Specifications

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