I A P 2 0 2 0 . 0 0 1 - A F M /
J A B I R U J 1 6 0 / J 1 7 0
P a g e
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62
FOR SIMULATION USE ONLY
The performance information is not valid when the outside air temperature
and/or pressure height exceeds the maximum values for which this
information is scheduled.
Figure 4-3 Take Off Distance
For every 1 knot of head-wind component, the take-off distance can be
reduced by 11 meters.
For every 1 knot of tail-wind component the take-off distance required MUST
be increased by 16 meters.
Landing Distances
The landing distance table presented below provides information to achieve
the minimum landing distance for a variety of operating conditions. The data
is applicable when using a power off glide approach with the flaps extended
to the “Landing Flap” or fully extended position, and is based on landing
distances from a height of 15 metre (50 feet) to stop.
The landing distance is provided for a hard bitumen surface. Wet and/or
slippery surfaces will increase the landing distance over that scheduled and
the pilot should therefore ensure that adequate strip length is available to
cover these conditions.
The technique used in establishing the Power Off Approach Landing Chart
distance is such that the aircraft approaches with idle power down to the 15
metre (50 foot) height point at 63 KIAS. After touch down maximum wheel
braking is used to bring the aircraft to a stop.