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6. Right Wing Tip
a. Tip ..........................................................................Attachment
b. Strobe, Nav Light and Lens ..................Condition and Security
c. Fuel Vent (underside) ..........................................Unobstructed
(Continued on following page)
Revision A8
4-8 P/N 13772-001
Section 4 Cirrus Design
Normal Procedures SR22
7. Right Wing Forward and Main Gear
a. Leading Edge and Stall Strips ...................................Condition
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 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.
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. Vortex Generator .......................................................Condition
b. Cowling.................................................... Attachments Secure
c. Exhaust Pipe ....................Condition, Security, and Clearance
d. Transponder Antenna (underside) .. Condition and Attachment
e. 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
c. Wheel Fairing........................ Security, Accumulation of Debris
d. Wheel and Tire ..........................Condition, Inflation, and Wear
Revision A8
P/N 13772-001 4-9
Cirrus Design Section 4
SR22 Normal Procedures
e. Propeller ........................... Condition (indentations, nicks, etc.)
f. Spinner ............................... Condition, Security, and Oil Leaks
g. Air Inlets ..............................................................Unobstructed
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
(Continued on following page)
Revision A8
4-10 P/N 13772-001
Section 4 Cirrus Design
Normal Procedures SR22
c. Strobe, Nav Light and Lens ..................Condition and Security
d. Tip ..........................................................................Attachment
　
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