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Fuel Required ..............................................................................5-8
Landing ........................................................................................5-9
Demonstrated Operating Temperature........................................5-9
Airspeed Calibration......................................................................5-10
Normal Static Source.................................................................5-10
Airspeed Calibration......................................................................5-11
Alternate Static Source ..............................................................5-11
Altitude Correction ........................................................................5-12
Normal Static Source.................................................................5-12
Altitude Correction ........................................................................5-13
Alternate Static Source ..............................................................5-13
Temperature Conversion ..............................................................5-14
Outside Air Temperature for ISA Condition ..................................5-15
Stall Speeds..................................................................................5-16
Wind Components ........................................................................5-17
Takeoff Distance ...........................................................................5-18
Takeoff Distance ...........................................................................5-19
Takeoff Distance ...........................................................................5-20
Takeoff Climb Gradient .................................................................5-21
Takeoff Rate of Climb ...................................................................5-22
Enroute Climb Gradient ................................................................5-23
Enroute Rate of Climb...................................................................5-24
Enroute Rate of Climb Vs Density Altitude ...................................5-25
Time, Fuel and Distance to Climb.................................................5-26
Cruise Performance ......................................................................5-27
Cruise Performance ......................................................................5-28
March 2010
5-2 Information Manual
Section 5 Cirrus Design
Performance Data SR20
Range / Endurance Profile ............................................................5-29
Range / Endurance Profile ............................................................5-30
Balked Landing Climb Gradient ....................................................5-31
Balked Landing Rate of Climb.......................................................5-32
Landing Distance ..........................................................................5-33
Landing Distance ..........................................................................5-34
March 2010
Information Manual 5-3
Cirrus Design Section 5
SR20 Performance Data
Introduction
Performance data in this section are presented for operational
planning so that you will know what performance to expect from the
airplane under various ambient and field conditions. Performance data
are presented for takeoff, climb, and cruise (including range &
endurance).
Associated Conditions Affecting Performance
Computed performance data in this section are based upon data
derived from actual flight testing with the airplane and engine in good
condition and using average piloting techniques. Unless specifically
noted in the “Conditions” notes presented with each table, ambient
conditions are for a standard day (refer to Section 1). Flap position as
well as power setting technique is similarly noted with each table.
The charts in this section provide data for ambient temperatures from
–20 C (–4 F) to 40 C (104 F). If ambient temperature is below the
chart value, use the lowest temperature shown to compute
performance. This will result in more conservative performance
calculations. If ambient temperature is above the chart value, use
extreme caution as performance degrades rapidly at higher
temperatures.
All fuel flow data for cruise is based on the recommended lean mixture
setting detailed in Section 4 – Normal Procedures.
March 2010
5-4 Information Manual
Section 5 Cirrus Design
Performance Data SR20
Flight Planning
The performance tables in this section present sufficient information to
predict airplane performance with reasonable accuracy. However,
　
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