Piper SENECA III User Manual

PIPER
AIRCRAFT
CORPORATION SECTION
7
PA-34-220T,
SENECA III
DESCRIPTION &
OPERATION
To
remove
the
cabin
work
table
from
the
aft
baggage
compartment,
unlock
the stud
located
on
the
bottom
oftheclose-out bulkhead.
Loosen
the
white
tie-down
strap
and
remove
the
table
from
the
mounting
brackets
by
lifting
the
table
two
inches
straight
up
untilit clears the mounting
brackets.
Do
not
twist the
table
while
it is in the brackets.
To install the
cabin
work
table
during
flight,
hold the table in
place
and
tilt
the
free
end
of
the
table
upward
30°
until
the lobed
upper
knobs
on
the
table
supports
align
with
the
top
holes
of
the
escutcheons
located
below the
right
cabin window
trim.
Hold
the
upper
lobes
in
place
and
lower
the
free
end
of
the
table
to
the
level
work
position.
The
retaining
springs
will
click
when
secure.
To
stow
the
cabin
work
table,
remove
the
table
by
lifting
the free
end
of
the
table
upward
to
disengage
the
bottom
lobes
of the table
supports.
Lift
until
the
top
support
lobes
disengage
at
approximately 30°
of
tilt
and
remove
the
table.
Position the
table
in
the
stowage
area
and,
with
the
table
work
surface
facing
forwarð,
place
the
slots
in
the
table
support
into
the
receptacle
clips
mounted
on
the
hat
shelf,
Make
sure
the tie-down
strap
is
not
behind
the
table.
With
the
table
fully placed
in
the
clips,
bring
the
tie-down
strap
across
the
face
of
the
table
and
lock
over
the stud located
on
the
bottom
of
the
close-out
bulkhead.
7.29
STALL
WARNING
An
approaching stall
is
indicated
by
a
stall
warning
indicator
which
is
activated between
five
and
ten
knots
above
stall
speed.
Mild
airframe
buffeting
and
gentle
pitching
may
also
precede the
stall.
Stall
speeds
are
shown
on
a
graph
in
the
Performance Charts
Section.
The
stall
warning
indicator
consists
of
a
continuous
sounding
horn
located behind
the
instru-
ment
panel.
The
stall
warning
horn
has
a
different
sound
from
that
of
the
gear
warning horn
which
has
a
90
cycles
per
minute
beeping
sound.
The
stall
warning
indicàtor
is
activated
by
two
lift
detectors
on
the
leading
edge
of
the
left
wing,
outboard
of
the
engine
nacelle.
The inboard
detector
activates
the
indicator
when
the
flaps
are
in
the
25
and
40
degree
positions,
the
outboard
when
the
flaps
are
in
other
positions.
A
squat
switch
in the
stall
warning
system
does
not
allow the units
to
be
activated
on
the
ground.
ISSUED:
JANUARY 8,
1981
REPORT:
VB-IllO
REVISED:
AUGUST
9,
1982
7-35

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