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l. Fuel Selector ..............................................Select Fullest Tank
m. Flaps.................................................... 100%, Check Light ON
n. Oil Annunciator .................................................................... On
o. Bat 1 and 2 Master Switches.............................................OFF
p. Alternate Static Source............................................. NORMAL
q. Circuit Breakers .................................................................... IN
r. Fire Extinguisher ..................................Charged and Available
s. Emergency Egress Hammer ......................................Available
t. CAPS Handle .................................................... Pin Removed
2. Left Fuselage
a. COM 1 Antenna (top) ..................... Condition and Attachment
b. Wing/Fuselage Fairing....................................................Check
c. COM 2 Antenna (underside)........... Condition and Attachment
June 2007
Information Manual 4-7
Cirrus Design Section 4
SR22 Normal Procedures
d. Baggage Door ........................................... Closed and Secure
e. Static Button ..............................................Check for Blockage
f. Parachute Cover........................................ Sealed and Secure
3. Empennage
a. Tiedown Rope .............................................................Remove
b. Horizontal and Vertical Stabilizers.............................Condition
• Note •
Verify tape covering the forward and aft inspection holes
located on outboard ends of horizontal stabilizer is installed
and securely attached.
c. Elevator and Tab............................... Condition and Movement
d. Rudder.................................................. Freedom of Movement
e. Rudder Trim Tab ...................................Condition and Security
f. Attachment hinges, bolts and cotter pins ......................Secure
4. Right Fuselage
a. Static Button ..............................................Check for Blockage
b. Wing/Fuselage Fairings..................................................Check
5. Right Wing Trailing Edge
a. Flap and Rub Strips (if installed) ..........Condition and Security
b. Aileron and Tab ................................ Condition and Movement
c. Aileron Gap Seal .........................................................Security
d. Hinges, actuation arm, bolts, and cotter pins ................Secure
6. Right Wing Tip
a. Tip ..........................................................................Attachment
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
b. Fuel Cap.......................................Check Quantity and Secure
(Continued on following page)
June 2007
4-8 Information Manual
Section 4 Cirrus Design
Normal Procedures SR22
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
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AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR22(26)
