Cirrus DESIGN SR20 User Manual

Cirrus Design Section 1
SR20 General
P/N 11934-004 1-7
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)
Revision 1

Cirrus DESIGN SR20 Specifications

General

Brand	Cirrus
Model	DESIGN SR20
Category	Aircrafts
Language	English