Pipistrel VELIS Electro, Pilot Operating Handbook

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5-9
VELIS Electro
Pilot's Operating Handbook
POH - 128 - 00 - 40 - 001
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PAGE
SECTION 5
PERFORMANCE DATA
APPROVED
5.6 TAKE OFF DISTANCE
Conditions Power: MPTOP (50kW)
Flaps: (+1)
Wind: Calm
Mass: 600 kg
Runway condition: dry
Speed at lift o
ff : 50 KIAS
Speed over the obstacle: 57 KIAS (V
X
)
Take off performance data included in this POH are extrapolated from flight
test results. These extrapolated values serve as an estimation of actual take
off roll and total distance to clear a 50 ft obstacle (ground roll plus climb
distance to clear obstacle).
Correction Factors
Headwind: Subtract 10% for each 12 knots headwind.
Tailwind: Add 10% for each 2 knots tailwind up to 10 knots.
Wet Grass: Add 18% to ground roll on dry grass.
Runway Slope
Increase table distances by 22% of the ground roll distance at sea level for
each 1% of upslope.
Decrease table distances by 7% of the ground roll distance at sea level, for
each 1% of downslope.