Cirrus DESIGN SR20 Information Manual

1-6 P/N 13999-002 Info Manual
Section 1 Cirrus Design
General SR20
The Airplane
Engine
Number of Engines.............................................................................. 1
Number of Cylinders............................................................................ 6
Engine Manufacturer ........................................... Teledyne Continental
Engine Model........................................................................IO-360-ES
Fuel Metering.................................................................... Fuel Injected
Engine Cooling ..................................................................... Air Cooled
Engine Type....................................Horizontally Opposed, Direct Drive
Horsepower Rating................................................200 hp @ 2700 rpm
Propeller
Hartzell
Propeller Type.............................................................. Constant Speed
Two-Blade Propeller:
Model Number ...................................................BHC-J2YF-1BF/F7694
Diameter .............................................................76.0” (73.0” Minimum)
Three-Blade Propeller:
Model Number ............................................... PHC-J3YF-1MF/F7392-1
Diameter .............................................................74.0” (72.0” Minimum)
Model Number ............................................... PHC-J3YF-1RF/F7392-1
Diameter .............................................................74.0” (72.0” Minimum)
September 2011

Cirrus DESIGN SR20 Specifications

General

Brand	Cirrus
Model	DESIGN SR20
Category	Aircrafts
Language	English