Aircraft Specs
| Model | King Air A90 | King Air A90 | King Air A200 | King Air 200T | King Air 350 | DHC-8 100 | DHC-8 200 | DHC-8 300 | Gulfstream IV | Boeing 737-500 |
|---|---|---|---|---|---|---|---|---|---|---|
| Engines | ||||||||||
| Manufacturer | Pratt & Whitney Canada | Pratt & Whitney Canada | Pratt & Whitney Canada | Pratt & Whitney Canada | Pratt & Whitney Canada | Pratt & Whitney Canada | Pratt & Whitney Canada | Pratt & Whitney Canada | Rolls-Royce | CFM International |
| Type | PT6A-20 turboprop engines | PT6A-28 turboprop engines | PT6A-41 turboprop engines | PT6A-41 turboprop engines | PT6A-60A turboprop engines | PW120A turboprop engines | PW123D turboprop engines | PW123B turboprop engines | TAY 611-8 turbofan engines | CFM56-3C-1 turbofan engines |
| Power Rating | 550 shp. (410 kW.) per engine | 680 shp. (500 kW.) per engine | 850 shp. (625 kW.) per engine | 850 shp. (625 kW.) per engine | 1,050 shp. (783 kW.) per engine | 1,800 shp. (1,342 kW.) per engine | 2,150 shp. (1,604 kW.) per engine | 2,150 shp. (1,604 kW.) per engine | 13,850 lbs. (61.6 kN.) thrust per engine | 20,000 lbs (89 kN.) thrust per engine |
| Dimensions (Exterior) | ||||||||||
| Length | 35 ft. 6 in. (10.82 m.) | 35 ft. 6 in. (10.82 m.) | 43 ft. 10 in. (13.3 m.) | 43 ft. 10 in. (13.3 m.) | 46 ft. 8 in. (14.22 m.) | 73 ft. 0 in. (22.25 m.) | 73 ft. 0 in. (22.25 m.) | 84 ft. 3 in. (25.68 m.) | 88 ft. 4 in. (26.92 m.) | 101 ft. 9 in. (31.01 m.) |
| Height | 14 ft. 3 in. (4.34 m.) | 14 ft. 3 in. (4.34 m.) | 15 ft. 5 in. (4.69 m.) | 14 ft. 6 in. (4.41 m.) | 14 ft. 4 in. (4.37 m.) | 24 ft. 7 in. (7.5 m.) | 24 ft. 7 in. (7.5 m.) | 24 ft. 7 in. (7.5 m.) | 24 ft. 5 in. (7.45 m.) | 37 ft. 6 in. (11.43 m.) |
| Wingspan | 45 ft. 10.5 in. (13.99 m.) | 50 ft. 3 in. (15 m.) | 54 ft. 6 in. (16.6 m.) | 56 ft. 7 in. (17.2 m.) | 57 ft. 11 in. (17.65 m.) | 85 ft. 0 in. (25.91 m.) | 85 ft. 0 in. (25.91 m.) | 90 ft. 0 in. (27.43 m.) | 77 ft. 10 in. (23.72 m.) | 94 ft. 9 in. (28.88 m.) |
| Dimensions (Interior) | ||||||||||
| Length | 12 ft. 10 in. (3.91 m.) | 12 ft. 10 in. (3.91 m.) | 16 ft. 8 in. (5.07 m.) | 16 ft. 8 in. (5.07 m.) | 19 ft. 2 in. (5.84 m.) | 30 ft. 9 in. (9.37 m.) | 30 ft. 9 in. (9.37 m.) | 39 ft. 0 in. (11.89 m.) | 45 ft. 1 in. (13.74 m.) | 71 ft. 5 in. (21.76 m.) |
| Width | 4 ft. 6 in. (1.37 m.) | 4 ft. 6 in. (1.37 m.) | 4 ft. 6 in. (1.37 m.) | 4 ft. 6 in. (1.37 m.) | 4 ft. 6 in. (1.37 m.) | 8 ft. 10 in. (2.69 m.) | 8 ft. 10 in. (2.69 m.) | 8 ft. 10 in. (2.69 m.) | 7 ft. 4 in. (2.24 m.) | 11 ft. 7 in. (3.54 m.) |
