866 257400.6985 11810 52533.478 0.334 9.3845E-06 0.576 1.6186E-05 30.40 35000 10.668 218.818 0.80 3.3758E-08 8.1778E-06 5.15 1972 9360 4245.6211 2 93.0 2.3622 160.90 4.0869 106.0 2.6924 23.2680
GE CF6-80C2A2 A310-204/-304/-304ET/-304F 52460 233353.6212 11330 50398.333 0.317 8.9069E-06 0.578 1.6242E-05 27.80 35000 10.668 218.818 0.80 3.5750E-08 7.7616E-06 5.05 1982 9360 4245.6211 2 93.0 2.3622 160.90 4.0869 106.0 2.6924 23.2680
GE CF6-80C2A3 A300B4-603, MD-11 (option) 58950 262222.5690 11340 50442.815 0.329 9.2440E-06 0.576 1.6186E-05 31.10 35000 10.668 218.818 0.80 3.4274E-08 8.0554E-06 5.05 1972 9360 4245.6211 2 93.0 2.3622 160.90 4.0869 106.0 2.6924 23.2680
GE CF6-80C2A5 A300B4-605R, A300C4-605R, A300F4-605R 60100 267338.0220 11340 50442.815 0.340 9.5531E-06 0.585 1.6439E-05 31.50 35000 10.668 218.818 0.80 3.4205E-08 8.3247E-06 5.05 1987 9390 4259.2289 2 93.0 2.3622 160.90 4.0869 106.0 2.6924 23.2680
GE CF6-80C2A5F A300B4-605R, A300C4-605R, A300F4-605R 60100 267338.0220 11340 50442.815 0.340 9.5531E-06 0.585 1.6439E-05 31.50 35000 10.668 218.818 0.80 3.4205E-08 8.3247E-06 5.05 1987 9390 4259.2289 2 93.0 2.3622 160.90 4.0869 106.0 2.6924 23.2680
GE CF6-80C2A6 NA 64000 284686.0800 NA NA NA NA 0.564 1.5849E-05 NA NA NA NA NA NA NA 5.05 NA NA NA 2 NA NA NA NA NA NA NA
GE CF6-80C2A6F NA 63000 280237.8600 NA NA NA NA 0.564 1.5849E-05 NA NA NA NA NA NA NA 5.05 NA NA NA 2 NA NA NA NA NA NA NA
GE CF6-80C2A7 A310-308, A310-308ET (option) 59000 262444.9800 NA NA NA NA 0.564 1.5849E-05 NA NA NA NA NA NA NA 5.05 NA 9390 4259.2289 2 93.0 2.3622 160.90 4.0869 106.0 2.6924 23.2680
GE CF6-80C2A8 A300B4-608ST, A310-308/-308ET 57866 257400.6985 NA NA 0.344 9.6655E-06 0.564 1.5849E-05 30.40 NA NA NA NA NA NA 5.05 NA 9390 4259.2289 2 93.0 2.3622 160.90 4.0869 106.0 2.6924 23.2680
GE CF6-80C2B1 747-300/-300(M) 56700 252214.0740 12820 57026.180 0.323 9.0754E-06 0.576 1.6186E-05 29.30 35000 10.668 218.818 0.80 3.4894E-08 7.9085E-06 5.19 1980 9390 4259.2289 2 93.0 2.3622 160.90 4.0869 106.0 2.6924 23.2680
GE CF6-80C2B10F 747-XQLRF NA NA NA NA NA NA 0.564 1.5849E-05 NA NA NA NA NA NA NA NA NA NA NA 2 93.0 2.3622 160.90 4.0869 106.0 2.6924 23.2680
GE CF6-80C2B1F 747-400/-400D/-400ER/-400(M)/-400F 57160 254260.2552 12820 57026.180 0.320 8.9911E-06 0.560 1.5737E-05 30.40 35000 10.668 218.818 0.80 3.3308E-08 7.8350E-06 5.15 1989 9500 4309.1240 2 93.0 2.3622 160.90 4.0869 106.0 2.6924 23.2680
GE CF6-80C2B1F2 747-400/-400D/-400ER/-400(M)/-400F 57900 257551.9380 12820 57026.180 0.320 8.9911E-06 0.564 1.5849E-05 NA 35000 10.668 218.818 0.80 3.3782E-08 7.8350E-06 5.19 1986 9500 4309.1240 2 93.0 2.3622 160.90 4.0869 106.0 2.6924 23.2680
GE CF6-80C2B2 767-200ER/-300/-300ER, 737-200 (option) 51590 229483.6698 12000 53378.640 0.318 8.9350E-06 0.576 1.6186E-05 27.10 35000 10.668 218.818 0.80 3.5410E-08 7.7860E-06 5.31 1981 9390 4259.2289 2 93.0 2.3622 160.90 4.0869 106.0 2.6924 23.2680
GE CF6-80C2B2F 767-200/-200ER/-300, 767-300ER (option) 52010 231351.9222 12000 53378.640 0.318 8.9350E-06 0.576 1.6186E-05 NA 35000 10.668 218.818 0.80 3.5410E-08 7.7860E-06 5.31 1986 9500 4309.1240 2 93.0 2.3622 160.90 4.0869 106.0 2.6924 23.2680
GE CF6-80C2B2F2 767-200/-200ER/-300, 767-300ER (option) NA NA 12000 53378.640 0.318 8.9350E-06 0.576 1.6186E-05 NA 35000 10.668 218.818 0.80 3.5410E-08 7.7860E-06 5.31 1986 9500 4309.1240 2 93.0 2.3622 160.90 4.0869 106.0 2.6924 23.2680
GE CF6-80C2B3 747-300/-400 (option) 52010 231351.9222 NA NA NA NA 0.564 1.5849E-05 NA NA NA NA NA NA NA NA NA 9390 4259.2289 2 93.0 2.3622 160.90 4.0869 106.0 2.6924 23.2680
GE CF6-80C2B3F 747-300/-400 (option) 52010 231351.9222 NA NA NA NA 0.564 1.5849E-05 NA NA NA NA NA NA NA NA NA 9500 4309.1240 2 93.0 2.3622 160.90 4.0869 106.0 2.6924 23.2680
GE CF6-80C2B4 767-200ER/-300/-300ER 57180 254349.2196 NA NA 0.330 9.2721E-06 0.564 1.5849E-05 29.90 NA NA NA NA NA NA 5.15 NA 9400 4263.7648 2 93.0 2.3622 160.90 4.0869 106.0 2.6924 23.2680
GE CF6-80C2B4F 767-200ER/-300/-300ER 57280 254794.0416 NA NA 0.317 8.9069E-06 0.564 1.5849E-05 29.90 NA NA NA NA NA NA 5.14 NA 9760 4427.0579 2 93.0 2.3622 160.90 4.0869 106.0 2.6924 23.2680
GE CF6-80C2B5F 747-400/-400ER/-400F/-400FER 62100 276234.4620 NA NA 0.323 9.0754E-06 0.564 1.5849E-05 31.40 NA NA NA NA NA NA NA NA 9760 4427.0579 2 93.0 2.3622 160.90 4.0869 106.0 2.6924 23.2680
GE CF6-80C2B6 767-300/-300ER, 767-200ER (option), An-218-200/-300 (proposed) 60070 267204.5754 NA NA 0.334 9.3845E-06 0.564 1.5849E-05 31.10 NA NA NA NA NA NA 5.06 NA 9670 4386.2346 2 93.0 2.3622 160.90 4.0869 106.0 2.6924 23.2680
GE CF6-80C2B6F 767-300ER, 767-200ER (option) 60030 267026.6466 NA NA 0.323 9.0754E-06 0.564 1.5849E-05 31.40 NA NA NA NA NA NA 5.06 NA 9760 4427.0579 2 93.0 2.3622 160.90 4.0869 106.0 2.6924 23.2680
GE CF6-80C2B6FA 767-200ER 60030 267026.6466 NA NA 0.323 9.0754E-06 0.564 1.5849E-05 31.40 NA NA NA NA NA NA 5.06 NA 9760 4427.0579 2 93.0 2.3622 160.90 4.0869 106.0 2.6924 23.2680
GE CF6-80C2B7F 767-300ER/-300F, 767-200ER (option) 62100 276234.4620 NA NA 0.323 9.0754E-06 0.564 1.5849E-05 31.40 NA NA NA NA NA NA NA NA 9760 4427.0579 2 93.0 2.3622 160.90 4.0869 106.0 2.6924 23.2680
GE CF6-80C2B8F 767-400ER/-400FER 63500 282461.9700 NA NA NA NA 0.564 1.5849E-05 31.40 NA NA NA NA NA NA NA NA 9970 4522.3122 2 93.0 2.3622 160.90 4.0869 106.0 2.6924 23.2680
GE CF6-80C2B9F 747-400XQLR/-XQLRF 63300 281572.3260 NA NA NA NA 0.564 1.5849E-05 31.40 NA NA NA NA NA NA NA NA NA NA 2 93.0 2.3622 160.90 4.0869 106.0 2.6924 23.2680
GE CF6-80C2D1F MD-11/-11F/-11F(AF)/-11F(C) 60690 269962.4718 NA NA 0.322 9.0473E-06 0.564 1.5849E-05 31.80 NA NA NA NA NA NA 5.03 NA 9850 4467.8812 2 93.0 2.3622 160.90 4.0869 106.0 2.6924 23.2680
GE CF6-80C2G2 767-400ERX, 747-400X (not produced) NA NA NA NA NA NA 0.564 1.5849E-05 NA NA NA NA NA NA NA NA NA NA NA 2 93.0 2.3622 160.90 4.0869 106.0 2.6924 23.2680
GE CF6-80C2L1F (see military turbofan specifications) NA NA NA NA NA NA 0.564 1.5849E-05 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA
GE CF6-80E1 A330-200/-300 (option) 65500 291358.4100 NA NA 0.329 9.2440E-06 NA NA 32.40 NA NA NA NA NA NA 5.30 NA 11160 5062.0867 2 NA NA 164.30 4.1732 114.0 2.8956 27.4814
GE CF6-80E1A1 A330-200/-300 (option) 65500 291358.4100 NA NA 0.329 9.2440E-06 0.570 1.6018E-05 32.40 39000 11.887 216.650 0.82 3.3074E-08 8.0154E-06 5.30 NA 11160 5062.0867 2 NA NA 164.30 4.1732 114.0 2.8956 27.4814
GE CF6-80E1A2 A330-201 64533 287056.9813 NA NA 0.332 9.3283E-06 0.570 1.6018E-05 32.40 39000 11.887 216.650 0.82 3.2772E-08 8.0885E-06 5.30 NA 11160 5062.0867 2 NA NA 164.30 4.1732 114.0 2.8956 27.4814
GE CF6-80E1A3 A330-203 68531 304840.9648 NA NA 0.335 9.4126E-06 0.570 1.6018E-05 33.70 39000 11.887 216.650 0.82 3.2470E-08 8.1615E-06 5.00 NA 10730 4867.0422 2 NA NA 171.00 4.3434 114.0 2.8956 28.6020
GE CF6-80E1A4 A330-202 66870 297452.4714 NA NA 0.338 9.4969E-06 0.570 1.6018E-05 33.70 39000 11.887 216.650 0.82 3.2167E-08 8.2346E-06 5.00 NA 10730 4867.0422 2 NA NA 171.00 4.3434 114.0 2.8956 28.6020
GE CF700-2B Falcon 20 4301 19131.7942 944 4199.120 0.670 1.8825E-05 0.930 2.6134E-05 6.80 36090 11.000 216.658 0.80 4.1561E-08 1.6323E-05 1.90 1962 736 333.8437 2 NA NA 53.60 1.3614 33.2 0.8433 0.7604
GE CF700-2C Falcon 20C 4125 18348.9075 944 4199.120 0.652 1.8319E-05 0.930 2.6134E-05 6.90 36090 11.000 216.658 0.80 4.3418E-08 1.5885E-05 1.90 1962 725 328.8542 2 NA NA 53.60 1.3614 33.2 0.8433 0.7604
GE CF700-2D Mystere 20, Falcon 20D 4250 18904.9350 944 4199.120 0.652 1.8319E-05 0.930 2.6134E-05 6.20 36090 11.000 216.658 0.80 4.3418E-08 1.5885E-05 1.90 1962 737 334.2973 2 NA NA 53.60 1.3614 33.2 0.8433 0.7604
GE CF700-2D2 Falcon 20E/F, Sabreliner 75A/80A 4315 19194.0693 944 4199.120 0.643 1.8067E-05 0.900 2.5291E-05 6.80 36090 11.000 216.658 0.80 4.0776E-08 1.5666E-05 1.90 1963 767 347.9051 2 NA NA 53.60 1.3614 37.0 0.9398 0.9444
CFE CFE738-1-1B  Falcon 2000  5725 25466.0595 1464 6512.194 0.372 1.0452E-05 0.645 1.8125E-05 23.00 40000 12.192 216.650 0.80 3.8391E-08 9.0630E-06 5.30 1993 1325 601.0094 2 35.5 0.9017 99.00 2.5146 48.0 1.2192 2.9357
CFM  CFM56-2A2 (see military turbofan specifications) 24000 106757.2800 6047 26898.386 0.360 1.0115E-05 0.660 1.8547E-05 25.40 35000 10.668 218.818 0.80 4.1025E-08 8.8144E-06 5.90 NA 4819 2185.8598 NA NA NA NA NA NA NA NA
CFM  CFM56-2A3 (see military turbofan specifications) NA NA 5760 25621.747 0.360 1.0115E-05 0.670 1.8828E-05 NA 35000 10.668 218.818 0.80 4.2210E-08 8.8144E-06 5.90 NA NA NA NA NA NA NA NA NA NA NA
CFM  CFM56-2B1  (see military turbofan specifications) 22000 97860.8400 4970 22107.653 0.360 1.0115E-05 0.650 1.8266E-05 23.70 35000 10.668 218.818 0.80 3.9840E-08 8.8144E-06 6.00 NA 4672 2119.1818 NA NA NA NA NA NA NA NA
CFM  CFM56-2C1 DC-8-71F/-72/-72F/-73F, DC-8-71/-73 (option) 22000 97860.8400 4980 22152.136 0.350 9.8341E-06 0.671 1.8856E-05 24.70 35000 10.668 218.818 0.80 4.3360E-08 8.5695E-06 6.00 1979 4635 2102.3989 2 68.3 1.7348 95.70 2.4308 72.0 1.8288 6.3851
CFM  CFM56-2C2 Trident 24000 106757.2800 4980 22152.136 0.360 1.0115E-05 0.597 1.6776E-05 26.50 35000 10.668 218.818 0.80 3.3562E-08 8.8144E-06 6.00 1962 NA NA 2 68.3 1.7348 95.70 2.4308 72.0 1.8288 6.3851
CFM  CFM56-2C3 DC-8-71/-71F/-72/-72F/-73/-73F (option) NA NA 4980 22152.136 0.360 1.0115E-05 0.597 1.6776E-05 NA 35000 10.668 218.818 0.80 3.3562E-08 8.8144E-06 6.00 NA 4635 2102.3989 2 68.3 1.7348 95.70 2.4308 72.0 1.8288 6.3851
CFM  CFM56-2C5 DC-8-72, DC-8-71/-71F/-72F/-73/-73F (option) NA NA 4980 22152.136 0.360 1.0115E-05 0.597 1.6776E-05 NA 35000 10.668 218.818 0.80 3.3562E-08 8.8144E-06 6.00 NA 4635 2102.3989 2 68.3 1.7348 95.70 2.4308 72.0 1.8288 6.3851
CFM  CFM56-2C6 DC-8-71/-71F/-72/-72F/-73/-73F (option) NA NA 4980 22152.136 0.360 1.0115E-05 0.597 1.6776E-05 NA 35000 10.668 218.818 0.80 3.3562E-08 8.8144E-06 6.00 NA 4635 2102.3989 2 68.3 1.7348 95.70 2.4308 72.0 1.8288 6.3851
CFM  CFM56-3B1 737-300/-300(QC)/-500, 737-400 (option) 20000 88964.4000 4650 20684.223 0.380 1.0677E-05 0.667 1.8743E-05 22.60 35000 10.668 218.818 0.80 3.9790E-08 9.3041E-06 6.00 1981 4276 1939.5594 2 60.0 1.5240 93.10 2.3647 63.0 1.6002 4.7558
CFM  CFM56-3B2 737-300/-300(QC)/-300F/-400 22000 97860.8400 5040 22419.029 0.390 1.0958E-05 0.667 1.8743E-05 24.30 35000 10.668 218.818 0.80 3.8758E-08 9.5489E-06 5.90 1981 4301 1950.8992 2 60.0 1.5240 93.10 2.3647 63.0 1.6002 4.7558
CFM  CFM56-3C1 737-300/-300(QC)/-300F/-400/-500 23500 104533.1700 5370 23886.941 0.330 9.2721E-06 0.667 1.8743E-05 25.20 35000 10.668 218.818 0.80 4.4951E-08 8.0799E-06 6.00 1981 4301 1950.8992 2 60.0 1.5240 93.10 2.3647 63.0 1.6002 4.7558
CFM  CFM56-3C3 737-300, 737-300(QC)/-300F/-400/-500 (option) NA NA 5370 23886.941 0.330 9.2721E-06 0.667 1.8743E-05 NA 35000 10.668 218.818 0.80 4.4951E-08 8.0799E-06 6.00 1984 4301 1950.8992 2 60.0 1.5240 93.10 2.3647 63.0 1.6002 4.7558
CFM  CFM56-5A1 A320-211/-311 25000 111205.5000 5000 22241.100 0.330 9.2721E-06 0.596 1.6748E-05 26.50 35000 10.668 218.818 0.80 3.6540E-08 8.0799E-06 6.00 1987 4995 2265.6920 2 68.3 1.7348 95.40 2.4232 72.0 1.8288 6.3651
CFM  CFM56-5A3 A320-212 26500 117877.8300 5000 22241.100 0.330 9.2721E-06 0.596 1.6748E-05 27.80 35000 10.668 218.818 0.80 3.6540E-08 8.0799E-06 6.00 1987 4995 2265.6920 2 68.3 1.7348 95.40 2.4232 72.0 1.8288 6.3651
CFM  CFM56-5A4 A319-113 NA NA 5000 22241.100 0.320 8.9911E-06 0.596 1.6748E-05 24.10 35000 10.668 218.818 0.80 3.7572E-08 7.8350E-06 6.20 NA 4975 2256.6202 2 68.3 1.7348 95.40 2.4232 72.0 1.8288 6.3651
