The Saab 2000 is a twin-engined high-speed turboprop airliner built by Saab.

• Role: Regional airliner
• National origin: Sweden
  
• Manufacturer: Saab Aircraft
• Production line: Linköping
• First flight: 26 March 1992
• Introduction: 30 August 1994
• Status: In service
• Produced: 1992–1999
• Number built: 63
  
• Developed from: Saab 340

Specifications Saab 2000

General characteristics

• Crew: two
• 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)