| Height | 4 ft. 9 in. (1.45 m.) | 4 ft. 9 in. (1.45 m.) | 4 ft. 9 in. (1.45 m.) | 4 ft. 9 in. (1.45 m.) | 4 ft. 9 in. (1.45 m.) | 6 ft. 2 in. (1.88 m.) | 6 ft. 2 in. (1.88 m.) | 6 ft. 2 in. (1.88 m.) | 6 ft. 2 in. (1.88 m.) | 7 ft. 3 in. (2.20 m.) |
| Weights | ||||||||||
| Max Ramp Weight | 9,705 lbs. (4,402 kg.) | 10,540 lbs. (4,780 kg.) | 13,585 lbs. (6,162 kg.) | 14,085 lbs. (6,388 kg.) | 15,100 lbs. (6,849 kg.) | 34,700 lbs. (15,740 kg.) | 36,500 lbs. (16,556 kg.) | 43,200 lbs. (19,595 kg.) | 74,900 lbs. (33,975 kg.) | 133,500 lbs. (60,556 kg.) |
| Max Takeoff Weight | 9,650 lbs. (4,377 kg.) | 10,485 lbs. (4,755 kg.) | 13,500 lbs. (6,123 kg.) | 14,000 lbs. (6,350 kg.) | 15,000 lbs. (6,804 kg.) | 34,500 lbs. (15,650 kg.) | 36,300 lbs. (16,465 kg.) | 43,000 lbs. (19,505 kg.) | 74,600 lbs. (33,884 kg.) | 133,000 lbs. (60,328 kg.) |
| Max Zero Fuel Weight | N/A | N/A | 11,000 lbs. (4,989 kg.) | 11,000 lbs. (4,989 kg.) | 12,500 lbs. (5,670 kg.) | 31,000 lbs. (14,061 kg.) | 31,000 lbs. (14,061 kg.) | 39,000 lbs. (17,690 kg.) | 49,000 lbs. (22,226 kg.) | 113,000 lbs. (51,256 kg.) |
| Useable Fuel Capacity | 2,479 lbs. (1,124 kg.) | 2,479 lbs. (1,124 kg.) | 3,645 lbs. (1,653 kg.) | 4,355 lbs. (1,975 kg.) | 3,611 lbs. (1,638 kg.) | 5,500 lbs. (2,495 kg.) | 5,500 lbs. (2,495 kg.) | 5,800 lbs. (2,631 kg.) | 29,500 lbs. (13,381 kg.) | 40,300 lbs. (18,280 kg.) |
| Empty Weight | 5,150 lbs. (2,336 kg.) | 5,600 lbs. (2,540 kg.) | 8,000 lbs. (3,628 kg.) | 8,200 lbs. (3,719 kg.) | 9,955 lbs. (4,516 kg.) | 20,000 lbs. (9,072 kg.) | 20,000 lbs. (9,072 kg.) | 24,000 lbs. (10,886 kg.) | 41,000 lbs. (18,597 kg.) | 69,140 lbs. (31,359 kg.) |
| Max Payload | 2,000 lbs. (907 kg.) | 2,500 lbs. (1133 kg.) | 3,000 lbs. (1360 kg.) | 2,800 lbs. (1270 kg.) | 2,545 lbs. (1,154 kg.) | 11,000 lbs. (4,990 kg.) | 11,000 lbs. (4,990 kg.) | 15,000 lbs. (6,804 kg.) | 8,000 lbs. (3,629 kg.) | 43,860 lbs. (19,896 kg.) |
| Useful Load | 4,500 lbs. (2,041 kg.) | 4,885 lbs. (2,215 kg.) | 5,500 lbs. (2,494 kg.) | 5,800 lbs. (2,630 kg.) | 5,145 lbs. (2,334 kg.) | 14,500 lbs. (6,577 kg.) | 16,500 lbs. (7,484 kg.) | 19,200 lbs. (8,709 kg.) | 33,900 lbs. (15,376 kg.) | 63,860 lbs. (28,965 kg.) |
| Performance | ||||||||||
| Maximum Cruise Speed | 200 knots (370.4 km/h.) | 230 knots (425.9 km/h.) | 270 knots (500 km/h.) | 270 knots (500 km/h.) | 312 knots (578 km/h.) | 243 knots (450 km/h.) | 280 knots (518 km/h.) | 284 knots (526 km/h.) | Mach 0.80 (459 knots, 850 km/h.) | Mach 0.74 (485 knots, 898 km/h.) |
| Range: Max Payload | 1,100 nm. | 1,040 nm. | 1,000 nm. | 1,228 nm. | 1,500 nm. | 580 nm. | 600 nm. | 700 nm. | 3,800 nm. | 2,000 nm. |
