Piper SENECA III - Page 53

PIPER
AIRCRAFT
CORPORATION
SECTION 3
PA-34-220T,
SENECA III
EMERGENCV PROCEDURES
To
attempt to
restore
power
prior
to
feathering:
Mixtures...........
.
.
.,
..........as
required
Fuel
selector
.........
..........
ON
Magnetos
............
...........
Ieft
or
right
only
Aux.
fuel
pump........
.
..........
unlatch.
ON HI,
if
power
is
not
immediately
restored
-
OFF
Alternate
air
..........
.. ..........
ON
li
power
cannot
b
iestored
continue with
feathering procedure.
Prop
control
of
inop.
engine
........ ...........
feather before
RPM
drops
below
800
Mixture
of
inop,
engine...........
.
..............
idle
cut-off
Trim
.............. .
.........
as
required
(3°
to
5°
of
bank
toward
operative engine
-
ball I
/2
to
I
out)
Aux.
fuel
pump
of
inop.
engine..........
.. .............
OFF
Magnetos
of
inop.
engine
.......... .
................
OFF
Cowl
flaps
..............
............
close
on
inop,
engine,
as
required
on
operative engine
Alternator
of
inop
engine............
.
. ...........
OFF
Electrical
load
...........
.
..
...........reduce
Fuel
selector
...........
........
OFF inop
engine,
consider
crossfeed
Aut
fuel
pump
operative
engine........
.........
OFF
Power
of
operative
engine
.
. . . .
. . . . . . . . . . . , , .
,
as
required
ENGINE
FAILURE
DURING
TAKEOFF (Below 85 K1AS)
li
engine
failure
occurs
during
takeoff
and
85 KIAS
has
not
been
attained:
Throttles..........
.
............
CLOSE both
immediately
Stop
straight
ahead.
If
nadequate
runway
remams
to
stop:
Throttles...............................................
CLOSED
Brakes......,.................................
apply
max.
braking
Batterv
switch
............,
. ..
...........
OFF
Fuelselectors..............
... ....
.,......
..........
OFF
Continue
straight
ahead,
turning
to
avoid
obstacles.
ISSUED:
JANUARY 8, 1981
REPORT:
VB-IIIO
3-3