The TBM achieves the cruising speed of a light jet while maintaining the fuel efficiency of a single-engine turboprop. The TBM's outstanding performance at its service ceiling and "mid-teen" altitudes is a distinguishing characteristic. This versatility enables flexibility among a multitude of missions. Manufactured by an aerostructures company, the build and reliability of the TBM is unmatched. The TBM's short-field performance and load-carrying capacity are exceptional.
Compare performance statistics between models using the chart below by clicking on weight, climb to and model number tabs.

- Take Off 1 Distance - 2,133
- Landing 2 Distance - 2,135
- Max Cruise 3 Speed - 300
- Maximun Attitude - 31,000
- SL Cabin Attitude - 14,000ft

- Take Off 1 Distance - 2,840
- Landing 2 Distance - 2,430
- Max Cruise 3 Speed - 294
- Maximun Attitude - 31,000
- SL Cabin Attitude - 14,000ft

- Take Off 1 Distance - 2,840
- Landing 2 Distance - 2,430
- Max Cruise 3 Speed - 320
- Maximun Attitude - 31,000
- SL Cabin Attitude - 14,000ft

- Take Off 1 Distance - 2,380
- Landing 2 Distance - 2,430
- Max Cruise 3 Speed - 320
- Maximun Attitude - 31,000
- SL Cabin Attitude - 14,000ft

- Take Off 1 Distance - 2,380
- Landing 2 Distance - 2,430
- Max Cruise 3 Speed - 328
- Maximun Attitude - 31,000
- SL Cabin Attitude - 14,000ft





The TBM 700A Performance Data is derived directly from the Daher-Socata Pilot Information Manual. Select between aircraft operating weights and cruise altitudes for climb, cruise and descent performance.
Start by selecting between TBM 700’s, TBM 850’s, TBM 900’s, TBM 930’s listed to your right! Select between max, mid and light take off weights for landing takeoff distances. Also, select between max efficiency and max speed cruise altitudes for time to climb and descend data as well as cruise fuel burn rate and true airspeed.
Below are the conditions the performance data is predicated on:
TBM 700A
1) MTOW 6579 LBS distance to clear 50ft obs. ISA
2) MLW 6250 LBS distance to clear 50ft obs. ISA
3) Max Cruise @ ISA conditions @ mid weight 5512lbs FL 260
The TBM 700B Performance Data is derived directly from the Daher-Socata Pilot Information Manual. Select between aircraft operating weights and cruise altitudes for climb, cruise and descent performance.
Start by selecting between TBM 700’s, TBM 850’s, TBM 900’s, TBM 930’s listed to your right! Select between max, mid and light take off weights for landing takeoff distances. Also, select between max efficiency and max speed cruise altitudes for time to climb and descend data as well as cruise fuel burn rate and true airspeed.
Below are the conditions the performance data is predicated on:
TBM 700B
1)MTOW 6579 LBS distance to clear 50ft obs. ISA
2) MLW 6250 LBS distance to clear 50ft obs. ISA
3) Max Cruise @ ISA conditions @ mid weight 5512lbs FL 260
The TBM 700C2 Performance Data is derived directly from the Daher-Socata Pilot Information Manual. Select between aircraft operating weights and cruise altitudes for climb, cruise and descent performance.
Start by selecting between TBM 700’s, TBM 850’s, TBM 900’s, TBM 930’s listed to your right! Select between max, mid and light take off weights for landing takeoff distances. Also, select between max efficiency and max speed cruise altitudes for time to climb and descend data as well as cruise fuel burn rate and true airspeed.
Below are the conditions the performance data is predicated on:
TBM 700C2
1)MTOW 7394 LBS distance to clear 50ft obs. ISA
2) MLW 7024 LBS distance to clear 50ft obs. ISA
3) Max Cruise @ ISA conditions @ mid weight 6614lbs FL 260
The TBM 850L Performance Data is derived directly from the Daher-Socata Pilot Information Manual. Select between aircraft operating weights and cruise altitudes for climb, cruise and descent performance.