| Range: Full Fuel/Available Payload | 1,340 nm. / 1,651 lbs. | 1,340 nm. / 1,651 lbs. | 1,600 nm. / 1,485 lbs. | 1,890 nm. / 1,075 lbs. | 1,806 nm. / 1,150 lbs. | 1,174 nm. / 8,000 lbs. | 1,174 nm. / 8,000 lbs. | 1,020 nm. / 12,000 lbs. | 4,220 nm. / 2,000 lbs. | 2,400 nm. / 38,000 lbs. |
| Range: Ferry | 1,340 nm. | 1,340 nm. | 1,600 nm. | 1,890 nm. | 2,692 nm. | 1,200 nm. | 1,300 nm. | 1,550 nm. | 4,350 nm. | 2,935 nm. |
| Max Endurance | 6.2 hours | 6.2 hours | 6.0 hours | 7.4 hours | 8 hours | 5 hours | 6 hours | 7 hours | 9 hours | 6 hours |
| Max Operating Altitude | 25,000 ft. | 25,000 ft. | 31,000 ft. | 35,000 ft. | 35,000 ft. (10,668 m.) | 25,000 ft. (7,620 m.) | 25,000 ft. (7,620 m.) | 25,000 ft. (7,620 m.) | 45,000 ft. (13,716 m.) | 37,000 ft. (11,278 m.) |
| Take-off Field Length | 1,900 ft. | 2,200 ft. | 2,500 ft. | 2,900 ft. | 3,300 ft. (1,006 m.) | 2,800 ft. (853 m.) | 2,850 ft. (869 m.) | 3,280 ft. (1,000 m.) | 5,450 ft. (1,661 m.) | 5,700 ft. (1,737 m.) |
| Landing Field Length | 1,400 ft. | 1,700 ft. | 2,000 ft. | 2,250 ft. | 2,692 ft. (821 m.) | 2,100 ft. (640 m.) | 2,200 ft. (670 m.) | 2,600 ft. (792 m.) | 3,436 ft. (1,047 m.) | 4,000 ft. (1,219 m.) |
Model: King Air A90
Engines:
Manufacturer - Pratt & Whitney Canada
Type - PT6A-20 turboprop
Power Rating - 550 shp (410 kW)
Dimensions (Exterior):
Length - 35 ft 6 in (10.82 m)
Height - 14 ft 3 in (4.34 m)
Wingspan - 45 ft 10.5 in (13.99 m)
Dimensions (Interior):
Length - 12 ft 10 in (3.91 m)
Width - 4 ft 6 in (1.37 m)
Height - 4 ft 9 in (1.45 m)
Weights:
Max Ramp Weight - 9,705 lbs (4,402 kg)
Max Takeoff Weight - 9,650 lbs (4,377 kg)
Max Zero Fuel Weight - N/A
Useable Fuel Capacity - 2,479 lbs (1,124 kg)
Empty Weight - 5,150 lbs (2,336 kg)
Max Payload - 2,000 lbs (907 kg)
Useful Load - 4,500 lbs (2,041 kg)
Performance:
Maximum Cruise Speed - 200 knots (370.4 km/h)
Range: Max Payload - 1,100 nm
Range: Full Fuel/Available Payload - 1,340 nm / 1,651 lbs
Range: Ferry - 1,340 nm
Max Endurance - 6.2 hours
Max Operating Altitude - 25,000 ft
Take-off Field Length - 1,900 ft
Landing Field Length - 1,400 ft
Model: King Air A90
Engines:
Manufacturer - Pratt & Whitney Canada
Type - PT6A-28 turboprop
Power Rating - 680 shp (500 kW)
Dimensions (Exterior):
Length - 35 ft 6 in (10.82 m)
Height - 14 ft 3 in (4.34 m)
Wingspan - 50 ft 3 in (15 m)
Dimensions (Interior):
Length - 12 ft 10 in (3.91 m)
Width - 4 ft 6 in (1.37 m)
Height - 4 ft 9 in (1.45 m)
Weights:
Max Ramp Weight - 10,540 lbs (4,780 kg)
Max Takeoff Weight - 10,485 lbs (4,755 kg)
Max Zero Fuel Weight - N/A
Useable Fuel Capacity - 2,479 lbs (1,124 kg)
Empty Weight - 5,600 lbs (2,540 kg)
Max Payload - 2,500 lbs (1133 kg)
Useful Load - 4,885 lbs (2,215 kg)
Performance:
Maximum Cruise Speed - 230 knots (425.9 km/h)
Range: Max Payload - 1,040 nm
Range: Full Fuel/Available Payload - 1,340 nm / 1,651 lbs
Range: Ferry - 1,340 nm
Max Endurance - 6.2 hours
Max Operating Altitude - 25,000 ft
Take-off Field Length - 2,200 ft
Landing Field Length - 1,700 ft
Model: King Air A200
Engines:
Manufacturer - Pratt & Whitney Canada
Type - PT6A-41 turboprop
Power Rating - 850 shp (625 kW)
Dimensions (Exterior):
Length - 43 ft 10 in (13.3 m)
Height - 15 ft 5 in (4.69 m)
Wingspan - 54 ft 6 in (16.6 m)
Dimensions (Interior):
Length - 16 ft 8 in (5.07 m)
Width - 4 ft 6 in (1.37 m)
Height - 4 ft 9 in (1.45 m)
Weights:
Max Ramp Weight - 13,585 lbs (6,162 kg)
Max Takeoff Weight - 13,500 lbs (6,123 kg)
Max Zero Fuel Weight - 11,000 lbs (4,989 kg)
Useable Fuel Capacity - 3,645 lbs (1,653 kg)
Empty Weight - 8,000 lbs (3,628 kg)
Max Payload - 3,000 lbs (1360 kg)
Useful Load - 5,500 lbs (2,494 kg)
Performance:
Maximum Cruise Speed - 270 knots (500 km/h)
Range: Max Payload - 1,000 nm
Range: Full Fuel/Available Payload - 1,600 nm / 1,485 lbs
Range: Ferry - 1,600 nm
Max Endurance - 6.0 hours
Max Operating Altitude - 31,000 ft
Take-off Field Length - 2,500 ft
Landing Field Length - 2,000 ft
Model: King Air 200T
Engines:
Manufacturer - Pratt & Whitney Canada
Type - PT6A-41 turboprop
Power Rating - 850 shp (625 kW)
Dimensions (Exterior):
Length - 43 ft 10 in (13.3 m)
Height - 14 ft 6 in (4.41 m)
Wingspan - 56 ft 7 in (17.2 m)
Dimensions (Interior):
Length - 16 ft 8 in (5.07 m)
Width - 4 ft 6 in (1.37 m)
Height - 4 ft 9 in (1.45 m)
Weights:
Max Ramp Weight - 14,085 lbs (6,388 kg)
Max Takeoff Weight - 14,000 lbs (6,350 kg)
Max Zero Fuel Weight - 11,000 lbs (4,989 kg)
Useable Fuel Capacity - 4,355 lbs (1,975 kg)
Empty Weight - 8,200 lbs (3,719 kg)
Max Payload - 2,800 lbs (1270 kg)
Useful Load - 5,800 lbs (2,630 kg)
Performance:
Maximum Cruise Speed - 270 knots (500 km/h)
Range: Max Payload - 1,228 nm
Range: Full Fuel/Available Payload - 1,890 nm / 1,075 lbs
Range: Ferry - 1,890 nm
Max Endurance - 7.4 hours
Max Operating Altitude - 35,000 ft
Take-off Field Length - 2,900 ft
Landing Field Length - 2,250 ft
Model: King Air 350
Engines:
Manufacturer - Pratt & Whitney Canada
Type - PT6A-60A turboprop
Power Rating - 1,050 shp (783 kW)
Dimensions (Exterior):
Length - 46 ft 8 in (14.22 m)
Height - 14 ft 4 in (4.37 m)
Wingspan - 57 ft 11 in (17.65 m)
Dimensions (Interior):
Length - 19 ft 2 in (5.84 m)
Width - 4 ft 6 in (1.37 m)
Height - 4 ft 9 in (1.45 m)
Weights:
Max Ramp Weight - 15,100 lbs (6,849 kg)
Max Takeoff Weight - 15,000 lbs (6,804 kg)
Max Zero Fuel Weight - 12,500 lbs (5,670 kg)
Useable Fuel Capacity - 3,611 lbs (1,638 kg)