CFM  CFM56-5A5 A319-114 23500 104533.1700 5000 22241.100 0.320 8.9911E-06 0.596 1.6748E-05 25.40 35000 10.668 218.818 0.80 3.7572E-08 7.8350E-06 6.20 1987 4975 2256.6202 2 68.3 1.7348 95.40 2.4232 72.0 1.8288 6.3651
CFM  CFM56-5B1 A321-111 30000 133446.6000 5840 25977.605 0.350 9.8341E-06 0.596 1.6748E-05 32.00 35000 10.668 218.818 0.80 3.4476E-08 8.5695E-06 5.50 1993 5250 2381.3580 2 68.3 1.7348 102.40 2.6010 72.0 1.8288 6.8321
CFM  CFM56-5B1/2 A321-111 30000 133446.6000 5840 25977.605 0.350 9.8341E-06 0.575 1.6158E-05 32.00 35000 10.668 218.818 0.80 3.1988E-08 8.5695E-06 5.50 1994 5250 2381.3580 2 68.3 1.7348 102.40 2.6010 72.0 1.8288 6.8321
CFM  CFM56-5B1/2P NA NA NA 5840 25977.605 0.350 9.8341E-06 0.575 1.6158E-05 32.00 35000 10.668 218.818 0.80 3.1988E-08 8.5695E-06 5.50 NA 5250 2381.3580 2 68.3 1.7348 102.40 2.6010 72.0 1.8288 6.8321
CFM  CFM56-5B1/P A321-111 30000 133446.6000 5840 25977.605 0.350 9.8341E-06 0.575 1.6158E-05 32.00 35000 10.668 218.818 0.80 3.1988E-08 8.5695E-06 5.50 1996 5250 2381.3580 2 68.3 1.7348 102.40 2.6010 72.0 1.8288 6.8321
CFM  CFM56-5B2 A321-112 31000 137894.8200 5840 25977.605 0.350 9.8341E-06 0.545 1.5315E-05 32.90 35000 10.668 218.818 0.80 2.8435E-08 8.5695E-06 5.50 1993 5250 2381.3580 2 68.3 1.7348 102.40 2.6010 72.0 1.8288 6.8321
CFM  CFM56-5B2/2 NA NA NA 5840 25977.605 0.350 9.8341E-06 0.572 1.6074E-05 32.90 35000 10.668 218.818 0.80 3.1633E-08 8.5695E-06 5.50 NA 5250 2381.3580 2 68.3 1.7348 102.40 2.6010 72.0 1.8288 6.8321
CFM  CFM56-5B2/2P NA NA NA 5840 25977.605 0.350 9.8341E-06 0.572 1.6074E-05 32.90 35000 10.668 218.818 0.80 3.1633E-08 8.5695E-06 5.40 NA 5250 2381.3580 2 68.3 1.7348 102.40 2.6010 72.0 1.8288 6.8321
CFM  CFM56-5B2/P A321-112 31000 137894.8200 5840 25977.605 0.350 9.8341E-06 0.572 1.6074E-05 32.90 35000 10.668 218.818 0.80 3.1633E-08 8.5695E-06 5.50 NA 5250 2381.3580 2 68.3 1.7348 102.40 2.6010 72.0 1.8288 6.8321
CFM  CFM56-5B3 A321-211 32000 142343.0400 5840 25977.605 0.360 1.0115E-05 0.570 1.6018E-05 33.70 35000 10.668 218.818 0.80 3.0364E-08 8.8144E-06 5.40 NA 5250 2381.3580 2 68.3 1.7348 102.40 2.6010 72.0 1.8288 6.8321
CFM  CFM56-5B3/2P  A321-211 32000 142343.0400 5840 25977.605 0.360 1.0115E-05 0.570 1.6018E-05 33.70 35000 10.668 218.818 0.80 3.0364E-08 8.8144E-06 5.40 1996 5250 2381.3580 2 68.3 1.7348 102.40 2.6010 72.0 1.8288 6.8321
CFM  CFM56-5B3/P  A321-211 32000 142343.0400 5840 25977.605 0.360 1.0115E-05 0.570 1.6018E-05 33.70 35000 10.668 218.818 0.80 3.0364E-08 8.8144E-06 5.40 2003 5250 2381.3580 2 68.3 1.7348 102.40 2.6010 72.0 1.8288 6.8321
CFM  CFM56-5B4 A320-214 27000 120101.9400 5000 22241.100 0.340 9.5531E-06 0.545 1.5315E-05 29.10 35000 10.668 218.818 0.80 2.9467E-08 8.3247E-06 5.70 1987 5250 2381.3580 2 68.3 1.7348 102.40 2.6010 72.0 1.8288 6.8321
CFM  CFM56-5B4/2 A320-214 27000 120101.9400 5000 22241.100 0.340 9.5531E-06 0.586 1.6467E-05 29.10 35000 10.668 218.818 0.80 3.4324E-08 8.3247E-06 5.70 1994 5250 2381.3580 2 68.3 1.7348 102.40 2.6010 72.0 1.8288 6.8321
CFM  CFM56-5B4/2P A320-214 27000 120101.9400 5000 22241.100 0.340 9.5531E-06 0.586 1.6467E-05 29.10 35000 10.668 218.818 0.80 3.4324E-08 8.3247E-06 5.70 1996 5250 2381.3580 2 68.3 1.7348 102.40 2.6010 72.0 1.8288 6.8321
CFM  CFM56-5B4/P A320-214 27000 120101.9400 5000 22241.100 0.340 9.5531E-06 0.586 1.6467E-05 29.10 35000 10.668 218.818 0.80 3.4324E-08 8.3247E-06 5.70 1996 5250 2381.3580 2 68.3 1.7348 102.40 2.6010 72.0 1.8288 6.8321
CFM  CFM56-5B5 A319-111 22000 97860.8400 5020 22330.064 0.320 8.9911E-06 0.600 1.6861E-05 24.40 35000 10.668 218.818 0.80 3.8046E-08 7.8350E-06 6.00 1996 5250 2381.3580 2 68.3 1.7348 102.40 2.6010 72.0 1.8288 6.8321
CFM  CFM56-5B5/P A319-111 22000 97860.8400 5020 22330.064 0.320 8.9911E-06 0.610 1.7142E-05 24.40 35000 10.668 218.818 0.80 3.9231E-08 7.8350E-06 6.00 1996 5250 2381.3580 2 68.3 1.7348 102.40 2.6010 72.0 1.8288 6.8321
CFM  CFM56-5B6  A319-112 23500 104533.1700 5020 22330.064 0.330 9.2721E-06 0.600 1.6861E-05 25.80 35000 10.668 218.818 0.80 3.7014E-08 8.0799E-06 5.90 1996 5250 2381.3580 2 68.3 1.7348 102.40 2.6010 72.0 1.8288 6.8321
CFM  CFM56-5B6/2 A319-112 23500 104533.1700 5020 22330.064 0.330 9.2721E-06 0.600 1.6861E-05 25.80 35000 10.668 218.818 0.80 3.7014E-08 8.0799E-06 5.90 1995 5250 2381.3580 2 68.3 1.7348 102.40 2.6010 72.0 1.8288 6.8321
CFM  CFM56-5B6/2P A319-112 23500 104533.1700 5020 22330.064 0.330 9.2721E-06 0.600 1.6861E-05 25.80 35000 10.668 218.818 0.80 3.7014E-08 8.0799E-06 5.90 1996 5250 2381.3580 2 68.3 1.7348 102.40 2.6010 72.0 1.8288 6.8321
CFM  CFM56-5B6/P A319-112 23500 104533.1700 5020 22330.064 0.330 9.2721E-06 0.600 1.6861E-05 25.80 35000 10.668 218.818 0.80 3.7014E-08 8.0799E-06 5.90 1996 5250 2381.3580 2 68.3 1.7348 102.40 2.6010 72.0 1.8288 6.8321
CFM  CFM56-5B7 NA 27000 120101.9400 5840 25977.605 0.340 9.5531E-06 0.580 1.6299E-05 29.10 35000 10.668 218.818 0.80 3.3613E-08 8.3247E-06 5.70 1999 5250 2381.3580 2 68.3 1.7348 102.40 2.6010 72.0 1.8288 6.8321
CFM  CFM56-5B7/P A319-115/-115CJ/-115XCJ 27000 120101.9400 5840 25977.605 0.340 9.5531E-06 0.590 1.6580E-05 29.10 35000 10.668 218.818 0.80 3.4797E-08 8.3247E-06 5.90 1999 5250 2381.3580 2 68.3 1.7348 102.40 2.6010 72.0 1.8288 6.8321
CFM  CFM56-5B8 A318-111  21600 96081.5520 5020 22330.064 0.340 9.5531E-06 0.580 1.6299E-05 26.00 35000 10.668 218.818 0.80 3.3613E-08 8.3247E-06 6.00 2002 5250 2381.3580 2 68.3 1.7348 102.40 2.6010 72.0 1.8288 6.8321
CFM  CFM56-5B9 A318-112  23300 103643.5260 5020 22330.064 NA NA NA NA 26.00 35000 10.668 218.818 0.80 NA NA 5.90 2002 5250 2381.3580 2 68.3 1.7348 102.40 2.6010 72.0 1.8288 6.8321
CFM  CFM56-5C2 A340-211/-311 31200 138784.4640 6915 30759.441 0.320 8.9911E-06 0.545 1.5315E-05 31.50 35000 10.668 218.818 0.80 3.1531E-08 7.8350E-06 6.60 1991 5700 2585.4744 2 72.3 1.8364 103.00 2.6162 76.6 1.9456 7.7783
CFM  CFM56-5C2/4 NA NA NA 6915 30759.441 0.320 8.9911E-06 0.545 1.5315E-05 NA 35000 10.668 218.818 0.80 3.1531E-08 7.8350E-06 6.60 1994 5700 2585.4744 2 72.3 1.8364 103.00 2.6162 76.6 1.9456 7.7783
CFM  CFM56-5C2/F NA NA NA 6915 30759.441 0.320 8.9911E-06 0.545 1.5315E-05 NA 35000 10.668 218.818 0.80 3.1531E-08 7.8350E-06 6.60 1994 5700 2585.4744 2 72.3 1.8364 103.00 2.6162 76.6 1.9456 7.7783
CFM  CFM56-5C2/F4 NA NA NA 6915 30759.441 0.320 8.9911E-06 0.545 1.5315E-05 NA 35000 10.668 218.818 0.80 3.1531E-08 7.8350E-06 6.60 1994 5700 2585.4744 2 72.3 1.8364 103.00 2.6162 76.6 1.9456 7.7783
CFM  CFM56-5C2/G NA NA NA 6915 30759.441 0.320 8.9911E-06 0.545 1.5315E-05 NA 35000 10.668 218.818 0.80 3.1531E-08 7.8350E-06 6.60 1994 5700 2585.4744 2 72.3 1.8364 103.00 2.6162 76.6 1.9456 7.7783
CFM  CFM56-5C2/G4 NA NA NA 6915 30759.441 0.320 8.9911E-06 0.545 1.5315E-05 NA 35000 10.668 218.818 0.80 3.1531E-08 7.8350E-06 6.60 1994 5700 2585.4744 2 72.3 1.8364 103.00 2.6162 76.6 1.9456 7.7783
CFM  CFM56-5C3 A340-212/-312 32500 144567.1500 6910 30737.200 0.320 8.9911E-06 0.545 1.5315E-05 32.60 35000 10.668 218.818 0.80 3.1531E-08 7.8350E-06 6.50 1991 5700 2585.4744 2 72.3 1.8364 103.00 2.6162 76.6 1.9456 7.7783
CFM  CFM56-5C3/F A340-312 32500 144567.1500 6910 30737.200 0.320 8.9911E-06 0.545 1.5315E-05 32.60 35000 10.668 218.818 0.82 3.0762E-08 7.8350E-06 6.50 1993 5700 2585.4744 2 72.3 1.8364 103.00 2.6162 76.6 1.9456 7.7783
CFM  CFM56-5C3/F4  NA NA NA 6910 30737.200 0.320 8.9911E-06 0.545 1.5315E-05 NA 35000 10.668 218.818 0.82 3.0762E-08 7.8350E-06 6.30 NA 5700 2585.4744 2 72.3 1.8364 103.00 2.6162 76.6 1.9456 7.7783
CFM  CFM56-5C3/G NA NA NA 6910 30737.200 0.320 8.9911E-06 0.545 1.5315E-05 NA 35000 10.668 218.818 0.82 3.0762E-08 7.8350E-06 6.30 NA 5700 2585.4744 2 72.3 1.8364 103.00 2.6162 76.6 1.9456 7.7783
CFM  CFM56-5C3/G4 NA NA NA 6910 30737.200 0.320 8.9911E-06 0.545 1.5315E-05 NA 35000 10.668 218.818 0.82 3.0762E-08 7.8350E-06 6.30 NA 5700 2585.4744 2 72.3 1.8364 103.00 2.6162 76.6 1.9456 7.7783
CFM  CFM56-5C4 A340-213/-213X/-313/-313X 34000 151239.4800 7100 31582.362 0.330 9.2721E-06 0.545 1.5315E-05 33.90 35000 10.668 218.818 0.80 3.0499E-08 8.0799E-06 6.40 1991 5700 2585.4744 2 72.3 1.8364 103.00 2.6162 76.6 1.9456 7.7783
CFM  CFM56-5C4/P NA 34000 151239.4800 7100 31582.362 0.330 9.2721E-06 0.545 1.5315E-05 33.90 35000 10.668 218.818 0.80 3.0499E-08 8.0799E-06 6.40 2003 5700 2585.4744 2 72.3 1.8364 103.00 2.6162 76.6 1.9456 7.7783
CFM  CFM56-7B18 737-600 (option) 18500 82292.0700 5420 24109.352 0.350 9.8341E-06 0.570 1.6018E-05 21.70 35000 10.668 218.818 0.80 3.1396E-08 8.5695E-06 5.60 NA 5216 2365.9359 2 61.0 1.5494 98.90 2.5121 65.0 1.6510 5.3779
CFM  CFM56-7B20 737-600/-700 20600 91633.3320 5450 24242.799 0.360 1.0115E-05 0.633 1.7788E-05 22.70 35000 10.668 218.818 0.80 3.7827E-08 8.8144E-06 5.60 1997 5216 2365.9359 2 61.0 1.5494 98.90 2.5121 65.0 1.6510 5.3779
CFM  CFM56-7B20/2 NA NA NA 5450 24242.799 0.360 1.0115E-05 0.633 1.7788E-05 NA 35000 10.668 218.818 0.80 3.7827E-08 8.8144E-06 5.60 1997 5216 2365.9359 2 61.0 1.5494 98.90 2.5121 65.0 1.6510 5.3779
CFM  CFM56-7B22  737-600/-700/-700BBJ/-800/-800BBJ2 22000 97860.8400 5450 24242.799 0.360 1.0115E-05 0.610 1.7142E-05 24.60 35000 10.668 218.818 0.80 3.5102E-08 8.8144E-06 5.40 NA 5216 2365.9359 2 61.0 1.5494 98.90 2.5121 65.0 1.6510 5.3779
CFM  CFM56-7B22/2 NA NA NA 5450 24242.799 0.360 1.0115E-05 0.610 1.7142E-05 NA 35000 10.668 218.818 0.80 3.5102E-08 8.8144E-06 5.40 NA 5216 2365.9359 2 61.0 1.5494 98.90 2.5121 65.0 1.6510 5.3779
CFM  CFM56-7B22/B1 NA NA NA 5450 24242.799 0.360 1.0115E-05 0.610 1.7142E-05 NA 35000 10.668 218.818 0.80 3.5102E-08 8.8144E-06 5.40 NA 5216 2365.9359 2 61.0 1.5494 98.90 2.5121 65.0 1.6510 5.3779
CFM  CFM56-7B24 737-700/-800/-900, 737-700BBJ/-800BBJ2 (option) 24000 106757.2800 5480 24376.246 0.370 1.0396E-05 0.627 1.7619E-05 26.00 35000 10.668 218.818 0.80 3.6084E-08 9.0592E-06 5.30 1997 5216 2365.9359 2 61.0 1.5494 98.90 2.5121 65.0 1.6510 5.3779
CFM  CFM56-7B24/2 NA NA NA 5480 24376.246 0.370 1.0396E-05 0.627 1.7619E-05 NA 35000 10.668 218.818 0.80 3.6084E-08 9.0592E-06 5.30 NA 5216 2365.9359 2 61.0 1.5494 98.90 2.5121 65.0 1.6510 5.3779
CFM  CFM56-7B24/B1 NA NA NA 5480 24376.246 0.370 1.0396E-05 0.627 1.7619E-05 NA 35000 10.668 218.818 0.80 3.6084E-08 9.0592E-06 5.30 NA 5216 2365.9359 2 61.0 1.5494 98.90 2.5121 65.0 1.6510 5.3779
CFM  CFM56-7B26 737-700/-700BBJ/-800/-800BBJ2/-900 26400 117433.0080 5480 24376.246 0.380 1.0677E-05 0.600 1.6861E-05 27.90 35000 10.668 218.818 0.80 3.1854E-08 9.3041E-06 5.10 NA 5216 2365.9359 2 61.0 1.5494 98.90 2.5121 65.0 1.6510 5.3779
CFM  CFM56-7B26/2  NA NA NA 5480 24376.246 0.380 1.0677E-05 0.600 1.6861E-05 NA 35000 10.668 218.818 0.80 3.1854E-08 9.3041E-06 5.10 NA 5216 2365.9359 2 61.0 1.5494 98.90 2.5121 65.0 1.6510 5.3779
CFM  CFM56-7B26/B1 NA NA NA 5480 24376.246 0.380 1.0677E-05 0.600 1.6861E-05 NA 35000 10.668 218.818 0.80 3.1854E-08 9.3041E-06 5.10 NA 5216 2365.9359 2 61.0 1.5494 98.90 2.5121 65.0 1.6510 5.3779
CFM  CFM56-7B27 737-600/-800, 737-700/-900 (option) 27300 121436.4060 5480 24376.246 0.380 1.0677E-05 0.600 1.6861E-05 28.90 35000 10.668 218.818 0.80 3.1854E-08 9.3041E-06 5.10 1996 5216 2365.9359 2 61.0 1.5494 98.90 2.5121 65.0 1.6510 5.3779
CFM  CFM56-7B27/2 NA NA NA 5480 24376.246 0.380 1.0677E-05 0.600 1.6861E-05 NA 35000 10.668 218.818 0.80 3.1854E-08 9.3041E-06 5.30 NA 5216 2365.9359 2 61.0 1.5494 98.90 2.5121 65.0 1.6510 5.3779
