Piper PA-32RT-300T User Manual

840
.12
MIN.
UP
LIMIT
SWITCH
DOWN
UMIT
SWITCH
.06
to.08
.06
Figure
7-10.
Adjustment
of
Nose
Figure
7-11.
Adjustment
of
Main
Gear
Limit
Switches
Gear
Down
Limit
Switch
7-34.
ADJUSTMENT
OF
MAIN
GEAR
DOWN
LIMIT
SWITCH.
A
gear
down
limit
switch
is
mounted
on
a
bracket
which
is
attached
to
the
lower
drag
link
of
each
main
gear.
The
switch
should
be
adjusted
to
allow
it
to
actuate
thus
turning
on
the
green
indicator
light
with
the
cockpit
when
the
downlock
hook
has
entered
the
locked
position
and
is
within
.025
and
.035
of
an
inch
of
contacting
the
downlock
pin.
(Refer
to
Figure
7-11.)
Adjustment
of
the
switch
may
be
as
follows:
a.
Ascertain
that
the
main
gear
downlock
is
properly
adjusted
as
described
in
Paragraph
7-25.
b.
Raise
the
airplane
on
jacks.
(Refer
to
Jacking,
Section
II.)
c.
Ascertain
that
the
landing
gear
is
down
and
pressure
is
relieved
from
the
hydraulic
system.
To
relieve
pressure,
hold
down
the
emergency
extender
lever.
d.
Raise
the
downlock
hook
assembly
and
place
a
.030
of
an
inch
feeler
gauge
between
the
horizontal
surface
of
the
hook
that
is
next
to
the
switch
(the
surface
that
contacts
the
downlock
pin)
and
the
rounded
surface
of
the
pin.
Lower
the
hook
and
allow
it
to
rest
on
the
feeler
gauge.
e.
Loosen
the
attaching
screws
of
the
switch
and,
while
pushing
up
on
the
center
of
the
link
assembly,
rotate
the
switch
toward
the
hook
until
it
is
heard
to
actuate.
Retighten
the
attaching
screws
of
the
switch.
f.
Manually
move
the
hook
assembly
up
from
the
pin
until
the
hook
nearly
disengages
from
the
pin.
Then,
with
pressure
against
the
bottom
of
the
link
assembly,
move
back
to
ascertain
that
the
switch
actuates
within
.025
to
.035
of
an
inch
of
full
lock.
g.
Retract
and
extend
the
gear
hydroelectrically
by
turning
the
master
switch
on,
raising
the
emergency
gear
extension
lever
and
moving
the
gear
selector
handle
to
the
up
position.
As
the
gear
begins
to
retract,
the
green
light
below
the
selector
should
go
out
and
the
red
gear
unsafe
light
at
the
top
of
the
instrument
panel
should
come
on.
Issued:
1/3/78
LANDING
GEAR
AND
BRAKE
SYSTEM
LANCE
II
SERVICE
MANUAL
IK18

Piper PA-32RT-300T Specifications

General

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