Piper SENECA III - Page 54

SECTION
3
PIPER AIRCRAFT
CORPORATION
EMERGENCY
PROCEDURES
PA-34-220T,
SENECA
IH
ENGINE
FAll
URE
DURlNG
TAKEOFF
(85
KIAS
or
above)
If
engine
failure
occurs
during
takeoff
ground
roll
or
after
lift-off
with
gear
stil
down
and
85
KlAS has been
attained:
If
adequate
runway
remains.
CLOSE both throttles
immediately,
land
if
airborne
and
stop
straight
ahead,
If
runway
remaining
is inadequate
for
stopping,
decide
whether
to
abort
or
continue,
if
decision
is
made
to
continue. maintain
heading.
After
establishing
a
climb.
retract
landing
gear,
accelerate
to
92
KIAS,
and
feather
inoperative
engine
prop
(see
Engine Securing
Procedure).
WARNING
In
certain
combinations
of aircraft
weight,
configuration,
ambient
conditions
and
speeds,
negative
climb
performance
may
result.
Refer
to
One
Engine Inoperative
Climb Performance
chart,
Figure
5-21.
ENGINE
FAILURE
DURING FLIGHT (Below 66 KIAS)
Rudder
.............
.
..........
apply
toward
operative engine
Throttles
(both).............
........
retard
to
stop
turn
Pitch
attitude
, . .
. . . . . .
. . .
,
. .
.
- -
-
lower
nose
to
accelerate
above 66
KIAS*
Operative
engme
. . . .
. . , .
. . . . . . . . . .
mcrease
power
as
airspeed
mcreases
above
66
KlAS*
If
altitude
permits.
a
restart
may
be
attempted.
If
restart
fads
or
if
altitude
does
not
permit
restart,
see
Engine
Securing
Procedure.
ONE
ENGINE
1NOPERATlVE
LANDING
inop.
engine
prop
.......... .
........feather
When
certain
of
making
field:
Landing
gear
.....--....
..........extend
Wingflaps(assequired)
............ .....
..................lower
Maintain
additional altitude
and speed
during
approach.
Final
approach
speed
......... -
- ----
........90
KlAS
*67
KIAS
with
aft
doors
removed.
REPORT:
VB-III0
ISSUED:
JANUARY
8.
1981
3-4
REVISED:
FEBRUARY
25.1982