Piper Lance II User Manual

LANCE
II SERVICE
MANUAL
h. Connect the
steering rods (21)
to the rudder pedals
(32 and 33)
and secure with
bolts
and nuts (24).
Check steering
rod
adjustment per
Alignment
of Nose Gear,
Section
VII.
i
Connect the
rudder trim
to the arm of
the torque
tube and secure
with bolt,
washer,
nut
and cotter pin.
A thin washer
is installed
under the
nut which
is tightened
only finger
tight.
j.
Connect the
ends of the
rudder control
cables
(19) to the
arms provided
on the
torque
tube and
secure with
bolts, washers,
nuts and cotter
pins (2).
Allow the ends
free to
rotate.
k. Swing
the tee bar
into place
and secure
with attachment
bolts, washers
and nuts
(15)
with the
bolts inserted
in through
each side of
the floor tunnel.
1. Connect
the stabilator
control
cables to
the lower
end of the
tee bar with
bolt,
washer
and nut,
and secure
with cotter
pin. Allow
the cable
ends free
to rotate.
m.
Set rudder
cable
tension
and
check
rigging
and adjustment
per
paragraph
5-28.
n. Set
stabilator
cable
tension
and
check
rigging
and
adjustment
per
paragraph
5-15.
o.
Check
aileron
cable
tension.
p. Check
safety
of bolt
and turnbuckles.
q.
Install
the
floor
tunnel
plate
and
secure
with
screws.
Fasten
the
tunnel
carpet
in
place.
r.
Install the
fuel
selector
lever
on the
selector
torque
tube,
secure
with clevis
pin
and
safety
with
cotter pin.
s. Install
the
fuel selector
covers
and the
rudder
trim control
knob.
t.
Install
the access
to the
aft section
of
the fuselage.
5-25.
RUDDER CONTROLS.
5-26.
REMOVAL
OF
RUDDER
CONTROL
CABLES.
(Refer
to Figure
5-12.)
a. To
remove
either
the
forward
(13 and
14)
or aft
(17) rudder
cable,
first remove
the
access
panel
to the
aft section
of the
fuselage.
b.
Disconnect
the
desired
cable
at the
turnbuckle
(15
or
16) in
the
aft section
of the
fuselage.
c. Either
forward
rudder
cable
(13
or 14)
may
be removed
by
the following
procedure:
1. Remove
the
tunnel
cover
in the
aft
area of
the
cabin
by removing
the carpet
over
the
tunnel and the cover
attachment screws.
2.
Remove
the
cable
guard plate
(10)
from
the underside
of the
pulley
cluster
(12)
that
is located
in
the aft
area
of the
floor tunnel,
by removing
the guard
attachment
screws.
3. Remove
the
floor
panel
located
directly
aft of
the
main
spar by
removing
the
center
seats,
seat
belt attachments
and
the screws
securing
the
floor
panel.
Lift
the
panel
and remove
from airplane.
4.
From
within
the
area
of
the floor
opening,
remove
the
cable
rub
blocks
(6)
that
are
attached
to
the
spar
housing
by
removing
the
block
attachment
screws.
Also
remove
the
cable
guard
pin
(9)
at the
pulley
(8) cluster
in
the aft
area
of
the
opening
by
removing
a
cotter
pin
from
one
end of
the
guard.
5.
Remove
the
fuel
selector
panel
cover
by removing
the rudder
trim
knob
and the
cover
attachment
screws.
6. Remove
the
lower
selector
cover,
and
the fuel
selector
control
lever
by removing
the
attachment
pin,
at
the bottom
of
the lever,
that
holds
the
lever
on
the
selector
torque
tube.
7.
Remove
the
tunnel
plate
just
aft
of the
tee bar
by
removing
enough
carpet
from
the
tunnel
to allow
the plate
attachment
screws
and
the
plate
to be
removed.
Issued:
1/3/78
SURFACE
CONTROLS
1G15

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