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the use of the seat belts, doors, emergency exits, egress
hammer, and CAPS.
Verify CAPS handle safety pin is removed.
5. Seats, Seat Belts, and Harnesses ................ADJUST & SECURE
• Caution •
Crew seats must be locked in position and control handles
fully down before flight. Ensure seat belt harnesses are not
twisted.
March 2010
4-10 Information Manual
Section 4 Cirrus Design
Normal Procedures SR22
Starting Engine
If the engine is warm, no priming is required. For the first start of the
day and in cold conditions, prime will be necessary.
Weak intermittent firing followed by puffs of black smoke from the
exhaust stack indicates over-priming or flooding. Excess fuel can be
cleared from the combustion chambers by the following procedure:
• Turn fuel pump off.
• Allow fuel to drain from intake tubes.
• Set the mixture control full lean and the power lever full open.
• Crank the engine through several revolutions with the starter.
• When engine starts, release ignition switch, retard power lever,
and slowly advance the mixture control to FULL RICH position.
If the engine is under-primed, especially with a cold soaked engine, it
will not fire, and additional priming will be necessary. As soon as the
cylinders begin to fire, open the power lever slightly to keep it running.
Refer to Cold Weather Operation in this section or additional
information regarding cold weather operations.
• WARNING •
If airplane will be started using external power, keep all
personnel and power unit cables well clear of the propeller
rotation plane.
• Caution •
Alternators should be left OFF during engine starting to avoid
high electrical loads.
After starting, if the oil gage does not begin to show pressure
within 30 seconds in warm weather and about 60 seconds in
very cold weather, shut down engine and investigate cause.
Lack of oil pressure indicates loss of lubrication, which can
cause severe engine damage.
1. External Power (If applicable) .......................................CONNECT
2. Brakes ..................................................................................HOLD
3. Bat Master Switches ........................................... ON (Check Volts)
4. Strobe Lights ............................................................................. ON
5. Mixture ......................................................................... FULL RICH
March 2010
Cirrus Design Section 4
SR22 Normal Procedures
Information Manual 4-11
6. Power Lever ........................................................FULL FORWARD
7. Fuel Pump ....................................................PRIME, then BOOST
• Note •
On first start of the day, especially under cool ambient
conditions, holding Fuel Pump switch to PRIME for 2 seconds
will improve starting.
8. Propeller Area.....................................................................CLEAR
9. Power Lever ...........................................................OPEN ¼ INCH
10. Ignition Switch....................... START (Release after engine starts)
• Caution •
Limit cranking to intervals of 20 seconds with a 20 second
cooling period between cranks. This will improve battery and
contactor life.
11. Power Lever ..............................RETARD (to maintain 1000 RPM)
12. Oil Pressure ....................................................................... CHECK
13. Alt Master Switches ...................................................................ON
14. Avionics Power Switch ...............................................................ON
15. Engine Parameters ........................................................MONITOR
16. External Power (If applicable) ................................. DISCONNECT
17. Amp Meter/Indication......................................................... CHECK
March 2010
4-12 Information Manual
Section 4 Cirrus Design
Normal Procedures SR22
Before Taxiing
1. Flaps ................................................................................. UP (0%)
2. Radios/Avionics...................................................... AS REQUIRED
3. Cabin Heat/Defrost ............................................... AS REQUIRED
4. Fuel Selector ...........................................................SWITCH TANK
Taxiing
When taxiing, directional control is accomplished with rudder
deflection and intermittent braking (toe taps) as necessary. Use only
as much power as is necessary to achieve forward movement.
Deceleration or taxi speed control using brakes but without a reduction
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西锐20飞机信息手册 SR22 AIRPLANE INFORMATION MANUAL 2979(32)
