Daher TBM Resources

TBM Sales Inventory

Model Comparison Chart

Click on models to have a side-by-side comparison.

Piper M600
Characteristics
Seating 1+4/5
Wing Loading (lbs) 28.7
Power Loading (lbs) 10
Noise 76.8
External Dimensions (ft.)
Length 29.6
Height 11.3
Span 43.2
Internal Dimensions (ft)
Length 12.3
Height 3.9
Width 4.1
Power
Engine P&W PT6A-42A
Output (shp) 600/ISA+55C
Inspection Interval 3,600t
Weights (lb)
Max Ramp 6,050
Max Takeoff 6,000
Max Landing 5,800
Zero Fuel 4,850c
BOW 3,850
Max Payload 1,000
Useful Load 2,200
Max Fuel 1,742
Available Payload w/Max Fuel 458
Available Fuel w/Max Payload 1,200
Limits
Vmo 250 kt
Va 151 kt
PSI 5.6
Airport Performance
TO (SL elev./ISA temp) 2,635
TO (5,000-ft. [email protected]) 3,998
Vso 62
Vx 95
Vy 122
Climb
Time to Climb (min.)/Attitude 21/FL 250
Initial Gradient (ft/min) 785
Ceilings (ft)
Certified 30,000
Service 30,000
Sea-Level Cabin 12,600 ft
Cruise
Long Range
TAS 184 kt
Fuel Flow 155 lbs/hr
Altitude FL 280
Specific Range (nm/lb) 1.187
High Speed
TAS 274 kt
Fuel Flow 324 lbs/hr
Altitude FL 280
Specific Range (nm/lb) 0.846
NBAA IFR Ranges
Full Fuel (with available payload)
Nautical Miles 1,406
Average Speed 179
Trip Fuel 1,324
Specific Range/Altitude 1.062/FL 280
Ferry
Nautical Miles 1,406
Average Speed 179
Trip Fuel 1,324
Specific Range/Altitude 1.062/FL 280
Missions
300nm
Runway 1,593
Flight Time 1+21
Fuel Used 429
Specific Range/Altitude 0.699/FL 280
600nm
Runway 1,687
Flight Time 2+31
Fuel Used 735
Specific Range/Altitude 0.816/FL 280
1,000nm
Runway 1,812
Flight Time 4+06
Fuel Used 1,142
Specific Range/Altitude 0.876/FL 280
Epic E1000
Characteristics
Seating 1+5/6
Wing Loading (lbs) 36.9
Power Loading (lbs) 6.25
Noise 76.0
External Dimensions (ft.)
Length 35.8
Height 12.5
Span 43.0
Internal Dimensions (ft)
Length 10.5
Height 4.9
Width 4.6
Power
Engine P&W PT6A-67A
Output (shp) 1,200/ISA+35C
Inspection Interval 3,500t
Weights (lb)
Max Ramp 7,500
Max Takeoff 7,500
Max Landing 7,500
Zero Fuel 5,400c
BOW 4,600
Max Payload 800
Useful Load 2,900
Max Fuel 1,876
Available Payload w/Max Fuel 1,024
Available Fuel w/Max Payload 2,100
Limits
Vmo 280 kt
Va 170 kt
PSI 6.7
Airport Performance
TO (SL elev./ISA temp) 1,600
TO (5,000-ft. [email protected]) N/A
Vso 65
Vx 124
Vy 144
Climb
Time to Climb (min.)/Attitude 10/FL 250
Initial Gradient (ft/min) 1,500
Ceilings (ft)
Certified 34,000
Service 34,000
Sea-Level Cabin 18,000 ft
Cruise
Long Range
TAS 265 kt
Fuel Flow 268 lbs/hr
Altitude FL 280
Specific Range (nm/lb) 0.989
High Speed
TAS 330 kt
Fuel Flow 402 lbs/hr
Altitude FL 280
Specific Range (nm/lb) 0.821
NBAA IFR Ranges
Full Fuel (with available payload)
Nautical Miles 1,650
Average Speed 265
Trip Fuel 1,599
Specific Range/Altitude 1.032/FL 310
Ferry
Nautical Miles 1,594
Average Speed 252
Trip Fuel 1,598
Specific Range/Altitude 0.997/FL 310
Missions
300nm
Runway 1,765
Flight Time 1+00
Fuel Used 440
Specific Range/Altitude 0.682/FL 280
600nm
Runway 2,005
Flight Time 1+55
Fuel Used 830
Specific Range/Altitude 0.723/FL 280
1,000nm
Runway 2,380
Flight Time 3+10
Fuel Used 1,320
Specific Range/Altitude 0.758/FL 290
Daher TBM 910
Characteristics
Seating 1+5/6
Wing Loading (lbs) 38.2
Power Loading (lbs) 8.70
Noise 76.2
External Dimensions (ft.)
