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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
Revision A5
P/N 13772-001 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
Revision A6
4-14 P/N 13772-001
Section 4 Cirrus Design
Normal Procedures SR22
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.......................................................................... BOOST
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
Revision A9
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CIRRUS DESIGN SR22西锐22飞行员操作手册和飞机飞行手册(33)
