Aircraft Specifications and Performance
Cessna 172
Crew: 1 pilot
Passengers: Up to 3
Length: 27.2 ft (8.3 m)
Wingspan: 36.1 ft (11.0 m)
Height: 8.3 ft (2.5 m)
Maximum takeoff weight: 2,450 lb (1,111 kg)
Fuel capacity: 56 gallons (212 liters)
Maximum speed: 124 knots (143 mph)
Cruise speed: 122 knots (140 mph)
Range: 640 nm (740 miles, 1,191 km)
Service ceiling: 13,500 ft (4,115 m)
Rate of climb: 730 ft/min (3.7 m/s)
Takeoff distance: 1,320 ft (402 m)
Landing distance: 590 ft (180 m) Fuel burn: 8-10 gph
Cessna 182
Crew: 1 pilot
Passengers: Up to 3-4
Length: 29.2 ft (8.9 m)
Wingspan: 36.0 ft (11.0 m)
Height: 9.2 ft (2.8 m)
Maximum takeoff weight: 3,100 lb (1,406 kg)
Fuel capacity: 87 gallons (329 liters)
Maximum speed: 145 knots (167 mph)
Cruise speed: 140 knots (161 mph)
Range: 915 nm (1,055 miles, 1,700 km)
Service ceiling: 18,100 ft (5,517 m)
Rate of climb: 924 ft/min (4.7 m/s)
Takeoff distance: 1,095 ft (334 m)
Landing distance: 795 ft (242 m)
Fuel burn: 12-15 gph
Cessna 208 Caravan
Crew: 1-2 pilots
Passengers: Up to 14 (depending on configuration)
Length: 41.7 ft (12.7 m)
Wingspan: 52.1 ft (15.9 m)
Height: 15.1 ft (4.6 m)
Maximum takeoff weight: 8,000 lb (3,629 kg)
Fuel capacity: 335 gallons (1,270 liters)
Maximum speed: 186 knots (214 mph)
Cruise speed: 180 knots (207 mph)
Range: 912 nm (1,050 miles, 1,689 km)
Service ceiling: 25,000 ft (7,620 m)
Rate of climb: 975 ft/min (4.95 m/s)
Takeoff distance: 2,160 ft (658 m)
Landing distance: 1,710 ft (521 m)
Fuel burn: 45-50 gph for the turboprop engine.
Cessna 310
Crew: 1 pilot
Passengers: Up to 4-5
Length: 28.7 ft (8.8 m)
Wingspan: 35.8 ft (10.9 m)
Height: 9.8 ft (3.0 m)
Maximum takeoff weight: 5,500 lb (2,495 kg)
Fuel capacity: 102 gallons (386 liters)
Maximum speed: 215 knots (247 mph)
Cruise speed: 190 knots (219 mph)
Range: 1,200 nm (1,380 miles, 2,222 km)
Service ceiling: 20,000 ft (6,096 m)
Rate of climb: 1,400 ft/min (7.1 m/s)
Takeoff distance: 1,850 ft (564 m)
Landing distance: 1,900 ft (579 m)
Fuel burn: 25-30 gph per engine.
Cessna 340
Crew: 1 pilot
Passengers: Up to 4-5
Length: 36.0 ft (11.0 m)
Wingspan: 41.0 ft (12.5 m)
Height: 12.7 ft (3.9 m)
Maximum takeoff weight: 5,990 lb (2,718 kg)
Fuel capacity: 166 gallons (628 liters)
Maximum speed: 246 knots (283 mph)
Cruise speed: 220 knots (253 mph)
Range: 1,300 nm (1,495 miles, 2,408 km)
Service ceiling: 29,000 ft (8,839 m)
Rate of climb: 1,700 ft/min (8.6 m/s)
Takeoff distance: 2,100 ft (640 m)
Landing distance: 2,400 ft (732 m)
Fuel burn: 30-35 gph per engine.
Cessna 414
Crew: 1 pilot
Passengers: Up to 6-8
Length: 36.3 ft (11.1 m)
Wingspan: 44.1 ft (13.4 m)
Height: 11.5 ft (3.5 m)
Maximum takeoff weight: 6,850 lb (3,107 kg)
Fuel capacity: 206 gallons (779 liters)
Maximum speed: 237 knots (273 mph)
Cruise speed: 218 knots (251 mph)
Range: 1,315 nm (1,513 miles, 2,436 km)
Service ceiling: 28,000 ft (8,534 m)
Rate of climb: 1,960 ft/min (9.9 m/s)
Takeoff distance: 2,240 ft (683 m)
Landing distance: 1,920 ft (585 m)
Fuel burn: 30-35 gph per engine.
(based on 414A Chancellor)
Cessna 421
Crew: 1 pilot
Passengers: Up to 6-8
Length: 36.2 ft (11.0 m)
Wingspan: 41.6 ft (12.7 m)
Height: 11.6 ft (3.5 m)
Maximum takeoff weight: 7,450 lb (3,379 kg)
Fuel capacity: 170 gallons (643 liters)
Maximum speed: 247 knots (284 mph)
Cruise speed: 230 knots (265 mph)
Range: 1,285 nm (1,479 miles, 2,381 kmm)
Service ceiling: 30,200 ft (9,205 m)
Rate of climb: 1,620 ft/min (8.2 m/s)
Takeoff distance: 2,180 ft (664 m)
Landing distance: 2,400 ft (732 m)
Fuel burn: 40-45 gph per engine.
(based on 421C Golden Eagle)
Cessna 441
Crew: 1-2 pilots
Passengers: Up to 9
Length: 39.9 ft (12.2 m)
Wingspan: 49.4 ft (15.0 m)
Height: 13.0 ft (4.0 m)
Maximum takeoff weight: 10,100 lb (4,580 kg)
Fuel capacity: 371 gallons (1,404 liters)
Maximum speed: 286 knots (329 mph)
Cruise speed: 260 knots (299 mph)
Range: 1,500 nm (1,725 miles, 2,778 kmm)
Service ceiling: 35,000 ft (10,668 m)
Rate of climb: 2,080 ft/min (10.6 m/s)
Takeoff distance: 3,080 ft (939 m)
Landing distance: 2,600 ft (792 m)
Fuel burn: 125-135 gph for the turboprop engine.