Length 35.2
Height 14.3
Span 42.1
Internal Dimensions (ft)
Length 15.0
Height 4.1
Width 4.0
Power
Engine P&W PT6A-66D
Output (shp) 850/ISA+49C
Inspection Interval 3,500t
Weights (lb)
Max Ramp 7,430
Max Takeoff 7,394
Max Landing 7,024
Zero Fuel 6,032c
BOW 4,829
Max Payload 1,203
Useful Load 2,601
Max Fuel 2,017
Available Payload w/Max Fuel 584
Available Fuel w/Max Payload 1,398
Limits
Vmo 266 kt
Va 160 kt
PSI 6.2
Airport Performance
TO (SL elev./ISA temp) 2,380
TO (5,000-ft. [email protected]) 3,475
Vso 65
Vx 100
Vy 124
Climb
Time to Climb (min.)/Attitude 13/FL 250
Initial Gradient (ft/min) 1,000
Ceilings (ft)
Certified 31,000
Service 31,000
Sea-Level Cabin 14,390 ft
Cruise
Long Range
TAS 252 kt
Fuel Flow 241 lbs/hr
Altitude FL 310
Specific Range (nm/lb) 1.046
High Speed
TAS 330 kt
Fuel Flow 412 lbs/hr
Altitude FL 260
Specific Range (nm/lb) 0.801
NBAA IFR Ranges
Full Fuel (with available payload)
Nautical Miles 1,514
Average Speed 252
Trip Fuel 1,599
Specific Range/Altitude 0.947/FL 310
Ferry
Nautical Miles 1,594
Average Speed 252
Trip Fuel 1,598
Specific Range/Altitude 0.997/FL 310
Missions
300nm
Runway 1,765
Flight Time 1+00
Fuel Used 440
Specific Range/Altitude 0.682/FL 280
600nm
Runway 2,005
Flight Time 1+55
Fuel Used 830
Specific Range/Altitude 0.723/FL 280
1,000nm
Runway 2,380
Flight Time 3+10
Fuel Used 1,320
Specific Range/Altitude 0.758/FL 290
Daher TBM 930
Characteristics
Seating 1+5/6
Wing Loading (lbs) 38.2
Power Loading (lbs) 8.70
Noise 76.2
External Dimensions (ft.)
Length 35.2
Height 14.3
Span 42.1
Internal Dimensions (ft)
Length 15.0
Height 4.1
Width 4.0
Power
Engine P&W PT6A-66D
Output (shp) 850/ISA+49C
Inspection Interval 3,500t
Weights (lb)
Max Ramp 7,430
Max Takeoff 7,394
Max Landing 7,024
Zero Fuel 6,032c
BOW 4,829
Max Payload 1,203
Useful Load 2,601
Max Fuel 2,017
Available Payload w/Max Fuel 584
Available Fuel w/Max Payload 1,398
Limits
Vmo 266 kt
Va 160 kt
PSI 6.2
Airport Performance
TO (SL elev./ISA temp) 2,380
TO (5,000-ft. [email protected]) 3,475
Vso 65
Vx 100
Vy 124
Climb
Time to Climb (min.)/Attitude 13/FL 250
Initial Gradient (ft/min) 1,000
Ceilings (ft)
Certified 31,000
Service 31,000
Sea-Level Cabin 14,390 ft
Cruise
Long Range
TAS 252 kt
Fuel Flow 241 lbs/hr
Altitude FL 310
Specific Range (nm/lb) 1.046
High Speed
TAS 330 kt
Fuel Flow 412 lbs/hr
Altitude FL 260
Specific Range (nm/lb) 0.801
NBAA IFR Ranges
Full Fuel (with available payload)
Nautical Miles 1,514
Average Speed 252
Trip Fuel 1,599
Specific Range/Altitude 0.947/FL 310
Ferry
Nautical Miles 1,594
Average Speed 252
Trip Fuel 1,598
Specific Range/Altitude 0.997/FL 310
Missions
300nm
Runway 1,765
Flight Time 1+00
Fuel Used 440
Specific Range/Altitude 0.682/FL 280
600nm
Runway 2,005
Flight Time 1+55
Fuel Used 830
Specific Range/Altitude 0.723/FL 280
1,000nm
Runway 2,380
Flight Time 3+10
Fuel Used 1,320
Specific Range/Altitude 0.758/FL 290
Pilatus PC-12
Characteristics
Seating 1+7/10
Wing Loading (lbs) 37.6
Power Loading (lbs) 8.71
Noise 77.0
External Dimensions (ft.)