Start by selecting between TBM 700’s, TBM 850’s, TBM 900’s, TBM 930’s listed to your right! Select between max, mid and light take off weights for landing takeoff distances. Also, select between max efficiency and max speed cruise altitudes for time to climb and descend data as well as cruise fuel burn rate and true airspeed.
Below are the conditions the performance data is predicated on:
TBM 850L
1) MTOW 7394 LBS distance to clear 50ft obs. ISA
2) MLW 7024 LBS distance to clear 50ft obs. ISA
3) Max Cruise @ ISA conditions @ mid weight 6300lbs FL 260
The TBM 850G Performance Data is derived directly from the Daher-Socata Pilot Information Manual. Select between aircraft operating weights and cruise altitudes for climb, cruise and descent performance..
Start by selecting between TBM 700’s, TBM 850’s, TBM 900’s, TBM 930’s listed to your right! Select between max, mid and light take off weights for landing takeoff distances. Also, select between max efficiency and max speed cruise altitudes for time to climb and descend data as well as cruise fuel burn rate and true airspeed.
Below are the conditions the performance data is predicated on:
TBM 850G
1) MTOW 7394 LBS distance to clear 50ft obs. ISA
2) MLW 7024 LBS distance to clear 50ft obs. ISA
3) Max Cruise @ ISA conditions @ mid weight 6300lbs FL 260
The TBM 900 Performance Data is derived directly from the Daher-Socata Pilot Information Manual. Select between aircraft operating weights and cruise altitudes for climb, cruise and descent performance.
Start by selecting between TBM 700’s, TBM 850’s, TBM 900’s, TBM 930’s listed to your right! Select between max, mid and light take off weights for landing takeoff distances. Also, select between max efficiency and max speed cruise altitudes for time to climb and descend data as well as cruise fuel burn rate and true airspeed.
Below are the conditions the performance data is predicated on:
TBM 900
1)MTOW 7394 LBS distance to clear 50ft obs. ISA
2) MLW 7024 LBS distance to clear 50ft obs. ISA
3)Max Cruise @ ISA conditions @ mid weight 6300lbs FL 280
The TBM 910 Performance Data is derived directly from the Daher-Socata Pilot Information Manual. Select between aircraft operating weights and cruise altitudes for climb, cruise and descent performance.
Start by selecting between TBM 700’s, TBM 850’s, TBM 900’s, TBM 910/930’s listed to your right! Select between max, mid and light take off weights for landing takeoff distances. Also, select between max efficiency and max speed cruise altitudes for time to climb and descend data as well as cruise fuel burn rate and true airspeed.
Below are the conditions the performance data is predicated on:
TBM 910
1)MTOW 7394 LBS distance to clear 50ft obs. ISA
2)MLW 7024 LBS distance to clear 50ft obs. ISA
3)Max Cruise @ ISA conditions @ mid weight 6300lbs FL 280
The TBM 930 Performance Data is derived directly from the Daher-Socata Pilot Information Manual. Select between aircraft operating weights and cruise altitudes for climb, cruise and descent performance.
Start by selecting between TBM 700’s, TBM 850’s, TBM 900’s, TBM 910/930’s listed to your right! Select between max, mid and light take off weights for landing takeoff distances. Also, select between max efficiency and max speed cruise altitudes for time to climb and descend data as well as cruise fuel burn rate and true airspeed.
Below are the conditions the performance data is predicated on:
TBM 930
1)MTOW 7394 LBS distance to clear 50ft obs. ISA
2)MLW 7024 LBS distance to clear 50ft obs. ISA
3)Max Cruise @ ISA conditions @ mid weight 6300lbs FL 280
TBM 700A Performance Data
Select Weight
ISA @ 0Ft.
- Take-off Distance GR/D50- 1,017 ft / 1,591 ft
- Landing Distance GR/D50- 1,030 ft / 2,135 ft
ISA + 10C @ 0Ft.
