Socata 850 700 Performance Specifications, Pilatus PC 12, Meridian, King Air C-90, Pilatus, Citation Mustang .

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Piper Aircraft Meridian
Characteristics
Seating 1+5/6
Wing Loading (lbs) 27.8
Power Loading (lbs) 10.2
Capacity
Fuel (lbs) 1,160
Usuable Fuel (lbs) 1,140
Usuable Oil (quarts) 9.2
External Dimensions (ft)
Overall Length 29ft 7in
Overall Height 11ft 4in
Wing Area (ft²) 183
Span 43ft
Internal Dimensions (ft)
Cabin Length (Bulkhead to Bulkhead) 12ft 4in
Cabin Height 3ft 9in
Cabin Width 4ft 1in
Power
Engine P&WC PT6A-42A
Output (shp/Flat Rating) 500/ISA+55°C
Inspection Interval 3,600
Weights (lb)
Max Ramp 5,134
Max Takeoff 5,092
Max Landing 4,850
Zero Fuel (lbs) 4,850
Empty Weight 3,466
Max Payload 1,384
Useful Load (lbs) 1,668
Available Payload w/Max Fuel 528
Available Fuel w/Max Payload 284
Baggage Capacity 100
Limits
Vmo 188
Va 127
Vle 168
Crosswind 17
PSI 5.5
Airport
Max Weight
TO (SL elev./ISA temp.) 1,727
TO (SL elev./ISA temp.) *50ft obs 2,400
TO (5,000' elev. @ ISA + 20) *50ft obs 3,700
Min Weight
Landing (SL ele./ISA temp.) 1,000
Landing (SL ele./ISA temp.) *50ft obs 2,100
Vso 69
Climb
Time to Climb (min./Attitude ISA) 19/FL 250
Max
Initial Climb Gradient (ft/min) ISA 1Eng
1,569
Max
Initial Climb Gradient (ft/nm) ISA 1Eng
753
Ceilings (ft)
Service Ceiling 30,000
Sea-Level Cabin Pressure 12,400
Cruise
Long Range (Mid Weight)
Long Range Speed TAS 182
Long Range Fuel Flow 138
Long Range Altitude FL 280
Long Range Specific Range (nm/lb) 1.32
High Speed (Mid Weight)
High Speed TAS 257
High Speed Fuel Flow 240
High Speed Altitude FL 280
High Speed Specific Range (nm/lb) 1.07
Missions
200nm
Cruise TAS 251
Flight Time 0.94
Cabin Payload with required fuel 1074
400nm
Cruise TAS 259
Flight Time (w/o reserves) 1.72
Cabin Payload with required fuel 929
800nm
Cruise TAS 255
Flight Time (w/o reserves) 3.33
Cabin Payload with required fuel 645
1000nm
Cruise TAS Unable
Flight Time (w/o reserves) Unable
Cabin Payload with required fuel Unable
1200nm
Cruise TAS Unable
Flight Time (w/o reserves) Unable
Cabin Payload with required fuel Unable
Socata TBM 700 A
Characteristics
Seating 1+5/6
Wing Loading (lbs) 34
Power Loading (lbs) 9.4
Capacity
Fuel (lbs) 1,947
Usuable Fuel (lbs) 1,887
Usuable Oil (quarts) 6.0
External Dimensions (ft)
Overall Length 34ft 11in
Overall Height 14ft 4in
Wing Area (ft²) 194
Span 41ft 7in
Internal Dimensions (ft)
Cabin Length (Bulkhead to Bulkhead) 14ft 11in
Cabin Height 4ft
Cabin Width 3ft 11in
Power
Engine P&WC PT6A-64
Output (shp/Flat Rating) 700/ISA+49°C
Inspection Interval 3,500
Weights (lb)
Max Ramp 6,614
Max Takeoff 6,579
Max Landing 6,250
Zero Fuel (lbs) 6,001
Empty Weight 4,328
Max Payload 1,673
Useful Load (lbs) 2,286
Available Payload w/Max Fuel 399