Length 47.3
Height 14.0
Span 53.3
Internal Dimensions (ft)
Length 16.9
Height 4.8
Width 5.0
Power
Engine P&W PT6A-67P
Output (shp) 1,200/ISA+35C
Inspection Interval 3,500t
Weights (lb)
Max Ramp 10,495
Max Takeoff 10,450
Max Landing 9,921
Zero Fuel 9,039c
BOW 6,782
Max Payload 2,257
Useful Load 3,713
Max Fuel 2,704
Available Payload w/Max Fuel 1,009
Available Fuel w/Max Payload 1,456
Limits
Vmo 240 kt
Va 163 kt
PSI 5.8
Airport Performance
TO (SL elev./ISA temp) 2,600
TO (5,000-ft. [email protected]) 4,270
Vso 67
Vx 120
Vy 130/td>
Climb
Time to Climb (min.)/Attitude 20/FL 250
Initial Gradient (ft/min) 860
Ceilings (ft)
Certified 30,000
Service 30,000
Sea-Level Cabin 13,100 ft
Cruise
Long Range
TAS 255 kt
Fuel Flow 268 lbs/hr
Altitude FL 300
Specific Range (nm/lb) 0.840
High Speed
TAS 285 kt
Fuel Flow 497 lbs/hr
Altitude FL 200
Specific Range (nm/lb) 0.573
NBAA IFR Ranges
Full Fuel (with available payload)
Nautical Miles 1,608
Average Speed 261
Trip Fuel 2,282
Specific Range/Altitude 0.705/FL 300
Ferry
Nautical Miles 1,650
Average Speed 2\64
Trip Fuel 2,294
Specific Range/Altitude 0.719/FL 260
Missions
300nm
Runway 1,563
Flight Time 1+10
Fuel Used 549
Specific Range/Altitude 0.546/FL 260
600nm
Runway 1,753
Flight Time 2+16
Fuel Used 975
Specific Range/Altitude 0.615/FL 270
1,000nm
Runway 2,026
Flight Time 3+46
Fuel Used 1,520
Specific Range/Altitude 0.658/FL 280
Piper M500
Characteristics
Seating 1+4/5
Wing Loading (lbs) 27.8
Power Loading (lbs) 10.18
Noise 76.8
External Dimensions (ft.)
