P/N 13772-115 7 of 20
Cirrus Design Section 9
SR22 / SR22T Supplements
a. Slinger Ring.......................... EVIDENCE OF DEICING FLUID
5. Left Wing Forward and Main Gear
a. Serials with G3 Wing:
(1) Fluid Tank.......................... VERIFY DESIRED QUANTITY
(a) Filler Cap ..............................CONDITION / SECURITY
(b) Vent (underside of wing).................. UNOBSTRUCTED
b. Wing Porous Panels ........................CONDITION / SECURITY
(1) Verify Evidence of Deicing Fluid Along Length of Panels.
6. Cabin
a. Serials w/ Perspective Avionics:
(1) Fluid Quantity........................................................ CHECK
7. Ice Protection System ..............................................................OFF
8. BAT 1 Switch............................................................................ OFF
Revision 10: 09-20-12