(Based on 441 Conquest II)
Cessna Citation Mustang
Crew: 1-2 pilots
Passengers: Up to 4-5
Length: 40.6 ft (12.4 m)
Wingspan: 43.2 ft (13.2 m)
Height: 13.5 ft (4.1 m)
Maximum takeoff weight: 8,645 lb (3,924 kg)
Fuel capacity: 3,290 lb / 495 gal / 1,493 kg
Maximum speed: 340 knots (391 mph)
Cruise speed: 340 knots (391 mph)
Range: 1,150 nm (1,323 miles, 2,130 km)
Service ceiling: 41,000 ft (12,497 m)
Rate of climb: 3,010 ft/min (15.3 m/s)
Takeoff distance: 3,110 ft (948 m)
Landing distance: 2,380 ft (725 m)
Fuel burn: 70-91 gph / 460 lbs/hr
Cessna Citation I
Crew: 1-2 pilots
Passengers: Up to 5-6
Length: 43.1 ft (13.1 m)
Wingspan: 43.2 ft (13.2 m)
Height: 14.3 ft (4.4 m)
Maximum takeoff weight: 10,500 lb (4,760 kg)
Fuel capacity: 3,660 lb / 551 gal / 1,660 kg
Maximum speed: 340 knots (391 mph)
Cruise speed: 322 knots (370 mph)
Range: 1,290 nm (1,484 miles, 2,388 km)
Service ceiling: 35,000 ft (10,668 m)
Rate of climb: 2,380 ft/min (12.1 m/s)
Takmeoff distance: 4,360 ft (1,329 m)
Landing distance: 3,740 ft (1,140 m)
Fuel burn: 89-106 gph / 600-700 lb/hr
Cessna Citation M2
Crew: 1-2 pilots
Passengers: Up to 6
Length: 42.7 ft (13.02 m)
Wingspan: 47.2 ft (14.38 m)
Height: 14.3 ft (4.36 m)
Maximum takeoff weight: 10,700 lb (4,853 kg)
Fuel capacity: 3,620 lb / 545 gal / 1,642 kg
Cruise speed: 404 knots (or 464 mph)
Range: 1,550 nmi (2,871 km)
Service ceiling: 41,000 ft (12,497 m)
Rate of climb: 3,944 ft/min (20 m/s)
Takeoff distance: 3,210 feet (978 m)
Landing distance: 2,510 ft (765 m)
Fuel burn: Appx. 100 gph / 700 lbs/hr
Cessna Citation CJ3
Crew: 1-2 pilots
Passengers: Up to 6-8
Length: 51.0 ft (15.55 m)
Wingspan: 53.6 ft (16.34 m)
Height: 14.0 ft (4.27 m)
Maximum takeoff weight: 13,870 lb (6,285 kg)
Fuel capacity: 5,208 lb / 2,364 kg
Maximum speed: 416 knots (479 mph)
Cruise speed: 400 knots (460 mph)
Range: 1,875 nm (2,161 miles, 3,478 km)
Service ceiling: 45,000 ft (13,716 m)
Rate of climb: 3,280 ft/min (16.66 m/s)
Takeoff distance: 3,180 ft (969 m)
Landing distance: 2,770 ft (844 m)
Fuel burn: 860 lbs/hr
Cessna Citation CJ4
Crew: 1-2 pilots
Passengers: Up to 6-8
Length: 53.4 ft (16.3 m)
Wingspan: 50.1 ft (15.3 m)
Height: 15.0 ft (4.6 m)
Maximum takeoff weight: 17,110 lb (7,762 kg)
Fuel capacity: 6,775 lb / 3,072 kg
Maximum speed: 451 knotss (519 mph)
Cruise speed: 438 knotss (504 mph)
Range: 2,165 nm (2,491 miles, 4,006 km)
Service ceiling: 45,000 ft (13,716 m)
Rate of climb: 3,623 ft/min (18.4 m/s)
Takeoff distance: 3,410 ft (1,040 m)
Landing distance: 2,810 ft (856 m)
Fuel burn: 1,600 lbs/hr
Beechcraft A36
Passengers: Up to 6 passengers
Length: 27 feet 6 inches (8.38 m)
Wingspan: 33 feet 6 inches (10.21 m)
Height: 8 feet 7 inches (2.62 m)
Maximum Takeoff Weight: 3,650 pounds (1,656 kg)
Maximum Landing Weight: 3,600 pounds (1,633 kg)
Basic Empty Weight: 2,500 pounds (1,134 kg)
One Continental IO-550-BB engine
Horsepower: 300 HP
Maximum Cruise Speed: 176 knotss (202 mph)
Range: 740 nm (851 sm)
Service Ceiling: 18,500 feet (5,639 m)
Takeoff Distance: 1,340 feet (408 m)
Landing Distance: 1,440 feet (439 m)
Maximum Climb Rate: 1,000 ft/min
Beechcraft G36
Length: 27 feet 6 inches (8.38 m)
Wingspan: 33 feet 6 inches (10.21 m)
Height: 8 feet 7 inches (2.62 m)
Maximum Takeoff Weight: 3,650 pounds (1,656 kg)
Maximum Landing Weight: 3,600 pounds (1,633 kg)
Basic Empty Weight: 2,560 pounds (1,161 kg)
One Continental IO-550-B engine
Horsepower: 300 HP
Maximum Cruise Speed: 176 knots (202 mph)
Range: 920 nm (1,059 sm, 1,706 km)
Service Ceiling: 18,500 feet (5,639 m)
Takeoff Distance: 1,340 feet (408 m)
Landing Distance: 1,440 feet (439 m)
Maximum Climb Rate: 1,200 ft/min (366 mpm)
Beechcraft B55 Baron
Coming
Beechcraft B58 Baron
Crew: 1-2 pilots
Passengers: Up to 6-8
Length: 29 feet 2 inches (8.89 m)
Wingspan: 37 feet 10 inches (11.53 m)
Height: 9 feet 7 inches (2.92 m)
Maximum Takeoff Weight: 5,400 pounds (2,449 kg)
Maximum Landing Weight: 5,400 pounds (2,449 kg)
Basic Empty Weight: 3,470 pounds (1,575 kg)
Two Continental IO-550-C engines
Horsepower: 300 HP each