CFM  CFM56-7B27/B1 NA NA NA 5480 24376.246 0.380 1.0677E-05 0.600 1.6861E-05 NA 35000 10.668 218.818 0.80 3.1854E-08 9.3041E-06 5.30 NA 5216 2365.9359 2 61.0 1.5494 98.90 2.5121 65.0 1.6510 5.3779
CFM  CFM56-7B27/B3 NA NA NA 5480 24376.246 0.380 1.0677E-05 0.600 1.6861E-05 NA 35000 10.668 218.818 0.80 3.1854E-08 9.3041E-06 5.30 NA 5216 2365.9359 2 61.0 1.5494 98.90 2.5121 65.0 1.6510 5.3779
CFM  CFM56-9  A316/A317 (A31X), BRJ-X, AE-100, N-2130 (not produced) 20000 88964.4000 5480 24376.246 0.380 1.0677E-05 0.600 1.6861E-05 32.20 35000 10.668 218.818 0.80 3.1854E-08 9.3041E-06 5.08 NA 4252 1928.6732 2 NA NA 91.70 2.3292 56.0 1.4224 3.7011
GE CJ610-1 Learjet 23, HFB 320, 1121A Commdore 2850 12677.4270 NA NA 0.990 2.7816E-05 NA NA NA NA NA NA NA NA NA NA NA 399 180.9832 1 NA NA 51.10 1.2979 17.7 0.4496 0.2060
GE CJ610-4 Learjet 23/24 2850 12677.4270 NA NA 0.990 2.7816E-05 NA NA NA NA NA NA NA NA NA NA NA 389 176.4473 1 NA NA 45.40 1.1532 17.7 0.4496 0.1831
GE CJ610-5 HFB 320, 1121B/1122 Commodore 2950 13122.2490 NA NA 0.980 2.7535E-05 NA NA 6.80 NA NA NA NA NA NA NA NA 402 182.3440 1 NA NA 51.10 1.2979 17.7 0.4496 0.2060
GE CJ610-6 Learjet 24B/D, Learjet 24C (not produced) 2950 13122.2490 NA NA 0.980 2.7535E-05 NA NA 6.80 NA NA NA NA NA NA NA NA 392 177.8081 1 NA NA 45.40 1.1532 17.7 0.4496 0.1831
GE CJ610-8 HFB 320 2950 13122.2490 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 407 184.6119 1 NA NA 45.40 1.1532 17.7 0.4496 0.1831
GE CJ610-8A Learjet 24E/F/25B/25C/25D/28/29 2950 13122.2490 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 407 184.6119 1 NA NA 45.40 1.1532 17.7 0.4496 0.1831
GE CJ610-9 HFB 320, 1123 Commodore 3100 13789.4820 NA NA 1.000 2.8097E-05 NA NA 6.80 NA NA NA NA NA NA NA NA 417 189.1479 1 NA NA 51.10 1.2979 17.7 0.4496 0.2060
GE CJ805-21 Caravelle 7/10A 14997 66709.9553 2867 12753.047 0.560 1.5735E-05 0.760 2.1357E-05 12.00 36090 11.000 216.658 0.80 3.2676E-08 1.3643E-05 1.50 1960 3704 1680.1048 2 NA NA NA NA NA NA NA
GE CJ805-23B Convair CV-990/-990A 16100 71616.3420 NA NA 0.530 1.4892E-05 NA NA 13.00 NA NA NA NA NA NA NA NA NA NA 2 NA NA NA NA NA NA NA
GE CJ805-3 Convair CV-880 11200 49820.0640 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 2 NA NA NA NA NA NA NA
GE CJ805-3A Convair CV-880 11200 49820.0640 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 2 NA NA NA NA NA NA NA
GE CJ805-3B Convair CV-880 11650 51821.7630 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 2 NA NA NA NA NA NA NA
Rolls-Royce Conway RCo.12 Mk.508 707-420/-420F 17500 77843.8500 4625 20573.018 0.726 2.0399E-05 0.822 2.3099E-05 14.10 36000 10.973 216.837 0.83 2.2057E-08 1.7695E-05 0.30 1957 4540 2059.3077 2 NA NA 132.40 3.3630 42.0 1.0668 3.0059
Rolls-Royce Conway RCo.12 Mk.508A 707-420 18000 80067.9600 4625 20573.018 0.735 2.0652E-05 0.822 2.3099E-05 14.00 36000 10.973 216.837 0.83 2.1161E-08 1.7914E-05 0.30 1957 4540 2059.3077 2 NA NA 132.40 3.3630 42.0 1.0668 3.0059
Rolls-Royce Conway RCo.12 Mk.509 DC-8-41/-42/-43/-43F 17500 77843.8500 4625 20573.018 0.735 2.0652E-05 0.822 2.3099E-05 14.10 36000 10.973 216.837 0.83 2.1161E-08 1.7914E-05 0.30 1960 4540 2059.3077 2 NA NA 132.40 3.3630 42.0 1.0668 3.0059
Rolls-Royce Conway RCo.12 Mk.509A DC-8-41/-42/-43/-43F 18000 80067.9600 4625 20573.018 0.735 2.0652E-05 0.822 2.3099E-05 14.00 36000 10.973 216.837 0.83 2.1161E-08 1.7914E-05 0.30 1960 4540 2059.3077 2 NA NA 132.40 3.3630 42.0 1.0668 3.0059
Rolls-Royce Conway RCo.42 Mk.540 VC,10 Type 1101/1102/1103/1109 20370 90610.2414 5250 23353.155 0.656 1.8432E-05 0.840 2.3605E-05 14.80 36000 10.973 216.837 0.83 3.1085E-08 1.5989E-05 0.60 1962 5000 2267.9600 2 NA NA 154.00 3.9116 50.0 1.2700 4.9551
Rolls-Royce Conway RCo.43D Mk.550B Super VC,10 Type 1151/1154 21800 96971.1960 5345 23775.736 0.590 1.6577E-05 0.819 2.3015E-05 15.80 36000 10.973 216.837 0.83 3.5242E-08 1.4380E-05 0.60 1965 5100 2313.3192 2 NA NA 154.00 3.9116 50.0 1.2700 4.9551
Perm Aviadvigatel D-100 NA 42000 186825.2400 NA NA NA NA NA NA 35.00 NA NA NA NA NA NA 8.00 NA NA NA 2 NA NA NA NA NA NA NA
Perm Aviadvigatel D-110 NA 44090 196122.0198 NA NA NA NA NA NA 31.00 NA NA NA NA NA NA 3.00 NA NA NA 2 NA NA NA NA NA NA NA
Perm Aviadvigatel D-120 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 5.00 NA NA NA 2 NA NA NA NA NA NA NA
Instytut Lotnictwa D-18A NA 3968 17650.5370 NA NA 0.740 2.0792E-05 NA NA 8.00 NA NA NA NA NA NA 0.70 NA 838 380.1101 2 NA NA 76.40 1.9406 35.4 0.8992 1.2322
Lotarev (Motor Sich) D-18T An-124-100 'Condor', An-225 'Mriya' 51660 229795.0452 10716 47667.126 0.360 1.0115E-05 0.570 1.6018E-05 25.00 36100 11.003 216.639 0.75 3.2750E-08 8.7704E-06 5.60 1982 9040 4100.4717 3 91.7 2.3292 212.60 5.4000 115.6 2.9362 36.5654
Lotarev (Motor Sich) D-18T-1 An-218-100 48148 214172.8966 11596 51581.559 0.360 1.0115E-05 0.615 1.7282E-05 NA 36100 11.003 216.639 0.80 3.6060E-08 8.7704E-06 5.60 1982 9040 4100.4717 3 91.7 2.3292 212.60 5.4000 115.6 2.9362 36.5654
Lotarev (Motor Sich) D-18T-3 An-124-100M (proposed) 51660 229795.0452 NA NA NA NA NA NA NA NA NA NA NA NA NA 5.60 1982 9040 4100.4717 3 91.7 2.3292 212.60 5.4000 115.6 2.9362 36.5654
Lotarev (Progress) D-18TM An-218 (proposed) 55777 248108.3669 NA NA NA NA NA NA NA NA NA NA NA NA NA 5.50 NA 10470 4749.1082 3 NA NA 224.50 5.7023 117.6 2.9870 39.9597
Lotarev (Progress) D-18TR An-218-200/-300 (proposed) 60627 269682.2339 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 10470 4749.1082 3 NA NA 224.50 5.7023 117.6 2.9870 39.9597
Solovyev D-20 NA 11905 52956.0591 2426 10791.382 0.620 1.7420E-05 0.780 2.1919E-05 NA 32808 10.000 223.161 0.82 2.6831E-08 1.5330E-05 1.00 1960 3236 1467.8237 2 NA NA NA NA NA NA NA
Solovyev D-20P Tu-124K/K2/V 11905 52956.0591 2426 10791.382 0.620 1.7420E-05 0.780 2.1919E-05 13.60 32808 10.000 223.161 0.80 2.7502E-08 1.5330E-05 1.00 1960 3236 1467.8237 2 NA NA 130.00 3.3020 38.3 0.9728 2.4543
Perm Aviadvigatel D-21A1 S-21 11750 52266.5850 NA NA NA NA NA NA 20.20 NA NA NA NA NA NA 0.83 NA 4630 2100.1310 2 NA NA NA NA NA NA NA
Solovyev D-30-1 Tu-134/-134K/-134LK 14990 66678.8178 NA NA 0.600 1.6858E-05 NA NA 18.60 NA NA NA NA NA NA 1.00 1963 3420 1551.2846 2 NA NA 156.80 3.9827 41.3 1.0490 3.4422
Solovyev D-30-2 Tu-134A/AK/AN/B/B-1 14990 66678.8178 NA NA NA NA NA NA NA NA NA NA NA NA NA 1.00 NA NA NA 2 NA NA NA NA NA NA NA
Solovyev D-30-3 Tu-134A-3/B-3/BW 14990 66678.8178 NA NA 0.608 1.7083E-05 NA NA 17.70 NA NA NA NA NA NA 1.00 1963 3420 1551.2846 2 NA NA 156.80 3.9827 41.3 1.0490 3.4422
Solovyev (Perm Aviadvigatel) D-30K Tu-154M 25362 112815.7556 6065 26978.454 0.481 1.3515E-05 0.781 2.1947E-05 20.00 36090 11.000 216.658 0.80 4.3330E-08 1.1719E-05 2.30 1982 4740 2150.0261 2 NA NA NA NA NA NA NA
Solovyev D-30KP Il-76T 26460 117699.9012 NA NA 0.481 1.3515E-05 NA NA 18.40 NA NA NA NA NA NA 2.42 NA NA NA 2 NA NA NA NA NA NA NA
Solovyev D-30KP-2 Il-76TD/MDP/LL 26460 117699.9012 NA NA NA NA NA NA NA NA NA NA NA NA NA 2.42 NA NA NA 2 NA NA NA NA NA NA NA
Solovyev D-30KPV A-40 26460 117699.9012 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 2 NA NA 224.00 5.6896 61.4 1.5596 10.8687
Solovyev (Perm Aviadvigatel) D-30KU Il-62M (Il-62-200) 24250 107869.3350 6063 26969.558 0.495 1.3908E-05 0.700 1.9671E-05 17.40 36090 11.000 216.658 0.80 3.2242E-08 1.2060E-05 2.35 1982 5880 2667.1210 2 NA NA NA NA NA NA NA
Solovyev (Perm Aviadvigatel) D-30KU-2 Il-62M (Il-62-200) 23850 106090.0470 6063 26969.558 0.495 1.3908E-05 0.700 1.9671E-05 NA 36090 11.000 216.658 0.80 3.2242E-08 1.2060E-05 2.35 1982 5110 2317.8551 2 NA NA NA NA NA NA NA
Solovyev (Perm Aviadvigatel) D-30KU-90 NA 26455 117677.6601 6063 26969.558 0.495 1.3908E-05 0.700 1.9671E-05 NA 36090 11.000 216.658 0.80 3.2242E-08 1.2060E-05 2.44 1982 5290 2399.5017 2 NA NA 224.40 5.6998 61.4 1.5596 10.8881
Solovyev (Perm Aviadvigatel) D-30U-154 Tu-154M 14990 66678.8178 NA NA 0.600 1.6858E-05 NA NA 18.60 NA NA NA NA NA NA 1.00 1968 3420 1551.2846 2 NA NA 156.80 3.9827 41.3 1.0490 3.4422
Progress D-36-1 An-74 14330 63742.9926 3527 15688.872 0.360 1.0115E-05 0.650 1.8266E-05 18.70 26250 8.001 236.154 0.75 3.9425E-08 9.1569E-06 6.30 1993 2450 1111.3004 3 NA NA 136.60 3.4696 54.1 1.3741 5.1456
Progress D-36-1A An-74 NA NA NA NA NA NA NA NA 18.70 NA NA NA NA NA NA 6.30 NA 2450 1111.3004 3 NA NA 136.60 3.4696 54.1 1.3741 5.1456
Progress D-36-2A An-74, An-74D-200 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 6.30 NA 2450 1111.3004 3 NA NA 136.60 3.4696 54.1 1.3741 5.1456
Progress D-36-3A An-74-200, An-74T-100/-200A, An-74TK-100/200, An-74D-200, An-74VIP 14330 63742.9926 NA NA 0.360 1.0115E-05 NA NA NA NA NA NA NA NA NA 6.30 NA 2450 1111.3004 3 NA NA 136.60 3.4696 54.1 1.3741 5.1456
Progress D-36-4A AN-74T-300, An-74TK-300 14330 63742.9926 NA NA NA NA NA NA NA NA NA NA NA NA NA 6.30 NA 2450 1111.3004 3 NA NA 136.60 3.4696 54.1 1.3741 5.1456
Progress D-36-5A An-148 (proposed engine) NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 6.30 NA 2450 1111.3004 3 NA NA 136.60 3.4696 54.1 1.3741 5.1456
Progress D-436-148 An-148 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA
Progress D-436K (see military turbofan specifications) 16535 73551.3177 NA NA NA NA NA NA 21.00 NA NA NA NA NA NA 6.20 NA NA NA NA NA NA NA NA NA NA NA
Progress D-436T1 Tu-334-100 16865 75019.2303 3307 14710.264 0.370 1.0396E-05 0.611 1.7170E-05 25.20 36090 11.000 216.658 0.75 3.6852E-08 9.0144E-06 4.95 1996 3200 1451.4944 3 54.1 1.3741 NA NA NA NA NA
Progress D-436T1-134 Tu-134M (proposed) NA NA 3307 14710.264 NA NA 0.611 1.7170E-05 NA 36090 11.000 216.658 0.75 NA NA 4.95 1996 3200 1451.4944 3 54.1 1.3741 NA NA NA NA NA
Progress D-436T2 Tu-334-100D, Tu-354 (Tu-334-200) 18078 80414.9212 NA NA NA NA NA NA 26.20 NA NA NA NA NA NA 4.90 NA 3200 1451.4944 3 54.1 1.3741 NA NA NA NA NA
Progress D-436TM Yak-42-200 (Yak-42M) (proposed) 16865 75019.2303 NA NA NA NA NA NA 25.20 NA NA NA NA NA NA 4.95 NA 3200 1451.4944 3 NA NA NA NA NA NA NA
Progress D-436TP Be-200 16535 73551.3177 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA
Rolls-Royce Derwent RB.37 5/17 C-102 Jetliner 3600 16013.5920 NA NA NA NA NA NA 4.00 NA NA NA NA NA NA NA NA NA NA 1 NA NA NA NA NA NA NA
Williams EJ22-1 Eclipse 500 (candidate engine) 700 3113.7540 NA NA 0.460 1.2925E-05 NA NA NA NA NA NA NA NA NA 6.43 2000 85 38.5553 2 NA NA 41.00 1.0414 14.5 0.3683 0.1109
Williams FJ22-1 (see EJ22-1) NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA
Williams FJ33-1 Aerostar, Century Jet, FJ-100, Leopard Six 1200 5337.8640 NA NA 0.410 1.1520E-05 NA NA NA NA NA NA NA NA NA 7.93 1988 300 136.0776 2 NA NA 47.90 1.2167 19.0 0.4826 0.2226
Williams FJ33-4 S-26 Safire, Javelin Mk,10, D-Jet 1200 5337.8640 NA NA 0.410 1.1520E-05 NA NA NA NA NA NA NA NA NA 7.93 2005 300 136.0776 2 NA NA 47.90 1.2167 19.0 0.4826 0.2226
Williams/Rolls-Royce FJ44-1A Citation CJ1, SigmaJet, MagnaJet 1900 8451.6180 600 2668.932 0.456 1.2812E-05 0.749 2.1048E-05 12.80 30000 9.144 228.724 0.70 4.5391E-08 1.1415E-05 3.28 1991 445 201.8484 2 20.9 0.5309 41.90 1.0643 NA NA NA
Williams/Rolls-Royce FJ44-1AP Citation CJ1+ 1965 8740.7523 600 2668.932 0.456 1.2812E-05 0.749 2.1048E-05 NA 30000 9.144 228.724 0.70 4.5391E-08 1.1415E-05 3.28 1992 460 208.6523 2 20.7 0.5258 41.40 1.0516 NA NA NA
Williams/Rolls-Royce FJ44-1C SK60 1500 6672.3300 600 2668.932 0.460 1.2925E-05 0.749 2.1048E-05 10.30 30000 9.144 228.724 0.70 4.4919E-08 1.1515E-05 3.40 1963 447 202.7556 2 NA NA 41.90 1.0643 NA NA NA