Available Fuel w/Max Payload 613
Baggage Capacity 330
Limits
Vmo 266
Va 158
Vle 178
Crosswind 20
PSI 6.2
Airport
Max Weight
TO (SL elev./ISA temp.) 1,378
TO (SL elev./ISA temp.) *50ft obs 2,133
TO (5,000' elev. @ ISA + 20) *50ft obs 3,149.5
Min Weight
Landing (SL ele./ISA temp.) 1,030
Landing (SL ele./ISA temp.) *50ft obs 2,135
Vso 60
Climb
Time to Climb (min./Attitude ISA) 15/FL 250
Max
Initial Climb Gradient (ft/min) ISA 1Eng
1,875
Max
Initial Climb Gradient (ft/nm) ISA 1Eng
876
Ceilings (ft)
Service Ceiling 30,000
Sea-Level Cabin Pressure 14,390
Cruise
Long Range (Mid Weight)
Long Range Speed TAS 242
Long Range Fuel Flow 245
Long Range Altitude FL 290
Long Range Specific Range (nm/lb) 0.99
High Speed (Mid Weight)
High Speed TAS 300
High Speed Fuel Flow 370
High Speed Altitude FL 260
High Speed Specific Range (nm/lb) 0.81
Missions
200nm
Cruise TAS 281
Flight Time 0.81
Cabin Payload with required fuel 1530
400nm
Cruise TAS 300
Flight Time (w/o reserves) 1.47
Cabin Payload with required fuel 1354
800nm
Cruise TAS 294
Flight Time (w/o reserves) 2.87
Cabin Payload with required fuel 994
1000nm
Cruise TAS 294
Flight Time (w/o reserves) 3.55
Cabin Payload with required fuel 779
1200nm
Cruise TAS 294
Flight Time (w/o reserves) 4.23
Cabin Payload with required fuel 563
Socata TBM 700 B
Characteristics
Seating 1+5/6
Wing Loading (lbs) 34
Power Loading (lbs) 9.4
Capacity
Fuel (lbs) 1,947
Usuable Fuel (lbs) 1,887
Usuable Oil (quarts) 6.0
External Dimensions (ft)
Overall Length 34ft 11in
Overall Height 14ft 4in
Wing Area (ft²) 194
Span 41ft 7in
Internal Dimensions (ft)
Cabin Length (Bulkhead to Bulkhead) 14ft 11in
Cabin Height 4ft
Cabin Width 3ft 11in
Power
Engine P&WC PT6A-64
Output (shp/Flat Rating) 700/ISA+49°C
Inspection Interval 3,500
Weights (lb)
Max Ramp 6,614
Max Takeoff 6,579
Max Landing 6,250
Zero Fuel (lbs) 6,001
Empty Weight 4,427
Max Payload 1,574
Useful Load (lbs) 2,187
Available Payload w/Max Fuel 300
Available Fuel w/Max Payload 613
Baggage Capacity 330
Limits
Vmo 266
Va 158
Vle 178
Crosswind 20
PSI 6.2
Airport
Max Weight
TO (SL elev./ISA temp.) 1,378
TO (SL elev./ISA temp.) *50ft obs 2,133
TO (5,000' elev. @ ISA + 20) *50ft obs 3,149.5
Min Weight
Landing (SL ele./ISA temp.) 1,030
Landing (SL ele./ISA temp.) *50ft obs 2,135
Vso 60
Climb
Time to Climb (min./Attitude ISA) 15/FL 250
Max
Initial Climb Gradient (ft/min) ISA 1Eng
1,875
Max
Initial Climb Gradient (ft/nm) ISA 1Eng
876
Ceilings (ft)
Service Ceiling 30,000
Sea-Level Cabin Pressure 14,390
Cruise
Long Range (Mid Weight)
Long Range Speed TAS 242
Long Range Fuel Flow 245
Long Range Altitude FL 290
Long Range Specific Range (nm/lb) 0.99
High Speed (Mid Weight)
High Speed TAS 300
High Speed Fuel Flow 370
High Speed Altitude FL 260
