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power setting described under cruise.
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4-30 Information Manual
Section 4 Cirrus Design
Normal Procedures SR20
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Intentionally Left Blank
Information Manual 5-1
Cirrus Design Section 5
SR20 Performance Data
Section 5
Performance Data
Table of Contents
Introduction .....................................................................................5-3
Associated Conditions Affecting Performance.............................5-3
Flight Planning ................................................................................5-4
Sample Problem .............................................................................5-4
Takeoff.........................................................................................5-5
Climb............................................................................................5-6
Cruise ..........................................................................................5-7
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
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西锐20飞机信息手册CIRRUS DESIGN SR20 AIRPLANE INFORMATION MA(35)
