Piper COMANCHE 260 User Manual

THE
PIPER
COMANCHE
SECTION
Il
rienced.
This
condition
may
be
eliminated
by
proper
leaning
of
the
mixture
or
by
use
of
the
electric
fuel
pump.
(13)
Ahighfuel
pressure
indicationon
the
fuel
flow
indicator
is
a
possible
indication
of
restricted
air
bleed
nozzles.
RADIO OPERATION
Communication
and
navigational
equipment
controls
are
located
in
the
center
of
the
instrument
panel.
Associated
aux-
iliary
switches
are
located
on
a
separate
panel
below
the
con-
trol
column
on
the
lower
right
side
of
the
instrument
panel.
Circuit
breakers
for
the
radios
are
located
to
the
left
of
the
main
switch
panel.
All
sets
are
turned
"ON"
by
the
switch
located
on
the
con-
trol
head
of
each
particular
unit,
with
the
exception
of
the
marker
beacon
and
glide
slope
power
switches
which
are
lo-
cated
on
the
Audio
Sclector
Switch
Panel.
After
power
is
supplied,
the
pilot
may
wish
to
operate
one
of
the
two
transmitters
by
moving
the
transmitter
selector
switch
to
the
proper
position.
The
switch
is
located
on
the
selector
switch
panel.
A
separate
three
positionaudio
selector
switch
is
provided
foreach
receiver.
Eachreceiver
audio
output
may
be
connected
to
either
the
speaker
or
the
headset.
In
addition
they
may
be
placed
on
the
"OFF"
or
standby
position.
To
receive
audio
through
the
speaker
from
the
Marker
Beacon
and
DME
UDI-2
the
top
Mark
12
must
be
in
operation.
Power
from
this
radio
is
not
required
when
the
headphonesare
connected
to
the
Marker
Beacon
or
DME.
Two
or
more
sets
may
be
simultaneously
connectedto
either
the
headset
or
speaker
position
by
placing
the
selector
switches
in
the
desired
combination.
For
example,
the
A.D.F.
and
the
top
Mark
12
may
be
selected
to
operate
on
the
speaker
and
the
lower
Mark
12
may
be
selected
for
headsetoperation.
If
desired
the
pilot
may
listen
to
the
speaker
and
the
co-pilot
the
headset.
640901
36

Piper COMANCHE 260 Specifications

General

Brand	Piper
Model	COMANCHE 260
Category	Aircrafts
Language	English