Balked Landing Climb Gradient - Kodiak 100 Series Information Manual

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BALKED LANDING CLIMB GRADIENT

(Refer to the tables on the following page)
Conditions:
Power ........................................................................................Max Takeoff
Flaps ........................................................................................... 35° (Down)
Climb Airspeed ................................................................................74 KIAS
Winds ....................................................................................................Zero
Air Conditioning ....................................................................................... Off
Example:
Outside Air Temp .................................................................................. 20°C
Weight ..................................................................................... 6690 pounds
Pressure Altitude ........................................................................... 6000 feet
NOT ES :
• Balked Landing Climb Gradients shown represent the gain in altitude
for the horizontal distance traveled and is expressed as Feet per
Nautical Mile.
• For operation in air colder than provided in this table, use the coldest
charted data.
• This chart is required data for aircraft certification. However,
significantly better performance may be achieved by climbing at the
Best Rate of Climb speeds with the flaps positioned at 20° or following
the Go-Around / Balked Landing procedure outlined in "Section 4."
• Dashed entries correspond to outside air temperatures beyond the
aircraft operating limits.
Blue numbers
NOT E:
ON
, black numbers indicate performance with
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: 74 KIAS
Climb Gradient: 558 FT/NM
Air Conditioning
Air Conditioning
OFF.
5 - 6 5