Piper Lance II User Manual

LANCE
II
SERVICE
MANUAL
5-18.
INSTALLATION
OF
STABILATOR
TRIM
ASSEMBLY
(FORWARD).
(Refer
to
Figure
5-9.)
a.
The
trim
control
wheel
(1)
with
drum
(3)
may
be
installed
by
the
following
procedure:
1.
Wrap
the
right
trim
cable
(8)
on
the
trim
drum
by
inserting
the
swagged
ball
of
the
cable
in
the
slot
provided
in
the
side
(right
side)
of
the
drum
that
mates
with
the
control
wheel,
and
looking
at
this
side,
wrap
the
drum
with
three
wraps
of
the
cable
in a
clockwise
direction.
2.
Attach
the
control
wheel
(1)
to
the
cable
drum
(3)
by
aligning
the
long
lug
of
the
drum
with
the
long
slot
of
the
wheel
and
pushing
the
two
pieces
together.
3.
Wrap
the
left
trim
cable
(9)
on
the
drum
by
inserting
the
swagged
ball
of the
cable
in
the
slot
provided
in
the
flanged
side
(left
side)
of
the
drum
and
looking
at
this
side,
wrap
the
drum
with
three
wraps
of
the
cable
in
a
clockwise
direction.
4.
Lubricate
and
install
the
bushing
in
the
control
wheel
and
drum.
5.
Align
the
control
cables
and
position
the
control
wheel
assembly
between
its
mounting
brackets
(4).
Ascertain
that
the
end
of
the
trim
indicator
wire
(2)
is
positioned
in
the
spiraled
slot
of
the
drum
(3)
with
no
bind
on
the
end.
Install
the
retainer
bolt
(7)
from
the
left
side
and
install
washer
and
nut.
AN960-616L
washers
may
be
added
as
required
between
right
hand
side
of
the
control
wheel
and
right
hand
mounting
bracket
to
eliminate
end
play.
6.
Install
the
cover
over
the
control
wheel
and
secure
with
screws,
unless
the
control
cables
have
yet
to
be
installed.
b.
The
trim
control
cables
(8
and
9)
may
be
installed
by
the
following
procedure:
1.
Draw
the
cable(s)
through
the
floor
tunnel.
2.
Wrap
the
cable
drum
(3)
and
install
the
trim
control
wheel
as
given
in
Step
a.
3.
Position
the
cable
pulleys
(6)
on
their
mounting
bracket
and
install
the
clevis
pin,
washer
and
cotter
pin
(5).
4.
Connect
the
cable
(8
or
9) to
the
aft
cable
(12)
at the
turnbuckle
(10
or
1
) in
the
aft
section
of
the
fuselage.
Install
aft
cable
(12)
if
not
installed.
5.
Install
the
cable
guard
at
the
cable
pulleys
(13)
in
the
aft
lower
section
of
the
fuselage
forward
of
the
cable
turnbuckles.
6.
Install
the
cable
guard
plate
(33)
at
the
underside
of
the
pulley
cluster
(34)
located
in
the
aft
area
of
the
aft
floor
tunnel
and
secure
with
screws.
7.
Install
the
pin
type
cable
guard
(38)
at
the
underside
of
the
pulleys
(36)
located
in
the
forward
area
of
the
aft
floor
tunnel
and
secure
it with
a
tinnerman
nut.
8.
Install
the
cable
rub
blocks
(39)
located
on
the
aft
side
of
the
main
spar
housing
and
secure
with
screws.
9.
Remove
the
blocks
that
secure
the
aft
trim
cable
and
check
that
the
cables
are
seated
on
their
pulleys.
10.
Set
cable
tension
and
check
rigging
and
adjustment
per
Paragraph
5-21.
Check
safety
of
all
turnbuckles.
11.
Install
the
tunnel
cover
on
the
forward
tunnel
and
secure
with
screws.
12.
Install
the
carpet
over
the
floor
tunnel.
13.
Install
the
heat
deflectors
on
each
side
of
the
floor
tunnel.
14.
Install
the
cover
over
the
trim
control
wheel
and
secure
with
screws
and
special
washers.
15.
Install
the
seat
belts
removed
from
the
top
of
the
floor
tunnel
and
secure
with
bolt,
washer
and
nut.
16.
Install
the
floor
panel
and
seat
belt
attachments
aft
of
the
main
spar,
and
secure
panel
with
screws.
17.
Install
the
aft
floor
tunnel
and
secure
with
screws.
18.
Install
the
carpet
over
the
aft
floor
tunnel.
19.
Install
the
trim
plate
on
top
of
the
forward
end
of
the
aft
floor
tunnel.
c.
Install
the
panel
to
the
aft
section
of
the
airplane
and
the
seats.
Revised:
10/3/80
SURFACE
CONTROLS
1G10

Piper Lance II Specifications

General

Manufacturer	Piper Aircraft
Max Takeoff Weight	3, 600 lb (1, 633 kg)
Crew	1
Horsepower	300 hp
Seats	6
Length	27 ft 7 in (8.41 m)
Capacity	5 passengers