Pilot’s Operating Handbook
5-25
DO NOT USE FOR FLIGHT OPERATIONS
Section 5
PERFORMANCE
100 SERIES
Performance
5-13 TAKEOFF CLIMB GRADIENT
(Refer to the tables on the following page)
Conditions:
Flaps
........................................................................................................20°
Power
............................................................................... Maximum Takeoff
Inertial Separator
...............................................................................Normal
Airspeed
...................................................................................................
Winds ....................................................................................................Zero
Air Conditioning
....................................................................................... Off
Example:
Outside Air Temp
.................................................................................. 40°C
Weight
..................................................................................... 7255 pounds
Pressure Altitude
.............................................................................2000 FT
Climb Airspeed: 88 KIAS
Climb Gradient: 479 FT/NM
NOTES:
• Do not exceed the maximum climb power torque, ITT and
limits.
• This table represents the gain in altitude for the horizontal distance
traveled and is expressed as feet per Nautical Mile.
• Dashed entries correspond to outside air temperatures beyond the
aircraft operating limits.
NOTE: Blue numbers indicate performance with Air Conditioning
ON, black numbers indicate performance with Air Conditioning OFF.
NOTE: Red shaded areas represent data at temperatures greater than
the maximum approved operating OAT, but may be used for the purpose of
interpolating.
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