Empty Weight - 9,955 lbs (4,516 kg)
Max Payload - 2,545 lbs (1,154 kg)
Useful Load - 5,145 lbs (2,334 kg)
Performance:
Maximum Cruise Speed - 312 knots (578 km/h)
Range: Max Payload - 1,500 nm
Range: Full Fuel/Available Payload - 1,806 nm / 1,150 lbs
Range: Ferry - 2,692 nm
Max Endurance - 8 hours
Max Operating Altitude - 35,000 ft (10,668 m)
Take-off Field Length - 3,300 ft (1,006 m)
Landing Field Length - 2,692 ft (821 m)
Model: DHC-8 100
Engines:
Manufacturer - Pratt & Whitney Canada
Type - PW120A turboprop
Power Rating - 1,800 shp (1,342 kW)
Dimensions (Exterior):
Length - 73 ft 0 in (22.25 m)
Height - 24 ft 7 in (7.5 m)
Wingspan - 85 ft 0 in (25.91 m)
Dimensions (Interior):
Length - 30 ft 9 in (9.37 m)
Width - 8 ft 10 in (2.69 m)
Height - 6 ft 2 in (1.88 m)
Weights:
Max Ramp Weight - 34,700 lbs (15,740 kg)
Max Takeoff Weight - 34,500 lbs (15,650 kg)
Max Zero Fuel Weight - 31,000 lbs (14,061 kg)
Useable Fuel Capacity - 5,500 lbs (2,495 kg)
Empty Weight - 20,000 lbs (9,072 kg)
Max Payload - 11,000 lbs (4,990 kg)
Useful Load - 14,500 lbs (6,577 kg)
Performance:
Maximum Cruise Speed - 243 knots (450 km/h)
Range: Max Payload - 580 nm
Range: Full Fuel/Available Payload - 1,174 nm / 8,000 lbs
Range: Ferry - 1,200 nm
Max Endurance - 5 hours
Max Operating Altitude - 25,000 ft (7,620 m)
Take-off Field Length - 2,800 ft (853 m)
Landing Field Length - 2,100 ft (640 m)
Model: DHC-8 200
Engines:
Manufacturer - Pratt & Whitney Canada
Type - PW123D turboprop
Power Rating - 2,150 shp (1,604 kW)
Dimensions (Exterior):
Length - 73 ft 0 in (22.25 m)
Height - 24 ft 7 in (7.5 m)
Wingspan - 85 ft 0 in (25.91 m)
Dimensions (Interior):
Length - 30 ft 9 in (9.37 m)
Width - 8 ft 10 in (2.69 m)
Height - 6 ft 2 in (1.88 m)
Weights:
Max Ramp Weight - 36,500 lbs (16,556 kg)
Max Takeoff Weight - 36,300 lbs (16,465 kg)
Max Zero Fuel Weight - 31,000 lbs (14,061 kg)
Useable Fuel Capacity - 5,500 lbs (2,495 kg)
Empty Weight - 20,000 lbs (9,072 kg)
Max Payload - 11,000 lbs (4,990 kg)
Useful Load - 16,500 lbs (7,484 kg)
Performance:
Maximum Cruise Speed - 280 knots (518 km/h)
Range: Max Payload - 600 nm
Range: Full Fuel/Available Payload - 1,174 nm / 8,000 lbs
Range: Ferry - 1,300 nm
Max Endurance - 6 hours
Max Operating Altitude - 25,000 ft (7,620 m)
Take-off Field Length - 2,850 ft (869 m)
Landing Field Length - 2,200 ft (670 m)
Model: DHC-8 300
Engines:
Manufacturer - Pratt & Whitney Canada
Type - PW123B turboprop
Power Rating - 2,150 shp (1,604 kW)
Dimensions (Exterior):
Length - 84 ft 3 in (25.68 m)
Height - 24 ft 7 in (7.5 m)
Wingspan - 90 ft 0 in (27.43 m)
Dimensions (Interior):
Length - 39 ft 0 in (11.89 m)
