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Information Manual 4-13
Cirrus Design Section 4
SR20 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. Directional Gyro/HSI Orientation ....................................... CHECK
4. Attitude Gyro ...................................................................... CHECK
5. Turn Coordinator ............................................................... CHECK
March 2010
4-14 Information Manual
Section 4 Cirrus Design
Normal Procedures SR20
Before Takeoff
During cold weather operations, the engine should be properly
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.
• WARNING •
Do not takeoff with frost, ice, snow, or other contamination on
the fuselage, wing, stabilizers, and control surfaces.
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. Flaps ...............................................................SET 50% & CHECK
8. Transponder .............................................................................SET
9. Autopilot ............................................................................. CHECK
10. Navigation Radios/GPS ......................................... SET for Takeoff
11. Cabin Heat/Defrost ................................................ AS REQUIRED
12. Brakes ...................................................................................HOLD
13. Power Lever ...................................................................1700 RPM
14. 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
March 2010
Information Manual 4-15
Cirrus Design Section 4
SR20 Normal Procedures
to extinguish ALT 2 caution light. ALT 2 caution light should go
out below 2200 RPM.
15. Voltage............................................................................... CHECK
16. Pitot Heat ............................................................... AS REQUIRED
• Note •
Pitot Heat should be turned ON for flight into IMC, flight into
visible moisture, or whenever ambient temperatures are 41° F
(5° C) or less.
　
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