CESSNA
SECTION 8
MODEL 208B 867 SHP
AIRPLANE HANDLING, SERVICE
GARMIN G1000
AND MAINTENANCE
U.S.
GROUND DEICE/ANTI-ICE OPERATIONS
(Continued)
HOLDOVER TIMETABLE (TYPE I, TYPE II, TYPE III, AND
TYPE IV FLUIDS)
(Continued)
TYPE I DEICE FLUID
NOTE
•
Freezing point of Type I fluid mixture must be at least
10°C (18°F) below OAT.
•
Holdover time starts when last application has begun.
•
Type I fluid should be sprayed on the airplane (with
engine off) in a manner which minimizes heat loss to the
air. If possible, fluid should be sprayed in a solid cone
pattern of large coarse droplets at a temperature of
160°F to 180°F. The fluid should be sprayed as close as
possible to the airplane surfaces, but not closer than 10
feet if a high pressure nozzle is used.
WARNING
When ground icing conditions are present, a
pretakeoff contamination check should be
conducted by the pilot in command within 5
minutes of takeoff, preferably just prior to taxiing
onto the active runway. Critical areas of the
airplane such as empennage, wings, windshield,
control surfaces, and engine inlets should be
checked to make sure they are free of ice, slush,
and snow, and that the anti-ice fluid is still
protecting the airplane.
208BPHCUS-00
8-37
Summary of Contents for Cessna Grand Caravan Ex 208B
Page 2: ......
Page 351: ...CESSNA SECTION 5 MODEL 208B 867 SHP PERFORMANCE GARMIN G1000 U S Figure 5 23 208BPHCUS 00 5 63...
Page 352: ...SECTION 5 CESSNA PERFORMANCE MODEL 208B 867 SHP GARMIN G1000 U S Figure 5 24 208BPHCUS 00 5 64...
Page 353: ...CESSNA SECTION 5 MODEL 208B 867 SHP PERFORMANCE GARMIN G1000 U S Figure 5 25 208BPHCUS 00 5 65...
