Helio HT-295 Owner's Manual page 20

It
a s p i n .
flaps dm,
altitude
The asost emoa cause of HeIia crsahe~ and major daarage -- though
the
pull aircraft
power full-on, the
or
fail
takes considerable
the nose high attitude
This condition is
thrust drag curve, or simply as "the back side rof the mer curve".
barrier should be strictly 8~ cpergeiacy ptocadure fur expcrfenced
d a
Distance
With
to
the
for
build up
rotation to the point that will
After consfdtrable
be attained by hoEding the aircraft
to clcrar the barrier without lass
can lowered and
be
the
barrier,
thaa cmcrgency
at
too low u. apeed with
off the ground prematurely at toa law B speed
the propeller a;t km fmrvmrd
starts to reduce
often referred to am **the back side"* af the
a
speeds below 50 MPH
aircraft to accelerate as quickly
of airrpted.
Such technique kr not rscmnmdcd for
the Helis Cmrier, there
sink ?mck
the
the
rate-of-climb
despite full power.
arc
Weight
Barrier (Grass
50 MPH, then
climb the
aircraft
airspeed
just
18
Thus, with
a
at
the sirsaecsd
to
can
after