Piper Lance II User Manual

LANCE
II SERVICE
MANUAL
Figure
5-6. Stabilator
Rigging Tool
3. Secure
the
control
column
in the near
forward
position.
Allow
.500 +
.250 inch
between
the
column
and
the
stop
bumper.
4. Check
each control
cable
for the correct
tension
as given
in Table
V-I.
5. Should
tension be
incorrect,
loosen the
turnbuckle
of the lower
cable in the
aft
section
of the fuselage
and
adjust the
turnbuckle
of the upper
cable
to obtain
correct tension.
Cable
tension
should
be obtained
with
control
wheel
at the
.500
+ .250
inch dimension
from
the stop and the stabilator
contacting
its stop.
6. After
setting
tension,
recheck
control
column
travel
per Step
2.
7. With
control
wheel forward
and stabilator
on
primary down
stop,
check for
.250
inch
minimum
clearance
between
tee
bar and
secondary
forward
stop.
8.
Check safety
of all
turnbuckles
and
bolts.
9. With the
tension of
the upper
cable correct
and the control
wheel
still forward,
adjust
the turnbuckle
of
the lower
cable to
obtain correct
tension.
10. Check
the
full travel
of the
control wheel
with
relation
to the
full travel
of the
stabilator
to determine
that
the stabilator
contacts
its
stops before
the control
wheel
contacts
its stops.
With
the control
wheel
in the fore
and aft positions,
the
travel distance
from
the point
where
the stabilator
contacts
its stops
and
the control
wheel
contacts
its
stops
should
be
approximately
equal.
Readjust
turnbuckles
if incorrect.
II. Reinstall
access
panels and
fin tip.
Revised:
10/3/80
SURFACE
CONTROLS
1G6

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