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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
March 2010
Cirrus Design Section 4
SR22 Normal Procedures
Information Manual 4-13
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.
(Continued on following page)
March 2010
4-14 Information Manual
Section 4 Cirrus Design
Normal Procedures SR22
16. Voltage ............................................................................... CHECK
17. 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.
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
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西锐20飞机信息手册 SR22 AIRPLANE INFORMATION MANUAL 2979(33)