- Take-off Distance GR/D50 - 1,083 ft / 1,690 ft
- Landing Distance GR/D50 - 1,080 ft / 2,200 ft
ISA @ 0Ft.
- Take-off Distance GR/D50- 1,378 ft / 2,133 ft
- Landing Distance GR/D50- 1,215 ft / 2,135 ft
ISA + 10C @ 0Ft.
- Take-off Distance GR/D50 - 1,476 ft / 2,264 ft
- Landing Distance GR/D50 - 1,280 ft / 2,200 ft
Climb To
- Time - 12:15 min
- Fuel - 13.5 gal
- Distance - 33 nm
- Time - 15:30 min
- Fuel - 15.9 gal
- Distance - 43 nm
Cruise Performance
- Fuel Burn - 55.2 gal/hr
- Tas - 300 kts
- Fuel Burn - 47.9 gal/hr
- Tas - 294 kts
Descent
- Time - 17:20 min
- Fuel - 16.6 gal
- Distance - 80 nm
- Time - 20:00 min
- Fuel - 18.5 gal
- Distance - 93 nm
-
RANGE
1500 nm -
SPEED
285 Ktas -
PAYLOAD
1673 lbs -
AVIONICS
GNS 530
-
TAKE OFF
DISTANCE2133
sl, isa, mtow -
YEARS
1991 to 1999
MANUFACTURED -
TBM 700A
139
QUANTITY -
ENGINE
PT6A-64
TBM 700B Performance Data
Select Weight
ISA @ 0Ft.
- Take-off Distance GR/D50- 1,017 ft / 1,591 ft
- Landing Distance GR/D50- 1,030 ft / 2,135 ft
ISA + 10C @ 0Ft.
- Take-off Distance GR/D50 - 1,083 ft / 1,690 ft
- Landing Distance GR/D50 - 1,080 ft / 2,200 ft
ISA @ 0Ft.
- Take-off Distance GR/D50- 1,378 ft / 2,133 ft
- Landing Distance GR/D50- 1,215 ft / 2,135 ft
ISA + 10C @ 0Ft.
- Take-off Distance GR/D50 - 1,476 ft / 2,264 ft
- Landing Distance GR/D50 - 1,280 ft / 2,200 ft
Climb To
- Time - 12:15 min
- Fuel - 13.5 gal
- Distance - 33 nm
- Time - 15:30 min
- Fuel - 15.9 gal
- Distance - 43 nm
Cruise Performance
- Fuel Burn - 55.2 gal/hr
- Tas - 300 kts
- Fuel Burn - 47.9 gal/hr
- Tas - 294 kts
Descent
- Time - 17:20 min
- Fuel - 16.6 gal
- Distance - 80 nm
- Time - 20:00 min
- Fuel - 18.5 gal
- Distance - 93 nm
-
RANGE
1500 nm -
SPEED
285 Ktas -
PAYLOAD
1574 lbs -
AVIONICS
GNS 530
-
TAKE OFF
DISTANCE2133
sl, isa, mtow -
YEARS
2000 to 2004
MANUFACTURED -
TBM 700B
102
QUANTITY -
ENGINE
PT6A-64
TBM 700C2 Performance Data
Select Weight
ISA @ 0Ft.
- Take-off Distance GR/D50- 1,017 ft / 1,591 ft
- Landing Distance GR/D50- 1,030 ft / 2,135 ft
ISA + 10C @ 0Ft.
- Take-off Distance GR/D50 - 1,083 ft / 1,690 ft
- Landing Distance GR/D50 - 1,080 ft / 2,200 ft
ISA @ 0Ft.
- Take-off Distance GR/D50- 1,378 ft / 2,133 ft
- Landing Distance GR/D50- 1,215 ft / 2,135 ft
ISA + 10C @ 0Ft.
- Take-off Distance GR/D50 - 1,476 ft / 2,264 ft
- Landing Distance GR/D50 - 1,280 ft / 2,200 ft
ISA @ 0Ft.
- Take-off Distance GR/D50- 2,035 ft / 2,840 ft
- Landing Distance GR/D50- 1,840 ft / 2,430 ft
ISA + 10C @ 0Ft.
