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