Cirrus SR20 Information Manual

AIRPLANE INFORMATION MANUAL
for the
CIRRUS DESIGN SR20
Aircraft Serials 2016 and Subsequent with
Cirrus Perspective Avionics System
At the time of issuance, this Information Manual was harmo-
nized with the SR20 Pilot's Operating Handbook September
2011 (P/N 11934-004), and will not be kept current.
Therefore, this Information Manual is for reference only and can-
not be used as a substitute for the official Pilot's Operating
Handbook and FAA Approved Airplane Flight Manual.
Information Manual
P/N 13999-004 September 2011

Cirrus SR20 Specifications

General

Manufacturer	Cirrus Aircraft
Engine	Continental IO-360-ES
Horsepower	215 hp
Max Cruise Speed	155 knots (178 mph, 287 km/h)
Seats	4
Aircraft Type	Single-engine light aircraft
Service Ceiling	17, 500 feet (5, 334 m)
Wingspan	38 ft 4 in
Length	26.0 feet (7.92 m)
Height	8 ft 11 in
Maximum Takeoff Weight	3, 050 pounds (1, 383 kg)
Fuel Capacity	56 gallons (212 liters)
Cabin Height	50 in
Avionics	Garmin Perspective+
Safety Features	Cirrus Airframe Parachute System (CAPS)
Stall Speed	56 knots (64 mph, 104 km/h) flaps down
Cabin Width	49 in (124 cm)