WMU College of Aviation
Jump to Content
The Cirrus SR-20 is a state-of-the-art, technically advanced aircraft, constructed primarily of composite materials and designed to be aerodynamically efficient. The single engine, low-wing monoplane comfortably seats four people, including a crew of one or two. The SR-20 is FAA certified for day, night, VFR, and IFR flight.
- Number in Fleet
- 28
- Primary Use
- Private, commercial, and instrument instruction
- Engine
- Teledyne Continental IO-360-E (200BHP @ 2700RPM)
- Fuel Capacity
- 56 gal
- Weight
- 2050 lbs (Standard Empty)
- 3000 lbs (Max Takeoff)
- 950 lbs (Max Useful Load)
- Dimensions
- 26' Long
- 9'2" High
- 35'6" Wing Span
- 135.2 ft2 Wing Area
- Speed
- 160 kts (Max @ Sea Level)
- 157 kts (Cruise, 80% Power @ 8000 ft)
- Stall Speed
- 56 kts (Flaps Down, Power Off)
- 65 kts (Flaps Up, Power Off)
- Cruising Range
- 5.4 hr, 768 nm (55% Power @ 10,000 ft)
- 4 hr, 627 nm (75% Power @ 8,000 ft)
- Max Operating Altitude
- 17,500 ft
- Takeoff Distance
- 2,064 ft (Total Distance over 50 ft Obstacle)
- Landing Distance
- 2,040 ft (Total Distance Over 50 ft Obstacle)