Piper Lance II User Manual

LANCE
II SERVICE
MANUAL
TABLE
V-III.
TROUBLESHOOTING
CHART
(SURFACE
CONTROLS)
(cont.)
Trouble
Cause
Remedy
AILERON
CONTROL
SYSTEM
(cont.)
Control
wheels
not
synchronized.
Control
wheels
not
hori-
zontal
when
ailerons
are
neutral.
Incorrect
aileron
travel.
Incorrect
control
column
rigging.
Incorrect
rigging
of
aileron
system.
Aileron
control
rods
not
adjusted
properly.
Rig in accordance
with
paragraph
5-5.
Rig in accordance
with
paragraph
5-1 1.
Adjust
in
accordance
with
paragraph
5-1
1.
Aileron
bellcrank
stops
not
adjusted
properly.
Adjust
in
accordance
with
paragraph
5-11.
Correct
aileron
travel
cannot be
obtained
by
adjusting
bellcrank
stops.
Control
wheel
stops
before
control
surfaces
reach
full
travel.
Incorrect
rigging
of
aileron
cables,
control
wheel
and
control
rod.
Incorrect
rigging
between
control
wheel
and control
cables.
Rig
in accordance
with
paragraph
5-11.
Rig
in
accordance
with
paragraph
5-1
1.
Issued:
1/3/78
SURFACE
CONTROLS
1H7

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