Williams/Rolls-Royce FJ44-2A Premier 1, SJ30-2, Citation Eagle II, NauticAir 450 2300 10230.9060 600 2668.932 0.456 1.2812E-05 0.749 2.1048E-05 NA 30000 9.144 228.724 0.70 4.5391E-08 1.1415E-05 3.28 1992 447 202.7556 2 NA NA 47.20 1.1989 NA NA NA
Williams/Rolls-Royce FJ44-2C Citation CJ2, Spirit Wing Learjet 25D 2400 10675.7280 600 2668.932 0.460 1.2925E-05 0.749 2.1048E-05 NA 30000 9.144 228.724 0.70 4.4919E-08 1.1515E-05 3.40 1992 447 202.7556 2 NA NA 47.20 1.1989 NA NA NA
Williams/Rolls-Royce FJ44-3A Citation CJ2+, CJ3 2819 12539.5322 600 2668.932 0.456 1.2812E-05 0.749 2.1048E-05 NA 30000 9.144 228.724 0.70 4.5391E-08 1.1415E-05 3.28 1992 447 202.7556 NA NA NA NA NA NA NA NA
Williams FJX-1 V-Jet II 540 2402.0388 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 2 NA NA NA NA NA NA NA
Williams FJX-2 V-Jet II, Eclipse 500 (candidate engine) 700 3113.7540 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 85 38.5553 2 NA NA 41.00 1.0414 14.5 0.3683 0.1109
GE GE1 Technology demonstrator 5000 22241.1000 NA NA 0.700 1.9668E-05 NA NA 44.00 NA NA NA NA NA NA 8.00 NA NA NA 1 NA NA NA NA NA NA NA
GE GE39 Technology demonstrator NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 2 NA NA NA NA NA NA NA
GE GE4/J5P B-2707-200/-300 (not produced) 51500 229083.3300 NA NA 1.040 2.9221E-05 NA NA 12.50 NA NA NA NA NA NA 8.00 NA 11300 5125.5896 1 NA NA 308.00 7.8232 89.5 2.2733 31.7532
GE GE90-110B1 777-200LR, 777-300ER (option), 777-200F (proposed) 109999 489299.7518 NA NA NA NA NA NA NA NA NA NA NA NA NA 8.30 NA NA NA 2 123.0 3.1242 192.80 4.8971 134.0 3.4036 44.5562
GE GE90-113B NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 8.30 NA NA NA 2 123.0 3.1242 192.80 4.8971 134.0 3.4036 44.5562
GE GE90-115B 777-300ER, 777-200LR (option) 114999 511540.8518 NA NA NA NA NA NA 42.00 NA NA NA NA NA NA 8.30 NA 18260 8282.5899 2 123.0 3.1242 192.80 4.8971 134.0 3.4036 44.5562
GE GE90-76B 777-200 76400 339844.0080 17500 77843.850 0.330 9.2721E-06 0.545 1.5315E-05 39.30 35000 10.668 218.818 0.83 2.9397E-08 8.0799E-06 8.40 1994 15600 7076.0352 2 123.0 3.1242 192.80 4.8971 134.0 3.4036 44.5562
GE GE90-85B 777-200/-200ER 84700 376764.2340 17500 77843.850 0.324 9.1035E-06 0.520 1.4613E-05 39.30 35000 10.668 218.818 0.83 2.7139E-08 7.9330E-06 8.40 1995 15600 7076.0352 2 123.0 3.1242 192.80 4.8971 134.0 3.4036 44.5562
GE GE90-90B 777-200ER, 777-200 (option) 90000 400339.8000 NA NA NA NA NA NA 40.00 NA NA NA NA NA NA 8.40 NA 15600 7076.0352 2 123.0 3.1242 192.80 4.8971 134.0 3.4036 44.5562
GE GE90-92B 777-200ER, 777-200 (option) 91999 409231.7918 NA NA NA NA NA NA 40.00 NA NA NA NA NA NA 8.30 NA 15600 7076.0352 2 123.0 3.1242 192.80 4.8971 134.0 3.4036 44.5562
GE GE90-94B 777-200/-200ER/-300 93699 416793.7658 NA NA NA NA NA NA 40.00 NA NA NA NA NA NA 8.30 NA 16644 7549.5852 2 123.0 3.1242 192.80 4.8971 134.0 3.4036 44.5562
GE Genx-2B67B 787-3/-8/-9, A350-800/-900 66993 297999.6025 58500 260220.870 0.490 1.3768E-05 0.530 1.4894E-05 45.00 42653 13.001 216.650 0.85 1.1785E-08 1.1938E-05 8.60 2011 12397 5623.1800 NA NA NA NA NA NA NA NA
de Havilland  Ghost 50 Mk.1 Comet 1 5000 22241.1000 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA
de Havilland Ghost 50 Mk.2 Comet 1A 5020 22330.0644 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA
Engine Alliance GP7168 747-500X/-600X (not produced) 68000 302478.9600 NA NA NA NA NA NA 42.30 35000 10.668 218.818 0.85 NA NA 7.00 NA 11500 5216.3080 2 NA NA 169.00 4.2926 99.0 2.5146 21.3181
Engine Alliance GP7172 767-400ERX, (not produced) 71000 315823.6200 NA NA NA NA NA NA 43.90 35000 10.668 218.818 0.85 NA NA 8.70 NA NA NA 2 NA NA NA NA NA NA NA
Engine Alliance GP7268 NA 68000 302478.9600 NA NA NA NA NA NA 46.00 35000 10.668 218.818 0.85 NA NA 8.00 NA NA NA 2 NA NA NA NA NA NA NA
Engine Alliance GP7270 A380-861 70000 311375.4000 12633 56194.363 NA NA 0.550 1.5456E-05 45.60 35000 10.668 218.818 0.85 NA NA 8.70 2005 13300 6032.7736 2 116.0 2.9464 187.10 4.7523 124.0 3.1496 37.0261
Engine Alliance GP7277 A380-863F 77000 342512.9400 13700 60940.614 NA NA 0.550 1.5456E-05 45.60 35000 10.668 218.818 0.85 NA NA 8.70 2005 13300 6032.7736 2 116.0 2.9464 187.10 4.7523 124.0 3.1496 37.0261
Pratt Whitney JT10D-132 (see PW2037) NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA
Pratt Whitney JT11D-20 (see military turbofan specifications J58-P-4) NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA
Pratt Whitney JT12A-3 (see military turbofan specifications) 3000 13344.6600 NA NA 0.960 2.6973E-05 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA
Pratt Whitney JT12A-5 (see military turbofan specifications) 3000 13344.6600 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA
Pratt Whitney JT12A-6 Sabreliner 40/50 3000 13344.6600 NA NA 0.960 2.6973E-05 NA NA NA NA NA NA NA NA NA NA NA 453 205.4772 1 NA NA NA NA 21.9 0.5563 NA
Pratt Whitney JT12A-6A Sabreliner 40/50, JetStar I 3000 13344.6600 NA NA 0.960 2.6973E-05 NA NA NA NA NA NA NA NA NA NA NA 453 205.4772 1 NA NA NA NA 21.9 0.5563 NA
Pratt Whitney JT12A-8 Sabreliner 60, JetStar I 3300 14679.1260 NA NA 0.995 2.7957E-05 NA NA 6.70 NA NA NA NA NA NA NA NA 468 212.2811 1 NA NA NA NA 21.9 0.5563 NA
Pratt Whitney JT12A-8A Sabreliner 60, JetStar I 3300 14679.1260 NA NA 0.995 2.7957E-05 NA NA 6.70 NA NA NA NA NA NA NA NA 468 212.2811 1 NA NA NA NA 21.9 0.5563 NA
Pratt Whitney Canada JT15D-1 Citation, SN,600 prototype 2200 9786.0840 2414 10738.003 0.540 1.5173E-05 0.540 1.5175E-05 NA 40000 12.192 216.650 0.80 8.5519E-09 1.3156E-05 3.30 1983 514 233.1463 2 27.3 0.6934 59.30 1.5062 27.2 0.6909 0.5647
Pratt Whitney Canada JT15D-1A Citation I/ISP 2200 9786.0840 2414 10738.003 0.540 1.5173E-05 0.540 1.5175E-05 NA 40000 12.192 216.650 0.80 8.5519E-09 1.3156E-05 3.30 1983 519 235.4142 2 27.3 0.6934 59.30 1.5062 27.2 0.6909 0.5647
Pratt Whitney Canada JT15D-1B Citation I/ISP 2200 9786.0840 2414 10738.003 0.540 1.5173E-05 0.540 1.5175E-05 10.00 40000 12.192 216.650 0.80 8.5519E-09 1.3156E-05 3.30 1983 519 235.4142 2 27.3 0.6934 59.30 1.5062 27.2 0.6909 0.5647
Pratt Whitney Canada JT15D-4 Citation II/IISP, SN,601 Corvette, Diamond I 2500 11120.5500 2414 10738.003 0.562 1.5791E-05 0.540 1.5175E-05 NA 40000 12.192 216.650 0.80 6.2813E-09 1.3692E-05 2.60 1983 557 252.6507 2 20.8 0.5283 63.00 1.6002 27.0 0.6858 0.5911
Pratt Whitney Canada JT15D-4B Citation S/II 2500 11120.5500 2414 10738.003 0.562 1.5791E-05 0.540 1.5175E-05 NA 40000 12.192 216.650 0.80 6.2813E-09 1.3692E-05 2.60 1983 568 257.6403 2 20.8 0.5283 63.00 1.6002 27.0 0.6858 0.5911
Pratt Whitney Canada JT15D-4C S211 2500 11120.5500 2414 10738.003 0.562 1.5791E-05 0.540 1.5175E-05 NA 40000 12.192 216.650 0.80 6.2813E-09 1.3692E-05 2.60 1983 575 260.8154 2 20.8 0.5283 63.00 1.6002 27.0 0.6858 0.5911
Pratt Whitney Canada JT15D-4D Diamond IA 2500 11120.5500 2414 10738.003 0.562 1.5791E-05 0.540 1.5175E-05 NA 40000 12.192 216.650 0.80 6.2813E-09 1.3692E-05 2.60 1983 560 254.0115 2 20.8 0.5283 63.00 1.6002 27.0 0.6858 0.5911
Pratt Whitney Canada JT15D-5 Beechjet 400 (Diamond II), Beechjet 400A/400T 3045 13544.8299 2414 10738.003 0.551 1.5482E-05 0.540 1.5175E-05 12.60 40000 12.192 216.650 0.80 7.4166E-09 1.3424E-05 2.00 1983 632 286.6701 2 20.5 0.5207 63.00 1.6002 27.0 0.6858 0.5911
Pratt Whitney Canada JT15D-5A Citation V 2900 12899.8380 2414 10738.003 0.551 1.5482E-05 0.540 1.5175E-05 12.60 40000 12.192 216.650 0.80 7.4166E-09 1.3424E-05 2.00 1983 632 286.6701 2 20.5 0.5207 63.00 1.6002 27.0 0.6858 0.5911
Pratt Whitney Canada JT15D-5B (see military turbofan specifications) 2900 12899.8380 2414 10738.003 0.551 1.5482E-05 0.540 1.5175E-05 NA 40000 12.192 216.650 0.80 7.4166E-09 1.3424E-05 2.00 1983 632 286.6701 NA NA NA NA NA NA NA NA
Pratt Whitney Canada JT15D-5C S211A 3190 14189.8218 2414 10738.003 0.551 1.5482E-05 0.540 1.5175E-05 13.50 40000 12.192 216.650 0.80 7.4166E-09 1.3424E-05 2.00 1983 665 301.6387 2 20.5 0.5207 63.00 1.6002 27.0 0.6858 0.5911
Pratt Whitney Canada JT15D-5D Citation V Ultra, VisionAire Vantage 3045 13544.8299 2414 10738.003 0.550 1.5454E-05 0.540 1.5175E-05 13.10 40000 12.192 216.650 0.80 7.5198E-09 1.3400E-05 2.00 1983 627 284.4022 2 20.5 0.5207 63.00 1.6002 27.0 0.6858 0.5911
Pratt Whitney JT3C-1 Prototype NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 2 NA NA NA NA NA NA NA
Pratt Whitney JT3C-10 DC-8-12 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 2 38.8 0.9855 138.60 3.5204 38.9 0.9881 2.6993
Pratt Whitney JT3C-12 720, 720F, 707-120 (option) 12000 53378.6400 NA NA 0.775 2.1775E-05 NA NA 13.80 NA NA NA NA NA NA NA NA 3550 1610.2516 2 38.8 0.9855 138.60 3.5204 NA NA NA
Pratt Whitney JT3C-2 DC-8-11/-12 11200 49820.0640 NA NA 0.950 2.6692E-05 NA NA NA NA NA NA NA NA NA NA NA 3870 1755.4010 2 38.8 0.9855 138.60 3.5204 38.9 0.9881 2.6993
Pratt Whitney JT3C-4 707-120, 720 11200 49820.0640 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 2 38.8 0.9855 138.60 3.5204 38.9 0.9881 2.6993
Pratt Whitney JT3C-6 707-120, DC-8-11/-12 11200 49820.0640 NA NA 0.775 2.1775E-05 NA NA NA NA NA NA NA NA NA NA NA 4230 1918.6942 2 38.8 0.9855 138.60 3.5204 38.9 0.9881 2.6993
Pratt Whitney JT3C-7 720, 720F 12000 53378.6400 3396 15106.155 0.785 2.2056E-05 0.900 2.5291E-05 13.00 36089 11.000 216.660 0.80 2.6120E-08 1.9125E-05 0.00 1957 3500 1587.5720 2 38.8 0.9855 138.60 3.5204 38.9 0.9881 2.6993
Pratt Whitney JT3D-1 707-120B/-120BF, 720B, 720BF, DC-8-51/52 17000 75619.7400 NA NA 0.520 1.4611E-05 NA NA 12.50 NA NA NA NA NA NA 1.40 NA 4150 1882.4068 2 53.1 1.3487 136.30 3.4620 53.0 1.3462 4.9276
Pratt Whitney JT3D-1 (HK) 707-120B NA NA NA NA 0.520 1.4611E-05 NA NA NA NA NA NA NA NA NA 1.40 NA NA NA 2 53.1 1.3487 136.30 3.4620 53.0 1.3462 4.9276
Pratt Whitney JT3D-1 (HK3) 707-120B NA NA NA NA 0.520 1.4611E-05 NA NA NA NA NA NA NA NA NA 1.40 NA NA NA 2 53.1 1.3487 136.30 3.4620 53.0 1.3462 4.9276
Pratt Whitney JT3D-1 (Q) 707-120B NA NA NA NA 0.520 1.4611E-05 NA NA NA NA NA NA NA NA NA 1.40 NA NA NA 2 53.1 1.3487 136.30 3.4620 53.0 1.3462 4.9276
Pratt Whitney JT3D-2 (see military turbofan specifications TF33-P-3) NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA
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) 18018 80148.0280 5013 22298.927 0.770 2.1635E-05 0.760 2.1357E-05 16.00 35000 10.668 218.818 0.80 1.0555E-08 1.8853E-05 1.25 1958 4784 2169.9841 2 NA NA NA NA 53.0 1.3462 NA
Pratt Whitney JT3D-3A NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 1.30 NA NA NA 2 NA NA NA NA NA NA NA
Pratt Whitney JT3D-3B 707-120B/-320B/-320BH/-320C/-320CH, 720B, 720BF, DC-8-53F/-55/-62/-62F 18000 80067.9600 NA NA 0.530 1.4892E-05 NA NA 13.60 NA NA NA NA NA NA 1.37 NA 4340 1968.5893 2 53.1 1.3487 145.50 3.6957 53.0 1.3462 5.2602
Pratt Whitney JT3D-3B (HK) 707-120B/-320B/-320BH/-320C/-320CH, 720B, 720BF, DC-8-51F/-53F/-54/-55/-62F(AF) NA NA NA NA 0.510 1.4330E-05 NA NA NA NA NA NA NA NA NA 1.40 NA NA NA 2 53.1 1.3487 NA NA 53.0 1.3462 NA
Pratt Whitney JT3D-3B (HK2) 707-320B/-320C, DC-8-51F/-52F/-54F/-55F/-61F/-62F(CF) NA NA NA NA 0.510 1.4330E-05 NA NA NA NA NA NA NA NA NA 1.40 NA NA NA 2 53.1 1.3487 NA NA 53.0 1.3462 NA
Pratt Whitney JT3D-3B (HK3) 707-320B, DC-8-51F/-54F/-55F/-61/-61F/-62/-62F/-62F(AF)/-62F(CF) NA NA NA NA 0.510 1.4330E-05 NA NA NA NA NA NA NA NA NA 1.40 NA NA NA 2 53.1 1.3487 NA NA 53.0 1.3462 NA
