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warmed up before takeoff. In most cases this is accomplished when
the oil temperature has reached at least 100° F (38° C). In warm or hot
weather, precautions should be taken to avoid overheating during
prolonged ground engine operation. Additionally, long periods of idling
may cause fouled spark plugs.
1. Doors ..............................................................................LATCHED
2. CAPS Handle ................................................. Verify Pin Removed
3. Seat Belts and Shoulder Harness....................................SECURE
4. Fuel Quantity..................................................................CONFIRM
5. Fuel Selector .........................................................FULLEST TANK
6. Fuel Pump................................................................................. ON
7. Mixture ................................................................... AS REQUIRED
8. Flaps ...............................................................SET 50% & CHECK
9. Transponder .............................................................................SET
10. Autopilot ............................................................................. CHECK
11. Navigation Radios/GPS ......................................... SET for Takeoff
12. Cabin Heat/Defrost ................................................ AS REQUIRED
13. Brakes ...................................................................................HOLD
14. Power Lever ...................................................................1700 RPM
15. Alternator ........................................................................... CHECK
a. Pitot Heat............................................................................ ON
b. Navigation Lights ................................................................ ON
c. Landing Light ...................................................................... ON
d. Annunciator Lights....................................................... CHECK
• Verify both ALT 1 and ALT 2 caution lights out and positive
amps indication for each alternator. If necessary, increase RPM
to extinguish ALT 2 caution light. ALT 2 caution light should go
out below 2200 RPM.
(Continued on following page)
June 2007
Information Manual 4-15
Cirrus Design Section 4
SR22 Normal Procedures
16. Voltage............................................................................... CHECK
17. Pitot Heat ............................................................... AS REQUIRED
• Note •
Pitot heat should be turned ON prior to flight into IMC or flight
into visible moisture and OAT of 40° F (4° C) or less.
18. Navigation Lights ................................................... AS REQUIRED
19. Landing Light ......................................................... AS REQUIRED
20. Magnetos ....................................................CHECK Left and Right
a. Ignition Switch ..................................R, note RPM, then BOTH
b. Ignition Switch .................................. L, note RPM, then BOTH
• Note •
RPM drop must not exceed 150 RPM for either magneto. RPM
differential must not exceed 75 RPM between magnetos. If
there is a doubt concerning operation of the ignition system,
RPM checks at higher engine speeds will usually confirm
whether a deficiency exists.
An absence of RPM drop may indicate faulty grounding of one
side of the ignition system or magneto timing set in advance of
the specified setting.
21. Engine Parameters ............................................................ CHECK
22. Power Lever ................................................................... 1000 RPM
23. Flight Instruments, HSI, and Altimeter ....................CHECK & SET
24. Flight Controls................................................. FREE & CORRECT
25. Trim..............................................................................SET Takeoff
26. Autopilot .................................................................. DISCONNECT
June 2007
4-16 Information Manual
Section 4 Cirrus Design
Normal Procedures SR22
Maximum Power Fuel Flow
Leaning for Takeoff and Maximum Climb is accomplished at full throttle
by leaning the mixture from full rich to the target fuel flow for the given
pressure altitude. The fuel flow values in the table below were
demonstrated to obtain the takeoff and climb performance presented
in Section 5.
• Note •
Excessively rich mixture will occur if the Mixture control is set to FULL
RICH above 7500 feet pressure altitude.
Pressure
Altitude
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AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR22(29)
