| Pilots and passengers | |
|---|---|
| Typical Passenger Capacity | 13 |
| Maximum Passenger Capacity | 14 |
| Single Pilot | No |
| External dimensions | |
|---|---|
| Length | 26.33 m |
| Height | 6.77 m |
| Wingspan | 21 m |
| External dimensions | |
|---|---|
| Length | 86.4 ft |
| Height | 22.2 ft |
| Wingspan | 68.9 ft |
| External dimensions | |
|---|---|
| Length | 26.33 m |
| Height | 6.77 m |
| Wingspan | 21 m |
| Cabin dimensions | |
|---|---|
| Length | 12.92 m |
| Height | 1.83 m |
| Width | 2.1 m |
| Flat Floor | No |
| Cabin dimensions | |
|---|---|
| Length | 42.4 ft |
| Height | 6 ft |
| Width | 6.9 ft |
| Flat Floor | No |
| Cabin dimensions | |
|---|---|
| Length | 12.92 m |
| Height | 1.83 m |
| Width | 2.1 m |
| Flat Floor | No |
| Luggage capacity | |
|---|---|
| Internal Baggage Volume | 8099 L |
| Internal Baggage Weight | 654 kg |
| External Baggage Volume | - |
| External Baggage Weight | - |
| Luggage capacity | |
|---|---|
| Internal Baggage Volume | 286 ft³ |
| Internal Baggage Weight | 1441 lb |
| External Baggage Volume | - |
| External Baggage Weight | - |
| Luggage capacity | |
|---|---|
| Internal Baggage Volume | 8099 L |
| Internal Baggage Weight | 654 kg |
| External Baggage Volume | - |
| External Baggage Weight | - |
| Engines | |
|---|---|
| Number | 2 |
| Manufacturer | Rolls-Royce |
| Model | AE 3007A2 |
| Thrust | 9020 lb |
| TBO | On Condition |
| Flat Rating | ISA+15°C |
| Weights and limits | |
|---|---|
| Maximum Takeoff Weight | 24300 kg |
| Maximum Payload | 2240 kg |
| Maximum Fuel Capacity | 9344 kg |
| Payload with Full Fuel | 866 kg |
| Maximum Operating Speed | Mach 0.8 |
| Cabin Pressure Differential | 8.4 psi |
| Weights and limits | |
|---|---|
| Maximum Takeoff Weight | 53572 lb |
| Maximum Payload | 4939 lb |
| Maximum Fuel Capacity | 20600 lb |
| Payload with Full Fuel | 1910 lb |
| Maximum Operating Speed | Mach 0.8 |
| Cabin Pressure Differential | 8.4 psi |
| Weights and limits | |
|---|---|
| Maximum Takeoff Weight | 24300 kg |
| Maximum Payload | 2240 kg |
| Maximum Fuel Capacity | 9344 kg |
| Payload with Full Fuel | 866 kg |
| Maximum Operating Speed | Mach 0.8 |
| Cabin Pressure Differential | 8.4 psi |
| Speeds | |
|---|---|
| Long-Range Cruise | 787 km/h |
| High-Speed Cruise | 850 km/h |
| Speeds | |
|---|---|
| Long-Range Cruise | 425 kt |
| High-Speed Cruise | 459 kt |
| Speeds | |
|---|---|
| Long-Range Cruise | 787 km/h |
| High-Speed Cruise | 850 km/h |
| Consumption | |
|---|---|
| Long-Range Cruise | 862 kg/h |
| High-Speed Cruise | 1166 kg/h |
| Consumption | |
|---|---|
| Long-Range Cruise | 1901 lb/h |
| High-Speed Cruise | 2570 lb/h |
| Consumption | |
|---|---|
| Long-Range Cruise | 862 kg/h |
| High-Speed Cruise | 1166 kg/h |
| Range | 3919 mn |
| Takeoff Distance - Sea Level | 1750 m |
| Takeoff Distance - Hot and High | 2432 m |
| Landing Distance | 715 m |
| Maximum Operating Altitude | 12497 m |
| Range | 3919 mn |
| Takeoff Distance - Sea Level | 5741 ft |
| Takeoff Distance - Hot and High | 7979 ft |
| Landing Distance | 2346 ft |
| Maximum Operating Altitude | 41000 ft |
| Range | 3919 mn |
| Takeoff Distance - Sea Level | 1750 m |
| Takeoff Distance - Hot and High | 2432 m |
| Landing Distance | 715 m |
| Maximum Operating Altitude | 41000 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. |