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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.
• Note •
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.
June 2007
4-28 Information Manual
Section 4 Cirrus Design
Normal Procedures SR22
Noise Characteristics/Abatement
The certificated noise levels for the Cirrus Design SR22 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 SR22.
• 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.
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)
June 2007
Information Manual 4-29
Cirrus Design Section 4
SR22 Normal Procedures
Fuel Conservation
Minimum fuel use at cruise will be achieved using the best economy
power setting described under cruise.
June 2007
4-30 Information Manual
Section 4 Cirrus Design
Normal Procedures SR22
June 2007
Intentionally Left Blank
Information Manual 5-1
Cirrus Design Section 5
SR22 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
　
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