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11. Ignition Switch....................... START (Release after engine starts)
• Caution •
Limit cranking to intervals of 20 seconds with a 20 second
cooling period between cranks.
12. Power Lever ...............................RETARD (to maintain 1000 RPM)
13. Oil Pressure ....................................................................... CHECK
14. Alt Master Switches ...................................................................ON
15. Avionics Power Switch ...............................................................ON
16. Engine Parameters ........................................................MONITOR
17. External Power (If applicable) ................................. DISCONNECT
18. Amp Meter/Indication......................................................... CHECK
19. Strobe Lights..............................................................................ON
Hot Weather Operation
Avoid prolonged engine operation on the ground. Fuel BOOST must
be ON for engine start and takeoff, and should be ON during climb for
vapor suppression which could occur under hot ambient conditions or
after extended idle.
March 2010
4-26 Information Manual
Section 4 Cirrus Design
Normal Procedures SR22
Noise Characteristics/Abatement
The certificated noise levels for the aircraft 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 3400 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 public.
The following suggested procedures minimize environmental noise
when operating the aircraft.
• 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
Hartzel 3-blade Propeller
PHC-J3YF-1RF/F7694
83.65 dB(A) 88.00 dB(A)
Hartzel 3-blade Propeller
PHC-J3YF-1RF/F7693DF
84.81 dB(A) 88.00 dB(A)
McCauley 3-blade Propeller
D3A34C443/78CYA-0
83.15 dB(A) 88.00 dB(A)
MT 3-blade Propeller
MTV-9-D/198-52
84.80 dB(A) 88.00 dB(A)
March 2010
Information Manual 5-1
Cirrus Design Section 5
SR22 Performance Data
Section 5
Performance Data
Table of Contents
Introduction ........................................................................................ 3
Associated Conditions Affecting Performance................................ 3
Demonstrated Operating Temperature........................................... 3
Airspeed Calibration - Normal Static Source...................................... 4
Airspeed Calibration - Alternate Static Source................................... 5
Altitude Correction - Normal Static Source ........................................ 6
Altitude Correction - Alternate Static Source ..................................... 7
Temperature Conversion ................................................................... 8
Outside Air Temperature for ISA Condition ....................................... 9
Stall Speeds..................................................................................... 10
Wind Components ........................................................................... 11
Takeoff Distance .............................................................................. 12
Takeoff Distance - 3400 LB ............................................................. 13
Takeoff Distance - 2900 LB ............................................................. 14
Takeoff Climb Gradient .................................................................... 15
Takeoff Rate of Climb ...................................................................... 16
Enroute Climb Gradient ................................................................... 17
Enroute Rate of Climb...................................................................... 18
　
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