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• WARNING •
If airplane is in day VFR conditions and turning off the master
switches eliminated the fire situation, leave the master
switches OFF. Do not attempt to isolate the source of the fire
by checking each individual electrical component.
7. Airflow Selector ........................................................................OFF
8. Bat-Alt Master Switches.............................................................ON
9. Avionics Power Switch ...............................................................ON
10. Activate required systems one at a time. Pause several seconds
between activating each system to isolate malfunctioning system.
Continue flight to earliest possible landing with malfunctioning
system off. Activate only the minimum amount of equipment
necessary to complete a safe landing.
11. Temperature Selector............................................................COLD
12. Vent Selector......................... FEET/PANEL/DEFROST POSITION
13. Airflow Selector ..... SET FAN SPEED TO FULL ON (3) POSITION
14. Panel Eyeball Outlets............................................................OPEN
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Section 9 Cirrus Design
Supplements SR20
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Cirrus Design Section 9
SR20 Supplements
Section 4 - Normal Procedures
Airspeeds for Normal Operation
Unless otherwise noted, the following speeds are based on a
maximum weight of 3050 lb. and may be used for any lesser weight.
However, to achieve the performance specified in Section 5 for takeoff
and landing distance, the speed appropriate to the particular weight
must be used.
Takeoff Rotation:
• Normal, Flaps 50%........................................................66 KIAS
• Short Field, Flaps 50%..................................................65 KIAS
• Obstacle Clearance, Flaps 50%....................................77 KIAS
Enroute Climb, Flaps Up:
• Normal, SL ....................................................................96 KIAS
• Normal, 10,000’ .............................................................92 KIAS
• Best Rate of Climb, SL ..................................................96 KIAS
• Best Rate of Climb, 10,000............................................92 KIAS
• Best Angle of Climb, SL.................................................83 KIAS
• Best Angle of Climb, 10,000..........................................87 KIAS
Landing Approach:
• Normal Approach, Flaps Up..........................................88 KIAS
• Normal Approach, Flaps 50% .......................................83 KIAS
• Normal Approach, Flaps 100%.....................................78 KIAS
• Short Field, Flaps 100%................................................78 KIAS
Go-Around, Flaps 50%:
• Full Power......................................................................78 KIAS
Maximum Recommended Turbulent Air Penetration:
• 3050 Lb .......................................................................131 KIAS
• 2600 Lb .......................................................................122 KIAS
• 2200 Lb .......................................................................111 KIAS
Maximum Demonstrated Crosswind Velocity:
• Takeoff or Landing........................................................20 Knots
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Section 9 Cirrus Design
Supplements SR20
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Cirrus Design Section 9
SR20 Supplements
Section 5 - Performance
Airspeed Calibration
Normal Static Source
• Note •
• Indicated airspeed values assume zero instrument error.
Conditions:
• Power for level flight or maximum continuous, whichever is less.
KIAS
KCAS
Flaps
0%
Flaps
50%
Flaps
100%
60 57 56 57
70 68 68 70
80 79 80 80
90 89 91 89
100 100 101 99
110 111 111
120 121 121
130 132
140 142
150 152
160 163
170 173
180 183
190 193
200 204
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Section 9 Cirrus Design
Supplements SR20
Airspeed Calibration
Alternate Static Source
• Note •
• Indicated airspeed values assume zero instrument error.
Conditions:
• Power for level flight or maximum continuous, whichever is less.
• Heater, Defroster & Vents...................................................................................ON
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西锐20飞机信息手册CIRRUS DESIGN SR20 AIRPLANE INFORMATION MA(130)
