Textron Cessna Grand Caravan Ex 208B Pilot's Operating Handbook And Faa Approved Airplane Flight Manual page 727

CESSNA SECTION 9 - SUPPLEMENTS
MODEL 208B 867 SHP SUPPLEMENT 1
GARMIN G1000
AIRPLANE SYSTEMS AND DESCRIPTIONS
(Continued)
ICE DETECTION AND WING INSPECTION LIGHTS
The windshield ice detection and wing inspection lights are used at
night, or in conditions of poor visibility, to detect the presence of ice
accumulating on the lower center portion of the windshield and leading
edge of the left wing.
The windshield ice detection light is located on the left side of the
windshield center post. This light would typically be used first to visually
detect the presence of ice accumulating on the windshield. The
windshield ice detection light is activated anytime the NAV Switch is in
the ON position.
The wing inspection light is flush-mounted in the left wing leading edge-
to-fuselage fairing to help detect ice on the wing at night by lighting the
leading edge of the wing. The system consists of the wing inspection
light, a two-position toggle switch located on the anti-ice switch panel
and a pull-off type circuit breaker, labeled WING ICE DET LIGHT,
located on the left sidewall circuit breaker panel. The WING LIGHT
switch is spring-loaded to the OFF, or down position, and must be held
in the ON or up position to activate the light.
ENGINE INERTIAL SEPARATOR, STANDBY ELECTRICAL,
AND HEATED STALL WARNING SYSTEMS
Refer to Section 7, Airplane and System Description of the POH/AFM
for descriptions of these standard/required equipment items.
FAA APPROVED
208BPHCUS-S1-00 S1-75
U.S.