General characteristics

Crew: 2

Capacity: 8 occupants, crew included

Length: 42 ft 7 in (12.99 m)

Wingspan: 39 ft 9 in (12.12 m)

Height: 14 ft 11 in (4.54 m)

Max takeoff weight: 10,701 lb (4,854 kg) [96]

Pressurization: 8.8 psi (0.61 bar)

Cabin height: 4.83 ft (1.47 m)

Cabin width: 5.00 ft (1.52 m)

Powerplant: 2 × GE Honda HF120 turbofan, 2,050 lbf (9.1 kN) thrust each

Performance

Cruise speed: 422 kn (486 mph, 782 km/h) FL300

Range: 1,437 nmi (1,653 mi, 2,661 km) NBAA fuel reserve IFR Range with 4 occupants

Service ceiling: 43,000 ft (13,000 m)

Rate of climb: 4,100 ft/min (21 m/s)

General characteristics

Crew: 2 pilots

Capacity: 4 or 5 passengers (standard configurations); 7 occupants maximum (with optional belted lavatory)

Length: 12.82 m (42 ft 1 in)

Wingspan: 12.3 m (40 ft 4 in)

Height: 4.35 m (14 ft 3 in)

Wing area: 18.76 m2 (201.9 sq ft)

Empty weight: 3,275 kg (7,220 lb)

Max takeoff weight: 4,800 kg (10,582 lb) [4]

Fuel capacity: 1,272 kg (2,804 lb)[33]

Cabin height: 1.5 m (4 ft 11 in)[9]

Cabin length: 3.35 m (11 ft)[9]

Powerplant: 2 × Pratt & Whitney Canada PW617F1-E turbofan engines, 7.7 kN (1,730 lbf) thrust each at ISA + 8°C

Performance

Maximum speed: Mach 0.7

Cruise speed: 750 km/h (470 mph, 400 kn)

Minimum control speed: 180 km/h (110 mph, 97 kn)

Range: 2,182 km (1,356 mi, 1,178 nmi) (LRC, four 91 kg (200 lb) occupants, NBAA IFR reserves with 185 km (115 mi; 100 nmi) alternate)

Service ceiling: 12,497 m (41,001 ft)

Cabin altitude: 2,438 m (8,000 ft) at 12,497 m (41,000 ft)[7]

Take-off run: 975 m (3,199 ft) (MTOW, SL, ISA)

Landing run: 741 m (2,431 ft) (SL, ISA, four 91 kg (200 lb) occupants, NBAA IFR reserves with 185 km (115 mi; 100 nmi) alternate)

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