High Speed Specific Range (nm/lb) 0.81
Missions
200nm
Cruise TAS 281
Flight Time (w/o reserves) 0.81
Cabin Payload with required fuel 1456
400nm
Cruise TAS 300
Flight Time 1.47
Cabin Payload with required fuel 1255
800nm
Cruise TAS 294
Flight Time (w/o reserves) 2.87
Cabin Payload with required fuel 895
1000nm
Cruise TAS 294
Flight Time (w/o reserves) 3.55
Cabin Payload with required fuel 680
1200nm
Cruise TAS 294
Flight Time (w/o reserves) 4.23
Cabin Payload with required fuel 464
Socata TBM 700 C2
Characteristics
Seating 1+5/6
Wing Loading (lbs) 38.2
Power Loading (lbs) 10.6
Capacity
Fuel (lbs) 1,947
Usuable Fuel (lbs) 1,887
Usuable Oil (quarts) 6.0
External Dimensions (ft)
Overall Length 34ft 11in
Overall Height 14ft 4in
Wing Area (ft²) 194
Span 41ft 7in
Internal Dimensions (ft)
Cabin Length (Bulkhead to Bulkhead) 14ft 11in
Cabin Height 4ft
Cabin Width 3ft 11in
Power
Engine P&WC PT6A-64
Output (shp/Flat Rating) 700/ISA+49°C
Inspection Interval 3,500
Weights (lb)
Max Ramp 7,430
Max Takeoff 7,394
Max Landing 7,024
Zero Fuel (lbs) 6,032
Empty Weight 4,689
Max Payload 1,343
Useful Load (lbs) 2,741
Available Payload w/Max Fuel 854
Available Fuel w/Max Payload 1,398
Baggage Capacity 330
Limits
Vmo 266
Va 158
Vle 178
Crosswind 20
PSI 6.2
Airport
Max Weight
TO (SL elev./ISA temp.) 2,035
TO (SL elev./ISA temp.) *50ft obs 2,840
TO (5,000' elev. @ ISA + 20) *50ft obs 4,000
Min Weight
Landing (SL ele./ISA temp.) 1,840
Landing (SL ele./ISA temp.) *50ft obs 2,430
Vso 65
Climb
Time to Climb (min./Attitude ISA) 15/FL 250
Max
Initial Climb Gradient (ft/min) ISA 1Eng
1,570
Max
Initial Climb Gradient (ft/nm) ISA 1Eng
734
Ceilings (ft)
Service Ceiling 31,000
Sea-Level Cabin Pressure 14,390
Cruise
Long Range (Mid Weight)
Long Range Speed TAS 249
Long Range Fuel Flow 258
Long Range Altitude FL 310
Long Range Specific Range (nm/lb) 0.97
High Speed (Mid Weight)
High Speed TAS 294
High Speed Fuel Flow 370
High Speed Altitude FL 260
High Speed Specific Range (nm/lb) 0.79
Missions
200nm
Cruise TAS 278
Flight Time 0.83
Cabin Payload with required fuel 1343
400nm
Cruise TAS 294
Flight Time (w/o reserves) 1.52
Cabin Payload with required fuel 1343
800nm
Cruise TAS 282
Flight Time (w/o reserves) 3.01
Cabin Payload with required fuel 1343
1000nm
Cruise TAS 282
Flight Time (w/o reserves) 3.72
Cabin Payload with required fuel 1218
1200nm
Cruise TAS 282
Flight Time (w/o reserves) 4.43
Cabin Payload with required fuel 1002
Socata TBM 850 L
Characteristics
Seating 1+5/6
Wing Loading (lbs) 38.2
Power Loading (lbs) 8.7
Capacity
Fuel (lbs) 1,947
Usuable Fuel (lbs) 1,887
Usuable Oil (quarts) 6.0
External Dimensions (ft)
Overall Length 34ft 11in
Overall Height 14ft 4in
Wing Area (ft²) 194
Span 41ft 7in
Internal Dimensions (ft)
Cabin Length (Bulkhead to Bulkhead) 14ft 11in
