General characteristics
Crew: 1 or 2 pilots
Capacity: 8–10 passengers
Length: 39 ft 0 in (11.89 m)
Wingspan: 49 ft 4 in (15.04 m)
Height: 13 ft 2 in (4.01 m)
Wing area: 253.6 sq ft (23.56 m2)
Aspect ratio: 9.6:1
Airfoil: NACA 23018 at root, NACA 23019 at tip
Empty weight: 5,682 lb (2,577 kg)
Gross weight: 9,850 lb (4,468 kg)
Powerplant: 2 × Garrett TPE331-10-403S turboprops, 636 shp (474 kW) each
Propellers: 4-bladed McCauley
Performance
Maximum speed: 340 mph (550 km/h, 300 kn) at 16,000 ft (4,875 m)
Cruise speed: 298 mph (480 km/h, 259 kn) at 35,000 ft (10,700 m)
Stall speed: 86 mph (139 km/h, 75 kn) flaps and gear down
Range: 2,525 mi (4,064 km, 2,194 nmi) at 35,000 ft (10,700 m)
Service ceiling: 35,000 ft (11,000 m)
Rate of climb: 2,435 ft/min (12.37 m/s)
Avionics
Cessna 1000A Integrated Flight Control System