Maximum Cruise Speed: 200 knots (230 mph)
Range: 1,444 nm (1,663 sm)
Service Ceiling: 19,700 feet (5,997 m)
Takeoff Distance: 2,348 feet (716 m)
Landing Distance: 1,900 feet (579 m)
Maximum Climb Rate: 1,850 ft/min (564 mpm)
Beechcraft King Air A200
Coming
Beechcraft King Air B200
Coming
Beechcraft King Air 350i
Coming
Beechcraft King Air C90
Coming
Beechcraft Premier 1
Crew: 1-2 pilots
Passengers: Up to 8
Length: 46 feet 10 inches (14.27 m)
Wingspan: 44 feet 6 inches (13.56 m)
Height: 15 feet (4.57 m)
Maximum Takeoff Weight: 12,500 pounds (5,670 kg)
Maximum Landing Weight: 11,700 pounds (5,307 kg)
Maximum Zero Fuel Weight: 10,800 pounds (4,899 kg)
Basic Empty Weight: 7,759 pounds (3,518 kg)
Fuel Capacity: 3,670 lb / 1,665 kg
Engine: 2 × Williams FJ44-2A Turbofan
Thrust: 2,300 lb
Maximum Cruise Speed: 460 knots (529 mph)
Maximum Range: 1,500 nm (1,726 sm)
Service Ceiling: 41,000 feet (12,497 m)
Takeoff Distance: 3,792 feet (1,156 m)
Landing Distance: 3,000 feet (914 m)
Maximum Climb Rate: 3,210 fmp (976 mmp)
Fuel burn: 160 gph
Beechcraft Premier 1a
Crew: 1-2 pilots
Passengers: Up to 8
Length: 46 feet 10 inches (14.27 m)
Wingspan: 44 feet 6 inches (13.56 m)
Height: 15 feet (4.57 m)
Maximum Takeoff Weight: 12,500 pounds (5,670 kg)
Maximum Landing Weight: 11,700 pounds (5,307 kg)
Maximum Zero Fuel Weight: 10,800 pounds (4,899 kg)
Basic Empty Weight: 7,759 pounds (3,518 kg)
Fuel Capacity: 3,670 lb / 1,665 kg
Engine: 2 × Williams FJ44-2A Turbofan
Thrust: 2,300 lb
Maximum Cruise Speed: 465 knots (529 mph)
Maximum Range: 1,500 nm (1,726 sm, 2,778 km)
Service Ceiling: 41,000 feet (12,497 m)
Takeoff Distance: 3,792 feet (1,156 m)
Landing Distance: 3,000 feet (914 m)
Maximum Climb Rate: 3,210 ft/min (976 mpm)
Fuel burn: 160 gph
Cirrus SR22
Crew: 1 pilot
Passengers: Up to 5
Length: 26 feet (7.92 meters)
Wingspan: 38 feet 4 inches (11.68 meters)
Height: 8 feet 11 inches (2.72 meters)
Seating Capacity: Up to 4 or 5 passengers
Cabin Length: 10 feet 9 inches (3.28 meters)
Cabin Width: 4 feet 1 inch (1.24 meters)
Cabin Height: 4 feet 2 inches (1.27 meters)
Baggage Capacity: 31 cubic feet (0.88 cubic meters)
Maximum Takeoff Weight: 3,600 pounds (1,633 kilograms)
Basic Empty Weight: 2,450 pounds (1,111 kilograms)
Engine: Continental IO-550-N engine
Horsepower: 310 HP
Maximum Cruise Speed: 183 knots (211 mph)
Range: Approximately 1,073 nm (1,234 sm)
Service Ceiling: 17,500 feet (5,334 m)
Takeoff Distance: 1,050 feet (320 meters)
Landing Distance: 1,340 feet (408 meters)
Maximum Climb Rate: 1,200 ft/min (366 mpm)
Cirrus SR22-G2
Crew: 1 pilot
Passengers: Up to 5
Length: 26 feet (7.92 meters)
Wingspan: 38 feet 4 inches (11.68 meters)
Height: 8 feet 11 inches (2.72 meters)
Seating Capacity: Up to 4 or 5 passengers
Cabin Length: 10 feet 9 inches (3.28 meters)
Cabin Width: 4 feet 1 inch (1.24 meters)
Cabin Height: 4 feet 2 inches (1.27 meters)
Baggage Capacity: 31 cubic feet (0.88 cubic meters)
Maximum Takeoff Weight: 3,050 pounds (1,383 kilograms)
Basic Empty Weight: 2,200 pounds (998 kilograms)
Engine: Continental IO-550-N engine
Horsepower: 310 HP
Maximum Cruise Speed: 183 knots (211 mph)
Range: Approximately 1,073 nm (1,234 sm)
Service Ceiling: 17,500 feet (5,334 m)
Takeoff Distance: 1,115 feet (340 m)
Landing Distance: 1,460 feet (445 m)
Maximum Climb Rate: 1,200 ft/min (366 mpm)
Cirrus SR22-G3
Crew: 1 pilot
Passengers: Up to 5
Length: 26 feet (7.92 meters)
Wingspan: 38 feet 4 inches (11.68 meters)
Height: 8 feet 11 inches (2.72 meters)
Seating Capacity: Up to 4 or 5 passengers
Cabin Length: 10 feet 9 inches (3.28 meters)
Cabin Width: 4 feet 1 inch (1.24 meters)
Cabin Height: 4 feet 2 inches (1.27 meters)
Baggage Capacity: 31 cubic feet (0.88 cubic meters)
Maximum Takeoff Weight: 3,400 pounds (1,542 kilograms)
Basic Empty Weight: 2,405 pounds (1,091 kilograms)
Engine: Continental IO-550-N engine
Horsepower: 310 HP
Maximum Cruise Speed: 183 knots (211 mph)
Range: Approximately 1,070 nm (1,230 sm)
Service Ceiling: 17,500 feet (5,334 m)
Takeoff Distance: 1,050 feet (320 m)
