Textron Cessna Grand Caravan Ex 208B Pilot's Operating Handbook And Faa Approved Airplane Flight Manual page 673

CESSNA
MODEL 208B 867 SHP
GARMIN G1000
EMERGENCY PROCEDURES
AMBER A-ICE
ANNUNCIATOR COMES ON
1. Icing Conditions . . . . . . . . . . . EXIT AS SOON AS POSSIBLE
2. TKS Ice Protection System. . . . . . . . . . . . . . . . . . . . MONITOR
FAILURE OF ICE PROTECTION SYSTEM OR EXCESSIVE
ICE ACCUMULATION (OBSERVED OR SUSPECTED) ON
PROTECTED AIRPLANE SURFACES
1. MAX FLOW Switch . . . . . . . . . . . . . . . . . . . . . . . . . AIRFRAME
2. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . MAINTAIN 120 KIAS
3. Icing Conditions . . . . . . . . . . . EXIT AS SOON AS POSSIBLE
4. Landing Distance . . . . . MULTIPLY POH/AFM DISTANCE BY:
5. Minimum Approach Airspeed . . . . . . . . . . . . . . AT OR ABOVE:
•
With an inoperative TKS Ice Protection System
porous panel(s), increase power to Maximum
Rated and exit icing conditions as soon as
possible. In heavy icing conditions, it may not be
possible to maintain altitude or proper glide path
on approach. In this case, it is imperative that a
safe airspeed be maintained.
•
Stall speeds will increase with ice accumulation
on the wing and tail leading edges. Expect higher
than normal rates of descent with power
reduction.
FAA APPROVED
208BPHCUS-S1-00
PRESS HI OR
(or greater until final approach and landing)
110 KIAS - WING FLAPS TO/APR
WARNING
(Continued Next Page)
SECTION 9 - SUPPLEMENTS
SUPPLEMENT 1
(Continued)
A-ICE FLUID
2.2 - WING FLAPS UP
2.1 - WING FLAPS TO/APR
120 KIAS - WING FLAPS UP
U.S.
LO
S1-21