Length 29.6
Height 11.3
Span 43.0
Internal Dimensions (ft)
Length 12.3
Height 3.9
Width 4.1
Power
Engine P&W PT6A-42A
Output (shp) 500/ISA+55C
Inspection Interval 3,600t
Weights (lb)
Max Ramp 5,134
Max Takeoff 5,092
Max Landing 4,850
Zero Fuel 4,850c
BOW 3,634
Max Payload 1,216
Useful Load 1,500
Max Fuel 1,160
Available Payload w/Max Fuel 340
Available Fuel w/Max Payload 284
Limits
Vmo 188 kt
Va 127 kt
PSI 5.6
Airport Performance
TO (SL elev./ISA temp) 2,438
TO (5,000-ft. [email protected]) 3,691
Vso 69
Vx 95
Vy 125
Climb
Time to Climb (min.)/Attitude 19/FL 250
Initial Gradient (ft/min) 753
Ceilings (ft)
Certified 30,000
Service 30,000
Sea-Level Cabin 12,600 ft
Cruise
Long Range
TAS 179 kt
Fuel Flow 135 lbs/hr
Altitude FL 280
Specific Range (nm/lb) 1.326
High Speed
TAS 258 kt
Fuel Flow 242 lbs/hr
Altitude FL 280
Specific Range (nm/lb) 1.066
NBAA IFR Ranges
Full Fuel (with available payload)
Nautical Miles 834
Average Speed 171
Trip Fuel 748
Specific Range/Altitude 1.115/FL 280
Ferry
Nautical Miles 834
Average Speed 171
Trip Fuel 748
Specific Range/Altitude 1.115/FL 280
Missions
300nm
Runway 1,550
Flight Time 1+22
Fuel Used 379
Specific Range/Altitude 0.792/FL 280
600nm
Runway 1,625
Flight Time 2+32
Fuel Used 660
Specific Range/Altitude 0.909/FL 280
1,000nm
Runway 1,700
Flight Time 4+18
Fuel Used 985
Specific Range/Altitude 1.015/FL 280
Hawker Beechcraft King Air C90GTX
Characteristics
Seating 1+7/8
Wing Loading (lbs) 34.4
Power Loading (lbs) 9.53
Noise 74.8
External Dimensions (ft)
Overall Length 35.5
Overall Height 14.3
Span 50.3
Internal Dimensions (ft)
Cabin Length (Bulkhead to Bulkhead) 12.4/12.4
Cabin Height 4.8
Cabin Width 4.5/4.1
Power
Engine 2 P&WC PT6A-135A
Output (shp) 550/ISA+30C
Inspection Interval 3,600t
Weights (lb)
Max Ramp 10,545
Max Takeoff 10,485
Max Landing 9,832
Zero Fuel (lbs) 9,378c
BOW 7,265
Max Payload 2,113
Useful Load (lbs) 3,280
Max Fuel 2,573
Available Payload w/Max Fuel 707
Available Fuel w/Max Payload 1,167
Limits
Vmo 226
Va 169
PSI 5.0
Airport
TO (SL elev./ISA temp) 1,984
TO (5,000-ft. [email protected]) 3,375
Vso 80
Vx 97
Vy 100
Climb
Time to Climb (min.)/Attitude 18/FL 250
Initial Gradient (ft/min) 1,900
Ceilings (ft)
Certified 30,000
Service 30,000
Sea-Level Cabin 19,230 ft
Cruise
Long Range
TAS 208
Fuel Flow 332
Altitude FL 260
Specific Range (nm/lb) 0.627
High Speed
TAS 270
Fuel Flow 612
Altitude FL 200
Specific Range (nm/lb) 0.441
NBAA IFR Ranges
Full Fuel (with available payload)
Nautical Miles 1,026
Average Speed 252
Trip Fuel 2,044
Specific Range/Altitude 0.502/FL 270
Ferry
Nautical Miles 975
Average Speed 252
Trip Fuel 1,949
Specific Range/Altitude 0.500/FL 270
Missions
300nm
Runway 3,004
Flight Time 1+13
Fuel Used 748
Specific Range/Altitude 0.401/FL 210
600nm
Runway 3,347
Flight Time 2+22
Fuel Used 1,353
Specific Range/Altitude 0.443/FL 230
1,000nm
Runway 3,690
Flight Time 3+57
Fuel Used 1,990
Specific Range/Altitude 0.503/FL 270
Cirrus SF-50
Characteristics
Seating 1+4/6
Wing Loading (lbs) 30.7
Power Loading (lbs) 1.67
Noise N/A
External Dimensions (ft.)