Landing Distance: 1,340 feet (408 m)
Maximum Climb Rate: 1,200 ft/min (366 mpm)
Cirrus SF50
Crew: 1-2 pilots
Passengers: Up to 6
Length: 30 feet 7 inches (9.32 meters)
Wingspan: 38 feet 7 inches (11.76 meters)
Height: 10 feet 2 inches (3.10 meters)
Seating Capacity: Up to 7 passengers (incl 1 pilot)
Cabin Length: 11 feet 4 inches (3.45 meters)
Cabin Width: 5 feet 1 inch (1.55 meters)
Cabin Height: 4 feet 2 inches (1.27 meters)
Baggage Capacity: 30 cubic feet (0.85 cubic meters)
Maximum Takeoff Weight: 6,000 pounds (2,722 kilograms)
Basic Empty Weight: 3,600 pounds (1,633 kilograms)
Engine: One Williams International FJ33-5A turbofan engine
Thrust: 1,800 pounds
Maximum Cruise Speed: 345 knots (397 mph)
Maximum Range: Approximately 1,200 nm (1,381 sm)
Maximum Operating Altitude: 28,000 feet (8,534 m)
Takeoff Distance: 2,036 feet (621 m)
Landing Distance: 2,244 feet (684 m)
Maximum Climb Rate: 1,540 ft/min (469 mpm)
Diamond DA40
Four-seat, single-engine light aircraft
First Flight: November 1997
Wingspan: 39.4 feet (12 m)
Length: 26.5 feet (8.1 m)
Height: 6.6 feet (2 m)
Wing Area: 145.3 sq. feet (13.5 m²)
Empty Weight: Typically around 1,543 lbs (700 kg), but can vary with specific versions and equipment.
Max Takeoff Weight (MTOW): 2,645 lbs (1,200 kg)
Engine: Typically powered by a Lycoming IO-360-M1A engine
Horsepower: 180 hp
Cruise Speed: Approx 147 knots (170 mph or 273 km/h) at 80% power.
Stall Speed (flaps down, power off): Around 49 knots (56 mph or 91 km/h)
Range: Approx 600 nautical miles (690 miles or 1,110 km) with reserves.
Rate of Climb: Approx 1,200 feet per minute (fpm) at sea level.
Service Ceiling: About 16,400 feet (5,000 m)
Fuel Capacity: Around 50 gallons (190 liters) depending on the specific variant.
Avionics: Most newer DA40 models come equipped with the Garmin G1000 NXi integrated flight deck, but older models might have different avionics setups.
Diamond DA42
Role: Four-seat, twin-engine light aircraft
First Flight: 9 January 2002
Wingspan: 44.3 feet (13.5 m)
Length: 28.2 feet (8.6 m)
Height: 8.2 feet (2.5 m)
Wing Area: 175.5 sq. feet (16.3 m²)
Empty Weight: Typically around 3,119 lbs (1,415 kg) for the DA42-VI variant, but can vary with specific versions and equipment.
Max Takeoff Weight (MTOW): 4,189 lbs (1,900 kg) for the DA42-VI variant.
Engine: Typically powered by two Austro AE300 turbocharged diesel engines, though earlier versions used Thielert engines.
Horsepower: 168 hp each for the Austro AE300 engines.
Performance (data for DA42-VI variant with Austro engines):
Cruise Speed: Approx 173 knots (199 mph or 320 km/h) at 92% power.
Stall Speed (flaps down, power off): Around 57 knots (66 mph or 106 km/h)
Range: Approx 1,200 nautical miles (1,380 miles or 2,220 km) with reserves.
Rate of Climb: Approx 1,400 feet per minute (fpm) at sea level.
Service Ceiling: About 18,000 feet (5,486 m)
Fuel Capacity: Around 76.4 gallons (289 liters) for the DA42-VI variant.
Avionics: Typically equipped with the Garmin G1000 NXi integrated flight deck.
Keep in mind that these specifications and performance numbers are for general reference.
Diamond DA62
Manufacturer: Diamond Aircraft
Role: Five to seven-seat, twin-engine light aircraft
First Flight: April 2012
Wingspan: 47.8 feet (14.55 m)
Length: 30.9 feet (9.42 m)
Height: 8.5 feet (2.6 m)
Empty Weight: Typically around 3,461 lbs (1,570 kg), but can vary with specific configurations and equipment.
Max Takeoff Weight (MTOW): 5,071 lbs (2,300 kg)
Engine: Powered by two Austro AE330 turbocharged diesel engines.
Horsepower: 180 hp each
Cruise Speed: Approx 197 knots (227 mph or 365 km/h) at 80% power.
Stall Speed (full flaps, power off): Around 60 knots (69 mph or 111 km/h)
Range: Approx 1,283 nautical miles (1,476 miles or 2,376 km) with reserves.
Rate of Climb: Approx 1,520 feet per minute (fpm) at sea level.
Service Ceiling: About 20,000 feet (6,096 m)
Fuel Capacity: Around 86.2 gallons (326 liters).
Avionics: Typically equipped with the Garmin G1000 NXi integrated flight deck.
