| Pilots and passengers | |
|---|---|
| Typical Passenger Capacity | 8 |
| Maximum Passenger Capacity | 10 |
| Single Pilot | Yes |
| External dimensions | |
|---|---|
| Length | 15.61 m |
| Height | 5.09 m |
| Wingspan | 15.91 m |
| External dimensions | |
|---|---|
| Length | 51.2 ft |
| Height | 16.7 ft |
| Wingspan | 52.2 ft |
| External dimensions | |
|---|---|
| Length | 15.61 m |
| Height | 5.09 m |
| Wingspan | 15.91 m |
| Cabin dimensions | |
|---|---|
| Length | 5.24 m |
| Height | 1.49 m |
| Width | 1.55 m |
| Flat Floor | No |
| Cabin dimensions | |
|---|---|
| Length | 17.2 ft |
| Height | 4.9 ft |
| Width | 5.1 ft |
| Flat Floor | No |
| Cabin dimensions | |
|---|---|
| Length | 5.24 m |
| Height | 1.49 m |
| Width | 1.55 m |
| Flat Floor | No |
| Luggage capacity | |
|---|---|
| Internal Baggage Volume | 283 L |
| Internal Baggage Weight | 35 kg |
| External Baggage Volume | 2010 L |
| External Baggage Weight | 260 kg |
| Luggage capacity | |
|---|---|
| Internal Baggage Volume | 10 ft³ |
| Internal Baggage Weight | 77 lb |
| External Baggage Volume | 71 ft³ |
| External Baggage Weight | 573 lb |
| Luggage capacity | |
|---|---|
| Internal Baggage Volume | 283 L |
| Internal Baggage Weight | 35 kg |
| External Baggage Volume | 2010 L |
| External Baggage Weight | 260 kg |
| Engines | |
|---|---|
| Number | 2 |
| Manufacturer | Pratt & Whitney |
| Model | PW 535E |
| Thrust | 3360 lb |
| TBO | 5000h |
| Flat Rating | ISA+15°C |
| Weights and limits | |
|---|---|
| Maximum Takeoff Weight | 8150 kg |
| Maximum Payload | 1096 kg |
| Maximum Fuel Capacity | 2428 kg |
| Payload with Full Fuel | 518 kg |
| Maximum Operating Speed | Mach 0.78 |
| Cabin Pressure Differential | 9.4 psi |
| Weights and limits | |
|---|---|
| Maximum Takeoff Weight | 17968 lb |
| Maximum Payload | 2416 lb |
| Maximum Fuel Capacity | 5353 lb |
| Payload with Full Fuel | 1142 lb |
| Maximum Operating Speed | Mach 0.78 |
| Cabin Pressure Differential | 9.4 psi |
| Weights and limits | |
|---|---|
| Maximum Takeoff Weight | 8150 kg |
| Maximum Payload | 1096 kg |
| Maximum Fuel Capacity | 2428 kg |
| Payload with Full Fuel | 518 kg |
| Maximum Operating Speed | Mach 0.78 |
| Cabin Pressure Differential | 9.4 psi |
| Speeds | |
|---|---|
| Long-Range Cruise | 709 km/h |
| High-Speed Cruise | 822 km/h |
| Speeds | |
|---|---|
| Long-Range Cruise | 383 kt |
| High-Speed Cruise | 444 kt |
| Speeds | |
|---|---|
| Long-Range Cruise | 709 km/h |
| High-Speed Cruise | 822 km/h |
| Consumption | |
|---|---|
| Long-Range Cruise | 343 kg/h |
| High-Speed Cruise | 595 kg/h |
| Consumption | |
|---|---|
| Long-Range Cruise | 757 lb/h |
| High-Speed Cruise | 1312 lb/h |
| Consumption | |
|---|---|
| Long-Range Cruise | 343 kg/h |
| High-Speed Cruise | 595 kg/h |
| Range | 1995 mn |
| Takeoff Distance - Sea Level | 956 m |
| Takeoff Distance - Hot and High | 1514 m |
| Landing Distance | 677 m |
| Maximum Operating Altitude | 13716 m |
| Range | 1995 mn |
| Takeoff Distance - Sea Level | 3138 ft |
| Takeoff Distance - Hot and High | 4967 ft |
| Landing Distance | 2220 ft |
| Maximum Operating Altitude | 45000 ft |
| Range | 1995 mn |
| Takeoff Distance - Sea Level | 956 m |
| Takeoff Distance - Hot and High | 1514 m |
| Landing Distance | 677 m |
| Maximum Operating Altitude | 45000 ft |
| Range |
Passengers: - 4 passengers for aircraft with a range of up to 6.000 nm - 8 passengers for aircraft with a range over 6.000 nm Fuel reserves: NBAA IFR, with an alternate airport at: - 100 nm for FAR Part 23 aircraft - 200 nm for FAR Part 25 aircraft ISA temperature en route. |
| Interior Cabin Height | Measured at the center of the cabin cross-section. |
| Passenger Capacity | For single-pilot aircraft, passenger capacity assumes one pilot. |
| Interior Cabin Length | For jets, measured from the cockpit/cabin partition to the typical location of the lavatory and/or the rearmost passenger seat. |
| Payload | Passengers + fuel. |
| Takeoff Distance - Hot and High | At a 5,000 ft elevation airport and a 25°C temperature (ISA +20°C). |
| Takeoff Distance - Sea Level | At a sea-level airport and a 15°C temperature (ISA). |
| Legacy 600 | Launched in 2003 with a flat floor. In 2008, the aisle between the seats was lowered, increasing the cabin interior height by 5 cm. |
| TBO (Time Between Overhauls) | Aircraft with two TBO numbers have Williams engines, which have a longer interval when enrolled in the manufacturer’s engine program. |
| Flat Rating | Maximum temperature at which maximum engine power is maintained without degradation. |