Piper Cherokee Six - Page 15

Model
PA-32-260
PA-32-300
For
S/Ns
32-7940001
and up
PA-32R-300
Engine
O-540-E4B5
10-540-K
I
A5
10-540-K1G5D
10-540-K
IA5D
Propeller
F.P.
-
I P235PFAS266
C.S.
-
HC-C2Y
K-1A
8477-2
C.S.
- HC-C2YK-1/8475D-4
C.S.
-
HC-C2YK-1
(
) F/F8475D-4
C.S.-
HC-C2YK-1/8475D-4
PIPER
CHEROKEE
SIX
SERVICE
MANUAL
1-8.
LANDING
GEAR
(PA-32R-300).
The
tricycle
landing
gear
is
a
hydraulically
operated,
fully
retractable
unit
consisting
of
shock
absorbing
air-oil
type
oleo
struts.
1-9.
HYDRAULIC
SYSTEM
(PA-32R-300).
The
hydraulic
system
incorporates
an
electrically
driven
pump
which
is
controlled
by
a
switch
on
the
instrument
panel
which
in
turn
operates
the
retraction
and
extension
of
the
landing
gear.
1-10.
BRAKE
SYSTEM.
The
brake
system
is
operated
hydraulically
by
toe
brakes
located
on
the
rudder
pedals
or
by
a
hand
lever
connected
to
a
single
brake
cylinder
below
and
behind
the
left
center
of
the
instrument
panel.
1-11.
ENGINES
AND
PROPELLER.
H.P.
300
300
Octane
260
100/130
100/130
100/130
1-12.
FUEL
SYSTEM
(PA-32-260
and
PA-32-300).
The
fuel
system
consists
of
two
aluminum
fuel
tanks
in
the
wings
plus
an
auxiliary
tank
in
each
wing
tip,
giving
a total
capacity
of
84
U.S.
gallons
with
83.5
gallons
usable.
Incorporated
in
the
system
is
a
combination
selector
valve-fuel
filter,
electric
auxiliary
fuel
pump(s)
and
an
engine
driven
pump.
1-13.
FUEL
SYSTEM
(PA-32-300
S/N
32-7940001
and
up,
and
PA-32R-300).
The
fuel
system
consists
of
two
interconnected
aluminum
fuel
tanks
in
each
wing,
giving
a
total
capacity
of
98
U.S.
gallons
with
94
gallons
usable.
Incorporated
in
the
system
is
a
three
position
fuel
valve
(off-left-right),
gascolator
and
electric
emergency
fuel
pump.
1-14.
FLIGHT
CONTROLS.
The
flight
controls
are
conventional
equipment,
consisting
of
a
control
wheel
which
operates
the
ailerons
and
stabilator,
and
pedals
which
operate
the
rudder.
Duplicate
controls
are
provided
for
the
copilot.
INTRODUCTION
A15
Revised:
11
4 83
1A15