Seating: Two front seats, a middle row of up to three seats, and an optional third row for two more seats, making it a 5-7 seater depending on the configuration.
Embraer Phenom 100
Crew: 1-2 pilots
Passengers: Up to 6
Length: 42 feet 2 inches (12.85 meters)
Wingspan: 40 feet 4 inches (12.29 meters)
Height: 14 feet 3 inches (4.35 meters)
Seating Capacity: Up to 4 or 5 passengers (incl 1 or 2 pilots)
Cabin Length: 11 feet (3.35 meters)
Cabin Width: 5 feet 1 inch (1.55 meters)
Cabin Height: 4 feet 11 inches (1.50 meters)
Baggage Capacity: 70 cubic feet (1.98 cubic meters)
Maximum Takeoff Weight: 10,472 pounds (4,750 kilograms)
Maximum Landing Weight: 10,251 pounds (4,650 kilograms)
Basic Empty Weight: 7,160 pounds (3,250 kilograms)
Two Pratt & Whitney Canada PW617F-E turbofan engines
Thrust: 1,695 pounds each
Maximum Cruise Speed: 380 knots (437 mph)
Maximum Range: 1,178 nautical miles (1,356 sm)
Service Ceiling: 41,000 feet (12,497 m)
Takeoff Distance: 3,125 feet (953 m)
Landing Distance: 2,430 feet (741 m)
Maximum Climb Rate: 3,622 ft/min (1,104 mpm)
Embraer Phenom 300
Crew: 1-2 pilots
Passengers: Up to 8
Length: 51 feet 2 inches (15.59 meters)
Wingspan: 52 feet 2 inches (15.90 meters)
Height: 16 feet 11 inches (5.16 meters)
Seating Capacity: Up to 6 to 10 passengers (incl 1 or 2 pilots)
Cabin Length: 17 feet 2 inches (5.23 meters)
Cabin Width: 5 feet 1 inch (1.55 meters)
Cabin Height: 4 feet 11 inches (1.50 meters)
Baggage Capacity: 74 cubic feet (2.09 cubic meters)
Maximum Takeoff Weight: 17,968 pounds (8,150 kilograms)
Maximum Landing Weight: 17,968 pounds (8,150 kilograms)
Basic Empty Weight: 14,890 pounds (6,750 kilograms)
Two Pratt & Whitney Canada PW535E1 turbofan engines
Thrust: 3,360 pounds each
Maximum Cruise Speed: 453 knots (521 mpm)
Maximum Range: 2,268 nm (2,610 sm)
Service Ceiling: 45,000 feet (13,716 m)
Takeoff Distance: 3,138 feet (956 m)
Landing Distance: 2,621 feet (799 m)
Maximum Climb Rate: 3,306 ft/min (1,008 mpm)
Embraer Praetor 500
Crew: 2 pilots
Passengers: Up to 8
Length: 55 feet 7 inches (16.94 meters)
Wingspan: 67 feet 9 inches (20.65 meters)
Height: 20 feet 1 inch (6.12 meters)
Seating Capacity: Up to 8 passengers (incl 1 or 2 pilots)
Cabin Length: 23 feet 5 inches (7.14 meters)
Cabin Width: 6 feet 10 inches (2.08 meters)
Cabin Height: 5 feet 9 inches (1.75 meters)
Baggage Capacity: 155 cubic feet (4.39 cubic meters)
Maximum Takeoff Weight: 31,019 pounds (14,070 kilograms)
Basic Operating Weight: 21,170 pounds (9,605 kilograms)
Two Pratt & Whitney Canada PW545E turbofan engines
Thrust: 6,540 pounds each
Maximum Cruise Speed: 466 knots (536 mph)
Maximum Range: 3,340 nm (3,842 sm)
Service Ceiling: 45,000 feet (13,716 m)
Takeoff Distance: 4,222 feet (1,287 m)
Landing Distance: 2,595 feet (791 m)
Maximum Climb Rate: 3,650 ft/min (1,112 mpm)
Embraer Praetor 600
Crew: 2 pilots
Length: 55 feet 9 inches (17 meters)
Wingspan: 67 feet 9 inches (20.65 meters)
Height: 20 feet 1 inch (6.12 meters)
Seating Capacity: Up to 9 passengers (incl 1 or 2 pilots)
Cabin Length: 26 feet 3 inches (8 meters)
Cabin Width: 6 feet 10 inches (2.08 meters)
Cabin Height: 6 feet (1.83 meters)
Baggage Capacity: 155 cubic feet (4.39
Maximum Takeoff Weight: 41,196 pounds (18,700 kilograms)
Basic Operating Weight: 27,890 pounds (12,655 kilograms)
Two Pratt & Whitney Canada PW610F-A turbofan engines
Thrust: 7,528 pounds each
Maximum Cruise Speed: 466 knots (536 mph)
Maximum Range: 4,018 nm (4,619 sm, 7,435 kilometers)
Service Ceiling: 45,000 feet (13,716 m)
Takeoff Distance: 4,222 feet (1,287 m)
Landing Distance: 2,930 feet (893 m)
Maximum Climb Rate: 3,650 ft/min (1,112 mpm)
Gulfstream G450
Crew: 2 pilots
Length: 88 feet 4 inches (26.92 meters)
Wingspan: 77 feet 10 inches (23.72 meters)
Height: 25 feet 2 inches (7.67 meters)
Seating Capacity: Up to 14 passengers (incl 2 pilots)
Cabin Length: 45 feet 1 inch (13.74 meters)
Cabin Width: 7 feet 4 inches (2.24 meters)
Cabin Height: 6 feet 2 inches (1.88 meters)
Baggage Capacity: 169 cubic feet (4.78 cubic meters)
Maximum Takeoff Weight: 74,600 pounds (33,838 kilograms)
Basic Operating Weight: 48,800 pounds (22,134 kilograms)