Pratt Whitney JT3D-3B (Q) 707-120B, DC-8-51/-51F/-52/-52F/-54/-55/-55F/-61/-61F(AF)/-62/-62F(CF) NA NA NA NA 0.510 1.4330E-05 NA NA NA NA NA NA NA NA NA 1.40 NA NA NA 2 53.1 1.3487 NA NA 53.0 1.3462 NA
Pratt Whitney JT3D-3C NA 18000 80067.9600 NA NA 0.510 1.4330E-05 NA NA 13.00 NA NA NA NA NA NA 1.66 NA 4340 1968.5893 2 53.1 1.3487 145.50 3.6957 53.0 1.3462 5.2602
Pratt Whitney JT3D-5 (see military turbofan specifications TF33-P-7) NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA
Pratt Whitney JT3D-7 707-320B/-320C, DC-8-62/-62F/-63/-63F 19000 84516.1800 NA NA 0.520 1.4611E-05 NA NA 13.50 NA NA NA NA NA NA 1.43 NA 4340 1968.5893 2 53.1 1.3487 145.50 3.6957 53.0 1.3462 5.2602
Pratt Whitney JT3D-7 (HK) 707-320B/-320C NA NA NA NA 0.520 1.4611E-05 NA NA NA NA NA NA NA NA NA 1.43 NA NA NA 2 53.1 1.3487 NA NA 53.0 1.3462 NA
Pratt Whitney JT3D-7 (HK2) 707-320B/-320C NA NA NA NA 0.520 1.4611E-05 NA NA NA NA NA NA NA NA NA 1.43 NA NA NA 2 53.1 1.3487 NA NA 53.0 1.3462 NA
Pratt Whitney JT3D-7 (HK3) 707-320B/-320C, DC-8-62/-62F/-62F(AF)/-62F(CF)/-63/-63F/-63F(CF) NA NA NA NA 0.520 1.4611E-05 NA NA NA NA NA NA NA NA NA 1.43 NA NA NA 2 53.1 1.3487 NA NA 53.0 1.3462 NA
Pratt Whitney JT3D-7 (Q) DC-8-62F/-63F/-63F(AF) NA NA NA NA 0.520 1.4611E-05 NA NA NA NA NA NA NA NA NA 1.43 NA NA NA 2 53.1 1.3487 NA NA 53.0 1.3462 NA
Pratt Whitney JT3D-7A NA 19000 84516.1800 NA NA 0.520 1.4611E-05 NA NA 13.50 NA NA NA NA NA NA 1.43 NA 4340 1968.5893 2 53.1 1.3487 145.50 3.6957 53.0 1.3462 5.2602
Pratt Whitney JT4A-10 707-320 (option) 16800 74730.0960 NA NA 0.810 2.2759E-05 NA NA NA NA NA NA NA NA NA NA NA 5100 2313.3192 2 42.5 1.0795 144.10 3.6601 43.0 1.0922 3.4292
Pratt Whitney JT4A-11 DC-8-33F/-33F(AF), 707-320 (option) 17500 77843.8500 4697 20893.289 0.840 2.3602E-05 0.920 2.5853E-05 12.50 36089 11.000 216.660 0.80 2.2824E-08 2.0465E-05 0.00 1956 5100 2313.3192 2 42.5 1.0795 144.10 3.6601 NA NA NA
Pratt Whitney JT4A-12 707-320/-320F 17500 77843.8500 NA NA 0.840 2.3602E-05 NA NA 12.50 NA NA NA NA NA NA NA NA 4900 2222.6008 2 42.5 1.0795 144.10 3.6601 NA NA NA
Pratt Whitney JT4A-3 707-220, DC-8-21/-21F (option) 15800 70281.8760 NA NA 0.770 2.1635E-05 NA NA NA NA NA NA NA NA NA NA NA 5020 2277.0318 2 42.5 1.0795 144.10 3.6601 NA NA NA
Pratt Whitney JT4A-5 707-220 (option) 15800 70281.8760 NA NA 0.770 2.1635E-05 NA NA NA NA NA NA NA NA NA NA NA 4820 2186.3134 2 42.5 1.0795 144.10 3.6601 NA NA NA
Pratt Whitney JT4A-7 707-320 (option) 15800 70281.8760 NA NA 0.770 2.1635E-05 NA NA NA NA NA NA NA NA NA NA NA NA NA 2 NA NA NA NA NA NA NA
Pratt Whitney JT4A-9 DC-8-21/-21F/-33F/-33F(AF) 16800 74730.0960 NA NA 0.810 2.2759E-05 NA NA NA NA NA NA NA NA NA NA NA 5050 2290.6396 2 42.5 1.0795 144.10 3.6601 43.0 1.0922 3.4292
Pratt Whitney JT8D-1 Caravelle 10B1R/10B3, DC-9-15 14000 62275.0800 NA NA 0.585 1.6437E-05 NA NA 15.40 NA NA NA NA NA NA 1.06 NA 3096 1404.3208 2 42.5 1.0795 123.50 3.1369 42.5 1.0795 2.8710
Pratt Whitney JT8D-11 DC-9-21/-32/-41 15000 66723.3000 4750 21129.045 0.620 1.7420E-05 0.806 2.2650E-05 16.20 30000 9.144 228.724 0.80 2.9395E-08 1.5520E-05 1.05 1965 3310 1501.3895 2 42.5 1.0795 123.50 3.1369 42.5 1.0795 2.8710
Pratt Whitney JT8D-11 (HK) DC-9-21 15000 66723.3000 4750 21129.045 0.620 1.7420E-05 0.806 2.2650E-05 NA 30000 9.144 228.724 0.80 2.9395E-08 1.5520E-05 1.05 1965 3310 1501.3895 2 42.5 1.0795 NA NA 42.5 1.0795 NA
Pratt Whitney JT8D-11 (HK3) DC-9-21/-32/-33F/-41 15000 66723.3000 4750 21129.045 0.620 1.7420E-05 0.806 2.2650E-05 NA 30000 9.144 228.724 0.80 2.9395E-08 1.5520E-05 1.05 1965 3310 1501.3895 2 42.5 1.0795 NA NA 42.5 1.0795 NA
Pratt Whitney JT8D-15 727-200/-200A/-200F/-200AF, 737-200A/-200CA, DC-9-33/-34/-41, Mercure-100 15500 68947.4100 4920 21885.242 0.630 1.7701E-05 0.810 2.2762E-05 16.50 30000 9.144 228.724 0.80 2.8826E-08 1.5770E-05 1.03 1963 3414 1548.5631 2 42.5 1.0795 123.50 3.1369 42.5 1.0795 2.8710
Pratt Whitney JT8D-15 (HK) 727-200A, 737-200/-200A 15000 66723.3000 4920 21885.242 0.630 1.7701E-05 0.810 2.2762E-05 NA 30000 9.144 228.724 0.80 2.8826E-08 1.5770E-05 1.03 1963 3414 1548.5631 2 42.5 1.0795 NA NA 42.5 1.0795 NA
Pratt Whitney JT8D-15 (HK3) 727-200A/-200AF, 737-200/-200A/-200C/-200CA, DC-9-31/-32/-41 15000 66723.3000 4920 21885.242 0.630 1.7701E-05 0.810 2.2762E-05 NA 30000 9.144 228.724 0.80 2.8826E-08 1.5770E-05 1.03 1963 3414 1548.5631 2 42.5 1.0795 NA NA 42.5 1.0795 NA
Pratt Whitney JT8D-15A 727-200A, 737-200A/-200CA, DC-9-30/-40/-50 (option) 15500 68947.4100 4920 21885.242 0.590 1.6577E-05 0.810 2.2762E-05 16.60 30000 9.144 228.724 0.80 3.2954E-08 1.4769E-05 1.04 1963 3474 1575.7786 2 42.5 1.0795 123.50 3.1369 42.5 1.0795 2.8710
Pratt Whitney JT8D-15A (HK3) 727-200A/-200AF, 737-200A/-200CA 15000 66723.3000 4920 21885.242 0.590 1.6577E-05 0.810 2.2762E-05 NA 30000 9.144 228.724 0.80 3.2954E-08 1.4769E-05 1.04 1963 3474 1575.7786 2 42.5 1.0795 NA NA 42.5 1.0795 NA
Pratt Whitney JT8D-17 727-200A/-200AF, 737-200/-200A/-200CA/-200F/-200AF, DC-9-31/-32/-34/-34F(CF)/-51 16000 71171.5200 5140 22863.851 0.600 1.6858E-05 0.814 2.2874E-05 16.90 30000 9.144 228.724 0.80 3.2386E-08 1.5019E-05 1.01 1963 3430 1555.8206 2 42.5 1.0795 123.50 3.1369 42.5 1.0795 2.8710
Pratt Whitney JT8D-17 (HK3) 727-200A/-200AF, 737-200A/-200CA, DC-9-51 16000 71171.5200 5140 22863.851 0.600 1.6858E-05 0.814 2.2874E-05 NA 30000 9.144 228.724 0.80 3.2386E-08 1.5019E-05 1.01 1963 3430 1555.8206 2 42.5 1.0795 NA NA 42.5 1.0795 NA
Pratt Whitney JT8D-17A 727-200A, 737-200A/-200CA/-200AF, DC-9-41/-51 16000 71171.5200 5140 22863.851 0.600 1.6858E-05 0.773 2.1722E-05 17.10 30000 9.144 228.724 0.80 2.7635E-08 1.5019E-05 1.02 1963 3475 1576.2322 2 42.5 1.0795 123.50 3.1369 42.5 1.0795 2.8710
Pratt Whitney JT8D-17A (HK3) 727-200A/-200AF, 737-200A/-200CA, DC-9-41/-51 16000 71171.5200 5140 22863.851 0.600 1.6858E-05 0.773 2.1722E-05 NA 30000 9.144 228.724 0.80 2.7635E-08 1.5019E-05 1.02 1963 3475 1576.2322 2 42.5 1.0795 NA NA 42.5 1.0795 NA
Pratt Whitney JT8D-17AR 727-200A, 737-200 17400 77399.0280 5140 22863.851 0.610 1.7139E-05 0.780 2.1919E-05 17.30 30000 9.144 228.724 0.80 2.7414E-08 1.5270E-05 1.00 1963 3495 1585.3040 2 42.5 1.0795 123.50 3.1369 42.5 1.0795 2.8710
Pratt Whitney JT8D-17R 727-200/-200A/-200AF 17400 77399.0280 5140 22863.851 0.660 1.8544E-05 0.820 2.3043E-05 17.50 30000 9.144 228.724 0.80 2.6888E-08 1.6521E-05 1.00 1963 3495 1585.3040 2 42.5 1.0795 123.50 3.1369 42.5 1.0795 2.8710
Pratt Whitney JT8D-17R (HK3) 727-200A/-200AF 17400 77399.0280 5140 22863.851 0.790 2.2197E-05 0.820 2.3043E-05 NA 30000 9.144 228.724 0.80 1.3471E-08 1.9776E-05 1.00 1963 3495 1585.3040 2 42.5 1.0795 NA NA 42.5 1.0795 NA
Pratt Whitney JT8D-1A NA 14000 62275.0800 NA NA 0.585 1.6437E-05 NA NA 15.40 NA NA NA NA NA NA 1.06 NA 3096 1404.3208 2 42.5 1.0795 123.50 3.1369 42.5 1.0795 2.8710
Pratt Whitney JT8D-1B NA 14000 62275.0800 NA NA 0.585 1.6437E-05 NA NA 15.40 NA NA NA NA NA NA 1.06 NA 3096 1404.3208 2 42.5 1.0795 123.50 3.1369 42.5 1.0795 2.8710
Pratt Whitney JT8D-209 MD-81 19250 85628.2350 4945 21996.448 0.510 1.4330E-05 0.724 2.0345E-05 17.40 35000 10.668 218.818 0.80 3.3125E-08 1.2487E-05 1.82 1980 4410 2000.3407 2 49.2 1.2497 154.20 3.9167 NA NA NA
Pratt Whitney JT8D-216 MD-95-30 (not produced) NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 4410 2000.3407 2 49.2 1.2497 154.20 3.9167 NA NA NA
Pratt Whitney JT8D-217 MD-81/-82 20000 88964.4000 5240 23308.673 0.530 1.4892E-05 0.753 2.1160E-05 18.60 35000 10.668 218.818 0.80 3.4496E-08 1.2977E-05 1.77 1980 4430 2009.4126 2 49.2 1.2497 154.20 3.9167 NA NA NA
Pratt Whitney JT8D-217A MD-81/-82/-82(SA) 20000 88964.4000 5240 23308.673 0.530 1.4892E-05 0.753 2.1160E-05 18.60 35000 10.668 218.818 0.80 3.4496E-08 1.2977E-05 1.77 1980 4430 2009.4126 2 49.2 1.2497 154.20 3.9167 NA NA NA
Pratt Whitney JT8D-217C 727-100(RE)/-200A(RE)/-200AF(RE), MD-81/-82/-87/-88 20000 88964.4000 5240 23308.673 0.500 1.4049E-05 0.736 2.0682E-05 20.10 35000 10.668 218.818 0.80 3.5578E-08 1.2242E-05 1.72 1963 4500 2041.1640 2 49.2 1.2497 154.20 3.9167 NA NA NA
Pratt Whitney JT8D-218 MD-95-30 (not produced) NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 4500 2041.1640 2 49.2 1.2497 154.20 3.9167 NA NA NA
Pratt Whitney JT8D-219 MD-82/-83/-87/-88, 707-330C(RE), 727-200AF(RE) 21700 96526.3740 5250 23353.155 0.519 1.4583E-05 0.737 2.0711E-05 19.20 35000 10.668 218.818 0.80 3.3736E-08 1.2707E-05 1.77 1980 4500 2041.1640 2 49.2 1.2497 154.20 3.9167 NA NA NA
Pratt Whitney JT8D-3 (see military turbofan specifications TF33-P-102) NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 3096 1404.3208 NA NA NA NA NA NA NA NA
Pratt Whitney JT8D-5 DC-9-11 12250 54490.6950 NA NA 0.565 1.5875E-05 NA NA 15.80 NA NA NA NA NA NA NA NA 3096 1404.3208 2 42.5 1.0795 123.50 3.1369 42.5 1.0795 2.8710
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 14000 62275.0800 4270 18993.899 0.585 1.6437E-05 0.796 2.2368E-05 NA 30000 9.144 228.724 0.80 3.1848E-08 1.4644E-05 1.07 1963 3155 1431.0828 2 42.5 1.0795 123.50 3.1369 42.5 1.0795 2.8710
Pratt Whitney JT8D-7 (HK3) 727-100/-100C, DC-9-15/-15F(RC) 14000 62275.0800 4270 18993.899 0.585 1.6437E-05 0.796 2.2368E-05 NA 30000 9.144 228.724 0.80 3.1848E-08 1.4644E-05 1.07 1963 3096 1404.3208 2 42.5 1.0795 NA NA 42.5 1.0795 NA
Pratt Whitney JT8D-7A 727-100/-100C/-100QC/-100F/-200, 737-100/-200, DC-9-14/-15/-15F(MC)/-31/-31 14000 62275.0800 4270 18993.899 0.585 1.6437E-05 0.796 2.2368E-05 15.80 30000 9.144 228.724 0.80 3.1848E-08 1.4644E-05 1.07 1963 3096 1404.3208 2 42.5 1.0795 123.50 3.1369 42.5 1.0795 2.8710
Pratt Whitney JT8D-7A (HK3) 727-100/-100C, DC-9-15/-15F(RC)/-32 14000 62275.0800 4270 18993.899 0.585 1.6437E-05 0.796 2.2368E-05 NA 30000 9.144 228.724 0.80 3.1848E-08 1.4644E-05 1.07 1963 3096 1404.3208 2 42.5 1.0795 NA NA 42.5 1.0795 NA
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 14000 62275.0800 4270 18993.899 0.585 1.6437E-05 0.796 2.2368E-05 15.80 30000 9.144 228.724 0.80 3.1848E-08 1.4644E-05 1.07 1963 3096 1404.3208 2 42.5 1.0795 123.50 3.1369 42.5 1.0795 2.8710
Pratt Whitney JT8D-7B (HK) 727-200F 14000 62275.0800 4270 18993.899 0.585 1.6437E-05 0.796 2.2368E-05 NA 30000 9.144 228.724 0.80 3.1848E-08 1.4644E-05 1.07 1963 3096 1404.3208 2 42.5 1.0795 NA NA 42.5 1.0795 NA
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 14000 62275.0800 4270 18993.899 0.585 1.6437E-05 0.796 2.2368E-05 NA 30000 9.144 228.724 0.80 3.1848E-08 1.4644E-05 1.07 1963 3096 1404.3208 2 42.5 1.0795 NA NA 42.5 1.0795 NA
Pratt Whitney JT8D-7B (Q) 727-100/-100F 14000 62275.0800 4270 18993.899 0.585 1.6437E-05 0.796 2.2368E-05 NA 30000 9.144 228.724 0.80 3.1848E-08 1.4644E-05 1.07 1963 3096 1404.3208 2 42.5 1.0795 NA NA 42.5 1.0795 NA
Pratt Whitney JT8D-9 727-100/-100C/-200/-200A, 737-200/-200A/-200C/-200CA, DC-9-32/-32F/-33F/-33F(RC), Caravelle 10B3/12 14500 64499.1900 4540 20194.919 0.565 1.5875E-05 0.800 2.2481E-05 15.90 30000 9.144 228.724 0.80 3.4376E-08 1.4143E-05 1.03 1963 3196 1449.6800 2 42.5 1.0795 123.50 3.1369 42.5 1.0795 2.8710
Pratt Whitney JT8D-9 (HK3) 727-200F, DC-9-31/-32/-32F/-33F 14500 64499.1900 4540 20194.919 0.565 1.5875E-05 0.800 2.2481E-05 NA 30000 9.144 228.724 0.80 3.4376E-08 1.4143E-05 1.03 1963 3196 1449.6800 2 42.5 1.0795 NA NA 42.5 1.0795 NA
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) 14500 64499.1900 4540 20194.919 0.565 1.5875E-05 0.800 2.2481E-05 15.90 30000 9.144 228.724 0.80 3.4376E-08 1.4143E-05 1.03 1963 3196 1449.6800 2 42.5 1.0795 123.50 3.1369 42.5 1.0795 2.8710
