SECTION 9 - SUPPLEMENTS
CESSNA
SUPPLEMENT 1
MODEL 208B 867 SHP
GARMIN G1000
U.S.
FAA APPROVED
NORMAL PROCEDURES
(Continued)
BEFORE STARTING ENGINE
1.
TKS Ice Protection System:
a.
Windshield Pump . . . . . . . . . . . . . . . . . . . . . . . . . .
CHECK
(1) MAX FLOW Switch . . . . . . . . . . . . . . . .
WINDSHIELD
(press momentarily and verify spray on pilot’s
windshield)
b.
TKS Ice Protection System Pumps. . . . . . . . . . . . .
CHECK
(1) PRIMARY Switch . . . . . . . . . . . . . . . . . . . . . . . .
HIGH
(verify white A-ICE HIGH annunciator comes on, listen
for pump operation)
(2) PRIMARY Switch . . . . . . . . . . . . . . . . . . . . . . .
NORM
(verify white A-ICE NORM annunciator comes on)
(3) MAX FLOW Switch . . . . . . . . . . . . . . . . . .
AIRFRAME
(press momentarily and check operation)
(4) PRIMARY Switch . . . . . . . . . . . . . . . . . . . . . . . . .
OFF
(verify white A-ICE NORM annunciator goes off)
c.
BACKUP Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
ON
(verify pump is running; then OFF)
d.
A-ICE Annunciator . . . . . . . . . . . . . . . . . . . . .
VERIFY OFF
2.
INERTIAL SEPARATOR . . . . . . . . . . . . . . . . . . . . . . .
BYPASS
(rotate counterclockwise and PULL out)
(visible moisture and OAT 5°C (41°F) or below)
CAUTION
If the INERTIAL SEPARATOR is set to BYPASS at any
point due to suspected or actual icing conditions, do not
return it to NORMAL until the inertial separator door has
been visually inspected and verified free of ice and ice
protection fluid.
208BPHCUS-S1-00
S1-38
Summary of Contents for Cessna Grand Caravan Ex 208B
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