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...

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 take off 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