- Take-off Distance GR/D50 - 2,165 ft / 3,020 ft
- Landing Distance GR/D50 - 1,905 ft / 2,530 ftt
Climb To
- Time - 16:00 min
- Fuel - 17.4 gal
- Distance - 43 nm
- Time - 22:33 min
- Fuel - 23.0 gal
- Distance - 65 nm
Cruise Performance
- Fuel Burn - 55.2 gal/hr
- Tas - 298 kts
- Fuel Burn - 45.9 gal/hr
- Tas - 287 kts
Descent
- Time - 17:20 min
- Fuel - 16.6 gal
- Distance - 80 nm
- Time - 20:40 min
- Fuel - 18.5 gal
- Distance - 95 nm
-
RANGE
1500 nm -
SPEED
285 Ktas -
PAYLOAD
1343 lbs -
AVIONICS
GNS 530
-
TAKE OFF
DISTANCE2840
sl, isa, mtow -
YEARS
2003 to 2005
MANUFACTURED -
TBM 700C2
100
QUANTITY -
ENGINE
PT6A-64
TBM 850L Performance Data
Select Weight
ISA @ 0Ft.
- Take-off Distance GR/D50- 1,017 ft / 1,591 ft
- Landing Distance GR/D50- 1,030 ft / 2,135 ft
ISA + 10C @ 0Ft.
- Take-off Distance GR/D50 - 1,083 ft / 1,690 ft
- Landing Distance GR/D50 - 1,080 ft / 2,200 ft
ISA @ 0Ft.
- Take-off Distance GR/D50- 1,378 ft / 2,133 ft
- Landing Distance GR/D50- 1,215 ft / 2,135 ft
ISA + 10C @ 0Ft.
- Take-off Distance GR/D50 - 1,476 ft / 2,264 ft
- Landing Distance GR/D50 - 1,280 ft / 2,200 ft
ISA @ 0Ft.
- Take-off Distance GR/D50- 2,035 ft / 2,840 ft
- Landing Distance GR/D50- 1,840 ft / 2,430 ft
ISA + 10C @ 0Ft.
- Take-off Distance GR/D50 - 2,165 ft / 3,020 ft
- Landing Distance GR/D50 - 1,905 ft / 2,530 ftt
Climb To
- Time- 12:30 min
- Fuel - 15.5 gal
- Distance - 33 nm
- Time - 16:15 min
- Fuel - 19.1 gal
- Distance - 46 nm
Cruise Performance
- Fuel Burn - 66.6 gal/hr
- Tas- 320 kts
- Fuel Burn - 55.8 gal/hr
- Tas - 315 kts
Descent
- Time - 17:20 min
- Fuel - 16.3 gal
- Distance - 81 nm
- Time - 20:40 min
- Fuel - 19.4 gal
- Distance - 101 nm
-
RANGE
1500 nm -
SPEED
305 Ktas -
PAYLOAD
1379 lbs -
AVIONICS
GNS 530
-
TAKE OFF
DISTANCE2840
sl, isa, mtow -
YEARS
2006 to 2007
MANUFACTURED -
TBM 850L
87
QUANTITY -
ENGINE
PT6A-66D
TBM 850G Performance Data
Select Weight
ISA @ 0Ft.
- Take-off Distance GR/D50- 1,017 ft / 1,591 ft
- Landing Distance GR/D50- 1,030 ft / 2,135 ft
ISA + 10C @ 0Ft.
- Take-off Distance GR/D50 - 1,083 ft / 1,690 ft
- Landing Distance GR/D50 - 1,080 ft / 2,200 ft
ISA @ 0Ft.
- Take-off Distance GR/D50- 1,378 ft / 2,133 ft
- Landing Distance GR/D50- 1,215 ft / 2,135 ft
ISA + 10C @ 0Ft.
- Take-off Distance GR/D50 - 1,476 ft / 2,264 ft
- Landing Distance GR/D50 - 1,280 ft / 2,200 ft
ISA @ 0Ft.
