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Piper SENECA III User Manual

Piper SENECA III
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SECTION 3
PIPER
AIRCRAFT
CORPORATION
EMERGENCV
PROCEDURES
PA-34-220T, SENECA
III
CRUISlNG
When
using
fuel
from
the
fuel
tank
on
the
same
side
as
the
operating
engine
the
fuel
selector
of the
operating
engine shouki
be
ON
and the
fuel
selector
for the
inoperative
engine
should
be OFF.
The AUX. fuel
pumps
should
be
OFF
except
in the
case
of
an
engine
driven
fuel
pump
failure.
If
an
engine
driven fuel
pump
has
failed
the
AUX
fuel
pump on
the
operating
engine
side
must
be
ON
-
H l.
lucreased
range
is
available
by
using
fuel from
the
tank
on
the
opposite
side
of
the
operating
engine. For
this
configuration
the
fuel
selector of
the
operating
engine
should
be
on
X-FEED
icrossfeed)
and
the
fuel
selector
of
the
inoperative
engine
should
be OFF.
The
AUX, fuel
pumps
should be
OFF.
NOTE
A
vapor
return
line
from
each
engine will
return
a
percentage
of
fuel
back.
to
the
tank
on
the
same
side
as
that
engine.
Therefore,
a
minimum
of
30 minutes
of
fuelshould
be
used
from
this
tank
before selecting crossfeed,
If
the tank
gauge
approaches
"FULl
go
back
to
that
tank
and
operate
for
30
minutes
to
bring
the
fuel
level down
before
returning
to
crossfeed
or
fuel
raay
be pumped overboard
through the
fuel
vent.
LANDING
During the
landing
sequence
the
fuel
selector
of the operating
engine
must
be
ON
and the
fuel
selector
of
the
inoperative
engine
OFF.
The AUX.
fuel
pump
of
the
operating engine should
be
OFF.
3.13
ENGINE DRIVEN
FUEL
PUMP
FAILURE
Should
a
malfunction
of
the
engine
driven fuel
pump
occur,
the
auxiliary
fuel
pump
system
can
supply
sufficient
fuel
pressure
for
engine
power
up
to
approximately
75 Any
combination
of
RPM
and Manifold
Pressure
defined
on
the
Power
Setting
Table
may
be
used,
but leaning
may
be
required
for
smooth
operation
at
altitudes above 15,000
feet
or
for
R
PM's
below
2300.
Normal
cruise.
descent
and
approach
procedures
should
be
used.
REPORT: VB-Illo
ISSUED:
JANUARY
8, 1981
3-18
REVISED:
APRIL
9,
1982

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Piper SENECA III Specifications

General IconGeneral
ManufacturerPiper Aircraft
ModelSeneca III
Engine TypePiston
Engine ModelContinental TSIO-360-KB
Seating Capacity6
Cruise Speed188 knots (216 mph, 348 km/h)
Length28 ft 7 in (8.71 m)
Max Takeoff Weight4, 750 lb (2, 155 kg)
Horsepower220 hp each
Service Ceiling25, 000 ft (7, 620 m)
Height9 ft 11 in (3.02 m)
Propellers2-bladed constant speed

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