Pilot’s Operating Handbook
5-27
DO NOT USE FOR FLIGHT OPERATIONS
Section 5
PERFORMANCE
100 SERIES
Performance
5-14 ENROUTE RATE OF CLIMB
(Refer to the tables on the following page)
Conditions:
Flaps
..........................................................................................................0°
Power
................................................................................. Maximum Climb
Inertial Separator
...............................................................................Normal
Airspeed
.............................................................................................V
Air Conditioning ....................................................................................... Off
MAXIMUM CLIMB POWER – FLAPS 0°
Example:
Outside Air Temp
.................................................................................... 0°C
Weight
..................................................................................... 7255 pounds
Pressure Altitude
...........................................................................10000 FT
Climb Airspeed: 101 KIAS
Rate of Climb: 788 FT/MIN
NOTES:
• Do not exceed the placarded maximum climb torque, ITT (765°C) and
(101.6%) limits, or the charted max climb torque from “Figure 5-3.”
• For operation in temperatures colder than provided in this table, use
the coldest data shown.
• For operation in temperatures warmer than provided in this table, use
extreme caution.
• Dashed entries correspond to outside air temperatures beyond the
aircraft operating limits, or appreciable rate of climb for the weight
shown cannot be expected.
NOTE: Blue numbers indicate performance with Air Conditioning
ON, black numbers indicate performance with Air Conditioning OFF.
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