Two Rolls-Royce Tay 611-8C turbofan engines
Thrust: 13,850 pounds each
Maximum Cruise Speed: Mach 0.88 (514 knots, 590 mph)
Maximum Range: 4,350 nm (5,006 sm)
Service Ceiling: 45,000 feet (13,716 meters)
Takeoff Distance: 5,910 feet (1,801 meters)
Landing Distance: 2,770 feet (844 meters)
Maximum Climb Rate: 4,330 fmp (1,320 meters per minute)
Gulfstream G4-SP
Crew: 2 pilots
Length: 88 feet 4 inches (26.92 meters)
Wingspan: 77 feet 10 inches (23.72 meters)
Height: 25 feet 2 inches (7.67 meters)
Seating Capacity: Up to 14 passengers (incl 2 pilots)
Cabin Length: 45 feet 1 inch (13.74 meters)
Cabin Width: 7 feet 4 inches (2.24 meters)
Cabin Height: 6 feet 2 inches (1.88 meters)
Baggage Capacity: 169 cubic feet (4.78 cubic meters)
Maximum Takeoff Weight: 74,600 pounds (33,838 kilograms)
Basic Operating Weight: 48,800 pounds (22,134 kilograms)
Two Rolls-Royce Tay 611-8C turbofan engines
Thrust: 13,850 pounds each
Maximum Cruise Speed: Mach 0.88 (514 knots, 590 mph)
Maximum Range: 4,350 nm (5,006 sm)
Service Ceiling: 45,000 feet (13,716 meters)
Takeoff Distance: 5,910 feet (1,801 meters)
Landing Distance: 2,770 feet (844 meters)
Maximum Climb Rate: 4,330 fmp (1,320 mpm)
Gulfstream G5
Crew: 2 pilots
Length: 96 feet 5 inches (29.39 meters)
Wingspan: 93 feet 6 inches (28.50 meters)
Height: 25 feet 10 inches (7.87 meters)
Seating Capacity: Up to 19 passengers (incl 2 pilots)
Cabin Length: 43 feet 11 inches (13.39 meters)
Cabin Width: 7 feet 4 inches (2.24 meters)
Cabin Height: 6 feet 2 inches (1.88 meters)
Baggage Capacity: 170 cubic feet (4.81 cubic meters)
Maximum Takeoff Weight: 90,500 pounds (41,045 kilograms)
Basic Operating Weight: 49,000 pounds (22,226 kilograms)
Two Rolls-Royce Tay 611-8 turbofan engines
Thrust: Approximately 13,850 pounds each
Maximum Cruise Speed: Mach 0.88 (513 knots, 590 mph)
Maximum Range: 5,760 nm (6,630 sm)
Service Ceiling: 51,000 feet (15,545 meters)
Takeoff Distance: 5,910 feet (1,801 meters)
Landing Distance: 2,770 feet (844 meters)
Maximum Climb Rate: 3,810 fmp (1,161 mpm)
Gulfstream G550
Crew: 2 pilots
Length: 96 feet 5 inches (29.39 meters)
Wingspan: 93 feet 6 inches (28.50 meters)
Height: 25 feet 10 inches (7.87 meters)
Seating Capacity: Up to 19 passengers (incl 2 pilots)
Cabin Length: 43 feet 11 inches (13.39 meters)
Cabin Width: 7 feet 4 inches (2.24 meters)
Cabin Height: 6 feet 2 inches (1.88 meters)
Baggage Capacity: 170 cubic feet (4.81 cubic meters)
Maximum Takeoff Weight: 91,000 pounds (41,277 kilograms)
Basic Operating Weight: 54,500 pounds (24,721 kilograms)
Two Rolls-Royce BR710-C4-11 turbofan engines
Thrust: 15,385 pounds each
Maximum Cruise Speed: Mach 0.885 (516 knots, 593 mph)
Maximum Range: 6,750 nm (7,775 sm)
Service Ceiling: 51,000 feet (15,545 meters)
Takeoff Distance: 5,910 feet (1,801 meters)
Landing Distance: 2,770 feet (844 meters)
Maximum Climb Rate: 3,500 fmp (1,067 mpm)
Hawker 400
Coming
Hawker 800
Coming
HondaJet HA420
Length: 42 feet 7 inches (12.98 meters)
Wingspan: 39 feet 8 inches (12.10 meters)
Height: 14 feet 9 inches (4.50 meters)
Maximum Takeoff Weight: 9,200 pounds (4,173 kilograms)
Basic Operating Weight: 7,020 pounds (3,179 kilograms)
Two GE Honda HF120 turbofan engines
Thrust: 2,050 pounds each
Seating Capacity: Up to 5 to 6 passengers (incl 1 or 2 pilots)
Cabin Length: 17 feet 9 inches (5.41 meters)
Cabin Width: 5 feet (1.52 meters)
Cabin Height: 4 feet 9 inches (1.45 meters)
Baggage Capacity: 66 cubic feet
Maximum Cruise Speed: 422 knots (486 mph)
Maximum Range: 1,223 nm (1,409 sm)
Service Ceiling: 43,000 feet (13,106 meters)
Takeoff Distance: 3,130 feet (954 meters)
Landing Distance: 2,699 feet (823 meters)
Maximum Climb Rate: 4,125 fpm
HondaJet Elite
Length: 42 feet 7 inches (12.98 meters)
Wingspan: 39 feet 8 inches (12.10 meters)
Height: 14 feet 9 inches (4.50 meters)
Maximum Takeoff Weight: 10,500 pounds (4,760 kilograms)
Basic Operating Weight: 7,625 pounds (3,461 kilograms)
Two GE Honda HF120 turbofan engines
Thrust: 2,050 pounds each
Seating Capacity: Up to 5 to 6 passengers (incl 1 or 2 pilots)
Cabin Length: 17 feet 9 inches (5.41 meters)
Cabin Width: 5 feet (1.52 meters)
