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

13. Left Wing Trailing Edge
a. Flap And Rub Strips (If installed)..........Condition and Security
b. Aileron ..................................................Freedom of movement
c. Aileron Gap Seal .........................................................Security
d. Hinges, actuation arm, bolts, and cotter pins ............... Secure
Before Starting Engine
1. Preflight Inspection .................................................. COMPLETED
• WARNING •
Ensure that the airplane is properly loaded and within the
AFM’s weight and balance limitations prior to takeoff.
2. Weight and Balance............................................Verify within limits
3. Emergency Equipment.................................................ON BOARD
4. Passengers ..................................................................... BRIEFED
• Note •
Ensure all the passengers have been fully briefed on smoking,
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.
Revision A8
P/N 13772-001 4-11
Cirrus Design Section 4
SR22 Normal Procedures
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)
Revision A5
4-12 P/N 13772-001
Section 4 Cirrus Design
Normal Procedures SR22
4. Strobe Lights ............................................................................. ON
5. Mixture ......................................................................... FULL RICH
6. Power Lever ........................................................FULL FORWARD
7. Fuel Pump.....................................................PRIME, then BOOST
• Note •
Serials 0002 - 0278 before SB 22-73-01: On first start of the
day, especially under cool ambient conditions, holding Fuel
Pump switch to PRIME for 30-60 seconds will improve
starting.
Serials 0002 - 0278 after SB 22-73-01 and serials 0279 and
subsequent: 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
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：CIRRUS DESIGN SR22西銳22飛行員操作手冊和飛機飛行手冊(32)