Piper PA-32RT-300T User Manual

2
LANCE
II SERVICE
MANUAL
SKETCH A
1.
ECCENTRIC
BUSHING
CLEARANCE
2. BEARING, DOWNLOCK
Figure
7-2b.
Adjustment
of Eccentric
Bushing
1. Ascertain
that
the upper
and
lower
links
(32 and
35)
are assembled
with the
downlock
hook
attached,
and
the
through
travel
of
the links
checked
according
to
Paragraph
7-10.
2. Position
the link
assembly
to
allow
the bolt
holes
in links
to align
with
holes
in
gear
housing
and
engine
mount.
3.
Add the
upper
gear tension
spring
arm (45),
bushings
and
washers
on
upper link
(35)
attachment
bolt.
4. Install
the
bolt
and tighten
nut to
allow
the link
to rotate
freely
and
safety.
5.
Install
the
lower
gear
tension
spring
arm
(43)
on
the drag
link
bolt
(29)
on the
right side
of
the gear
oleo
housing
(25),
secure
and
safety.
A washer
is installed
on
the bolt
between
the lower
drag link
and
the
arm.
d.
Connect
the
gear
downlock
spring
(39)
between
the
downlock
(40)
and
the
upper
drag
link
(35).
e.
Connect
the two
gear
tension
springs
(15
and 17).
f.
Adjust
the
eccentric
bushing
(used
for
downlock
pin)
with
the gear
extended
and
downlock
engaged
to obtain
.001
to .010
clearance
between
the bottom
of the
down
lock
pin
(bearing)
and
the
downlock
hook
(Refer
to
Figure
7-2b).
g.
Retract
gear
and tighten
with
eccentric
bushing
in
its
adjusted
position.
h
Ascertain
that
the
landing
gear
is lubricated
per
Lubrication
Chart,
Section
II.
L
Check
adjustment
of
the
gear per
Paragraph
7-12.
j.
Install
engine
cowling.
Issued: 1/3/78
LANDING GEAR
AND BRAKE SYSTEM
1J19

Piper PA-32RT-300T Specifications

General

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