Pratt Whitney JT8D-9A (HK3) 727-100/-200/-200A/-200AF/-200F, 737-200/-200A/-200C/-200CA, DC-9-31/-32/-33F(CF)/-33F(RC) 14500 64499.1900 4540 20194.919 0.565 1.5875E-05 0.800 2.2481E-05 NA 30000 9.144 228.724 0.80 3.4376E-08 1.4143E-05 1.03 1963 3196 1449.6800 2 42.5 1.0795 NA NA 42.5 1.0795 NA
Pratt Whitney JT9D-1 747-100 (option) 42000 186825.2400 NA NA NA NA NA NA 21.50 NA NA NA NA NA NA 5.00 NA NA NA 2 95.6 2.4282 154.20 3.9167 NA NA NA
Pratt Whitney JT9D-15 DC-10-20/-40 (option), MD-11 (proposed) 45500 202394.0100 NA NA 0.355 9.9746E-06 NA NA NA NA NA NA NA NA NA NA NA NA NA 2 95.6 2.4282 NA NA NA NA NA
Pratt Whitney JT9D-20 DC-10-40, MD-11 (proposed) 46300 205952.5860 10680 47506.990 0.370 1.0396E-05 0.624 1.7535E-05 21.10 35000 10.668 218.818 0.85 3.3627E-08 9.0592E-06 5.20 1971 8450 3832.8524 2 95.6 2.4282 153.60 3.9014 NA NA NA
Pratt Whitney JT9D-20J DC-10-40, MD-11 (proposed) 46300 205952.5860 10680 47506.990 0.370 1.0396E-05 0.624 1.7535E-05 23.50 35000 10.668 218.818 0.85 3.3627E-08 9.0592E-06 5.20 1971 8450 3832.8524 2 95.6 2.4282 153.60 3.9014 NA NA NA
Pratt Whitney JT9D-25 DC-10-20 (option), MD-11 (proposed) 47000 209066.3400 NA NA NA NA NA NA NA NA NA NA NA NA NA 5.20 NA NA NA 2 95.6 2.4282 153.60 3.9014 NA NA NA
Pratt Whitney JT9D-3 747-100 (option) 43500 193497.5700 NA NA 0.346 9.7217E-06 NA NA 22.00 NA NA NA NA NA NA 5.20 NA 8430 3823.7806 2 95.6 2.4282 154.20 3.9167 NA NA NA
Pratt Whitney JT9D-3A 747-100 44250 196833.7350 10200 45371.844 0.346 9.7217E-06 0.624 1.7535E-05 21.50 35000 10.668 218.818 0.85 3.5958E-08 8.4716E-06 5.20 1969 8610 3905.4271 2 95.6 2.4282 154.20 3.9167 NA NA NA
Pratt Whitney JT9D-59 A300B4-120/-220/-220F/-220FF (option) 53000 235755.6600 11950 53156.229 0.375 1.0537E-05 0.631 1.7732E-05 24.90 35000 10.668 218.818 0.85 3.3922E-08 9.1817E-06 4.90 1972 9140 4145.8309 2 95.6 2.4282 153.60 3.9014 NA NA NA
Pratt Whitney JT9D-59A A300B4-120/-220/-220F/-220FF, DC-10-40(D)/-40(I)/-40F, A300B4-320 (option) 51740 230150.9028 11950 53156.229 0.375 1.0537E-05 0.631 1.7732E-05 24.50 35000 10.668 218.818 0.85 3.3922E-08 9.1817E-06 4.90 1972 9140 4145.8309 2 95.6 2.4282 153.60 3.9014 NA NA NA
Pratt Whitney JT9D-59B NA 54500 242427.9900 12200 54268.284 0.410 1.1520E-05 0.631 1.7732E-05 25.20 35000 10.668 218.818 0.85 3.0522E-08 1.0039E-05 4.80 1972 9160 4154.9027 2 95.6 2.4282 153.60 3.9014 NA NA NA
Pratt Whitney JT9D-7 747-100/-200B 46300 205952.5860 10200 45371.844 0.355 9.9746E-06 0.620 1.7423E-05 22.30 35000 10.668 218.818 0.85 3.4638E-08 8.6920E-06 5.20 1969 8850 4014.2892 2 95.6 2.4282 154.20 3.9167 NA NA NA
Pratt Whitney JT9D-70A 747-200B/-200B(M)/-200B(SF)/-200F 53000 235755.6600 11950 53156.229 0.375 1.0537E-05 0.631 1.7732E-05 24.50 35000 10.668 218.818 0.85 3.3922E-08 9.1817E-06 4.90 1969 9160 4154.9027 2 95.6 2.4282 153.60 3.9014 NA NA NA
Pratt Whitney JT9D-70B NA 54500 242427.9900 12200 54268.284 0.410 1.1520E-05 0.631 1.7732E-05 25.20 35000 10.668 218.818 0.85 3.0522E-08 1.0039E-05 4.80 1969 9180 4163.9746 2 95.6 2.4282 153.60 3.9014 NA NA NA
Pratt Whitney JT9D-7A 747-SF/-SP/-100/-100A/-100(SF)/-100F/-100SR/-100SRB/-100SR(SF)/-200/-200B/-200C 46950 208843.9290 10830 48174.223 0.364 1.0227E-05 0.625 1.7563E-05 22.50 35000 10.668 218.818 0.85 3.4321E-08 8.9123E-06 5.10 1969 8850 4014.2892 2 95.6 2.4282 154.20 3.9167 NA NA NA
Pratt Whitney JT9D-7AH 747-SP/-100/-100(SF)/-100F/-200B 46950 208843.9290 NA NA NA NA NA NA NA NA NA NA NA NA NA 5.20 NA 8850 4014.2892 2 95.6 2.4282 154.20 3.9167 NA NA NA
Pratt Whitney JT9D-7ASP 747-SP (option) 46950 208843.9290 10680 47506.990 0.364 1.0227E-05 0.630 1.7704E-05 22.50 35000 10.668 218.818 0.85 3.4879E-08 8.9123E-06 5.10 1969 8780 3982.5378 2 95.6 2.4282 154.20 3.9167 NA NA NA
Pratt Whitney JT9D-7AW 747-200B/-200(SF)/-100SR/-200F, 747-100/-100B (option) 46950 208843.9290 10830 48174.223 0.360 1.0115E-05 0.620 1.7423E-05 22.50 35000 10.668 218.818 0.85 3.4152E-08 8.8144E-06 5.10 1974 8850 4014.2892 2 95.6 2.4282 154.20 3.9167 NA NA NA
Pratt Whitney JT9D-7F 747-SP/-100B/-200/-200B/-200B(M)/-200(SF)/-200F 48000 213514.5600 11050 49152.831 0.367 1.0312E-05 0.631 1.7732E-05 22.80 35000 10.668 218.818 0.85 3.4699E-08 8.9858E-06 5.10 1969 8850 4014.2892 2 95.6 2.4282 154.20 3.9167 NA NA NA
Pratt Whitney JT9D-7FW 747-SP/-200B(SF)/-200C(M) 48000 213514.5600 NA NA NA NA NA NA NA NA NA NA NA NA NA 5.10 1969 8850 4014.2892 2 95.6 2.4282 154.20 3.9167 NA NA NA
Pratt Whitney JT9D-7H NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 1969 8850 4014.2892 2 95.6 2.4282 154.20 3.9167 NA NA NA
Pratt Whitney JT9D-7J 747-100F/-200B/-200B(M)/-200B(SF)/-200C/-200F 50000 222411.0000 11050 49152.831 0.370 1.0396E-05 0.631 1.7732E-05 23.50 35000 10.668 218.818 0.85 3.4407E-08 9.0592E-06 5.10 1969 8850 4014.2892 2 95.6 2.4282 154.20 3.9167 NA NA NA
Pratt Whitney JT9D-7Q 747-200B/-200B(M)/-200B(SF)/-200F 53000 235755.6600 11950 53156.229 0.380 1.0677E-05 0.631 1.7732E-05 24.50 35000 10.668 218.818 0.85 3.3436E-08 9.3041E-06 4.90 1969 9300 4218.4056 2 93.6 2.3774 153.60 3.9014 NA NA NA
Pratt Whitney JT9D-7Q3 747-200B/-200B(M)/-200B(SF) 53000 235755.6600 11950 53156.229 0.380 1.0677E-05 0.631 1.7732E-05 24.50 35000 10.668 218.818 0.85 3.3436E-08 9.3041E-06 4.90 1969 9300 4218.4056 2 93.6 2.3774 153.60 3.9014 NA NA NA
Pratt Whitney JT9D-7R 767-200/-200ER/-200ET/-200PC/-300 48000 213514.5600 11200 49820.064 0.410 1.1520E-05 0.615 1.7282E-05 23.40 35000 10.668 218.818 0.85 2.8738E-08 1.0039E-05 4.90 1980 8910 4041.5047 2 93.4 2.3724 153.60 3.9014 NA NA NA
Pratt Whitney JT9D-7R4D 767-200/-200ER/-200ET/-200PC/-300 48000 213514.5600 11200 49820.064 0.343 9.6374E-06 0.615 1.7282E-05 23.40 35000 10.668 218.818 0.85 3.5246E-08 8.3982E-06 4.90 1980 8910 4041.5047 2 93.4 2.3724 153.60 3.9014 NA NA NA
Pratt Whitney JT9D-7R4D1 A310-221 (option) 48019 213599.0762 11200 49820.064 0.343 9.6374E-06 0.615 1.7282E-05 23.40 35000 10.668 218.818 0.85 3.5246E-08 8.3982E-06 4.90 1981 8910 4041.5047 2 93.4 2.3724 153.60 3.9014 NA NA NA
Pratt Whitney JT9D-7R4E 767-200ER 50000 222411.0000 11700 52044.174 0.343 9.6374E-06 0.620 1.7423E-05 24.20 35000 10.668 218.818 0.85 3.5804E-08 8.3982E-06 4.90 1981 8910 4041.5047 2 93.4 2.3724 153.60 3.9014 NA NA NA
Pratt Whitney JT9D-7R4E1 A310-222/-222F/-322 50020 222499.9644 11700 52044.174 0.343 9.6374E-06 0.620 1.7423E-05 24.20 35000 10.668 218.818 0.85 3.5804E-08 8.3982E-06 4.90 1981 8910 4041.5047 2 93.4 2.3724 153.60 3.9014 NA NA NA
Pratt Whitney JT9D-7R4E3 767-200ER (option) 50000 222411.0000 11700 52044.174 0.343 9.6374E-06 0.620 1.7423E-05 24.20 35000 10.668 218.818 0.85 3.5804E-08 8.3982E-06 4.90 1981 9100 4127.6872 2 93.4 2.3724 153.60 3.9014 NA NA NA
Pratt Whitney JT9D-7R4E4 767-200ER 50000 222411.0000 11700 52044.174 0.343 9.6374E-06 0.620 1.7423E-05 24.20 35000 10.668 218.818 0.85 3.5804E-08 8.3982E-06 4.90 1985 9100 4127.6872 2 93.4 2.3724 153.60 3.9014 NA NA NA
Pratt Whitney JT9D-7R4G2 747-200B/-200B(SF)/-200F/-300/-300(M)/-300(SF) 54750 243540.0450 12250 54490.695 0.360 1.0115E-05 0.639 1.7957E-05 26.30 35000 10.668 218.818 0.85 3.6271E-08 8.8144E-06 4.80 1969 9140 4145.8309 2 93.4 2.3724 153.60 3.9014 NA NA NA
Pratt Whitney JT9D-7R4H1 A300B4-620 56022 249198.1808 12250 54490.695 0.364 1.0227E-05 0.628 1.7648E-05 26.70 35000 10.668 218.818 0.85 3.4656E-08 8.9123E-06 4.80 1972 8890 4032.4329 2 93.4 2.3724 153.60 3.9014 NA NA NA
Pratt Whitney JT9D-7W 747-200B NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 4.90 NA NA NA 2 95.6 2.4282 154.20 3.9167 NA NA NA
Pratt Whitney JT9D-9 A300B2/B4 53000 235755.6600 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 2 95.6 2.4282 154.20 3.9167 NA NA NA
Pratt Whitney JTF14 Technology demonstrator NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA
Pratt Whitney JTF17A-21 L-2000-7B (not produced), B-2707-200/-300 (candidate engine) 38300 170366.8260 NA NA 0.750 2.1073E-05 NA NA NA NA NA NA NA NA NA NA NA NA NA 2 NA NA NA NA NA NA NA
Instytut Lotnictwa K-15 I-22 3307 14710.2635 NA NA 1.006 2.8266E-05 NA NA 5.30 NA NA NA NA NA NA 0.00 NA 705 319.7824 1 NA NA 61.40 1.5596 35.1 0.8915 0.9736
Turbomeca/Snecma Larzac 04-C20 Falcon 10, Corvette 3175 14123.0985 2731 12148.089 0.760 2.1354E-05 1.120 3.1473E-05 11.10 30000 9.144 228.724 0.80 5.1326E-08 1.9025E-05 1.04 1982 734 332.9365 2 NA NA NA NA NA NA NA
Avco Lycoming (Textron Lycoming) LF507-1F RJ-70/-85/-100/-115 7000 31137.5400 NA NA 0.406 1.1408E-05 0.413 1.1606E-05 13.80 26000 7.925 236.649 0.52 7.9073E-09 1.0338E-05 5.70 1980 1385 628.2249 2 40.0 1.0160 58.60 1.4884 41.7 1.0592 1.3115
Avco Lycoming (Textron Lycoming) LF507-1H  RJ-70/-85/-100/-115 7000 31137.5400 NA NA 0.406 1.1408E-05 0.413 1.1606E-05 13.80 26000 7.925 236.649 0.52 7.9073E-09 1.0338E-05 5.70 1980 1375 623.6890 2 40.0 1.0160 58.60 1.4884 41.7 1.0592 1.3115
Avco Lycoming (Textron Lycoming) LF507-1N Yak-40TL 7000 31137.5400 NA NA 0.406 1.1408E-05 0.413 1.1606E-05 NA 26000 7.925 236.649 0.52 7.9073E-09 1.0338E-05 5.70 1980 1375 623.6890 2 40.0 1.0160 58.60 1.4884 41.7 1.0592 1.3115
Rolls-Royce/Snecma M45F Technology demonstrator NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 2 NA NA NA NA NA NA NA
Rolls-Royce/Snecma M45H-01 NA 7763 34531.5319 2746 12214.812 0.451 1.2672E-05 0.730 2.0514E-05 18.00 20000 6.096 248.536 0.65 4.2573E-08 1.1768E-05 2.80 1968 1484 673.1305 2 NA NA NA NA NA NA NA
Rolls-Royce/Snecma M45H-D Mk.501 VFW 614 (not produced) 7760 34518.1872 2745 12210.364 0.451 1.2672E-05 0.730 2.0514E-05 18.80 20000 6.096 248.536 0.65 4.2573E-08 1.1768E-05 2.85 1971 1480 671.3162 2 41.7 1.0592 116.50 2.9591 NA NA NA
Rolls-Royce/Snecma M45H-E1 NA 9250 41146.0350 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 2 NA NA NA NA NA NA NA
Rolls-Royce/Snecma M45H-E2 NA 9600 42702.9120 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 2 NA NA NA NA NA NA NA
Turbomeca Marbore 2 Saulnier Paris 1 882 3923.3300 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 1 NA NA NA NA NA NA NA
Turbomeca Marbore 2A Noratlas N-2502 882 3923.3300 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 1 NA NA NA NA NA NA NA
Turbomeca Marbore 6C Saulnier Paris 2, Saulnier Paris 3 1060 4715.1132 NA NA 1.110 3.1188E-05 NA NA 3.80 NA NA NA NA NA NA NA NA NA NA 1 NA NA NA NA NA NA NA
Turbomeca Marbore 6F CM,191 (not produced) 1058 4706.2168 NA NA 1.110 3.1188E-05 NA NA 3.80 NA NA NA NA NA NA NA NA NA NA 1 NA NA NA NA NA NA NA
Maverick MC-750 MC-2400 Legend 750 3336.1650 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 1 NA NA NA NA NA NA NA
Rolls-Royce Nene RB.41-1 F26 (not produced) 4600 20461.8120 NA NA 1.049 2.9474E-05 NA NA 4.00 NA NA NA NA NA NA NA NA NA NA 1 NA NA NA NA NA NA NA
Kuznetsov NK-144 Tu-144/-144D/-144LL 28660 127485.9852 NA NA NA NA NA NA 14.20 NA NA NA NA NA NA 0.60 NA NA NA 2 NA NA NA NA NA NA NA
Kuznetsov NK-144A Tu-144S (not produced) 33070 147102.6354 NA NA NA NA NA NA 17.00 NA NA NA NA NA NA 0.53 NA NA NA 2 NA NA NA NA NA NA NA
Kuznetsov NK-321 Tu-144 30843 137196.4495 NA NA NA NA NA NA 28.40 NA NA NA NA NA NA 1.40 NA 7590 3442.7633 3 NA NA 236.00 5.9944 57.5 1.4605 10.0424
Kuznetsov NK-44 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA
Kuznetsov NK-44K NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA
Kuznetsov NK-8-2 Tu-154 20944 93163.5197 NA NA 0.579 1.6268E-05 NA NA 21.50 NA NA NA NA NA NA 1.05 NA 4630 2100.1310 2 NA NA 187.50 4.7625 56.8 1.4427 7.7855
