Cirrus SR22 Pilot's Operating Handbook And Flight Manual page 474

Section 9
Supplements
n. PITOT HEAT Switch........................ ON 45 seconds, then OFF
2. Empennage
a. Stabilizers Porous Panels ................CONDITION / SECURITY
(1) Verify Evidence of Deicing Fluid Along Length of Panels
and Elevator Horns.
3. Right Wing Forward and Main Gear
a. Fluid Tank ................................ VERIFY DESIRED QUANTITY
(1) Filler Cap........................... CONDITION AND SECURITY.
(2) Fluid Vent (underside wing).................. UNOBSTRUCTED
b. Porous Panels........................... CONDITION AND SECURITY
(1) Verify Evidence of Deicing Fluid Along Length of Panels.
Lift Transducer Faceplate and Vane may be HOT.
c. Lift Transducer Faceplate ........................ PERCEPTIBLY HOT
d. Lift Transducer Vane ...............................................VERY HOT
(1) Verify Stall Warning audio alert after lifting stall vane with
wooden tooth pick or tongue depressor.
4. Nose, Right Side
a. Ice-Inspection Light .........................CONDITION / SECURITY
5. Nose Gear, Propeller, Spinner
a. Slinger Ring .......................... EVIDENCE OF DEICING FLUID
6. Nose, Left Side
a. Ice-Inspection Light .........................CONDITION / SECURITY
b. Windshield Spray Nozzles ...............CONDITION / SECURITY
7. Left Wing Forward and Main Gear
a. Fluid Tank ................................ VERIFY DESIRED QUANTITY
(1) Filler Cap........................... CONDITION AND SECURITY.
(2) Fluid Vent (underside wing).................. UNOBSTRUCTED
b. Porous Panels..................................CONDITION / SECURITY
(1) Verify Evidence of Deicing Fluid Along Length of Panels.
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• WARNING •
Cirrus Design
P/N 13772-150
Original Issue: 02-01-13
SR22