Price upon request
General characteristics
Crew: 2 + jump seat
Capacity: 8 / 2,000 lb (907 kg) maximum payload
Length: 51 ft 2 in (15.60 m)
Wingspan: 51 ft 4.5 in (15.659 m)
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General characteristics
Crew: 2 + jump seat
Capacity: 8 / 2,000 lb (907 kg) maximum payload
Length: 51 ft 2 in (15.60 m)
Wingspan: 51 ft 4.5 in (15.659 m)
Height: 17 ft 7 in (5.36 m)
Wing area: 374 sq ft (34.7 m2)
Empty weight: 15,600 lb (7,076 kg) basic
Operating weight empty: 16,000 lb (7,257 kg)
Maximum ramp weight: 27,520 lb (12,483 kg)
Maximum zero-fuel weight: 18,000 lb (8,165 kg)
Max takeoff weight: 27,400 lb (12,428 kg)
Maximum landing weight: 23,350 lb (10,591 kg)
Fuel capacity: 1,248 imp gal (1,499 US gal; 5,674 l) total ; 1,060 imp gal (1,273 US gal; 4,819 l) in wing integral tanks + 188 imp gal (226 US gal; 855 l) in rear under-fuselage tank
Powerplant: 2 × Honeywell TFE731-5BR turbofan engines, 4,300 lbf (19 kN) thrust each
Performance
Maximum speed: 456 kn (525 mph, 845 km/h) max level speed and max cruising speed at 29,000 ft (8,839 m) / M0.87
Cruise speed: 400 kn (460 mph, 740 km/h) economical cruise at 39,000–43,000 ft (11,887–13,106 m)
Stall speed: 92 kn (106 mph, 170 km/h) in landing configuration at typical landing weight
Range: 2,580 nmi (2,970 mi, 4,780 km) with max payload
2,825 nmi (3,251 mi; 5,232 km) with max fuel and NBAA VFR reserves
Service ceiling: 43,000 ft (13,000 m)
Rate of climb: 3,100 ft/min (16 m/s)
Wing loading: 73.26 lb/sq ft (357.7 kg/m2)
Thrust/weight: 0.313
Take-off balanced field length: 5,620 ft (1,713 m) at MTOW
Landing distance from 50 ft (15 m): 4,500 ft (1,372 m) at typical landing weight and 6 pax
Avionics
Standard Honeywell SPZ-800
Dual RCZ-850 integrated comms
Motorola N1335BSelcal
Primus 870 weather radar