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• WARNING •
If airplane will be started using external power, keep all
personnel and power unit cables well clear of the propeller
rotation plane.
• Caution •
Alternators should be left OFF during engine starting to avoid
high electrical loads.
After starting, if the oil gage does not begin to show pressure
within 30 seconds in warm weather and about 60 seconds in
very cold weather, shut down engine and investigate cause.
Lack of oil pressure indicates loss of lubrication, which can
cause severe engine damage.
1. External Power (If applicable) ....................................... CONNECT
2. Brakes ..................................................................................HOLD
3. Bat Master Switches ........................................... ON (Check Volts)
June 2007
4-12 Information Manual
Section 4 Cirrus Design
Normal Procedures SR22
4. Strobe Lights ............................................................................. ON
5. Mixture ......................................................................... FULL RICH
6. Power Lever ........................................................FULL FORWARD
7. Fuel Pump.....................................................PRIME, then BOOST
• Note •
Serials 0002 - 0278 before SB 22-73-01: On first start of the
day, especially under cool ambient conditions, holding Fuel
Pump switch to PRIME for 30-60 seconds will improve
starting.
Serials 0002 - 0278 after SB 22-73-01 and serials 0279 and
subsequent: On first start of the day, especially under cool
ambient conditions, holding Fuel Pump switch to PRIME for 2
seconds will improve starting.
8. Propeller Area .....................................................................CLEAR
9. Power Lever ...........................................................OPEN ¼ INCH
10. 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.
11. Power Lever ..............................RETARD (to maintain 1000 RPM)
12. Oil Pressure ....................................................................... CHECK
13. Alt Master Switches .................................................................. ON
14. Avionics Power Switch .............................................................. ON
15. Engine Parameters ........................................................MONITOR
16. External Power (If applicable) ................................. DISCONNECT
17. Amp Meter/Indication ......................................................... CHECK
June 2007
Information Manual 4-13
Cirrus Design Section 4
SR22 Normal Procedures
Before Taxiing
1. Flaps ................................................................................. UP (0%)
2. Radios/Avionics ..................................................... AS REQUIRED
3. Cabin Heat/Defrost ............................................... AS REQUIRED
4. Fuel Selector...........................................................SWITCH TANK
Taxiing
When taxiing, directional control is accomplished with rudder
deflection and intermittent braking (toe taps) as necessary. Use only
as much power as is necessary to achieve forward movement.
Deceleration or taxi speed control using brakes but without a reduction
in power will result in increased brake temperature. Taxi over loose
gravel at low engine speed to avoid damage to the propeller tips.
• WARNING •
Maximum continuous engine speed for taxiing is 1000 RPM
on flat, smooth, hard surfaces. Power settings slightly above
1000 RPM are permissible to start motion, for turf, soft
surfaces, and on inclines. Use minimum power to maintain taxi
speed.
If the 1000 RPM taxi power limit and proper braking
procedures are not observed, the brake system may overheat
and result in brake damage or brake fire.
1. Parking Brake ............................................................DISENGAGE
2. Brakes................................................................................ CHECK
3. HSI Orientation .................................................................. CHECK
4. Attitude Gyro ...................................................................... CHECK
5. Turn Coordinator ............................................................... CHECK
June 2007
4-14 Information Manual
Section 4 Cirrus Design
Normal Procedures SR22
Before Takeoff
During cold weather operations, the engine should be properly
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AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR22(28)