Kuznetsov NK-8-2U Tu-154A/B 23150 102976.2930 NA NA 0.569 1.5987E-05 NA NA 23.20 NA NA NA NA NA NA 1.05 NA 4630 2100.1310 2 NA NA 187.50 4.7625 56.8 1.4427 7.7855
Kuznetsov NK-8-3 Il-62 20950 93190.2090 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 2 NA NA NA NA NA NA NA
Kuznetsov NK-8-4 Il-62 23150 102976.2930 NA NA 0.588 1.6521E-05 NA NA 23.20 NA NA NA NA NA NA 1.02 NA 4630 2100.1310 2 NA NA 201.00 5.1054 56.8 1.4427 8.3461
Kuznetsov NK-86 (see NK-86) 28660 127485.9852 NA NA NA NA NA NA 13.40 NA NA NA NA NA NA 1.15 NA NA NA 2 NA NA 143.00 3.6322 63.0 1.6002 7.3048
Kuznetsov NK-93 Il-96M, Tu-204-230, Tu-330 (proposed) 39683 176518.7143 7194 32000.495 0.235 6.6029E-06 0.490 1.3770E-05 28.90 36090 11.000 216.658 0.75 3.6349E-08 5.7254E-06 16.60 2008 8050 3651.4156 3 114.2 2.9007 235.10 5.9715 NA NA NA
Rolls-Royce/Snecma Olympus 593 Mk.601 Concorde 32600 145011.9720 10030 44615.647 0.700 1.9668E-05 1.190 3.3440E-05 15.50 53000 NA NA NA NA NA 1.35 1969 5810 2635.3695 2 NA NA 138.20 3.5103 47.9 1.2167 4.0810
Rolls-Royce/Snecma Olympus 593 Mk.610 Concorde 31352 139460.5934 10026 44597.854 0.880 2.4726E-05 1.190 3.3440E-05 14.50 53000 NA NA NA NA NA 0.28 1969 9985 4529.1161 2 NA NA 138.20 3.5103 47.9 1.2167 4.0810
Rolls-Royce/Snecma Olympus 593 Mk.611 Concorde 38400 170811.6480 10030 44615.647 0.700 1.9668E-05 1.190 3.3440E-05 NA 53000 NA NA NA NA NA 1.35 1969 5810 2635.3695 2 NA NA 138.20 3.5103 47.9 1.2167 4.0810
Rolls-Royce/Snecma Olympus 593 Mk.621 Concorde 38400 170811.6480 10030 44615.647 0.700 1.9668E-05 1.190 3.3440E-05 NA 53000 NA NA NA NA NA 1.35 1969 5810 2635.3695 2 NA NA 138.20 3.5103 47.9 1.2167 4.0810
Solovyev PS-12 MS-21-100/-200/-300, MS-21K, MS-12KP (candidate engine) 29762 132387.9236 5665 25199.166 NA NA 0.549 1.5428E-05 40.20 36000 10.973 216.837 0.80 NA NA 8.39 NA 5400 2449.3968 NA 73.6 1.8694 NA NA NA NA NA
Solovyev PS-12M NA 32740 145634.7228 6062 26965.110 NA NA 0.553 1.5540E-05 NA 36000 10.973 216.837 0.80 NA NA NA NA 5400 2449.3968 NA 73.6 1.8694 NA NA NA NA NA
Solovyev PS-7 NA 17000 75619.7400 3417 15199.568 NA NA 0.620 1.7423E-05 NA 36000 10.973 216.837 0.80 NA NA NA NA 2980 1351.7042 NA 47.6 1.2090 NA NA NA NA NA
Solovyev PS-9 Il-214-100, Il-214T (candidate engine) 22000 97860.8400 4630 20595.259 NA NA 0.590 1.6580E-05 NA 36000 10.973 216.837 0.80 NA NA NA NA 3860 1750.8651 NA 56.5 1.4351 NA NA NA NA NA
Solovyev (Perm Aviadvigatel) PS-90 Il-214, RRJ (candidate engine) 35250 156799.7550 7711 34300.224 0.380 1.0677E-05 0.600 1.6861E-05 31.90 36090 11.000 216.658 0.80 3.2207E-08 9.2581E-06 4.60 1992 6504 2950.1624 NA NA NA NA NA NA NA NA
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) 35275 156910.9605 7716 34322.466 0.380 1.0677E-05 0.600 1.6861E-05 35.50 36090 11.000 216.658 0.80 3.2207E-08 9.2581E-06 4.60 1992 6504 2950.1624 2 NA NA NA NA NA NA NA
Solovyev (Perm Aviadvigatel) PS-90A10 NA 20283 90223.2463 7716 34322.466 NA NA 0.600 1.6861E-05 23.10 36090 11.000 216.658 0.80 NA NA 3.76 1992 4180 1896.0146 2 55.1 1.3995 168.50 4.2799 NA NA NA
Solovyev (Perm Aviadvigatel) PS-90A12 Yak-242 26455 117677.6601 7716 34322.466 0.430 1.2082E-05 0.600 1.6861E-05 25.30 36090 11.000 216.658 0.80 2.7046E-08 1.0476E-05 5.05 1980 5070 2299.7114 2 65.8 1.6713 188.20 4.7803 NA NA NA
Solovyev (Perm Aviadvigatel) PS-90A-154 Tu-154M-2 (proposed) NA NA 7716 34322.466 NA NA 0.600 1.6861E-05 NA 36090 11.000 216.658 0.80 NA NA 4.60 1992 4180 1896.0146 2 NA NA NA NA NA NA NA
Solovyev (Perm Aviadvigatel) PS-90A2 Il-96-300, Il-76TF, Tu-204-500/-600 (proposed) NA NA 7716 34322.466 NA NA 0.600 1.6861E-05 NA 36090 11.000 216.658 0.80 NA NA 4.60 1992 4180 1896.0146 2 NA NA NA NA NA NA NA
Solovyev (Perm Aviadvigatel) PS-90AN-76 Il-76TF 35275 156910.9605 7716 34322.466 0.440 1.2363E-05 0.600 1.6861E-05 35.50 36090 11.000 216.658 0.80 2.6014E-08 1.0720E-05 4.60 1971 6503 2949.7088 2 74.8 1.8999 195.40 4.9632 NA NA NA
Solovyev (Perm Aviadvigatel) PS-90AP Tu-234 NA NA 7716 34322.466 NA NA 0.600 1.6861E-05 NA 36090 11.000 216.658 0.80 NA NA 4.60 1992 NA NA 2 NA NA NA NA NA NA NA
Pratt Whitney PW2037 757-200/-200ET 38250 170144.4150 6500 28913.430 0.335 9.4126E-06 0.582 1.6355E-05 27.40 35000 10.668 218.818 0.85 3.2344E-08 8.2023E-06 5.80 1982 7190 3261.3265 2 78.5 1.9939 141.40 3.5916 84.8 2.1539 13.0868
Pratt Whitney PW2040 757-200/-200ET/-200F 40100 178373.6220 6500 28913.430 0.330 9.2721E-06 0.582 1.6355E-05 29.90 35000 10.668 218.818 0.85 3.2830E-08 8.0799E-06 5.90 1982 7190 3261.3265 2 78.5 1.9939 141.40 3.5916 84.8 2.1539 13.0868
Pratt Whitney PW2043 757-300, 757-200/-200ET/-200F (option) 42600 189494.1720 NA NA 0.350 9.8341E-06 NA NA 31.90 NA NA NA NA NA NA 6.00 NA 7160 3247.7187 2 78.5 1.9939 141.40 3.5916 84.8 2.1539 13.0868
Pratt Whitney PW2143 A340-521, A340-621 (proposed) 42600 189494.1720 NA NA 0.350 9.8341E-06 NA NA 31.20 NA NA NA NA NA NA 6.00 NA 7160 3247.7187 2 78.5 1.9939 141.40 3.5916 84.8 2.1539 13.0868
Pratt Whitney PW2237 Tu-204-140/-140C (proposed) 36600 162804.8520 6500 28913.430 0.335 9.4126E-06 0.582 1.6355E-05 27.90 35000 10.668 218.818 0.85 3.2344E-08 8.2023E-06 5.80 1989 7190 3261.3265 2 78.5 1.9939 141.40 3.5916 84.8 2.1539 13.0868
Pratt Whitney PW2240 Tu-204-240/-240C, Tu-330 (Tu-204-330) (proposed) 40100 178373.6220 6500 28913.430 0.330 9.2721E-06 0.582 1.6355E-05 27.60 35000 10.668 218.818 0.85 3.2830E-08 8.0799E-06 5.90 1989 7190 3261.3265 2 78.5 1.9939 141.40 3.5916 84.8 2.1539 13.0868
Pratt Whitney PW2337 Il-96M/T 36600 162804.8520 6500 28913.430 0.335 9.4126E-06 0.582 1.6355E-05 27.40 35000 10.668 218.818 0.85 3.2344E-08 8.2023E-06 5.80 1988 7190 3261.3265 2 78.5 1.9939 141.40 3.5916 84.8 2.1539 13.0868
Pratt Whitney PW2643 NA 42600 189494.1720 NA NA 0.350 9.8341E-06 NA NA 31.20 NA NA NA NA NA NA 6.00 NA 7160 3247.7187 2 78.5 1.9939 141.40 3.5916 84.8 2.1539 13.0868
Pratt Whitney Canada PW305A Learjet 60 4679 20813.2214 1113 4950.869 0.388 1.0902E-05 0.675 1.8968E-05 15.50 40000 12.192 216.650 0.80 4.0311E-08 9.4528E-06 4.30 1990 993 450.4169 2 30.7 0.7798 81.50 2.0701 36.5 0.9271 1.3974
Pratt Whitney Canada PW305B BAe (Hawker) 1000 5258 23388.7408 1113 4950.869 0.391 1.0986E-05 0.675 1.8968E-05 15.50 40000 12.192 216.650 0.80 4.0001E-08 9.5259E-06 4.30 1990 993 450.4169 2 30.7 0.7798 81.50 2.0701 36.5 0.9271 1.3974
Pratt Whitney Canada PW306A G200 (Galaxy) 6040 26867.2488 1250 5560.275 0.394 1.1070E-05 0.700 1.9671E-05 18.30 40000 12.192 216.650 0.80 4.2668E-08 9.5990E-06 4.50 1995 1040 471.7357 2 31.7 0.8052 75.60 1.9202 NA NA NA
Pratt Whitney Canada PW306B 328JET, Envoy 3 6050 26911.7310 1130 5026.489 0.400 1.1239E-05 0.680 1.9109E-05 NA 40000 12.192 216.650 0.80 3.9668E-08 9.7451E-06 4.50 1999 1040 471.7357 2 31.7 0.8052 75.60 1.9202 NA NA NA
Pratt Whitney Canada PW306C Citation Sovereign 5686 25292.5789 1130 5026.489 0.407 1.1436E-05 0.681 1.9137E-05 NA 40000 12.192 216.650 0.80 3.9064E-08 9.9157E-06 4.50 2002 990 449.0561 2 31.7 0.8052 75.60 1.9202 NA NA NA
Pratt Whitney Canada PW307A Falcon 7X 6100 27134.1420 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 2 31.7 0.8052 75.60 1.9202 NA NA NA
Pratt Whitney Canada PW308A Hawker Horizon 6575 29247.0465 NA NA NA NA NA NA NA NA NA NA NA NA NA 4.10 NA NA NA 2 31.7 0.8052 75.60 1.9202 NA NA NA
Pratt Whitney Canada PW308B 428JET (not produced) 8089 35981.6516 NA NA NA NA NA NA NA NA NA NA NA NA NA 4.10 NA NA NA 2 31.7 0.8052 75.60 1.9202 NA NA NA
Pratt Whitney Canada PW308C Falcon 2000EX 7000 31137.5400 NA NA NA NA NA NA NA NA NA NA NA NA NA 4.10 NA NA NA 2 31.7 0.8052 75.60 1.9202 NA NA NA
Pratt Whitney PW4052 767-200ER/-300ER 52200 232197.0840 NA NA 0.310 8.7102E-06 0.590 1.6580E-05 26.40 35000 10.668 218.818 0.80 3.7894E-08 7.5902E-06 4.85 1986 9210 4177.5823 2 93.6 2.3774 132.20 3.3579 97.0 2.4638 16.0091
Pratt Whitney PW4056 747-400/-400(M)/-400F, 767-200ER/-300/-300ER 56750 252436.4850 NA NA 0.320 8.9911E-06 0.580 1.6299E-05 28.40 35000 10.668 218.818 0.80 3.5677E-08 7.8350E-06 4.85 1987 9210 4177.5823 2 93.6 2.3774 132.20 3.3579 97.0 2.4638 16.0091
Pratt Whitney PW4060 767-300/-300ER, An-218-200/-300 (proposed) 60000 266893.2000 NA NA 0.330 9.2721E-06 NA NA 30.00 NA NA NA NA NA NA 4.85 NA 9210 4177.5823 2 93.6 2.3774 132.20 3.3579 97.0 2.4638 16.0091
Pratt Whitney PW4060A 767-200ER 60000 266893.2000 NA NA 0.330 9.2721E-06 NA NA 31.50 NA NA NA NA NA NA 4.85 NA 9210 4177.5823 2 93.6 2.3774 132.20 3.3579 97.0 2.4638 16.0091
Pratt Whitney PW4062 767-300ER, 747-400/-400ER/-400F/-400FER, 767-200ER/-200FER/-300F/-400ER (option) 63300 281572.3260 NA NA NA NA NA NA 32.30 NA NA NA NA NA NA 4.85 NA 9210 4177.5823 2 93.6 2.3774 132.20 3.3579 97.0 2.4638 16.0091
Pratt Whitney PW4074 777-200 74500 331392.3900 NA NA NA NA NA NA 30.30 NA NA NA NA NA NA 6.00 NA 14550 6599.7636 2 112.0 2.8448 191.70 4.8692 118.5 3.0099 34.6457
Pratt Whitney PW4077 777-200 77000 342512.9400 NA NA NA NA NA NA 31.50 NA NA NA NA NA NA 6.20 NA 14550 6599.7636 2 112.0 2.8448 191.70 4.8692 118.5 3.0099 34.6457
Pratt Whitney PW4077D NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 6.20 NA 14550 6599.7636 2 112.0 2.8448 191.70 4.8692 118.5 3.0099 34.6457
Pratt Whitney PW4084 777-200 84000 373650.4800 NA NA NA NA 0.560 1.5737E-05 36.30 35000 10.668 218.818 0.83 NA NA 6.41 1994 14550 6599.7636 2 112.0 2.8448 191.70 4.8692 118.5 3.0099 34.6457
Pratt Whitney PW4084D NA NA NA NA NA NA NA 0.560 1.5737E-05 NA 35000 10.668 218.818 0.83 NA NA 6.41 1994 14500 6577.0840 2 112.0 2.8448 191.70 4.8692 118.5 3.0099 34.6457
Pratt Whitney PW4090 777-200ER/-300 90200 401229.4440 NA NA NA NA NA NA 38.60 NA NA NA NA NA NA 6.30 NA 15580 7066.9634 2 112.0 2.8448 191.70 4.8692 118.5 3.0099 34.6457
Pratt Whitney PW4090-3 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 6.30 NA 15580 7066.9634 2 112.0 2.8448 191.70 4.8692 118.5 3.0099 34.6457
Pratt Whitney PW4090D NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 6.30 NA 15580 7066.9634 2 112.0 2.8448 191.70 4.8692 118.5 3.0099 34.6457
Pratt Whitney PW4098 777-300 98000 435925.5600 14000 62275.080 0.380 1.0677E-05 0.581 1.6327E-05 42.80 35000 10.668 218.818 0.83 2.8533E-08 9.3041E-06 5.80 1985 16500 7484.2680 2 112.0 2.8448 194.70 4.9454 119.5 3.0353 35.7843
Pratt Whitney PW4152 A310-324/-324ET/-324F 52001 231311.8882 NA NA 0.312 8.7664E-06 0.574 1.6130E-05 27.30 35000 10.668 218.818 0.80 3.5792E-08 7.6391E-06 4.85 1986 9210 4177.5823 2 93.6 2.3774 132.20 3.3579 97.0 2.4638 16.0091
Pratt Whitney PW4156 A310-325ET 56750 252436.4850 NA NA 0.320 8.9911E-06 NA NA 30.20 NA NA NA NA NA NA 4.85 NA 9210 4177.5823 2 93.6 2.3774 132.20 3.3579 97.0 2.4638 16.0091
Pratt Whitney PW4156A A310-325ET 55995 249078.0789 NA NA 0.320 8.9911E-06 NA NA 29.80 NA NA NA NA NA NA 4.85 NA 9210 4177.5823 2 93.6 2.3774 132.20 3.3579 97.0 2.4638 16.0091
Pratt Whitney PW4158 A300B4-622/-622R/-622RF, A300F4-622R 58000 257996.7600 NA NA 0.323 9.0754E-06 0.580 1.6299E-05 30.70 31000 9.449 226.743 0.78 3.5032E-08 8.0504E-06 4.75 NA 9210 4177.5823 2 93.6 2.3774 132.20 3.3579 97.0 2.4638 16.0091
Pratt Whitney PW4164 A330-321, A330-221 (option) 64502 286919.0864 NA NA NA NA NA NA 32.00 NA NA NA NA NA NA 5.10 NA 12400 5624.5408 2 99.8 2.5349 163.10 4.1427 106.9 2.7153 23.9884
Pratt Whitney PW4168 A330-222/-322 68600 305147.8920 NA NA NA NA 0.570 1.6018E-05 33.40 35000 10.668 218.818 0.80 NA NA 5.10 1993 12400 5624.5408 2 99.8 2.5349 163.10 4.1427 106.9 2.7153 23.9884
