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PIK-20
E
Flight
manual
Note
1:
Use
of
+8°
flaps
shortens
the
takeoff
by
15
%.
Note
2:
Concrete
runway
shortens
the
takeoff
by
10
%.
Note
3:
10
km/h
headwind
shortens
the
takeoff
by
25
%.
10
km/h
tailwind
lengthens
the
takeoff
by
30
%.
Example:
Weight
420
kg
Temperature
25°
C
Pressure
altitude
1200
m
Headwind
component
10
km/h
Flaps:
neutral
and
grass
runway
From
figure
7.3.
and
7.4
Ground
roll
360
m
Total
to
clear
15
m
obs.
690
m
Airspeed
at
lift-off
86
km/h
at
15
m
102
km/h
Headwind
component
correction.
690
-
10
0,25
690
=
520
m
10
7.2.4.
Climb
Rate
of
climb
with
takeoff
power.
Sea
level,
temperature
+
15°C
(gear
retracted
flaps
0°.
.
.
+
8°)
W
=
360
kg
4.0
m/s
(790
fpm)
Optimum
speed
flaps
90
km/h
(56
mph,
49
kts)
flaps
+
85
km/h
(53
mph,
46
kts)
W
=
470
kg
2.8
m/s
(550
fpm)
Optimum
speed
flaps
100
km/h
(62
mph,
54
kts)
flaps
+
95
km/h
(59
mph,
51
kts)
Note
1:
Use
of
max
continuous
power
reduces
the
rate
of
climb
by
0.35
m/s
(70
fpm).
EIRI
KY
J
Kisällinkatu
8
SM5170
Lahti
17
page
I
-46

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