曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
d. Wheel and Tire ..........................Condition, Inflation, and Wear
e. Propeller ...........................Condition (indentations, nicks, etc.)
f. Spinner ...............................Condition, Security, and Oil Leaks
g. Air Inlets.............................................................. Unobstructed
June 2007
Information Manual 4-9
Cirrus Design Section 4
SR22 Normal Procedures
h. Alternator...................................................................Condition
10. Nose, Left Side
a. Landing Light.............................................................Condition
b. Engine Oil.........Check 6-8 quarts, Leaks, Cap & Door Secure
c. Cowling.....................................................Attachments Secure
d. External Power .....................................................Door Secure
e. Vortex Generator .......................................................Condition
f. Exhaust Pipe(s) .................Condition, Security, and Clearance
11. Left Main Gear and Forward Wing
a. Wheel fairings....................... Security, Accumulation of Debris
b. Tire ............................................Condition, Inflation, and Wear
• Caution •
Serials 0002 through 1727 after Service Bulletin SB 2X-32-14
and airplane serials 1728 and subsequent: Clean and inspect
temperature indicator installed to piston housing. If indicator
center is black, the brake assembly has been overheated. The
brake linings must be inspected and O-rings replaced.
c. Wheel and Brakes ....... Fluid Leaks, Evidence of Overheating,
General Condition, and Security.
d. Chocks and Tiedown Ropes........................................Remove
e. Fuel Drains (2 underside) ............................ Drain and Sample
f. Cabin Air Vent......................................................Unobstructed
g. Fuel Cap.......................................Check Quantity and Secure
h. Leading Edge and Stall Strips ...................................Condition
12. Left Wing Tip
a. Fuel Vent (underside) ..........................................Unobstructed
b. Pitot Mast (underside) .................Cover Removed, Tube Clear
c. Strobe, Nav Light and Lens ..................Condition and Security
d. Tip .........................................................................Attachment
(Continued on following page)
June 2007
4-10 Information Manual
Section 4 Cirrus Design
Normal Procedures SR22
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
2. Emergency Equipment.................................................ON BOARD
3. 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.
4. 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.
June 2007
Information Manual 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.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR22(27)
