Piper SENECA III - Page 117

PIPER
AIRCRAFT
CORPORATION
SECTION 4
PA-34-220T,
SENECA
III
NORMAL
PROCEDURES
v
CA
DEMONSTRAT1ON
(a)
Landing
Gear
UP
(b)
Flaps
UP
(c)
Airspeed
at
or
above
85
KIAS
(VssE)
(d)
Propeller
Controls
HlGH
RPM
(e)
Throttle
(Simulated
Inoperative
Engine)
IDLE
(f)
Throttle
(Other
Engine)
MAX
ALLOWABLE
(g)
Airspeed
Reduce
approximately
I knot
per
second
until
either
VMcA
or
STALL
WARNING
is
obtained
CAUTIONS
Ese
rudder
to
maintain
directional
control
(heading)
and
ailerons
to
maintain
5° bank
towards
the
operative
engine
(lateral
attitude).
At
the
first
sign
of
either
VMCA
Of
SInlÌ
Warning
(which
may
be
evidenced
by
an
inability
to
maintain
heading
or
lateral
attitude,
aero-
dynamic
stall
buffet,
or
stall
warning
horn)
immediately
initiate
recovery.
reduce
power
to
idle
on
the
operative
engine,
and
immediately
lower
the
nose
to
regain
VssE.
One
engine
inoperative
stalls
are
not
recom-
mended.
U
nder
no
circumstances
should
an
attempt
be made
to
fly
at
a
speed
below
Vru
a
with
only
one
engine
operating.
ISSUED:
JANUARY
8,
1981
REPORT:
VB-1110
REVISED:
FEBRUARY
25,
1982
4-37