曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

indications will be reversed (i.e., the needle will
indicate UP for descent and DOWN for climb).
With the alternate static source on, adjust indicated airspeed slightly
during climb or approach according to the Airspeed Calibration
(Alternate Static Source) table in Section 5 as appropriate for vent/
heater configuration.
1. Pitot Heat ...................................................................................ON
2. Alternate Static Source .........................................................OPEN
Pitot Tube Blocked
If only the airspeed indicator is providing erroneous information, and in
icing conditions, the most probable cause is pitot ice. If setting Pitot
Heat ON does not correct the problem, descend to warmer air. If an
approach must be made with a blocked Pitot tube, use known pitch
and power settings and the GPS groundspeed indicator, taking
surface winds into account.
1. Pitot Heat ...................................................................................ON
June 2007
3A-14 Information Manual
Section 3A Cirrus Design
Abnormal Procedures SR22
Electric Trim/Autopilot Failure
Any failure or malfunction of the electric trim or autopilot can be overridden
by use of the control yoke. If runaway trim is the problem, deenergize
the circuit by pulling the circuit breaker (PITCH TRIM, ROLL
TRIM, or AUTOPILOT) and land as soon as conditions permit.
1. Airplane Control ......................................... MAINTAIN MANUALLY
2. Autopilot (if engaged) .....................................................Disengage
If Problem Is Not Corrected:
3. Circuit Breakers................................................ PULL AS Required
• PITCH TRIM
• ROLL TRIM
• AUTOPILOT
4. Power Lever ........................................................... AS REQUIRED
5. Control Yoke................................. MANUALLY HOLD PRESSURE
6. Land as soon as practical.
June 2007
Information Manual 4-1
Cirrus Design Section 4
SR22 Normal Procedures
Section 4
Normal Procedures
Table of Contents
Introduction .....................................................................................4-3
Airspeeds for Normal Operation .....................................................4-4
Normal Procedures .........................................................................4-5
Preflight Inspection ......................................................................4-5
Preflight Walk-Around..................................................................4-6
Before Starting Engine...............................................................4-10
Starting Engine ..........................................................................4-11
Before Taxiing............................................................................4-13
Taxiing .......................................................................................4-13
Before Takeoff ...........................................................................4-14
Maximum Power Fuel Flow .......................................................4-16
Takeoff.......................................................................................4-17
Normal Takeoff ..........................................................................4-17
Short Field Takeoff ....................................................................4-18
Climb..........................................................................................4-18
Cruise ........................................................................................4-19
Cruise Leaning...........................................................................4-20
Descent......................................................................................4-20
Before Landing ..........................................................................4-20
Landing ......................................................................................4-21
Balked Landing/Go-Around .......................................................4-22
After Landing .............................................................................4-22
Shutdown...................................................................................4-23
Stalls ..........................................................................................4-24
Environmental Considerations ......................................................4-25
Cold Weather Operation ............................................................4-25
Hot Weather Operation..............................................................4-27
Noise Characteristics/Abatement..................................................4-28
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR22(24)