P/N 13999-002 Info Manual 2-7
Cirrus Design Section 2
SR20 Limitations
Propeller
• Note •
Two-blade propellers are not EASA approved for use on this
airplane. Airplanes registered in the European Union should
ignore all references to the two-blade propeller in this POH.
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)
Weight Limits
Maximum Takeoff Weight ......................................... 3000 lb. (1361 kg)
• Note •
All weights in excess of 2900 pounds (1315 kg) must consist
of wing fuel.
Maximum Landing Weight ....................................... 2900 lb. (1315 kg)
Maximum Weight in Baggage Compartment.................. 130 lb. (59 kg)
September 2011
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