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Turbofan Directory
 

























CFMI
Engine
Configuration
FTO
[kN]
FTO
[lbs]
BPR
[-]
FPR
[-]
OPR
[-]
Tt4
[K]
SFCTO
[g/kNs]
SFCc
[g/kNs]
Fs
[kNs/kg]
mL
[kg/s]
DFan
[mm]
L
[mm]
m
[kg]
EIS
[-]
Applications
CFM56-3C1
1-3-9-A-1-4
105
25000
6.0
1.64
25.7
1535
11.03
18.33
0.2877
297.4
1524
2360
1953
1984
Boeing 737-3/4/5
CFM56-5A1
1-3-9-A-1-4
111.2
3100
6.0
-
31.3
1535
9.33
16.83
0.3229
386.5
1735
2420
2268
1988
Airbus A319/320
CFM56-5B1
1-4-9-DAC-1-4
133
29900
5.5
-
35.5
-
9.9
-
0.3109
427.7
1735
2600
2383
1994
Airbus A321
CFM56-5B2
1-4-9-DAC-1-4
140
23500
5.5
-
35.5
-
10.18
-
0.3531
433.6
1735
2600
2383
1994
Airbus A321-200
CFM56-5C4
1-4-9-A-1-5
151.24
34000
6.4
-
38.2
1635
-
-
0.3131
483
1836
2620
2587
1995
Airbus A340
CFM56-7B18
1-3-9-A-1-4
82
19500
5.6
-
32.3
-
10.18
-
0.2713
302.5
1550
2510
2368
1998
Boeing 737-600
CFM56-7B20
1-3-9-A-1-4
86.6
20600
5.6
-
32.3
-
10.47
-
0.2783
311.2
1550
2510
2368
1998
Boeing 737-600/700
CFM56-7B22
1-3-9-A-1-4
94.3
22700
5.4
-
32.3
-
10.47
-
0.2864
329.3
1550
2510
2368
1998
Boeing 737-600/700
CFM56-7B24
1-3-9-A-1-4
100.6
24200
5.3
-
32.3
-
10.76?
-
0.2941
342
1550
2510
2368
1998
Boeing 737-700/800
CFM56-7B26
1-3-9-A-1-4
116.6
26300
5.1
-
34.3
-
10.74
-
0.3283
355.2
1550
2510
2368
1998
Boeing 737-800

General Electric Aircraft Engines
Engine
Configuration
FTO
[kN]
FTO
[lbs]
BPR
[-]
FPR
[-]
OPR
[-]
Tt4
[K]
SFCTO
[g/kNs]
SFCc
[g/kNs]
Fs
[kNs/kg]
mL
[kg/s]
DFan
[mm]
L
[mm]
m
[kg]
EIS
[-]
Applications
CF34-8C1
1-3-14-A-2-4
61
13790
6.2
-
27
-
11.3
-
-
-
1160
2640
1059
2000
Canadair CRJ Series 700
CF6-80A2
1-3-14-A-2-4
222
50000
4.7
-
28.4
1595
9.33
-
-
-
2190
3990
3857
1981
Boeing 767-200
CF6-80C2A5
1-4-14-A-2-5
267.3
61300
5.05
1.76
30.4
1595
9.62
16.35
0.3333
802.1
2362
4080
4147
1985
Airbus A300-600R
CF6-80E1A2
1-4-14-A-2-5
311
23500
5.3
-
32.6
1595
9.11
15.4
0.3560
873.6
2440
4180
6635
1993
Airbus A330
GE90-90B
1-3-10-A-2-6
400
23500
9.0
-
40.0
-
-
-
0.2903
1377.6
3350
4880
7556
1996
Boeing 777-200/2ER/300
GE90-94B
1-3-10-A-2-6
415.3
23500
9.0
-
40.0
-
-
-
0.3015
1377.6
3350
4880
7556
1996
Boeing 777-2ER/300

GE-P&W Engine Alliance
Engine
Configuration
FTO
[kN]
FTO
[lbs]
BPR
[-]
FPR
[-]
OPR
[-]
Tt4
[K]
SFCTO
[g/kNs]
SFCc
[g/kNs]
Fs
[kNs/kg]
mL
[kg/s]
DFan
[mm]
L
[mm]
m
[kg]
EIS
[-]
Applications
GP7168
1-3-9-A-2-5
302
68000
9.0
-
42.3
-
-
-
-
-
2510
4290
-
2005
Boeing 747X
GP7172
1-3-9-A-2-5
320
72000
9.0
-
42.3
-
-
-
-
-
-
-
-
2003
Boeing 767-400ERX
GP7270
1-3-9-A-2-5
311
70000
9.0
-
45.7
-
-
-
-
-
2790
4490
-
2006
Airbus A380-800