Cabin Height 4ft
Cabin Width 3ft 11in
Power
Engine P&W PT6A-66D
Output (shp/Flat Rating) 700/ISA+49°C
Inspection Interval 3,000
Weights (lb)
Max Ramp 7,430
Max Takeoff 7,394
Max Landing 7,024
Zero Fuel (lbs) 6,032
Empty Weight 4,653
Max Payload 1,379
Useful Load (lbs) 2,777
Available Payload w/Max Fuel 890
Available Fuel w/Max Payload 1,398
Baggage Capacity 297
Limits
Vmo 266
Va 158
Vle 178
Crosswind 20
PSI 6.2
Airport
Max Weight
TO (SL elev./ISA temp.) 2,035
TO (SL elev./ISA temp.) *50ft obs 2,840
TO (5,000' elev. @ ISA + 20) *50ft obs 4,000
Min Weight
Landing (SL ele./ISA temp.) 1,840
Landing (SL ele./ISA temp.) *50ft obs 2,430
Vso 65
Climb
Time to Climb (min./Attitude ISA) 14/FL 250
Max
Initial Climb Gradient (ft/min) ISA 1Eng
2,005
Max
Initial Climb Gradient (ft/nm) ISA 1Eng
937
Ceilings (ft)
Service Ceiling 31,000
Sea-Level Cabin Pressure 14,390
Cruise
Long Range (Mid Weight)
Long Range Speed TAS 252
Long Range Fuel Flow 263
Long Range Altitude FL 310
Long Range Specific Range (nm/lb) 0.96
High Speed (Mid Weight)
High Speed TAS 320
High Speed Fuel Flow 446
High Speed Altitude FL 260
High Speed Specific Range (nm/lb) 0.72
Missions
200nm
Cruise TAS 300
Flight Time (w/o reserves) 0.78
Cabin Payload with required fuel 1379
400nm
Cruise TAS 320
Flight Time (w/o reserves) 1.40
Cabin Payload with required fuel 1379
800nm
Cruise TAS 315
Flight Time (w/o reserves) 2.71
Cabin Payload with required fuel 1371
1000nm
Cruise TAS 315
Flight Time (w/o reserves) 3.34
Cabin Payload with required fuel 1137
1200nm
Cruise TAS 315
Flight Time (w/o reserves) 3.98
Cabin Payload with required fuel 902
Socata TBM 850 G
Characteristics
Seating 1+5/6
Wing Loading (lbs) 38.2
Power Loading (lbs) 8.7
Capacity
Fuel (lbs) 2,021
Usuable Fuel (lbs) 1,954
Usuable Oil (quarts) 6.0
External Dimensions (ft)
Overall Length 34ft 11in
Overall Height 14ft 4in
Wing Area (ft²) 194
Span 41ft 7in
Internal Dimensions (ft)
Cabin Length (Bulkhead to Bulkhead) 14ft 11in
Cabin Height 4ft
Cabin Width 3ft 11in
Power
Engine P&W PT6A-66D
Output (shp/Flat Rating) 700/ISA+49°C
Inspection Interval 3,000
Weights (lb)
Max Ramp 7,430
Max Takeoff 7,394
Max Landing 7,024
Zero Fuel (lbs) 6,032
Empty Weight 4,583
Max Payload 1,449
Useful Load (lbs) 2,847
Available Payload w/Max Fuel 893
Available Fuel w/Max Payload 1,398
Baggage Capacity 330
Limits
Vmo 266
Va 158
Vle 178
Crosswind 20
PSI 6.2
Airport
Max Weight
TO (SL elev./ISA temp.) 2,035
TO (SL elev./ISA temp.) *50ft obs 2,840
TO (5,000' elev. @  ISA + 20) *50ft obs 4,000
Min Weight
Landing (SL ele./ISA temp.) 1,840
Landing (SL ele./ISA temp.) *50ft obs 2,430
Vso 65
Climb
Time to Climb (min./Attitude ISA) 14/FL 250
Max
Initial Climb Gradient (ft/min) ISA 1Eng
2,005
Max
Initial Climb Gradient (ft/nm) ISA 1Eng
937
Ceilings (ft)
