Piper PA-32RT-300T User Manual

INSTRUMENT
PANEL
LANCE II SERVICE
MANUAL
SWITCH "A"
PA-32RT-300
&
PA-32RT-300T
SWITCH
"B"
-
PA-32RT-300
Figure 7-12.
Throttle
Warning
Switches
7-41. ADJUSTMENT
OF LANDING
GEAR UP/POWER
REDUCED
WARNING
SWITCH.
a. Remove
the
control quadrant
cover
as given
in Paragraph
7-39.
b.
Flight test the airplane
and at a safe
altitude, establish
a normal descent
with gear up
and the propeller
control
at a desired
low pitch
setting.
c. Retard
the throttle to a
manifold pressure
of approximately
14 inches. This setting
should
be an airspeed
above 104 KIAS.
d. In some
manner,
mark the
throttle lever
in relation
to its position
next to
the
mounting bracket.
e.
With the airplane
on the ground and
the throttle positioned
to the mark,
loosen the
screws that
secure the switch
and rotate
it toward
the throttle
until it is heard
to actuate.
Retighten
the
switch
attachment
screws.
f. Advance
and retard
the throttle to ascertain
that the switch
actuates at the
desired
throttle
lever
setting.
The airplane
may
also be
flown to
ascertain
that the
horn and
light
will actuate
when
the throttle
is reduced
below approximately
14
inches of
manifold
pressure
with
gear up.
g.
Reinstall
the quadrant
cover as given
in Paragraph
7-40.
Issued: 1/3/78
LANDING
GEAR AND
BRAKE SYSTEM
1K20

Piper PA-32RT-300T Specifications

General

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