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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
e. Note ammeter remains within one needle width.
15. Voltage ............................................................................... CHECK
March 2010
Information Manual 4-15
Cirrus Design Section 4
SR20 Normal Procedures
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.
17. Navigation Lights ................................................... AS REQUIRED
18. Landing Light ......................................................... AS REQUIRED
19. 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.
20. Engine Parameters ............................................................ CHECK
21. Power Lever ................................................................... 1000 RPM
22. Vacuum.............................................................................. CHECK
23. Flight Instruments, HSI, and Altimeter ....................CHECK & SET
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西锐20飞机信息手册 SR22 AIRPLANE INFORMATION MANUAL 1148-126(28)