Service Ceiling 31,000
Sea-Level Cabin Pressure 14,390
Cruise
Long Range (Mid Weight)
Long Range Speed TAS 252
Long Range Fuel Flow 263
Long Range Altitude FL 310
Long Range Specific Range (nm/lb) 0.96
High Speed (Mid Weight)
High Speed TAS 320
High Speed Fuel Flow 446
High Speed Altitude FL 260
High Speed Specific Range (nm/lb) 0.72
Missions
200nm
Cruise TAS 300
Flight Time 0.78
Cabin Payload with required fuel 1449
400nm
Cruise TAS 320
Flight Time (w/o reserves) 1.40
Cabin Payload with required fuel 1449
800nm
Cruise TAS 315
Flight Time (w/o reserves) 2.71
Cabin Payload with required fuel 1441
1000nm
Cruise TAS 315
Flight Time (w/o reserves) 3.34
Cabin Payload with required fuel 1207
1200nm
Cruise TAS 315
Flight Time (w/o reserves) 3.98
Cabin Payload with required fuel 1008
Pilatus PC-12
Characteristics
Seating 1+10/11
Wing Loading (lbs) 35.7
Power Loading (lbs) 8.2
Capacity
Fuel (lbs) 2,737
Usuable Fuel (lbs) 2,704
Usuable Oil (quarts) 14.4
External Dimensions (ft)
Overall Length 47ft 3in
Overall Height 14ft
Wing Area (ft²) 278
Span 53ft 4in
Internal Dimensions (ft)
Cabin Length (Bulkhead to Bulkhead) 16ft 11in
Cabin Height 4ft 10in
Cabin Width 5ft
Power
Engine P&WC PT6A-67P
Output (shp/Flat Rating) 1,200/ISA+35°C
Inspection Interval 3,500
Weights (lb)
Max Ramp 10,495
Max Takeoff 10,450
Max Landing 9,921
Zero Fuel (lbs) 9,039
Empty Weight 6,557
Max Payload 2,482
Useful Load (lbs) 3,938
Available Payload w/Max Fuel 1,234
Available Fuel w/Max Payload 1,456
Baggage Capacity 400
Limits
Vmo 236
Va 170
Vle 163
Crosswind 25
PSI 5.8
Airport
Max Weight
TO (SL elev./ISA temp.) 1,650
TO (SL elev./ISA temp.) *50ft obs 2,650
TO (5,000' elev. @ ISA + 20) *50ft obs 4,450
Min Weight
Landing (SL ele./ISA temp.) 940
Landing (SL ele./ISA temp.) *50ft obs 1,830w/r
Vso 67
Climb
Time to Climb (min./Attitude ISA) 21/FL 250
Max
Initial Climb Gradient (ft/min) ISA 1Eng
1,920
Max
Initial Climb Gradient (ft/nm) ISA 1Eng
886
Ceilings (ft)
Service Ceiling 30,000
Sea-Level Cabin Pressure 13,100
Cruise
Long Range (Mid Weight)
Long Range Speed TAS 208
Long Range Fuel Flow 248
Long Range Altitude FL 300
Long Range Specific Range (nm/lb) 0.84
High Speed (Mid Weight)
High Speed TAS 280
High Speed Fuel Flow 491
High Speed Altitude FL 200
High Speed Specific Range (nm/lb) 0.57
Missions
200nm
Cruise TAS 266
Flight Time 0.95
Cabin Payload with required fuel 2000
400nm
Cruise TAS 259
Flight Time (w/o reserves) 2.03
Cabin Payload with required fuel 2000
800nm
Cruise TAS 252
Flight Time (w/o reserves) 2.90
Cabin Payload with required fuel 2000
1000nm
Cruise TAS 252
Flight Time (w/o reserves) 4.09
Cabin Payload with required fuel 2000
1200nm
Cruise TAS 252
Flight Time (w/o reserves) 4.88
Cabin Payload with required fuel 1930
Hawker Beechcraft King Air C90GTi
