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c. Suction Gage...................................................... GREEN ARC
d. Attitude Gyro Flag............................................. OUT OF VIEW
7. Mixture ......................................................................... FULL RICH
8. Power lever..........................................................FULL FORWARD
9. Fuel Pump.....................................................PRIME, then BOOST
• Note •
Serials 1005 - 1227 before SB 20-73-02: In temperatures
down to 20°F, hold Fuel Pump switch to PRIME for 8-10
seconds prior to starting.
Serials 1005 - 1227 after SB 20-73-02 and serials 1228 and
subsequent: In temperatures down to 20°F, hold Fuel Pump
switch to PRIME for 10 seconds prior to starting.
10. Propeller Area .....................................................................CLEAR
March 2010
Information Manual 4-27
Cirrus Design Section 4
SR20 Normal Procedures
(Continued on following page)
11. Power Lever ............................................................OPEN ¼ INCH
12. Ignition Switch....................... START (Release after engine starts)
• Caution •
Limit cranking to intervals of 20 seconds with a 20 second
cooling period between cranks. This will improve battery and
contactor life
13. Power Lever ...............................RETARD (to maintain 1000 RPM)
14. Oil Pressure ....................................................................... CHECK
15. Alt Master Switches ...................................................................ON
16. Vacuum System Annunciators ................................................ OUT
17. Avionics Power Switch ...............................................................ON
18. Engine Parameters ........................................................MONITOR
19. External Power (If applicable) ................................. DISCONNECT
20. Amp Meter/Indication......................................................... CHECK
21. Strobe Lights..............................................................................ON
Hot Weather Operation
Avoid prolonged engine operation on the ground.
• Note •
Fuel BOOST should be left ON during takeoff and for climb as
required for vapor suppression with hot or warm fuel.
March 2010
4-28 Information Manual
Section 4 Cirrus Design
Normal Procedures SR20
Noise Characteristics/Abatement
The certificated noise levels for the Cirrus Design SR20 established in
accordance with FAR 36 Appendix G are:
No determination has been made by the Federal Aviation
Administration that the noise levels of this airplane are or should be
acceptable or unacceptable for operation at, into, or out of, any airport.
The above noise levels were established at 3000 pounds takeoff
weight and 2700 RPM.
Recently, increased emphasis on improving environmental quality
requires all pilots to minimize the effect of airplane noise on the
general public. The following suggested procedures minimize
environmental noise when operating the SR20.
• Note •
Do not follow these noise abatement procedures where they
conflict with Air Traffic Control clearances or instructions,
weather considerations, or wherever they would reduce safety.
1. When operating VFR over noise-sensitive areas, such as outdoor
events, parks, and recreational areas, fly not less than 2000 feet
above the surface even though flight at a lower level may be
allowed.
2. For departure from or approach to an airport, avoid prolonged
flight at low altitude near noise-sensitive areas.
Fuel Conservation
Minimum fuel use at cruise will be achieved using the best economy
power setting described under cruise.
Configuration Actual Maximum Allowable
Two-blade Propeller 84.79 dB(A) 87.6 dB(A)
Three-blade Propeller 83.42 dB(A) 87.6 dB(A)
March 2010
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
　
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