Piper Lance II User Manual

LANCE
II SERVICE
MANUAL
8. Remove the forward
head duct from one side of the floor
tunnel. (Preferably
from the side from
which the control cable
is to be removed.)
9. Move the cable guard (4) located under the pulley cluster (5) and below the fuel
selector by
removing the cotter pin from the exposed
end and sliding it to the left or right
as
required.
10. Disconnect the end of the cable from the arm on the rudder pedal torque tube
by removing the cotter pin, nut, washer and bolt (2).
11. Draw the cable from the floor tunnel.
d. The aft
rudder control cable (17) may be
removed by the following procedure:
1. Remove
the tail cone by removing
its attachment screws.
2. Disconnect
the cable
from the sector
assembly (18)
by removing cable
guards
from the sector assembly and pulleys.
3. Draw the cable through the fuselage.
5-27.
INSTALLATION OF RUDDER
CONTROL CABLES. (Refer to Figure
5-12.)
a. The forward
rudder control
cables (13 and
14) may be installed
by the following
procedure:
1.
Draw the control cable
through the floor tunnel.
2. Connect
the end of the cable to the arm on
the rudder pedal torque tube (1)
by
installing bolt, washer,
nut and cotter
pin (2). Allow
the cable end
free to rotate.
3. Connect
the cable (13 or
14) to the aft control
cable (17)
at the turnbuckles
(15
and
16) in
the aft section
of
the fuselage.
If the
aft control
cable is
not installed,
install
at
this
time per step
b. Ascertain
that
each cable
is in the
groove of its
pulley.
4. Move the
cable guard
(4) that
is located in
the forward
tunnel, under
the pulley
cluster (5) and below the fuel selector into position, and secure with cotter pin.
5. Within the area of the floor opening aft of the main spar, install the cable guard
blocks
(6)
onto
the spar
housing
and secure
with
screws,
and
the cable
guard
pin (9)
at the
pulley
cluster (8)
in the aft
area of
the opening
by sliding
it into
position
and fastening
it
with a cotter pin.
6. Install
the cable
guard
plate (10)
under
the pulley
cluster
(12) located
in the
aft
area
of the aft floor tunnel
and secure with screws.
7. Set
cable tension
and check
rigging
and adjustment
per
paragraph
5-28.
8.
Install
the heat
duct
and
secure
with
screws.
9.
Install the
forward
tunnel plate
aft of the
tee bar and
secure with
screws.
10.
Put
the floor
carpet
in
place
and secure.
11. Place
the fuel
selector
lever
on the selector
torque
tube
and secure
with
pin and
cotter
pin.
12.
Install
the lower
and
upper
selector
covers
and secure
with
screws.
13.
Install the
floor
panel and
seat belt
attachment
aft
of the main
spar securing
the
panel
with
screws,
and install
the seats.
14. Install
the
cover
and carpet
of
the aft
floor tunnel.
b.
The aft rudder
control
cable (17)
may be installed
by the
following
procedure:
1.
Refer to Figure 5-12 to
position the control
cable
2.
Connect cable
at turnbuckles
(15
and 16)
in the aft section
of the
fuselage.
3.
Install cable
guard cotter
pins above
pulleys
(19) and at
the aft portion
of the
sector assembly.
4. Set cable
tension
and check
rigging
and adjustment
per paragraph
5-28.
5. Install
tail cone
and secure
with
screws.
c. Install
the access panel
to the
aft section of
the fuselage.
Issued:
1/3/78
SURFACE
CONTROLS
1G16

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