SECTION 9 - SUPPLEMENTS
CESSNA
SUPPLEMENT 7
MODEL 208B 867 SHP
GARMIN G1000
U.S.
FAA APPROVED
PERFORMANCE
(Continued)
CLIMB
When climbing at altitudes above the critical altitude (if at maximum
climb ITT limit and torque below 2397 FT-LBS), there is a 25 FPM loss
in maximum rate of climb.
CRUISE
When cruising at altitudes where the maximum allowable cruise power
is below the torque limit, reduce this setting by 40 FT-LBS when the air
conditioner is operating, refer to Section 5, Performance, Cruise
Performance charts, for allowable cruise power torque limits. This
reduced power setting will result in an approximate 2 KTAS decrease in
maximum cruise performance and a slight increase (1%) in fuel
required for a given trip.
208BPHCUS-S7-00
S7-12
Summary of Contents for Cessna Grand Caravan Ex 208B
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