4-8
P/N 13772-005
Section 4
Cirrus Design
Normal Procedures
SR22T
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 •
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
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
Original Issue
