SECTION 9 - SUPPLEMENTS CESSNA
SUPPLEMENT 1 MODEL 208B 867 SHP
GARMIN G1000
U.S.
FAA APPROVED
NORMAL PROCEDURES (Continued)
PREFLIGHT INSPECTION
CABIN
1. BATTERY Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
2. AVIONICS No. 1 Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
IF OAT IS BELOW 15°C (59°F)
With TKS Ice Protection System fluid temperatures at
or above 15°C (59°F) the fluid viscosity will decrease,
or become thinner, and may affect proper fluid flow to
parts of individual panels. If OAT is above 15°C (59°F),
refer to the procedure on the following pages.
3. BACKUP Switch . . . . . . . . . ON FOR 4 MINUTES; THEN OFF
Listen for pump operation, verify red A-ICE PRESS LOW
annunciator initially comes ON then goes OFF as system
flow and pressure build.
4. NAV Lights Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
5. Windshield Ice Detection Light . . CHECK FOR ILLUMINATION
6. WING LIGHT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
(verify wing inspection light on)
7. LED PANELS/ANNUN Rheostat . . . . . . . . . . . . . . . . . ADJUST
(for ambient lighting conditions)
8. P/S HEAT/LOW A/S AWARE Switch. . ON FOR 30 SECONDS;
THEN OFF
9. BELOW ICING MIN SPD Light . . . . . . . . . . . . . . . . VERIFY ON
(check light brightness for ambient conditions)
10. STALL HEAT Switch . . . . . ON FOR 30 SECONDS; THEN OFF
11. All Switches. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
(Continued Next Page)
208BPHCUS-S1-00
S1-34