Characteristics
Seating 1+7/8
Wing Loading (lbs) 34.4
Power Loading (lbs) 9.18
Capacity
Fuel (lbs)  
Usuable Fuel (lbs) 2,573
Usuable Oil (quarts) 25
External Dimensions (ft)
Overall Length 35ft 6in
Overall Height 14ft 3in
Wing Area (ft²) 294
Span 50ft 3in
Internal Dimensions (ft)
Cabin Length (Bulkhead to Bulkhead) 19ft 10in
Cabin Height 4ft 9in
Cabin Width 4ft 2in
Power
Engine 2 P&WC PT6A-135A
Output (shp/Flat Rating) 550/ISA+30°C
Inspection Interval 3,600
Weights (lb)
Max Ramp 10,160
Max Takeoff 10,100
Max Landing 9,600
Zero Fuel (lbs) 9,212
Empty Weight 6,950
Max Payload 1,934
Useful Load (lbs) 3,210
Available Payload w/Max Fuel 637
Available Fuel w/Max Payload 1,276
Baggage Capacity 350
Limits
Vmo 226
Va 169
Vle 182
Crosswind 25
PSI 5.1
Airport
Max Weight
TO (SL elev./ISA temp.) 2,033
TO (SL elev./ISA temp.) *50ft obs 2,392
TO (5,000' elev. @ ISA + 20) *50ft obs 3,372
Min Weight
Landing (SL ele./ISA temp.) 1,400
Landing (SL ele./ISA temp.) *50ft obs 2,500
Vso 77
Climb
Time to Climb (min./Attitude ISA) 17/FL 250
Max
Initial Climb Gradient (ft/min) ISA 1Eng
1,950/480
Max
Initial Climb Gradient (ft/nm) ISA 1Eng
1040/267
Ceilings (ft)
Service Ceiling 30,000
Sea-Level Cabin Pressure 11,065
Cruise
Long Range (Mid Weight)
Long Range Speed TAS 202
Long Range Fuel Flow 302
Long Range Altitude FL 260
Long Range Specific Range (nm/lb) 0.67
High Speed (Mid Weight)
High Speed TAS 272
High Speed Fuel Flow 610
High Speed Altitude FL 200
High Speed Specific Range (nm/lb) 0.45
Missions
200nm
Cruise TAS 272
Flight Time 0.86
Cabin Payload with required fuel 1934
400nm
Cruise TAS 267
Flight Time (w/o reserves) 1.66
Cabin Payload with required fuel 1864
800nm
Cruise TAS 262
Flight Time (w/o reserves) 3.21
Cabin Payload with required fuel 1258
1000nm
Cruise TAS 262
Flight Time (w/o reserves) 3.98
Cabin Payload with required fuel 917
1200nm
Cruise TAS 262
Flight Time (w/o reserves) 4.74
Cabin Payload with required fuel 574
Hawker Beechcraft King Air C90GTx
Characteristics
Seating 1+7/8
Wing Loading (lbs) 35.7
Power Loading (lbs) 9.53
Capacity
Fuel (lbs)  
Usuable Fuel (lbs) 2,573
Usuable Oil (quarts) 25
External Dimensions (ft)
Overall Length 35ft 6in
Overall Height 14ft 3in
Wing Area (ft²) 295
Span 53ft 8in
Internal Dimensions (ft)
Cabin Length (Bulkhead to Bulkhead) 19ft 10in
Cabin Height 4ft 9in
Cabin Width 4ft 6in
Power
Engine 2 P&WC PT6A-135A
Output (shp/Flat Rating) 550/ISA+30°C
Inspection Interval 3,600
Weights (lb)
Max Ramp 10,545
Max Takeoff 10,485
Max Landing 9,700
Zero Fuel (lbs) 9,978
Empty Weight 7,035
Max Payload 2,143
Useful Load (lbs) 3,510
Available Payload w/Max Fuel 937
Available Fuel w/Max Payload 1,367
Baggage Capacity 350
Limits
Vmo 226
Va 169
Vle 182
Crosswind 25
PSI 5.1
Airport
Max Weight
TO (SL elev./ISA temp.)  
