Piper SENECA III User Manual

PIPER
AIRCRAFT
CORPORATION
SECTION
3
PA-34-220T,
SENECA Ill
EMERGENCV
PROCEDURES
Fuel
selector
inop.
engme
. .
.
. .
OFF
Aux.
'uel
pumps
. ..
.'.
OFF
When
using
fuel
from
tank
on
the
side opposite the operating
engine.
Fuel
selector
operating
engine
........... ...........
CROSSFEED
Fuel
selector
inop.
engine
...........
...........
OFF
Aut
fuel
pumps.............
..........
OFF
Use
crossfeed
in level
cruise
flight
only.
NOTE
Do
not
crossfeed with
full fuel
on same
side
as
operating engine
since
vapor
return
fuel flow
will
be
lost
through
the
vent system
LANDlNG
Fuel
selector
operating engine
. . . . . . .
.
.
. . ,
,
.
..
.
.
.
,
ON
Fuel
selector
inop,
engme
............. .
...........
OFF
ENGINE
DRIVEN
FUEL
PUMP FAILURE
Throttle
.........
...........
retard
Aux
fuel
pump...........
.
.........unlatch,
on
HI
Throttle
.........
...........reset
(7596
power
or
below)
CAUTION
If
normal
engine
operation
and
fuel
flow
is
not
immediately
re-established,
the
auxiliary
fuel
pump
should
be
turned
off.
The
lack
of
a
fuel
flow
indication
while
on
the
Hl
auxiliary
fuel
pump
position could
indicate
a
leak
in
the
fuel
system,
or
fuel
exhaustion.
ISSUED:
JANUARY
8,
1981
REPORT: VB-Ill0
REVISED:
APRIL 9, 1982
3-7

Piper SENECA III Specifications

General

Manufacturer	Piper Aircraft
Model	Seneca III
Engine Type	Piston
Engine Model	Continental TSIO-360-KB
Seating Capacity	6
Cruise Speed	188 knots (216 mph, 348 km/h)
Length	28 ft 7 in (8.71 m)
Max Takeoff Weight	4, 750 lb (2, 155 kg)
Horsepower	220 hp each
Service Ceiling	25, 000 ft (7, 620 m)
Height	9 ft 11 in (3.02 m)
Propellers	2-bladed constant speed