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

However, no electrical power will be available.
2. Fire Extinguisher ............................................................ ACTIVATE
Original: 03-27-07
13772-130 15 of 58
Cirrus Design Section 9
SR22 Supplements
• WARNING •
Halon gas used in the fire extinguisher can be toxic, especially
in a closed area. After extinguishing fire, ventilate cabin by and
unlatching door (if required).
If airflow is not sufficient to clear smoke or fumes from cabin:
3. Cabin Doors.......................................................PARTIALLY OPEN
Airspeed may need to be reduced to partially open door in flight.
4. Avionics Power Switch .............................................................OFF
5. All other switches .....................................................................OFF
6. Land as soon as possible.
If setting master switches off eliminated source of fire or fumes and
airplane is in night, weather, or IFR conditions:
• 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
Original: 03-27-07
16 of 58 13772-130
Section 9 Cirrus Design
Supplements SR22
Original: 03-27-07
Intentionally Left Blank
13772-130 17 of 58
Cirrus Design Section 9
SR22 Supplements
Section 4 - Normal Procedures
Airspeeds for Normal Operation
Unless otherwise noted, the following speeds are based on a
maximum weight of 3400 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%........................................................70 KIAS
• Obstacle Clearance, Flaps 50%....................................78 KIAS
Enroute Climb, Flaps Up:
• Normal..................................................................110-120 KIAS
• Best Rate of Climb, SL ................................................101 KIAS
• Best Rate of Climb, 10,000............................................96 KIAS
• Best Angle of Climb, SL.................................................79 KIAS
• Best Angle of Climb, 10,000..........................................83 KIAS
Landing Approach:
• Normal Approach, Flaps Up.....................................90-95 KIAS
• Normal Approach, Flaps 50% ..................................85-90 KIAS
• Normal Approach, Flaps 100%................................80-85 KIAS
• Short Field, Flaps 100% (VREF) ....................................77 KIAS
Go-Around, Flaps 50%:
• Full Power......................................................................80 KIAS
Maximum Recommended Turbulent Air Penetration:
• 3400 lb.........................................................................133 KIAS
• 2900 lb.........................................................................123 KIAS
Maximum Demonstrated Crosswind Velocity:
• Takeoff or Landing........................................................20 Knots
Original: 03-27-07
18 of 58 13772-130
Section 9 Cirrus Design
Supplements SR22
Original: 03-27-07
Intentionally Left Blank
13772-130 19 of 58
Cirrus Design Section 9
SR22 Supplements
Section 5 - Performance
Airspeed Calibration
Normal Static Source
• Note •
• Indicated airspeed values assume zero instrument error.
Conditions: Example:
• Power for level flight or maximum
continuous, whichever is less.
　
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(141)