Piper PA-32RT-300T User Manual

LANCE
II SERVICE MANUAL
A953
0.010
TO.030
STOP
Figure
8-5.
Adjustment
of Engine
Controls.
8-16. ADJUSTMENT
OF THROTTLE
AND
MIXTURE
CONTROLS.
(Refer to
Figure
8-5.) Throttle
and mixture
controls
are adjusted
so that
when the throttle
arm on
the
carburetor
is rotated
forward against
its full throttle
stop and
the mixture
control is rotated
forward against
its full
rich stop,
the cockpit
control levers
of the throttle
and mixture
should
have 0.010 to 0.030
of an inch spring
back on instrument
panel stop when
in full
rich position.
a. The
throttle
may
be
adjusted
as
follows:
1. At the carburetor,
disconnect
the clevis end
of the throttle
control cable from
the control arm. Loosen the jam nut that secures the clevis end.
2. Adjust the linkage by
rotating the clevis end on the cable
to obtain 0.010 to
0.030
of an inch spring back on instrument
panel stop when in full throttle
position.
3. On aircraft
equipped
with air conditioning
systems, a micro
switch is located
below the
throttle control which
is set to actuate
in the full open position.
With the throttle
control
adjusted to obtain a clearance of
.010 to .030, adjust the micro switch to
actuate at
this point also.
4. Reconnect
the clevis
end to the
control arm
and safety.
b.
The
mixture
may
be adjusted
as follows:
1. At the
carburetor,
disconnect
the clevis end
of the mixture
control
cable from
the control
arm. Loosen
the jam nut
that secures
the clevis end.
2. Adjust
the linkage
by rotating
the clevis
end on
the cable
to obtain 0.010
to
0.030
of an inch
spring back
on the instrument
panel
stop when
in full rich
position.
3.
Reconnect
the
clevis end
to the
control
arm and
safety.
c. Check security
of cable casing
attachments.
d.
Pull the throttle
and mixture
levers
in the cockpit
full aft
to ascertain
that the idle
screw
contacts its
stop and the
mixture control
arm contacts
its lean
position. A
mixture
control
lock is incorporated
in
the quadrant
cover which
prevents the
mixture control
from
being moved
to the
idle cutoff
position inadvertently.
The
lock must
be depressed
before
the
control can
be moved
completely
aft. Ascertain
that the lock
operates freely
without
any
tendency to
bind or hang
up.
Issued: 1/3/78
POWER
PLANT
2A20

Piper PA-32RT-300T Specifications

General

Brand	Piper
Model	PA-32RT-300T
Category	Aircrafts
Language	English