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Eiri KY PIK-20 E - Stalls

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PIK-20
E
Flight
manual
Unlock
the
cranking
lever
and
extend
the
engine
by
turning
fifteen
turns
clockwise.
The
lever
has
to
be
left
in
such
position
that
the
safety
cable
is
tautened.
When
the
door/brake
lever
is
moved
forward
the
propeller should
ro
tate
slowly
in
the
air.
This
can
be
checked
in
the
mirror.
When
starting
the
engine
the
main
switch
should
be
on.
Turn
ignition
and
electric
fuel
pump
on.
Adjust
the
choke
3/4
open,
if
the
engine
is
cold.
The
throttle
should
be
opened
about
1/4.
The
engine
needs
now
only
a
kick
with
the
starter
and
the
propeller
will
then
rotate
by
itself
in
the
airstream.
Adjust
the
choke
and
throttle
when
the
engine
is
running.
If
the
battery
is
dead
or
if
there
is
some
other
reason
not
to
use
the
starter,
the
engine
can
be
started
by
windmilling.
The
speed
required
to
get
the
propeller
rotating
(windmilling)
is
about
165
km/h
(103
mph,
89
kts).
When
the
propeller
once
is
rotating,
it
can
be
stopped
only
by
re
ducing
speed
and
using
the
brake.
The
altitude
required
to
extend
and
start
the
engine
is
normally
60
to
30
meter
(200
to
100
feet)
when
using
the
starter.
In
an
outlanding
this
operation
can
be
made
safely
on
the
downwind
leg.
The
height
in
the
beginning
of
the
downwind
leg
should
be
at
least
300
m
(1000
ft)
to
give
time
enough
if
something
goes
wrong.
If
the
engine
does
not
start
it
is
possible
to
land
with
the
engine
extended.
The
flight
should
be
planned
as
a
flight
with
a
sailplane
without
an
engine.
There
should
always
be
the
possibility
to
land
and
one
should
not
go
down
over
an
area
unacceptable
for
outlandings.
There
is
always
the
possibility
that
the
engine
does
not
start,
especially
when
one
tries
to
start
the
engine
in
a
rush
above
a
forest
or
rocky
area.
5.19
Stalls
In
stall
the
nose
drops
without
stall
warning
with
retracted
airbrakes.
With
airbrakes
extended
stall
warning
is
noticed
about
10
km/h
(6
mph,
5
kts)
before
the
stall.
With
the
engine
extended
one
wing
may
drop
slightly.
The
altitude
loss
is
about
12
to
6
m
(40
to
20
ft).
When
stalled
in
a
45°
banked
turn
with
the
engine
and
airbrakes
extended,
the
loss
of
height
may
be
60
m
(200
ft).
EIRI
KY
J
Kisällinkatu
8
SF-15170
Lahti
17
page
1-32

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