Piper SENECA III - Page 65

PIPER
AIRCRAFT
CORPORATION
SECTION
3
PA-34-220T.
SENECA
III
EMERGENCY PROCEDURES
ENGINE
EAILURE
DURING
TAKEOFF(85
KIAS
OR
ABOVE)
It
engine
failure
occurs
during
takeoff
ground
roll
or
after
lift-ofT
with
the
year
still
down
and
85 KIAS
has been
attained, the
course
01action
to
be
taken
will
depend
on
the
runway
remaining.
If adequate
runway
remains.
C1.OSE
both
throttles
immediately,
land
if
airborne
and
stop
straight
ahead
If
the
runway
remaining
is
inadequate
for
stopping.
the
pilot
must
decide
whether
to
abort
the
takeoff
or
to
continue.
The decision
must
be
bacd
on
the
pilors
judgment
considering
loading.densityaltitude.obstrue-
tions.
the
weather.
and
the
pilot-s
competence.
If
the
decision
is
made
to
continue
the
takeoff.
maintain
heading
and
airspeed.
When
climb
is
estab-
hshed
RETRACT the
landinggear.accelerate1092
KlAS,
and
FEATHER
the
moperative
engine
(refer
to
Engine
Securing
Proceduret
WARNING
ln
certain
combinations
of
aircraft
weight,
configuration, ambient
conditions and speeds,
negative
climb
performance
may
result.
Refer
to
One
Engine
lnoperative
Climb
Performance
chart,
Figure
5-21.
ENGINE
FAILURE
DURING
FLIGHT
(BELOW
66
KLAS)
Should
an
engine
fail
during
flight
at an
airspeed below
66 KIAS.apply
rudder
towards
the
operative
engine
to
maintain
directional
controL The
throule,
should
be
retarded
to
stop
the
yaw
force
produced
by
the
maperame
engine.
Lower
the
nose
of
the
aircraft
to
accelerate
above
66
KLAS
and
increase
the
power
on
the
operative
engine
as
the
airspeed
exceeds
66
KIAS*.
Aner
an
airspeed
above
66
KIAS*
has
been
established,
an
engine
restan
attempt
may
be
made
if
altitude
permits. If
the
restart
hasfailed,orif
aMtude
does
noi
permit,
the engine
should
be
secured,
see
Engine Securing
Procedure.
*6"
KIAS
with
aft
doors
removed.
ISSUED:
JANUARY 8,
1981
REPORT:
VB-1110
REVISED:
FEBRUARY
25, 1982
3-15