Pratt Whitney PW4168A A330-223/-323X 68600 305147.8920 NA NA NA NA 0.570 1.6018E-05 32.00 35000 10.668 218.818 0.80 NA NA 5.10 1993 12400 5624.5408 2 99.8 2.5349 163.10 4.1427 106.9 2.7153 23.9884
Pratt Whitney PW4460 MD-11/-11F/-11F(AF) 60000 266893.2000 NA NA 0.330 9.2721E-06 NA NA 31.50 NA NA NA NA NA NA 4.85 NA 9210 4177.5823 2 93.6 2.3774 132.20 3.3579 97.0 2.4638 16.0091
Pratt Whitney PW4462 MD-11/-11F/-11F(CF) 63300 281572.3260 NA NA NA NA NA NA 32.30 NA NA NA NA NA NA 4.85 NA 9210 4177.5823 2 93.6 2.3774 132.20 3.3579 97.0 2.4638 16.0091
Pratt Whitney Canada PW530 Citation Bravo 2923 13002.1471 607 2700.070 0.440 1.2363E-05 0.760 2.1357E-05 NA 40000 12.192 216.650 0.80 4.5063E-08 1.0720E-05 4.00 1995 606 274.8768 2 22.8 0.5791 60.00 1.5240 NA NA NA
Pratt Whitney Canada PW535A Citation Encore 2748 12223.7086 NA NA NA NA NA NA NA NA NA NA NA NA NA 2.60 NA NA NA 2 NA NA NA NA NA NA NA
Pratt Whitney Canada PW545A Citation Excel 3784 16832.0645 NA NA NA NA NA NA 15.70 NA NA NA NA NA NA 4.12 NA 815 369.6775 2 27.2 0.6909 68.00 1.7272 32.0 0.8128 0.8962
Pratt Whitney Canada PW610F Eclipse 500 1112 4946.4206 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA
Pratt Whitney PW6122 A318-121, Il-214 (candidate engine), A316/A317 (A31X) (not produced) 22000 97860.8400 NA NA 0.360 1.0115E-05 0.613 1.7226E-05 27.20 39000 11.887 216.650 0.80 3.5820E-08 8.7706E-06 4.90 NA 4120 1868.7990 2 56.5 1.4351 92.00 2.3368 60.0 1.5240 4.2627
Pratt Whitney Canada PW615F Citation Mustang, Eclipse 500, ProJet (candidate engine) 1350 6005.0970 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA
Pratt Whitney PW6162 A318-122 24000 106757.2800 NA NA 0.370 1.0396E-05 NA NA 29.60 NA NA NA NA NA NA 4.90 NA 4120 1868.7990 2 56.5 1.4351 92.00 2.3368 60.0 1.5240 4.2627
Pratt Whitney Canada PW625F Technology demonstrator 2500 11120.5500 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA
Pratt Whitney Canada PW645 Citation CJ3 (candidate engine) NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA
Pratt Whitney Canada PW800 (AFTI) Technology demonstrator 12500 55602.7500 NA NA NA NA NA NA NA NA NA NA NA NA NA 7.80 NA NA NA 2 NA NA NA NA NA NA NA
Pratt Whitney PW8160 A340-521, A340-621 (proposed) 65000 289134.3000 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 2 NA NA NA NA NA NA NA
Soyuz R123-300 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 6.00 NA NA NA 2 NA NA NA NA NA NA NA
Soyuz R126-300 Tu-324 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 2 NA NA NA NA NA NA NA
Soyuz R127-300 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 2 NA NA NA NA NA NA NA
Rolls-Royce RB.141-3 HFB 314 (not produced) NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA
Rolls-Royce RB.162-86 Trident 3B (booster) 5250 23353.1550 NA NA 1.120 3.1469E-05 NA NA 4.30 NA NA NA NA NA NA NA NA 520 235.8678 1 NA NA 97.70 2.4816 NA NA NA
Rolls-Royce RB.178 NA 28500 126774.2700 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA
Rolls-Royce RB.178-51 747-100 (proposed) NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 8.00 NA NA NA NA NA NA NA NA NA NA NA
Rolls-Royce RB.199-34R-04 MK.103 747-400/-400F (option) 9150 40701.2130 7868 34998.595 0.640 1.7982E-05 0.980 2.7539E-05 23.50 35000 10.668 218.818 0.90 4.4473E-08 1.5670E-05 1.06 NA 2339 1060.9517 NA NA NA NA NA NA NA NA
Rolls-Royce RB.202 Do 231C (lift engines, not produced) 13100 58271.6820 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 3 NA NA NA NA NA NA NA
Rolls-Royce RB.207 A300, L1011-1-1 (candidate engine) 47500 211290.4500 NA NA 0.540 1.5173E-05 NA NA 27.00 NA NA NA NA NA NA 5.00 NA NA NA 3 NA NA 128.70 3.2690 NA NA NA
Rolls-Royce RB.211-22-02 L1011-1 40600 180597.7320 NA NA NA NA NA NA 27.00 NA NA NA NA NA NA 4.80 NA 7190 3261.3265 3 84.8 2.1539 119.40 3.0328 NA NA NA
Rolls-Royce RB.211-22B-02 L1011-1/-1F/-50/-100/-150, L1011-400 (not produced) 42000 186825.2400 9495 42235.849 0.373 1.0480E-05 0.628 1.7648E-05 24.50 35000 10.668 218.818 0.85 3.3781E-08 9.1327E-06 4.80 1970 9210 4177.5823 3 NA NA NA NA NA NA NA
Rolls-Royce RB.211-22C-02 L1011-1/-50/-100/-150 (option) 42000 186825.2400 NA NA NA NA NA NA 24.50 NA NA NA NA NA NA 4.80 NA NA NA 3 NA NA NA NA NA NA NA
Rolls-Royce RB.211-22CA-02 L1011-1/-50/-100/-150 (option) NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 3 NA NA NA NA NA NA NA
Rolls-Royce RB.211-23 L1011-1/-50/-100/-150 (option) 38380 170722.6836 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 3 NA NA NA NA NA NA NA
Rolls-Royce RB.211-24 (see RB,211-524), L1011-2 (not produced) 50000 222411.0000 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 3 NA NA NA NA NA NA NA
Rolls-Royce RB.211-40 BAC 311 (not produced) 43040 191451.3888 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 3 NA NA NA NA NA NA NA
Rolls-Royce RB.211-52 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 4.40 NA NA NA 3 NA NA NA NA NA NA NA
Rolls-Royce RB.211-524 L1011-100/-200, 747-SP (option), L-1011-300 (not produced) 48000 213514.5600 NA NA NA NA 0.570 1.6018E-05 28.40 NA NA NA NA NA NA 4.30 NA NA NA 3 84.8 2.1539 119.40 3.0328 NA NA NA
Rolls-Royce RB.211-524B-02 747-SP, L1011-200/-200F/-500/-500F, 747-100 (option), L-1011-600 (not produced) 50000 222411.0000 11000 48930.420 NA NA 0.570 1.6018E-05 28.40 35000 10.668 218.818 0.85 NA NA 4.50 NA 9810 4449.7375 3 84.8 2.1539 119.40 3.0328 NA NA NA
Rolls-Royce RB.211-524B2-02 L1011-200/-200F/-500, 747-SP/-100 (option) 50000 222411.0000 11000 48930.420 NA NA 0.570 1.6018E-05 28.40 35000 10.668 218.818 0.85 NA NA 4.50 NA 9810 4449.7375 3 NA NA NA NA NA NA NA
Rolls-Royce RB.211-524B3-02 NA NA NA 11000 48930.420 NA NA 0.570 1.6018E-05 NA 35000 10.668 218.818 0.85 NA NA 4.30 NA 9810 4449.7375 3 85.8 2.1793 122.30 3.1064 NA NA NA
Rolls-Royce RB.211-524B4-02 L1011-200/-200F/-250/-500 50000 222411.0000 11000 48930.420 NA NA 0.606 1.7029E-05 29.00 35000 10.668 218.818 0.85 NA NA 4.40 NA 9810 4449.7375 3 85.8 2.1793 122.30 3.1064 NA NA NA
Rolls-Royce RB.211-524B4D-02 L1011-200/-500 50000 222411.0000 11000 48930.420 NA NA 0.570 1.6018E-05 28.60 35000 10.668 218.818 0.85 NA NA 4.40 NA 9810 4449.7375 3 84.8 2.1539 119.40 3.0328 NA NA NA
Rolls-Royce RB.211-524BD-02 L1011-200/-200F/-500, 747-100 (option) 50000 222411.0000 11000 48930.420 NA NA 0.570 1.6018E-05 28.40 35000 10.668 218.818 0.85 NA NA 4.50 NA 9810 4449.7375 3 84.8 2.1539 119.40 3.0328 NA NA NA
Rolls-Royce RB.211-524C 747-SP/-100B/-200B/-300 51500 229083.3300 11490 51110.048 0.410 1.1520E-05 0.642 1.8041E-05 28.60 35000 10.668 218.818 0.85 3.1748E-08 1.0039E-05 4.50 1972 9860 4472.4171 3 84.8 2.1539 119.40 3.0328 NA NA NA
Rolls-Royce RB.211-524C2 747-SP/-100B/-200B/-300 51500 229083.3300 11490 51110.048 NA NA 0.642 1.8041E-05 28.60 35000 10.668 218.818 0.85 NA NA 4.50 1972 9860 4472.4171 3 84.8 2.1539 119.40 3.0328 NA NA NA
Rolls-Royce RB.211-524C4 747-200B, 747-100B/-300 (option) NA NA NA NA NA NA 0.570 1.6018E-05 NA NA NA NA NA NA NA 4.50 NA 9860 4472.4171 3 85.8 2.1793 122.30 3.1064 NA NA NA
Rolls-Royce RB.211-524D4 747-SP/-200B/-200B(M)/-200B(SF)/-200F/-300, L1011-500H&H (not produced) 53000 235755.6600 11230 49953.511 0.420 1.1801E-05 0.617 1.7338E-05 29.30 35000 10.668 218.818 0.85 2.7990E-08 1.0283E-05 4.40 1972 9870 4476.9530 3 85.8 2.1793 122.30 3.1064 NA NA NA
Rolls-Royce RB.211-524D4B 747-200/-200F/-300 (option) 53000 235755.6600 11230 49953.511 NA NA 0.601 1.6889E-05 29.60 35000 10.668 218.818 0.85 NA NA 4.40 1970 9870 4476.9530 3 86.3 2.1920 125.00 3.1750 NA NA NA
Rolls-Royce RB.211-524G 747-400/-400F, 767-300ER (option) 58000 257996.7600 11813 52546.823 NA NA 0.570 1.6018E-05 32.90 35000 10.668 218.818 0.85 NA NA 4.30 1970 9670 4386.2346 3 86.3 2.1920 125.00 3.1750 NA NA NA
Rolls-Royce RB.211-524G/H NA NA NA 11813 52546.823 NA NA 0.570 1.6018E-05 NA 35000 10.668 218.818 0.85 NA NA 4.30 NA 9670 4386.2346 3 86.3 2.1920 125.00 3.1750 NA NA NA
Rolls-Royce RB.211-524G/H-T NA 58000 257996.7600 11813 52546.823 NA NA 0.570 1.6018E-05 NA 35000 10.668 218.818 0.85 NA NA 4.30 NA 9670 4386.2346 3 86.3 2.1920 125.00 3.1750 NA NA NA
Rolls-Royce RB.211-524G2-T 747-400ER (option) NA NA NA NA NA NA 0.570 1.6018E-05 NA NA NA NA NA NA NA 4.10 NA 9470 4295.5162 3 86.3 2.1920 125.00 3.1750 NA NA NA
Rolls-Royce RB.211-524G3 767-300ER/-300FER (option) 58000 257996.7600 NA NA NA NA 0.570 1.6018E-05 NA NA NA NA NA NA NA 4.10 NA 9670 4386.2346 3 86.3 2.1920 125.00 3.1750 NA NA NA
Rolls-Royce RB.211-524G3-T NA NA NA NA NA NA NA 0.570 1.6018E-05 NA NA NA NA NA NA NA 4.10 NA 9470 4295.5162 3 86.3 2.1920 125.00 3.1750 NA NA NA
Rolls-Royce RB.211-524G4-T 767-300ER/-300FER (option) 56400 250879.6080 NA NA NA NA 0.570 1.6018E-05 NA NA NA NA NA NA NA 4.10 NA 9670 4386.2346 3 86.3 2.1920 125.00 3.1750 NA NA NA
Rolls-Royce RB.211-524G-T 747-400/-400F, 767-300ER (option) NA NA 11813 52546.823 NA NA 0.570 1.6018E-05 NA 35000 10.668 218.818 0.85 NA NA 4.30 NA 9470 4295.5162 3 86.3 2.1920 125.00 3.1750 NA NA NA
Rolls-Royce RB.211-524H 747-400, 767-300ER, 767-300F/-300FER/-400F (option) 60600 269562.1320 11813 52546.823 0.565 1.5875E-05 0.575 1.6158E-05 34.50 35000 10.668 218.818 0.85 9.2219E-09 1.3834E-05 4.10 1989 9670 4386.2346 3 86.3 2.1920 125.00 3.1750 NA NA NA
Rolls-Royce RB.211-524H2 747-400/-400F 60000 266893.2000 11813 52546.823 0.565 1.5875E-05 0.575 1.6158E-05 NA 35000 10.668 218.818 0.85 9.2219E-09 1.3834E-05 4.10 1989 9670 4386.2346 3 86.3 2.1920 125.00 3.1750 NA NA NA
Rolls-Royce RB.211-524H2-T 747-400ER (option) 59500 264669.0900 11813 52546.823 0.565 1.5875E-05 0.575 1.6158E-05 NA 35000 10.668 218.818 0.85 9.2219E-09 1.3834E-05 4.10 1989 9470 4295.5162 3 86.3 2.1920 125.00 3.1750 NA NA NA
Rolls-Royce RB.211-524H3 767-300ER, 767-300FER (option) 60600 269562.1320 11813 52546.823 0.565 1.5875E-05 0.575 1.6158E-05 NA 35000 10.668 218.818 0.85 9.2219E-09 1.3834E-05 4.10 1989 9670 4386.2346 3 86.3 2.1920 125.00 3.1750 NA NA NA
Rolls-Royce RB.211-524H4 An-218-200/-300 (proposed) NA NA 11813 52546.823 0.565 1.5875E-05 0.575 1.6158E-05 NA 35000 10.668 218.818 0.85 9.2219E-09 1.3834E-05 4.10 1989 9670 4386.2346 3 86.3 2.1920 125.00 3.1750 NA NA NA
Rolls-Royce RB.211-524H-T 747-400/-400F, 767-300ER, An-124-210 (option) 60600 269562.1320 11813 52546.823 0.565 1.5875E-05 0.575 1.6158E-05 NA 35000 10.668 218.818 0.85 9.2219E-09 1.3834E-05 4.10 1989 9470 4295.5162 3 86.3 2.1920 125.00 3.1750 NA NA NA
Rolls-Royce RB.211-53 NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA NA 4.30 NA NA NA 3 NA NA NA NA NA NA NA
Rolls-Royce RB.211-535C-37 757-200/-200(SF)/-200F 37400 166363.4280 8453 37600.804 NA NA 0.646 1.8153E-05 21.10 35000 10.668 218.818 0.80 NA NA 4.40 1982 7290 3306.6857 3 73.2 1.8593 118.50 3.0099 NA NA NA
Rolls-Royce RB.211-535E4 757-300 43100 191718.2820 8495 37787.629 0.610 1.7139E-05 0.600 1.6861E-05 25.80 35000 10.668 218.818 0.80 8.1153E-09 1.4935E-05 4.30 1984 7264 3294.8923 3 74.1 1.8821 117.90 2.9947 NA NA NA
Rolls-Royce RB.211-535E4-37 757-200/-200ER/-200ET/-200F, Tu-204-120/-120C/-220/-220C/-222, Tu-224 40100 178373.6220 8700 38699.514 0.324 9.1035E-06 0.598 1.6804E-05 25.80 35000 10.668 218.818 0.80 3.7396E-08 7.9330E-06 4.30 1984 9260 4200.2619 3 74.1 1.8821 117.90 2.9947 NA NA NA
Rolls-Royce RB.211-535E4B-37 757-200/-200ET/-300, 757-200ER/-200F (option), Tu-214, Tu-330 (Tu-204-330) (proposed) 43100 191718.2820 8700 38699.514 0.324 9.1035E-06 0.598 1.6804E-05 25.80 35000 10.668 218.818 0.80 3.7396E-08 7.9330E-06 4.30 1984 9260 4200.2619