TO (SL elev./ISA temp.) *50ft obs 2,552
TO (5,000' elev. @ ISA + 20) *50ft obs 3,648
Min Weight
Landing (SL ele./ISA temp.)  
Landing (SL ele./ISA temp.) *50ft obs 2,335
Vso 77
Climb
Time to Climb (min./Attitude ISA) 18/FL 250
Max
Initial Climb Gradient (ft/min) ISA 1Eng
1,953/474
Max
Initial Climb Gradient (ft/nm) ISA 1Eng
668/259
Ceilings (ft)
Service Ceiling 30,000
Sea-Level Cabin Pressure 11,065
Cruise
Long Range (Mid Weight)
Long Range Speed TAS 202
Long Range Fuel Flow 302
Long Range Altitude FL 260
Long Range Specific Range (nm/lb) 0.67
High Speed (Mid Weight)
High Speed TAS 272
High Speed Fuel Flow 612
High Speed Altitude FL 200
High Speed Specific Range (nm/lb) 0.44
Missions
200nm
Cruise TAS 272
Flight Time 0.85
Cabin Payload with required fuel 1950
400nm
Cruise TAS 267
Flight Time (w/o reserves) 1.63
Cabin Payload with required fuel 1950
800nm
Cruise TAS 262
Flight Time (w/o reserves) 3.20
Cabin Payload with required fuel 1551
1000nm
Cruise TAS 262
Flight Time (w/o reserves) 3.97
Cabin Payload with required fuel 1210
1200nm
Cruise TAS 262
Flight Time (w/o reserves) 4.73
Cabin Payload with required fuel 868
Cessna Citation Mustang
Characteristics
Seating 1+5/6
Wing Loading (lbs) 41.2
Power Loading (lbs) 2.96
Capacity
Fuel (lbs) 2,633
Usuable Fuel (lbs) 2,580
Usuable Oil (quarts) 10.3
External Dimensions (ft)
Overall Length 40ft 7in
Overall Height 13ft 5in
Wing Area (ft²) 210
Span 43ft 2in
Internal Dimensions (ft)
Cabin Length (Bulkhead to Bulkhead) 14ft 8in
Cabin Height 4ft 6in
Cabin Width 4ft 7in
Power
Engine 2 P&WC PW615F
Output (shp/Flat Rating) 1,460/ISA+10°C
Inspection Interval 3,500
Weights (lb)
Max Ramp 8,730
Max Takeoff 8,645
Max Landing 8,000
Zero Fuel (lbs) 6,750
Empty Weight 5,350
Max Payload 1,400
Useful Load (lbs) 3,380
Available Payload w/Max Fuel 800
Available Fuel w/Max Payload 1,980
Baggage Capacity 620
Limits
Vmo 250
Va 162
Vle 250
Crosswind 25
PSI 8.3
Airport
Max Weight
TO (SL elev./ISA temp.) N/A
TO (SL elev./ISA temp.) *50ft obs 3,110
TO (5,000' elev. @ ISA + 20) *50ft obs 6,190
Min Weight
Landing (SL ele./ISA temp.) N/A
Landing (SL ele./ISA temp.) *50ft obs 2,380
Vso 73
Climb
Time to Climb (min./Attitude ISA) 20/FL 370
Max
Initial Climb Gradient (ft/min) ISA 2Eng/1Eng
3,010/870
Max
Initial Climb Gradient (ft/nm) ISA 2Eng/1Eng
1,250/450
Ceilings (ft)
Service Ceiling 41,000
Sea-Level Cabin Pressure 21,280
Cruise
Long Range (Mid Weight)
Long Range Speed TAS 317
Long Range Fuel Flow 468
Long Range Altitude FL 410
Long Range Specific Range (nm/lb) 0.68
High Speed (Mid Weight)
High Speed TAS 340
High Speed Fuel Flow 609
High Speed Altitude FL 350
High Speed Specific Range (nm/lb) 0.56
