Piper SENECA III - Page 55

PIPER
AIRCRAFT
CORPORATION
SECTION 3
PA-34-220T,
SENECA
III
EMERGENCV
PROCEDURES
ONE
ENGINE
INOPERATlVE
GO-AROUND
(SHOELD
BE
AVOIDED
IF AT
ALL
POSSIBLE)
Mixture
...........
.
...........forward
Propeller..........
..
.............forward
Throttle
.........
..
...........
(40
in.
Hg. Max.)
open
slowly
Flaps..........
..
.........
retract
landing
gear
.............
..........
retract
Airspeed
...........
.
,
...........92
KIAS
Trim
.....................................,..................
set
Coni
flap
operating
engine
..............................
as
required
AlR
START
(UNFEATHERING
PROCEDURE)
Fuel
selector
inop.
engine
.........
.
.........
ON
Aux.
fuel
pump
inop.
engine
.......
....
...........
LO boost
Throttle
...........
.
.
.
..........
open
174 inch
Mixture
.......
.
.
..........
RICH
Magneto
switches
............
............
ON
Prop
control
...........
.
.................
full forward
Starter...........
.
,..........engage
until propeller
windmills
Throttle
..........
.
.
............
reduce
power
until
engine
is
warm
Aux
luel
pump..........
.
...........
OFF
li
engine
does
not
start,
prime
as
required.
Alternator
(after
restart)
..........
.........
ON
AIR
ST
ART
(UNFEATHERlNG
PROCEDURE)
On
Airplanes
Equipped
With
Unfeathering
Accumulators
Fuel selector
inop.
engme
.........
..........
ON
Aux
fuel
pump
inop
engine
......-...
..........
LO
boost
Throule
...........
..
.
.........,
open
I
4inch
Mixture
..........
...........
RICH
Magneto
switches
...........
...........
ON
Prop
control &
latch
...........
..........
push
full forward
Throttle
..........
...........
reduce
power
until
engine
ts
warm
Aux.fuel
pump..........
.
...........
OFF
ISSUED:
JANUARY
8,
1981
REPORT:
VB-1110
REVISED:
APRIL 9,
1982
3-5