Width - 8 ft 10 in (2.69 m)
Height - 6 ft 2 in (1.88 m)
Weights:
Max Ramp Weight - 43,200 lbs (19,595 kg)
Max Takeoff Weight - 43,000 lbs (19,505 kg)
Max Zero Fuel Weight - 39,000 lbs (17,690 kg)
Useable Fuel Capacity - 5,800 lbs (2,631 kg)
Empty Weight - 24,000 lbs (10,886 kg)
Max Payload - 15,000 lbs (6,804 kg)
Useful Load - 19,200 lbs (8,709 kg)
Performance:
Maximum Cruise Speed - 284 knots (526 km/h)
Range: Max Payload - 700 nm
Range: Full Fuel/Available Payload - 1,020 nm / 12,000 lbs
Range: Ferry - 1,550 nm
Max Endurance - 7 hours
Max Operating Altitude - 25,000 ft (7,620 m)
Take-off Field Length - 3,280 ft (1,000 m)
Landing Field Length - 2,600 ft (792 m)
Model: Gulfstream IV
Engines:
Manufacturer - Rolls-Royce
Type - TAY 611-8 turbofan
Power Rating - 13,850 lbs (61.6 kN) thrust
Dimensions (Exterior):
Length - 88 ft 4 in (26.92 m)
Height - 24 ft 5 in (7.45 m)
Wingspan - 77 ft 10 in (23.72 m)
Dimensions (Interior):
Length - 45 ft 1 in (13.74 m)
Width - 7 ft 4 in (2.24 m)
Height - 6 ft 2 in (1.88 m)
Weights:
Max Ramp Weight - 74,900 lbs (33,975 kg)
Max Takeoff Weight - 74,600 lbs (33,884 kg)
Max Zero Fuel Weight - 49,000 lbs (22,226 kg)
Useable Fuel Capacity - 29,500 lbs (13,381 kg)
Empty Weight - 41,000 lbs (18,597 kg)
Max Payload - 8,000 lbs (3,629 kg)
Useful Load - 33,900 lbs (15,376 kg)
Performance:
Maximum Cruise Speed - Mach 0.80 (459 knots, 850 km/h)
Range: Max Payload - 3,800 nm
Range: Full Fuel/Available Payload - 4,220 nm / 2,000 lbs
Range: Ferry - 4,350 nm
Max Endurance - 9 hours
Max Operating Altitude - 45,000 ft (13,716 m)
Take-off Field Length - 5,450 ft (1,661 m)
Landing Field Length - 3,436 ft (1,047 m)
Model: Boeing 737-500
Engines:
Manufacturer - CFM International
Type - CFM56-3C-1 turbofan
Power Rating - 20,000 lbs (89 kN) thrust
Dimensions (Exterior):
Length - 101 ft 9 in (31.01 m)
Height - 37 ft 6 in (11.43 m)
Wingspan - 94 ft 9 in (28.88 m)
Dimensions (Interior):
Length - 71 ft 5 in (21.76 m)
Width - 11 ft 7 in (3.54 m)
Height - 7 ft 3 in (2.20 m)
Weights:
Max Ramp Weight - 133,500 lbs (60,556 kg)
Max Takeoff Weight - 133,000 lbs (60,328 kg)
Max Zero Fuel Weight - 113,000 lbs (51,256 kg)
Useable Fuel Capacity - 40,300 lbs (18,280 kg)
Empty Weight - 69,140 lbs (31,359 kg)
Max Payload - 43,860 lbs (19,896 kg)
Useful Load - 63,860 lbs (28,965 kg)
Performance:
Maximum Cruise Speed - Mach 0.74 (485 knots, 898 km/h)
Range: Max Payload - 2,000 nm
Range: Full Fuel/Available Payload - 2,400 nm / 38,000 lbs
Range: Ferry - 2,935 nm
Max Endurance - 6 hours
Max Operating Altitude - 37,000 ft (11,278 m)
Take-off Field Length - 5,700 ft (1,737 m)
Landing Field Length - 4,000 ft (1,219 m)