advcrntage
of the partial
power
approach is
eae,se
of glide path
cuntrol
by slight imxeases or reductiom in the amount of
pamr.
The
full-flap
no”~~“wer
landing,
while
not
difficult, fe usually
desirable
only
as
an.
emergency procedure,
Inatrucdon
in this
type of landing is
laeceasary,
In order to make
amooth
landings,
it
iavolves
a
different te&nique with which
Ccmrier
pilato
rahcmld
be famiI.iar. For
ful,I-flap,
no-pop~rer
Landingr,
it
is
advisable that the
pflot
keep
the
aipproach
*peed
st
60 to 65
MPH,
but not
below
60
WEi.
miatain
arpproach
speed of 60 to 63 MPH
=ii-&ec~f~s
just off
the
rummy,
With power-off, the
flare
out
ahould
not
be ataxted tm3.l
wfthfn
10
to
Z3
feet off
the ground m that the
n6se:
barely
ecmm
up to the full landing
positfsa
just
as
the
sircxaft
sinks
dowa
to
gmuad
level.
whfch
is
a
safety feature for emergency
or
forced
land$.ngs,
Consequently,
a
stfghtly
high flare-out will quickly
re8uft
in
a
xelcrtfvely
high rate of descent,
Le,
j
a hard landing!
:
Use
of
full-flape
without
.puwer
iar
nomally
done
ocrly
in
emelpgency
landings
s
Normal
SIXJL
approaches with full-flap8
are
best
accomplighed
with
part&al
power
so
a~
to
xmintaia
tssentially
the
mme
flight-psth’arrgle
at about 55 MPH
as
results from 70
MPH
at
half-flaps and ao
puww,
The throttle
thenmtts
the
approcrch
control device.
4
e
STOL Take-0f.f and
Landings
The shortest ground run take-off under
aandetrd
conditbons
at
3000
Iba,
or
less can usually be accomplished with full-flaps,
Le.
4o”*
(This
W.11
nut,
howmmr
s
provfde
the
beslt
angle
of
clkab
if barrier clearance
fs
the objective,) The use of
3am
or
less, depending on load
and
prerraure
gltltude,
is
reammended
for
take-off.
Align aircraft
along
intended take-off track, Apply full power
in a steady
mannetr.
Do not
*@japP”
throttle
farward
l Release
brake
aa
power
is
applied,
Holding
brakes
on
while
full
povclr
is
being
applied is
not
necessary, or desirable. Keep aircraft
strafght
on track by
wing
rudder.
Try
to avoid
application of
the foot
brakes
unless
requfred
tu
matntaifn
dire,ctiemal
cantrol,
At
approxiastrtcIy
35
MPH, apply back
pressure on the yoke in
a
positive
manner
but
nut
LIU
fast
that
the aircraft ~QIS~S an
excessive mse high
attjttude
after lift-off. When the aircraft
breaks
ground j
ullar
it
to
remain
just above
the ground for
apprmctitcly
2 or 3
aecsnds,
so
that the
airaped
will build
up to over
SO
KFH
before
the airplane
rtarts
full-climb-out.
EstabZirrh
a
climb-out speed
af
SO
to 64
&SPH
as
SQQ~
aa
prmtical,
I
16-