Specifications
Data from Brassey's World Aircraft & Systems Directory 1999/2000
General characteristics
- Crew: 2
- Capacity: 50–58 passengers
- Payload: 5,900 kg (13,010 lb)
- Length: 27.28 m (89 ft 6 in)
- Wingspan: 24.76 m (81 ft 3 in)
- Height: 7.73 m (25 ft 4 in)
- Wing area: 55.7 m² (600 sq ft)
- Airfoil: NASA MS(1)013
- Aspect ratio: 11:0
- Empty weight: 13,800 kg (30,424 lb)
- Max. takeoff weight: 22,800 kg (50,265 lb)
- Powerplant: 2 × Allison AE 2100A turboprop, 3,096 kW (4,152 shp) each
- Propellers: six blade constant speed Dowty propellers, 1 per engine
Performance
- Cruise speed: 665 km/h (370 knots, 424 mph)
- Service ceiling: 9,450 m (31,000 ft)
- Rate of climb: 11.4 m/s (2,250 ft/min)
Avionics
- Rockwell Collins Pro Line 4 avionics suite with integrated avionics processor (IAP)
Read more about this topic: Saab 2000