BALKED LANDING CLIMB GRADIENT
(Refer to the table on the following page)
Conditions:
Power
............................................................................... MAX TAKEOFF
Flaps
........................................................................................ 35° (Down)
Climb Airspeed
.............................................................................76 KIAS
Winds
..................................................................................................Zero
Air Conditioning
.................................................................................... Off
Example:
Outside Air Temp
............................................................................... 20°C
Weight
...............................................................................7255 POUNDS
Pressure Altitude
.....................................................................6000 FEET
Climb Airspeed: 76 KIAS
Climb Gradient: 414 FT/NM
NOTE: Blue numbers indicate performance with Air Conditioning
ON, black numbers indicate performance with Air Conditioning OFF.
NOTES:
• Balked Landing Climb Gradients shown represent the gain in altitude
for the horizontal distance traveled and are 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 certication. However,
signicantly better performance may be achieved by climbing at the
Best Rate of Climb speeds with the aps 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.
• The 6690 lb chart is provided for interpolation only. For landing weights
of 6690 lb or less, use the tables found in the main body of the manual
along with a climb speed of 74 KIAS.
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