The
HeHa
Cauricr
NT-295
ia
very
much
IEke
other
convmtianael
rsircraft
ia
cross-vind
apcratimr,
During take-offs, greater
attention
ts’dfrcctianal
cxmtrol.
is required when the
cram-
wind
ia
from
the
left, A left
Cross-wfnd
amplifies
the
*tprq
factor of the
propelIxr,
aad
the tendency of the
aimraft
to
wtlzther
v&ne
into
the
wtnd.
The
sburt
take-off ground
run
can
be
used
may times
to
elfimimte
mme
of the
crasrs-wind
c When
pasrrible,
the
take-off
psth
pslipsy
be at
a
slight dfagsnal
rriesasr
8B
existing
run-way,
_
Line
up
the
aircrrft
cm
thes
down wind
bide
of the
rummy
or take-off
arem
facing 8s
clasety
BI
pomible,
into
the
wind*
By
ddng
&hfr,
Lf6
&rt
ptartlble
tcs
&m~ase
t?m
crodl;~~~
-wfnd
cmnpanant
by
30
to
15
,
aad
#till
have sufficient
cunwap
for take-off.
The
maxfmum
cmss-Wfmd
ctrmponeat
demonetratsd
is
17
knots
rt
9$r
so
many
times
1Oo
to
tS*
will
make
da
differcncs.
The aircraft should be held
on
the
ground
a
little
lunger
thaa
uormal
OR
take-off,
Thfir
incxsosc
in
dtrepead
will
II
positivei
lift-off
without
fhg
danger
-of:
contmtttiag
the
gtmtmd
agafa in
a
side drift
due
to
the
era
The aide
fasd
imposed by drift produces
unwunte
the
tanding
gear, wheels,
and
tires,
When landfag
hn
u
crass-triad, either crab or
slip
for
exiatiag
wind
ercmdittaas
as
you
wauld
w5,th
any
coaveatkanat
aircraft
0111
the approach*
Just
prior to touch
~dmrt,
@liga
the
QQ~B
straight with the flight path, or touch
dam
on the up-wind
wheel
fimt
depend&i&
on the method
oaed.
tatnd
the
aircrrft
without
delay,
When
the
wheels
tartich
dawn,
art
slightly before,
reduce
power
completely and
retruet
flaps
88
soon
as
possible.
Apply both
brakes
evenly
and
alaw
aircraft
dawn
tu
taxi speed.
Asi
vith
any aircraft, extra cuatfoa should be used
when
taxffng
ia
gusty wind
conditiona,
The fuel
rtysteoe
coarrirtr
of
the two
fmel
bladder
cellr,
one
located
fn
each@in$’
panel, me
fuel
hat-off
vulvt,
a
fuel
selectar
vtlvt,
out
gascolator
located
under
the
right
hmd
widow,
aa
engine
driven
fuel pump,
oue
elecmrically
driven
booster
pump
and
a
hand
operated
tagint
primer, The
ftlel
quantity
troamittets
axct
of the float type
and
they are
locatead
on the
inbeard
Wia43
ribs,
Each cell is filled through
a filler neck which
axttztdsr
above the
wing
panel.
The
fuel
cell8
ilrt
of tha
collapaiblt
type. The
system
ir
suitable for
artraPnotic
frrelr
*
The
main
fueli
valve
LI
located on the right side of the cockpit,
below
the
forwrrd
window.
Tbtrt
urt
anlg 2
@mitLotta,
“DN
rrad
e@cm?‘,
when
eQN’8~
the
valve
handle
frr
hori~ontsl.
Thtr
valve
control@
the
fuel
flaw
from
both
wing
tanks,
which
are
interconnected.
21
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General