Cabin Height: 4 feet 9 inches (1.45 meters)
Baggage Capacity: 66 cubic feet
Maximum Cruise Speed: 430 knots (496 mph)
Maximum Range: 1,437 nm (1,654 sm)
Service Ceiling: 43,000 feet (13,106 meters)
Takeoff Distance: 3,180 feet (969 meters)
Landing Distance: 3,260 feet (994 meters)
Maximum Climb Rate: 4,080 fpm
HondaJet Elite II
Crew: 1-2 pilots
Length: 42 feet 7 inches (12.98 meters)
Wingspan: 39 feet 8 inches (12.10 meters)
Height: 14 feet 9 inches (4.50 meters)
Maximum Takeoff Weight: 11,000 pounds (4,989 kilograms)
Two GE Honda HF120 turbofan engines
Thrust: 2,050 pounds each
Seating Capacity: Up to 5 to 6 passengers (incl 1 or 2 pilots)
Cabin Length: 17 feet 9 inches (5.41 meters)
Cabin Width: 5 feet (1.52 meters)
Cabin Height: 4 feet 9 inches (1.45 meters)
Baggage Capacity: 62 cubic feet
Maximum Cruise Speed: 422 knots (485 mph)
Maximum Range: 1,547 nm (1,654 sm)
Service Ceiling: 43,000 feet (13,106 meters)
Takeoff Distance: 3,699 feet (1,127 meters)
Landing Distance: 2,717 feet (828 meters)
Maximum Climb Rate: 4,080 fpm
Learjet 35
Crew: 2 pilots
Length: 48 feet 8 inches (14.83 meters)
Wingspan: 39 feet 6 inches (12.04 meters)
Height: 12 feet 3 inches (3.73 meters)
Maximum Takeoff Weight: 18,300 pounds (8,301 kilograms)
Empty Weight: 11,850 pounds (5,369 kilograms)
Two Garrett TFE731-2 turbofan engines
Thrust: 3,500 pounds each
Seating Capacity: Up to 8 passengers (incl 2 pilots)
Cabin Length: 12 feet 9 inches (3.89 meters)
Cabin Width: 4 feet 9 inches (1.45 meters)
Cabin Height: 4 feet 4 inches (1.32 meters)
Baggage Capacity: 40 cubic feet
Maximum Cruise Speed: Mach 0.81 (470 knots / 541 mph)
Maximum Range: 1,800 nm (2,070 sm)
Service Ceiling: 51,000 feet (15,545 meters)
Takeoff Distance: 5,030 feet (1,533 meters)
Landing Distance: 3,540 feet (1,079 meters)
Maximum Climb Rate: 6,000 fpm
Learjet 40
Crew: 2 pilots
Length: 57 feet 2 inches (17.43 meters)
Wingspan: 43 feet 9 inches (13.34 meters)
Height: 14 feet 8 inches (4.47 meters)
Maximum Takeoff Weight: 20,500 pounds (9,299 kilograms)
Empty Weight: 13,950 pounds (6,328 kilograms)
Two Honeywell TFE731-20AR turbofan engines
Thrust: 3,850 pounds each
Seating Capacity: Up to 6 to 8 passengers (incl 2 pilots)
Cabin Length: 17 feet 8 inches (5.38 meters)
Cabin Width: 5 feet 1 inch (1.55 meters)
Cabin Height: 4 feet 11 inches (1.50 meters)
Baggage Capacity: 50 cubic feet
Maximum Cruise Speed: Mach 0.81 (465 knots / 535 mph)
Maximum Range: 1,740 nm (2,003 sm)
Service Ceiling: 51,000 feet (15,545 meters)
Takeoff Distance: 5,090 feet (1,551 meters)
Landing Distance: 2,825 feet (861 meters)
Maximum Climb Rate: 5,000 fpm
Learjet 45
Crew: 2 pilots
Length: 58 feet 10 inches (17.94 meters)
Wingspan: 47 feet 9 inches (14.55 meters)
Height: 14 feet 11 inches (4.55 meters)
Maximum Takeoff Weight: 21,500 pounds (9,752 kilograms)
Empty Weight: 13,500 pounds (6,124 kilograms)
Two Honeywell TFE731-20AR turbofan engines
Thrust: 3,850 pounds each
Seating Capacity: Up to 8 passengers (including 2 pilots)
Cabin Length: 19 feet 10 inches (6.04 meters)
Cabin Width: 5 feet 1 inch (1.55 meters)
Cabin Height: 4 feet 11 inches (1.50 meters)
Baggage Capacity: 50 cubic feet
Maximum Cruise Speed: Mach 0.81 (465 knots / 535 mph)
Maximum Range: 1,824 nm (2,100 sm)
Service Ceiling: 51,000 feet (15,545 meters)
Takeoff Distance: 4,600 feet (1,402 meters)
Landing Distance: 2,640 feet (805 meters)
Maximum Climb Rate: 6,000 fpm
Learjet 55
Crew: 2 pilots
Length: 55 feet 5 inches (16.89 meters)
Wingspan: 43 feet 10 inches (13.36 meters)
Height: 12 feet 3 inches (3.73 meters)
Maximum Takeoff Weight: 21,500 pounds (9,752 kilograms)
Empty Weight: 12,600 pounds (5,715 kilograms)
Two Garrett TFE731-3A-2B turbofan engines
Thrust: 3,700 pounds each
Seating Capacity: Up to 8 passengers (incl 2 pilots)
Cabin Length: 17 feet 7 inches (5.36 meters)
Cabin Width: 5 feet 10 inches (1.78 meters)
Cabin Height: 5 feet 9 inches (1.75 meters)
Baggage Capacity: Approximately 50 cubic feet
Maximum Cruise Speed: Mach 0.81 (465 knots / 535 mph)
Maximum Range: 2,000 nm (2,300 sm)
Service Ceiling: 51,000 feet (15,545 meters)
Takeoff Distance: 4,860 feet (1,481 meters)
