Cirrus DESIGN SR20 Information Manual page 90

Section 4
Normal Procedures
c. Fuel Drains (2 underside) ............................ Drain and Sample
d. Wheel Fairings...................... Security, Accumulation of Debris
e. Tire ............................................Condition, Inflation, and Wear
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
Keep clear of propeller rotation plane. Do not allow others to
approach propeller.
a. Tow Bar........................................................Remove and Stow
b. Strut ...........................................................................Condition
c. Wheel Fairing........................ Security, Accumulation of Debris
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
h. Alternator Belt....................................... Condition and Tension
4-8
• Note •
• WARNING •
Cirrus Design
P/N 13999-002 Info Manual
September 2011
SR20