3-8 P/N 23020-002
Cirrus SR20 and SR22 Flight Operations Manual
Section 3 Standard Operating Procedures
3. Empennage
a. Tie Down Rope............................................................Remove
Visually verify tail tie down is removed and stowed.
b. Horizontal and Vertical Stabilizers .............................Condition
Inspect leading edges and top of vertical stabilizer for any
abnormalities. Ensure the clear tape covering inspection hole
on outer tip of elevator, inside of elevator horn is intact.
c. Elevator and Tab............................... Condition and Movement
Check elevator for range of motion. Inspect tab on left side of
elevator for condition. Visually inspect counter weight inside
elevator horn for security. Check all hinges, bolts and cotter
pins.
d. Rudder............................................... Freedom and Movement
Inspect for full range of motion. Inspect all hinges, bolts and
cotter pins from the left side of the rudder. Visually inspect
counter weight inside top leading edge of rudder horn for
security.
e. Rudder Trim Tab ...................................Condition and Security
f. Attachment Hinges, Bolts and Cotter Pins ................... Secure
Verify all moveable control surfaces are secure and all bolts
and cotter pins are in place.
4. Right Fuselage
a. Static Button .............................................. Check for Blockage
Ensure removal of static covers and check for any blockage
within static port openings.
b. Wing/Fuselage Fairings ..................................................Check
Visually inspect the wing root fairing for attachment along
upper and lower surfaces of wing root.
c. Door Lock .................................................................. Unlocked
Ensure the door lock is in the unlocked position to allow
outside entry into the aircraft in the event of an accident.
June 2008
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