Missions
200nm
Cruise TAS 334.5
Flight Time 0.69
Cabin Payload with required fuel 1550
400nm
Cruise TAS 343
Flight Time (w/o reserves) 1.27
Cabin Payload with required fuel 1550
800nm
Cruise TAS 317
Flight Time (w/o reserves) 2.64
Cabin Payload with required fuel 1550
1000nm
Cruise TAS 317
Flight Time (w/o reserves) 3.27
Cabin Payload with required fuel 1302
1200nm
Cruise TAS 317
Flight Time (w/o reserves) 3.91
Cabin Payload with required fuel 1014
Socata TBM 900
Characteristics
Seating 1+5/6
Wing Loading (lbs) 38.2
Power Loading (lbs) 8.7
Capacity
Fuel (lbs) 2,021
Usuable Fuel (lbs) 1,954
Usuable Oil (quarts) 6.0
External Dimensions (ft)
Overall Length 34ft 11in
Overall Height 14ft 4in
Wing Area (ft²) 194
Span 41ft 6in
Internal Dimensions (ft)
Cabin Length (Bulkhead to Bulkhead) 14ft 11in
Cabin Height 4ft
Cabin Width 3ft 11in
Power
Engine P&W PT6A-66D
Output (shp/Flat Rating) 700*/ISA+49°C
Inspection Interval 3,000
Weights (lb)
Max Ramp 7,430
Max Takeoff 7,394
Max Landing 7,024
Zero Fuel (lbs) 6,032
Empty Weight 4,656
Max Payload 1,376
Useful Load (lbs) 2,774
Available Payload w/Max Fuel 820
Available Fuel w/Max Payload 1,398
Baggage Capacity 330
Limits
Vmo 266
Va 158
Vle 178
Crosswind 20
PSI 6.2
Airport
Max Weight
TO (SL elev./ISA temp.) 1,845
TO (SL elev./ISA temp.) *50ft obs 2,555
TO (5,000' elev. @ ISA + 20) *50ft obs 3,668
Min Weight
Landing (SL ele./ISA temp.) 1,840
Landing (SL ele./ISA temp.) *50ft obs 2,430
Vso 65
Climb
Time to Climb (min./Attitude ISA) 14/FL 250
Max
Initial Climb Gradient (ft/min) ISA 1Eng
2,005
Max
Initial Climb Gradient (ft/nm) ISA 1Eng
937
Ceilings (ft)
Service Ceiling 31,000
Sea-Level Cabin Pressure 14,390
Cruise
Long Range (Mid Weight)
Long Range Speed TAS 252
Long Range Fuel Flow 255
Long Range Altitude FL 310
Long Range Specific Range (nm/lb) 0.99
High Speed (Mid Weight)
High Speed TAS 325
High Speed Fuel Flow 432
High Speed Altitude FL 280
High Speed Specific Range (nm/lb) 0.75
Missions
200nm
Cruise TAS 298
Flight Time (w/o reserves) 0.78
Cabin Payload with required fuel 1376
400nm
Cruise TAS 318
Flight Time (w/o reserves) 1.41
Cabin Payload with required fuel 1376
800nm
Cruise TAS 325
Flight Time (w/o reserves) 2.65
Cabin Payload with required fuel 1367
1000nm
Cruise TAS 325
Flight Time (w/o reserves) 3.27
Cabin Payload with required fuel 1133
1200nm
Cruise TAS 325
Flight Time (w/o reserves) 3.88
Cabin Payload with required fuel 934

Contact Us

Avex, Inc.
Camarillo Airport
205 Durley Avenue, Suite A
Camarillo, California 93010

Toll Free: (800) 475-1057
Local: (805) 389-1188
Terry Winson's Cell Phone: (805) 312-5005 (24 Hours)
Fax: (805) 389-3323