| Pilots and passengers | |
|---|---|
| Typical Passenger Capacity | 14 |
| Maximum Passenger Capacity | 18 |
| Single Pilot | No |
| External dimensions | |
|---|---|
| Length | 29.38 m |
| Height | 7.86 m |
| Wingspan | 28.5 m |
| External dimensions | |
|---|---|
| Length | 96.4 ft |
| Height | 25.8 ft |
| Wingspan | 93.5 ft |
| External dimensions | |
|---|---|
| Length | 29.38 m |
| Height | 7.86 m |
| Wingspan | 28.5 m |
| Cabin dimensions | |
|---|---|
| Length | 13.38 m |
| Height | 1.89 m |
| Width | 2.23 m |
| Flat Floor | Yes |
| Cabin dimensions | |
|---|---|
| Length | 43.9 ft |
| Height | 6.2 ft |
| Width | 7.3 ft |
| Flat Floor | Yes |
| Cabin dimensions | |
|---|---|
| Length | 13.38 m |
| Height | 1.89 m |
| Width | 2.23 m |
| Flat Floor | Yes |
| Luggage capacity | |
|---|---|
| Internal Baggage Volume | 6400 L |
| Internal Baggage Weight | 1134 kg |
| External Baggage Volume | - L |
| External Baggage Weight | - kg |
| Luggage capacity | |
|---|---|
| Internal Baggage Volume | 226 ft³ |
| Internal Baggage Weight | 2500 lb |
| External Baggage Volume | - ft³ |
| External Baggage Weight | - lb |
| Luggage capacity | |
|---|---|
| Internal Baggage Volume | 6400 L |
| Internal Baggage Weight | 1134 kg |
| External Baggage Volume | - L |
| External Baggage Weight | - kg |
| Engines | |
|---|---|
| Number | 2 |
| Manufacturer | Rolls-Royce |
| Model | BR 710A1-10 |
| Thrust | 14750 lb |
| TBO | On Condition |
| Flat Rating | ISA+20ºC |
| Weights and limits | |
|---|---|
| Maximum Takeoff Weight | 41050 kg |
| Maximum Payload | 2767 kg |
| Maximum Fuel Capacity | 18595 kg |
| Payload with Full Fuel | 683 kg |
| Maximum Operating Speed | Mach 0.89 |
| Cabin Pressure Differential | 10.2 psi |
| Weights and limits | |
|---|---|
| Maximum Takeoff Weight | 90500 lb |
| Maximum Payload | 6100 lb |
| Maximum Fuel Capacity | 40994 lb |
| Payload with Full Fuel | 1506 lb |
| Maximum Operating Speed | Mach 0.89 |
| Cabin Pressure Differential | 10.2 psi |
| Weights and limits | |
|---|---|
| Maximum Takeoff Weight | 41050 kg |
| Maximum Payload | 2767 kg |
| Maximum Fuel Capacity | 18595 kg |
| Payload with Full Fuel | 683 kg |
| Maximum Operating Speed | Mach 0.89 |
| Cabin Pressure Differential | 10.2 psi |
| Speeds | |
|---|---|
| Long-Range Cruise | 850 km/h |
| High-Speed Cruise | 904 km/h |
| Speeds | |
|---|---|
| Long-Range Cruise | 459 kt |
| High-Speed Cruise | 488 kt |
| Speeds | |
|---|---|
| Long-Range Cruise | 850 km/h |
| High-Speed Cruise | 904 km/h |
| Consumption | |
|---|---|
| Long-Range Cruise | 1179 kg/h |
| High-Speed Cruise | 1433 kg/h |
| Consumption | |
|---|---|
| Long-Range Cruise | 2599 lb/h |
| High-Speed Cruise | 3160 lb/h |
| Consumption | |
|---|---|
| Long-Range Cruise | 1179 kg/h |
| High-Speed Cruise | 1433 kg/h |
| Range | 6425 mn |
| Takeoff Distance - Sea Level | 1862 m |
| Takeoff Distance - Hot and High | 2789 m |
| Landing Distance | 677 m |
| Maximum Operating Altitude | 15545 m |
| Range | 6425 mn |
| Takeoff Distance - Sea Level | 6110 ft |
| Takeoff Distance - Hot and High | 9150 ft |
| Landing Distance | 2220 ft |
| Maximum Operating Altitude | 51000 ft |
| Range | 6425 mn |
| Takeoff Distance - Sea Level | 1862 m |
| Takeoff Distance - Hot and High | 2789 m |
| Landing Distance | 677 m |
| Maximum Operating Altitude | 51000 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. |