International Aero Engines (IAE)
Engine
Configuration
FTO
[kN]
FTO
[lbs]
BPR
[-]
FPR
[-]
OPR
[-]
Tt4
[K]
SFCTO
[g/kNs]
SFCc
[g/kNs]
Fs
[kNs/kg]
mL
[kg/s]
DFan
[mm]
L
[mm]
m
[kg]
EIS
[-]
Applications
V2500-A1
1-3-10-A-2-5
112.2
25000
5.4
-
29.8 (35.8)
1698
-
15.02
0.3134
358
1600
3200
2365 (3356.6)
1989
Airbus A320-100
V2524-A5
1-4-10-A-2-5
106.8
24000
4.9
-
32.8
-
-
15.38
0.3015
364.3
1600
3200
2374 (3402)
1997
Airbus A319-100
V2527-A5
1-4-10-A-2-5
117.9
26500
4.8
-
32.8
-
-
15.38
0.2903
367.9
1600
3200
2374 (3402)
1993
Airbus A320
V2530-A5
1-4-10-A-2-5
140
31400
4.6
-
31.4 (35.2)
1698
10.18
15.38
0.3646
384
1600
3200
2374 (3402)
1994
Airbus A321-100
V2533-A5
1-4-10-A-2-5
146.85
33000
4.5
-
35.2
-
-
15.38
0.3713
395.5
1600
3200
2374 (3402)
1997
Airbus A321-200
V2525-D5
1-4-10-A-2-5
111.25
25000
4.8
-
34.5
-
-
15.38
0.3085
360.6
1600
3200
3583
1995
McDonnell Douglas MD90-30
V2528-D5
1-4-10-A-2-5
124.6
28000
4.7
-
35.2
-
-
15.38
0.3298
377.8
1600
3200
3583
1995
McDonnell Douglas MD90-30/50

Pratt&Whitney
Engine
Configuration
FTO
[kN]
FTO
[lbs]
BPR
[-]
FPR
[-]
OPR
[-]
Tt4
[K]
SFCTO
[g/kNs]
SFCc
[g/kNs]
Fs
[kNs/kg]
mL
[kg/s]
DFan
[mm]
L
[mm]
m
[kg]
EIS
[-]
Applications
JT8D-15A
1-6-7-Cn-1-3
69
15500
1.0
-
16.5
-
16.95
-
-
-
1250
3920
1577
1964
Boeing 737, 727, McDonnell Douglas DC-9
JT8D-219
1-6-7-Cn-1-3
97
21700
1.8
-
19.2
1397
14.15
-
0.4389
221
1250
3911
2049
1980
McDonnell Douglas MD-80
JT9D-7
1-3-11-A-2-4
203
45600
5.1
-
22.3
-
10.24
17.55
-
-
2470
3220
4014
1970
Boeing 747-100, 767, A300-600
PW2037
1-4-12-A-2-5
170
38200
6.0
1.65
27.6
1678
9.48
16.47
0.2988
569
1994
3600
3311
1984
Boeing 757-200
PW2040
1-4-12-A-2-5
185.5
41700
5.9
1.71
29.1
1698
9.76
16.47
0.3260
569
1994
3600
3025
1990
Boeing 757-200, Boeing C-17
PW2043
1-4-12-A-2-5
191.4
43000
5.3
1.74
31.9
-
-
-
-
-
1994
3600
-
1995
Boeing 757-200/300
PW4060
1-4-11-A-2-4
268
60200
4.8
1.8
31.2
-
10.32
-
-
-
2460
3370
4128
1989
Boeing 747-400, 767-3ER/400
PW4158
1-4-11-A-2-4
258
58000
4.75
1.8
30.6
1538
9.14
-
0.3336
773.4
2387
3370
4128
1989
Airbus A300-600R
PW4098
1-6-11-A-2-7
435.9
98000
6.4
1.7
42.8
1930
9.31
-
0.3336
1295
2844
4869
7303
1998
Boeing 777-300

Rolls-Royce
Engine
Configuration
FTO
[kN]
FTO
[lbs]
BPR
[-]
FPR
[-]
OPR
[-]
Tt4
[K]
SFCTO
[g/kNs]
SFCc
[g/kNs]
Fs
[kNs/kg]
mL
[kg/s]
DFan
[mm]
L
[mm]
m
[kg]
EIS
[-]
Applications
Tay 650
1-3-12-A-2-3
67.15
15100
3.06
-
16.2
1370
-
19.52
0.3483
192.8
1138
2410
1515
1987
Fokker 100
BR715-58
1-2-10-A-2-3
93
21000
4.7
-
32.6
-
10.47
17.26
-
-
1473
3730
2085
1999
Boeing 717-200
RB211-535-E4/F4
1-0-6-6-A-1-1-3
192
43100
4.1
-
33.0
1500
-
16.92
-
-
1892
2990
3296
1985
Boeing 757-200/-300, Tuploev Tu204
RB211-524-G/H
1-0-7-6-A-1-1-3
270
60700
4.1
-
33.0
1520
-
15.84
-
-
2190
3180
4277
2000?
Boeing 747-400, Boeing 767-300
Trent 553
1-0-8-6-A-1-1-5
240.4
53000
8.5
-
36.7?
-
-
16.07?
-
-
2476
3910
4717
2002
Airbus A340-500
Trent 556
1-0-8-6-A-1-1-5
254
56000
8.5
-
36.7
-
-
16.07
-
-
2476
3910
4717
2001
Airbus A340-600
Trent 772
1-0-8-6-A-1-1-4
316
71000
5.0
-
35.5
-
-
16.4
0.3606
876.4
2474
3910
4785
1995
Airbus A340-200/-300
Trent 895
1-0-8-6-A-1-1-5
423
95000
5.8
-
40.7
-
-
16.27
-
-
2790
4370
5942
1996
Boeing 777-300
Trent 900
1-0-8-6-A-1-1-5
334
75000
7.1
-
38.0
-
-
-
-
-
2790
4250
5800
2006
Airbus A380-800

Sources: Aviation Week & Space Technolgy, Flight International, Lecture Notes from the RWTH Aachen, Manufacturer Websites, ...
Comments, suggestions, additions and corrections are appreciated!
© 2001-2005
A. Stuermer
Update: 10/21/05


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