- Take-off Distance GR/D50- 2,035 ft / 2,840 ft
- Landing Distance GR/D50- 1,840 ft / 2,430 ft
ISA + 10C @ 0Ft.
- Take-off Distance GR/D50 - 2,165 ft / 3,020 ft
- Landing Distance GR/D50 - 1,905 ft / 2,530 ft
Climb To
- Time - 12:30 min
- Fuel - 15.5 gal
- Distance - 33 nm
- Time - 16:15 min
- Fuel - 19.1 gal
- Distance - 46 nm
Cruise Performance
- Fuel Burn - 66.6 gal/hr
- Tas - 320 kts
- Fuel Burn - 55.8 gal/hr
- Tas - 315 kts
Descent
- Time - 17:20 min
- Fuel - 16.3 gal
- Distance - 81 nm
- Time - 20:40 min
- Fuel - 19.4 gal
- Distance - 101 nm
-
RANGE
1500 nm -
SPEED
305 Ktas -
PAYLOAD
1449 lbs -
AVIONICS
G1000
-
TAKE OFF
DISTANCE2840
sl, isa, mtow -
YEARS
2008 to 2012
MANUFACTURED -
TBM 850G
176
QUANTITY -
ENGINE
PT6A-66D
TBM 900 Performance Data
Select Weight
ISA @ 0Ft.
- Take-off Distance GR/D50- 875 ft / 1,385 ft
- Landing Distance GR/D50- 1,030 ft / 2,135 ft
ISA + 10C @ 0Ft.
- Take-off Distance GR/D50 - 935 ft / 1,475 ft
- Landing Distance GR/D50 - 1,080 ft / 2,200 ft
ISA @ 0Ft.
- Take-off Distance GR/D50- 1,320 ft / 1,885 ft
- Landing Distance GR/D50- 1,215 ft / 2,135 ft
ISA + 10C @ 0Ft.
- Take-off Distance GR/D50 - 1,420 ft / 2,015 ft
- Landing Distance GR/D50 - 1,280 ft / 2,200 ft
ISA @ 0Ft.
- Take-off Distance GR/D50- 1,845 ft / 2,555 ft
- Landing Distance GR/D50- 1,840 ft / 2,430 ft
ISA + 10C @ 0Ft.
- Take-off Distance GR/D50 - 1,985 ft / 2,730 ft
- Landing Distance GR/D50 - 1,905 ft / 2,530 ft
Climb To
- Time - 12:30 min
- Fuel - 15.7 gal
- Distance - 32 nm
- Time - 16:15 min
- Fuel - 19.1 gal
- Distance - 44 nm
Cruise Performance
- Fuel Burn- 64.5 gal/hr
- Tas - 318 kts
- Fuel Burn- 57.4 gal/hr
- Tas - 322 kts
Descent
- Time - 17:20 min
- Fuel - 15.7 gal
- Distance - 81 nm
- Time - 20:40 min
- Fuel - 18.6 gal
- Distance - 101 nm
-
RANGE
1730 nm -
SPEED
325 Ktas -
PAYLOAD
1403 lbs -
AVIONICS
G1000
-
TAKE OFF
DISTANCE2380
sl, isa, mtow -
YEARS
2014 to 2016
MANUFACTURED -
TBM 900
113
QUANTITY -
ENGINE
PT6A-66D
TBM 910 Performance Data
Select Weight
ISA @ 0Ft.
- Take-off Distance GR/D50- 820 ft / 1,295 ft
- Landing Distance GR/D50- 1,030 ft / 2,135 ft
ISA + 10C @ 0Ft.
- Take-off Distance GR/D50 - 865 ft / 1,365 ft
- Landing Distance GR/D50 - 1,080 ft / 2,200 ft
ISA @ 0Ft.
- Take-off Distance GR/D50- 1,245 ft / 1,765 ft
- Landing Distance GR/D50- 1,215 ft / 2,135 ft
ISA + 10C @ 0Ft.
