Piper Lance II User Manual

LANCE
II SERVICE
MANUAL
6. Loosen
the
connecting
bolts (3)
of the
idler
sprockets
(15
and
18) to allow
the
chain
to
fit
snug
around
the
control
wheel
sprockets
and
over
the
idler
sprockets.
7. Connect
the
aileron
control
cables
(22)
to the
ends
of
the
chains
(14
and
16)
with
bolts,
bushings,
nuts
and
cotter
pins
(19).
8. Adjust
the
chain
turnbuckle
(6)
between
the
two
control
wheel
sprockets
to
allow
the
control
wheels
to
be neutral
and
obtain
proper
cable
tension
as
given
in
Table
V-I.
It
may
be
necessary
in order
to
have
both
control
wheels
neutral
to
set the
chain
turnbuckle
to
neutralize
the
wheels
and
then
set
cable
tension
with
the
turnbuckles
located
under
the
floor
panel
aft
of
the
main
spar
as
instructed
in
Paragraph
5-11.
Before
safetying
the
turnbuckle,
check
that
when
the
ailerons
are
neutral,
the
control
wheels
will
be
neutral
and
the
chain
turnbuckle
centered.
Also
the
aileron
bellcranks
should
contact
their
stops
before
the
control
wheel
hits
its
stop.
Maintain
.030
to
.040
clearance
between
sprocket
pin
and
adjustable
stop
bolts
on
models
having
adjustable
tee
bar
stops.
9.
Set
stabilator
cable
tension
with
the
turnbuckle
in
the
aft
section
of
the
fuselage
and
instruction
given
in Paragraph
5-15.
Check
safety
of
all
turnbuckles
upon
completion
of
adjustments.
10.
Tighten
the
connecting
bolts
(3)
of
the
idler
sprockets
(15
and
18).
11.
Install
the
floor
tunnel
plate
and
secure
with
screws.
Fasten
the
tunnel
carpet
in
place.
b.
Either
control
wheel
assembly
may
be
installed
by
the
following
procedure:
1.
Insert
the
control
wheel
tube
through
the
instrument
panel.
2.
Should
wires
for
the
various
Autopilot
systems
need
to
be
installed
in
the
control
tube,
route
them
through
the
hole
in
the
forward
side
of
the
tube
and
out
of the
small
hole
in the
side.
Position
the
rubber
grommet
in
the
hole
in the
side
of
the
tube.
3.
On the
left
control
tube,
install
the
stop
(12).
4.
Connect
the
control
wheel
tube
(4)
to
the
flexible
joint
(2)
of
the
tee
bar
assembly.
If
the
control
cables
and/or
chains
have
not
been
removed
or
loosened,
place
the
ailerons
in neutral
and
install
the
control
tube
on
the
flexible
joint
to allow
the
control
wheel
to
be
neutral.
Install
bolt,
washer
and
nut
(3)
and
tighten.
5-6.
AILERON
CONTROLS.
5-7.
REMOVAL
OF
AILERON
CONTROL
CABLES.
(Refer
to
Figure
5-2.)
a.
For
the
removal
of
any
of
the
control
cables
in
the
fuselage
or
wings,
first
remove
the
floor
panel
that
is
located
directly
aft
of
the
main
spar
by
removing
the
center
seats,
seat
belt
attachments
and
the
screws
securing
the
panel.
Lift
the
panel
and
remove
the
airplane.
b.
To
remove
either
the
right
or
left
primary
control
cables
(14
and
15)
that
are
located
in
the
fuselage,
the
following
procedure
may
be
used:
1.
Remove
the
fuel
selector
panel
cover
by
removing
the
rudder
trim
knob
and
the
cover
attachment
screws.
2.
Remove
the
lower
selector
cover
and
disconnect
the
fuel
selector
control
lever
from
the
selector
torque
tube
by
removing
the
attachment
pin
located
at the
bottom
of
the
lever.
3.
Remove
the
tunnel
plate
just
aft
of
the
tee
bar
by
laying
back
enough
tunnel
carpet
to
remove
the
plate
attachment
screws.
4.
Remove
the
forward
heat
duct
from
one
side
of
the
floor
tunnel
(preferably
from
the
side
from
which
the
cable
is
to
be
removed)
by
removing
the
trim
control
wheel
cover,
the
heater
baffles
from
the
side
of
the
duct,
the
floor
carpet
and
the
duct
attachment
screws.
Issued:
1/3/78
SURFACE
CONTROLS
1F19

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