Takeoff Climb Gradient - Kodiak 100 Series Information Manual

Uncontrolled if printed

5-13 TAKEOFF CLIMB GRADIENT

(Refer to the tables on the following page)
Conditions:
Flaps ........................................................................................................20°
Power ............................................................................... Maximum Takeoff
Inertial Separator ...............................................................................Normal
Airspeed ................................................................................................... V
Winds ....................................................................................................Zero
Air Conditioning ....................................................................................... Off
Example:
Outside Air Temp .................................................................................. 40°C
Weight ..................................................................................... 7255 pounds
Pressure Altitude .............................................................................2000 FT
NOTE S :
• Do not exceed the maximum climb power torque, ITT and N
• 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.
Blue numbers
NOT E:
ON
, black numbers indicate performance with
NO TE : Red shaded areas represent data at temperatures greater than
the maximum approved operating OAT, but may be used for the purpose of
interpolating.
P i l o t 's O p e r a t i n g H a n d b o o k
1 0 0 S E R I E S
indicate performance with
D O N OT U S E FO R FL I G H T O PE R AT I O N S
S e c t i o n 5
P E R FO R M A N C E
Climb Airspeed: 88 KIAS
Climb Gradient: 479 FT/NM
limits.
g
Air Conditioning
Air Conditioning
OFF.
y
5 - 2 5