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b. Strobe, Nav Light and Lens ..................Condition and Security
c. Fuel Vent (underside) ..........................................Unobstructed
7. Right Wing Forward and Main Gear
a. Leading Edge and Stall Strips ...................................Condition
(Continued on following page)
March 2010
4-8 Information Manual
Section 4 Cirrus Design
Normal Procedures SR20
b. Fuel Cap .......................................Check Quantity and Secure
c. Fuel Drains (2 underside) ............................Drain and Sample
d. Wheel Fairings...................... Security, Accumulation of Debris
e. Tire ............................................Condition, Inflation, and Wear
• Caution •
Serials 1005 through 1592 after Service Bulletin SB 2X-32-14
and airplane serials 1593 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.
f. Wheel and Brakes ....... Fluid Leaks, Evidence of Overheating,
General Condition, and Security.
g. Chocks and Tiedown Ropes........................................Remove
h. Cabin Air Vent..................................................... Unobstructed
8. Nose, Right Side
a. Cowling.................................................... Attachments Secure
b. Exhaust Pipe ....................Condition, Security, and Clearance
c. Transponder Antenna (underside) .. Condition and Attachment
d. Gascolator (underside) ................Drain for 3 seconds, Sample
9. Nose gear, Propeller, and Spinner
• WARNING •
Keep clear of propeller rotation plane. Do not allow others to
approach propeller.
a. Tow Bar........................................................Remove and Stow
b. Strut ...........................................................................Condition
• Note •
Serials 1337 and subsequent with SRV standard
configuration: The airplane is not equipped with a nose wheel
fairing.
c. Wheel Fairing........................ Security, Accumulation of Debris
d. Wheel and Tire ..........................Condition, Inflation, and Wear
March 2010
Information Manual 4-9
Cirrus Design Section 4
SR20 Normal Procedures
e. Propeller ........................... Condition (indentations, nicks, etc.)
f. Spinner ............................... Condition, Security, and Oil Leaks
g. Air Inlets ..............................................................Unobstructed
h. Alternator Belt........................................Condition and Tension
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. Exhaust Pipe .....................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 1005 through 1592 after Service Bulletin SB 2X-32-14
and airplane serials 1593 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
(Continued on following page)
March 2010
4-10 Information Manual
Section 4 Cirrus Design
Normal Procedures SR20
d. Tip ..........................................................................Attachment
13. Left Wing Trailing Edge
a. Flap And Rub Strips (If installed)..........Condition and Security
b. Aileron ..................................................Freedom of movement
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西锐20飞机信息手册CIRRUS DESIGN SR20 AIRPLANE INFORMATION MA(27)