Landing Distance: 3,320 feet (1,012 meters)
Maximum Climb Rate: 3,700 fpm
Learjet 60
Crew: 2 pilots
Length: 58 feet 7 inches (17.86 meters)
Wingspan: 43 feet 9 inches (13.34 meters)
Height: 14 feet 8 inches (4.47 meters)
Maximum Takeoff Weight: 23,500 pounds (10,659 kilograms)
Empty Weight: 14,640 pounds (6,642 kilograms)
Two Pratt & Whitney Canada PW305A turbofan engines
Thrust: 4,600 pounds each
Seating Capacity: Up to 7 to 9 passengers (incl 2 pilots)
Cabin Length: 17 feet 8 inches (5.38 meters)
Cabin Width: 5 feet 11 inches (1.80 meters)
Cabin Height: 5 feet 7 inches (1.70 meters)
Baggage Capacity: 48 cubic feet
Maximum Cruise Speed: Mach 0.81 (466 knots / 537 mph)
Maximum Range: 2,300 nautical miles (2,645 statute miles, 4,259 kilometers)
Service Ceiling: 51,000 feet (15,545 meters)
Takeoff Distance: 5,090 feet (1,551 meters)
Landing Distance: 3,110 feet (948 meters)
Maximum Climb Rate: 6,000 fpm
Learjet 75
Crew: 2 pilots
Length: 58 feet 0 inches (17.68 meters)
Wingspan: 43 feet 9 inches (13.34 meters)
Height: 14 feet 1 inch (4.29 meters)
Maximum Takeoff Weight: 21,500 pounds (9,752 kilograms)
Empty Weight: Approximately 13,990 pounds (6,349 kilograms
Two Honeywell TFE731-40BR turbofan engines
Thrust: 3,850 pounds each
Seating Capacity: Up to 8 passengers (incl 2 pilots)
Cabin Length: 19 feet 10 inches (6.04 meters)
Cabin Width: 5 feet 1 inch (1.55 meters)
Cabin Height: 4 feet 11 inches (1.50 meters)
Baggage Capacity: 50 cubic fee
Maximum Cruise Speed: Mach 0.81 (465 knots / 535 mph)
Maximum Range: 2,040 nm (2,347 sm)
Service Ceiling: 51,000 feet (15,545 meters)
Takeoff Distance: 4,440 feet (1,353 meters)
Landing Distance: 2,930 feet (893 meters)
Maximum Climb Rate: 4,420 fpm
Pilatus PC 12/45
Crew: 1 pilot
Length: 47 feet 3 inches (14.40 meters)
Wingspan: 53 feet 3 inches (16.23 meters)
Height: 14 feet 4 inches (4.37 meters)
Maximum Takeoff Weight: 10,450 pounds (4,740 kilograms)
Empty Weight: Approximately 6,254 pounds (2,836 kilograms)
Pratt & Whitney Canada PT6A-67P turboprop engine
Rated Power: 1,200 horsepower
Seating Capacity: Up to 9 passengers (incl 1 or 2 pilots)
Cabin Length: 16 feet 11 inches (5.16 meters)
Cabin Width: 5 feet (1.52 meters)
Cabin Height: 4 feet 10 inches (1.47 meters)
Baggage Capacity: 40 cubic feet
Maximum Cruise Speed: 285 knots (327 mph)
Maximum Range: 1,800 nm (2,071 sm, 3,333 kilometers)
Service Ceiling: 30,000 feet (9,144 meters)
Takeoff Distance: 2,650 feet (808 meters)
Landing Distance: 2,280 feet (695 meters)
Maximum Climb Rate: 1,920
Pilatus PC 12NG
Crew: 1 pilot
Length: 47 feet 3 inches (14.40 meters)
Wingspan: 53 feet 3 inches (16.23 meters)
Height: 14 feet 4 inches (4.37 meters)
Maximum Takeoff Weight: 10,450 pounds (4,740 kilograms)
Empty Weight: Approximately 6,254 pounds (2,836 kilograms)
Pratt & Whitney Canada PT6A-67P turboprop engine
Rated Power: 1,200 horsepower
Seating Capacity: Up to 9 passengers (incl 1 or 2 pilots)
Cabin Length: 16 feet 11 inches (5.16 meters)
Cabin Width: 5 feet (1.52 meters)
Cabin Height: 4 feet 10 inches (1.47 meters)
Baggage Capacity: 40 cubic feet
Maximum Cruise Speed: 285 knots (327 mph)
Maximum Range: 1,800 nm (2,071 sm)
Service Ceiling: 30,000 feet (9,144 meters)
Takeoff Distance: 2,650 feet (808 meters)
Landing Distance: 2,280 feet (695 meters)
Maximum Climb Rate: 1,920 fpm
Pilatus PC 24
Crew: 1 or 2 pilots
Length: 55 feet 11 inches (17.05 meters)
Wingspan: 55 feet 9 inches (17.00 meters)
Height: 17 feet 0 inches (5.18 meters)
Maximum Takeoff Weight: 17,650 pounds (8,000 kilograms)
Empty Weight: Approximately 10,450 pounds (4,740 kilograms)
Two Williams International FJ44-4A turbofan engines
Thrust: 3,400 pounds each
Seating Capacity: Up to 11 passengers (including 1 or 2 pilots)
Cabin Length: 23 feet 7 inches (7.19 meters)
Cabin Width: 5 feet 7 inches (1.70 meters)
Cabin Height: 5 feet 1 inch (1.55 meters)
Baggage Capacity: 90 cubic feet
Maximum Cruise Speed: 440 knots (506 mph)
Maximum Range: 2,035 nm (2,342 sm)
Maximum Operating Altitude: 45,000 feet (13,716 meters)
Takeoff Distance: 2,690 feet (820 meters)
Landing Distance: 2,525 feet (770 meters)
Maximum Climb Rate: 4,070 fpm