- Take-off Distance GR/D50 - 1,310 ft / 1,855 ft
- Landing Distance GR/D50 - 1,280 ft / 2,200 ft
ISA @ 0Ft.
- Take-off Distance GR/D50- 1,725 ft / 2,380 ft
- Landing Distance GR/D50- 1,840 ft / 2,430 ft
ISA + 10C @ 0Ft.
- Take-off Distance GR/D50 - 1,800 ft / 2,485 ft
- Landing Distance GR/D50 - 1,905 ft / 2,530 ft
Climb To
- Time - 12:00 min
- Fuel - 14.9 gal
- Distance - 30 nm
- Time - 15:30 min
- Fuel - 18.2 gal
- Distance - 41 nm
Cruise Performance
- Fuel Burn - 64.5 gal/hr
- Tas - 320 kts
- Fuel Burn - 57.5 gal/hr
- Tas - 326 kts
Descent
- Time - 17:20 min
- Fuel - 15.7 gal
- Distance - 81 nm
- Time - 20:40 min
- Fuel - 18.5 gal
- Distance - 101 nm
-
RANGE
1730 nm -
SPEED
328 Ktas -
PAYLOAD
1403 lbs -
AVIONICS
G1000 NXi
-
TAKE OFF
DISTANCE2380
sl, isa, mtow -
YEARS
2017 to 2021
MANUFACTURED -
TBM 910
512
QUANTITY -
ENGINE
PT6A-66D
TBM 930 Performance Data
Select Weight
ISA @ 0Ft.
- Take-off Distance GR/D50- 820 ft / 1,295 ft
- Landing Distance GR/D50- 1,030 ft / 2,135 ft
ISA + 10C @ 0Ft.
- Take-off Distance GR/D50 - 865 ft / 1,365 ft
- Landing Distance GR/D50 - 1,080 ft / 2,200 ft
ISA @ 0Ft.
- Take-off Distance GR/D50- 1,245 ft / 1,765 ft
- Landing Distance GR/D50- 1,215 ft / 2,135 ft
ISA + 10C @ 0Ft.
- Take-off Distance GR/D50 - 1,310 ft / 1,855 ft
- Landing Distance GR/D50 - 1,280 ft / 2,200 ft
ISA @ 0Ft.
- Take-off Distance GR/D50- 1,725 ft / 2,380 ft
- Landing Distance GR/D50- 1,840 ft / 2,430 ft
ISA + 10C @ 0Ft.
- Take-off Distance GR/D50 - 1,800 ft / 2,485 ft
- Landing Distance GR/D50 - 1,905 ft / 2,530 ft
Climb To
- Time - 12:00 min
- Fuel - 14.9 gal
- Distance - 30 nm
- Time - 15:30 min
- Fuel - 18.2 gal
- Distance - 41 nm
Cruise Performance
- Fuel Burn - 64.5 gal/hr
- Tas - 320 kts
- Fuel Burn - 57.5 gal/hr
- Tas - 326 kts
Descent
- Time - 17:20 min
- Fuel - 15.7 gal
- Distance - 81 nm
- Time - 20:40 min
- Fuel - 18.5 gal
- Distance - 101 nm
-
RANGE
1730 nm -
SPEED
325 Ktas -
PAYLOAD
1403 lbs -
AVIONICS
G3000
-
TAKE OFF
DISTANCE2380
sl, isa, mtow -
YEARS
2016 to 2019
MANUFACTURED -
TBM 930
115
QUANTITY -
ENGINE
PT6A-66D
TBM 940 Performance Data
TBM 960 Performance Data
While FAR Part 23 only requires Ground Roll to be used to determine runway length, the above charts identify runway lengths based on the distance required to clear a 50 ft obstacle and provide an enhanced safety margin. The TBM's range and short-field capability allow the aircraft to be utilized on the vast majority of general aviation runways, enabling the owner to fly closer to his planned destination without compromising runway safety margins while carrying a significant cabin load. This must be contrasted with the majority of light jets, for which operating from short fields (if at all possible) has a significant negative effect on aircraft payload.