Length 30.7
Height 10.9
Span 38.7
Internal Dimensions (ft)
Length 11.5/9.8
Height 4.1/NA
Width 5.1/3.1
Power
Engine 1 Wms Intl FJ33-5A
Output (shp) 1,800/ISA+10C
Inspection Interval 3,500t
Weights (lb)
Max Ramp 6,040
Max Takeoff 6,000
Max Landing 5,550
Zero Fuel 4,900c
BOW 3,772
Max Payload 1,128
Useful Load 2,268
Max Fuel 2,000
Available Payload w/Max Fuel 268
Available Fuel w/Max Payload 1,140
Limits
Vmo ---- kt
Va ---- kt
PSI ----
Airport Performance
TO (SL elev./ISA temp) 2,036
TO (5,000-ft. [email protected]) 3,679
Vso ----
Vx ----
Vy ----
Climb
Time to Climb (min.)/Attitude NA/FL 370
Initial Gradient (ft/min) NA
Ceilings (ft)
Certified 28,000
Service 28,000
Sea-Level Cabin NA ft
Cruise
Long Range
TAS 256 kt
Fuel Flow 358 lbs/hr
Altitude FL 280
Specific Range (nm/lb) 0.715
High Speed
TAS 300 kt
Fuel Flow 466 lbs/hr
Altitude FL 280
Specific Range (nm/lb) 0.644
NBAA IFR Ranges
Full Fuel (with available payload)
Nautical Miles 550
Average Speed 251
Trip Fuel 845
Specific Range/Altitude 0.651/FL 280
Ferry
Nautical Miles 1,167
Average Speed 248
Trip Fuel 1,602
Specific Range/Altitude 0.728/FL 280
Missions
300nm
Runway 1,857
Flight Time 1+10
Fuel Used 568
Specific Range/Altitude 0.528/FL 280
600nm
Runway 2,171
Flight Time 2+15
Fuel Used 1,033
Specific Range/Altitude 0.581/FL 280
1,000nm
Runway 2,437
Flight Time 3+36
Fuel Used 1,642
Specific Range/Altitude 0.609/FL 280
ECLIPSE EA-500
Characteristics
Seating 1+4/5
Wing Loading (lbs) 41.0
Power Loading (lbs) 3.33
Noise 69.2/78.9/81.9
External Dimensions (ft.)
Length 33.5
Height 11.0
Span 37.9
Internal Dimensions (ft)
Length 12.3/10.0
Height 4.2/NA
Width 4.7/3.1=0
Power
Engine 2 P&WC PW61OF
Output (shp) 900/ISA+10C
Inspection Interval 3,500t
Weights (lb)
Max Ramp 6,034
Max Takeoff 6,000
Max Landing 5,600
Zero Fuel 4,922c
BOW 3,923
Max Payload 999
Useful Load 2,111
Max Fuel 1,680
Available Payload w/Max Fuel 431
Available Fuel w/Max Payload 1,112
Limits
Vmo ---- kt
Va ---- kt
PSI ----
Airport Performance
TO (SL elev./ISA temp) 2,394
TO (5,000-ft. [email protected]) 4,171
Vso ----
Vx ----
Vy ----
Climb
Time to Climb (min.)/Attitude 25/FL 370
Initial Gradient (ft/min) 500
Ceilings (ft)
Certified 41,000
Service 41,000
Sea-Level Cabin 25,000 ft
Cruise
Long Range
TAS 334 kt
Fuel Flow 321 lbs/hr
Altitude FL 410
Specific Range (nm/lb) 1.040
High Speed
TAS 369 kt
Fuel Flow 462 lbs/hr
Altitude FL 350
Specific Range (nm/lb) 0.799
NBAA IFR Ranges
Full Fuel (with available payload)
Nautical Miles 530
Average Speed 307
Trip Fuel 677
Specific Range/Altitude 0.783/FL 410
Ferry
Nautical Miles 1,125
Average Speed 319
Trip Fuel 1,254
Specific Range/Altitude 0.897/FL 410
Missions
300nm
Runway 2,038
Flight Time 0+58
Fuel Used 456
Specific Range/Altitude 0.658/FL 350
600nm
Runway 2,258
Flight Time 1+46
Fuel Used 837
Specific Range/Altitude 0.717/FL 390
1,000nm
Runway 2,318
Flight Time 3+04
Fuel Used 1,137
Specific Range/Altitude 0.880/FL 410