CESSNA SECTION 9 - SUPPLEMENTS
MODEL 208B 867 SHP SUPPLEMENT 1
GARMIN G1000
U.S.
FAA APPROVED
EMERGENCY PROCEDURES (Continued)
AMBER A-ICE PRESS HI OR A-ICE FLUID LO
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
(or greater until final approach and landing)
3. Icing Conditions . . . . . . . . . . . EXIT AS SOON AS POSSIBLE
4. Landing Distance . . . . . MULTIPLY POH/AFM DISTANCE BY:
2.2 - WING FLAPS UP
2.1 - WING FLAPS TO/APR
5. Minimum Approach Airspeed . . . . . . . . . . . . . . AT OR ABOVE:
120 KIAS - WING FLAPS UP
110 KIAS - WING FLAPS TO/APR
• 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.
(Continued Next Page)
S1-21208BPHCUS-S1-00
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