Piper SENECA III - Page 66

SECTION
3
PIPER
AIRCRAFT
CORPORATION
EMERGENCY
PROCEDURES
PA-34-220T,
SËNECA
IH
ONE
ENGINE
INOPERATlVE
LANDING
Complete
the
Engine
Securing
Procedure.
The
landing
gear
should
not
be
extended
and the
wing
flaps
should
not
be
lowered until certain
of
making
the
field.
Maintain
additional
altitude and
speed
during
approach,
keeping
in
mind
that
landing
should
be
made
right
the
first
time
and that
a
go-around
should
be
avoided
if
at
all
possible.
Establish
a
final
approach
speed
of
90
KlAS
and
use
wing
flaps
as
required.
WARNING
Under
some
conditions of
loading
and
density
altitude
a
go-around
may
be
impossible.
and
in
any
event
the sudden
application of
power
during
one
engine
inoperative
operation makes
control
of
the
airplane
more
difficult.
ONE
ENGINE
lNOPERATlVE
GO-AROUND
NOTE
A
one
engine
inoperative
go-around
should
be
avoided if
at
all
possible,
To
execute
a one
engine
inoperative
go-around.
advance the mixture
and
propeller
levers
forward. The
throttle
should
be advanced slowly
to
40
in. Hg.
manifold
pressure.
Retract
the
flaps
and
landing
gear.
Maintain
airspeed
at
the
one
engine
inoperative
best
rate
of
climb speed of92
KIAS.
Set
the
trim
and
cowl
flaps
as
required.
AIR
START
(UNFEATHERlNG
PROCEDURE)
Move
the
fuel
selector
for
the
inoperative
engine
to
theON
position
and
check
to
make
sure
the AUX
fuel
pump
for
that
engine
is
on
LO
boost.
Open
the
throttle
1,4
inch
and the
mixtures
should
be
set
RICH.
Turn
ON
the
magneto
switches
and
push the
propeHer
control
latch
and
propeller
control
lever
full
forward.
On
airplanes
equipped
with the
optional
unfeathering
system
the
propeller
will
start to
windmilL
On
airplanes
not
so
equipped,
REPORT:
VB-1110
ISSUED:
JANUARY
8,
1981
3-16
REVISED:
APRIL
9, 1982