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Piper Lance II User Manual
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LANCE
II
SERVICE
MANUAL
2.
Attach
one
end
of
a
clean
plastic
hose
to
the
valve
stem
of
the
filler
plug
and
submerge
the
other
end
in
a
container
of
hydraulic
fluid.
NOTE
An
air-tight
connection
is
necessary
between
the
plastic
tube
and
the
valve
stem.
Without
such
a
connection,
a
small
amount
of
air
will
be
sucked
into
the
oleo
strut
during
each
sequence,
resulting
in
an
inordinate
amount
of
air
bubbles
and
a
prolonged
filling
operation.
3.
Fully
compress
and
extend
the
strut
thus
drawing
fluid
from
the
fluid
container
and
expelling
air
from
the
strut
chamber.
By
watching
the
fluid
pass
through
the
plastic
hose,
it
can
be
determined
when
the
strut
is
full
and
no
air
is
present
in
the
chamber.
4.
When
air
bubbles
cease
to
flow
through
the
hose,
compress
the
strut
fully
and
remove
the
hose
from
the
valve
stem.
5.
With
the
strut
compressed,
remove
the
filler
plug
to
determine
that
the
fluid
level
is
visible
up
to
the
bottom
of
the
filler
plug
hole.
6.
Reinstall
the
core
in
the
filler
plug
and
apply
thread
lubricant
(Parker
6PB)
to
the
threads
of
the
filler
plug
and
install
the
plug
in
the
top
of
the
strut
housing.
Torque
the
plug
to
45
foot-pounds.
Method
2:
1.
Remove
the
filler
plug
from
the
top
of
the
nose
gear
strut
housing
or
at
the
top
inboard
side
of
the
main
gear
housing.
2.
Raise
the
strut
piston
tube
until
it
is
fully
compressed.
3.
Pour
fluid
from
a
clean
container
through
the
filler
opening
until
it
reaches
the
bottom
of
the
filler
plug
hole.
(Air
pressure
type
oil
container
may
be
helpful.)
4.
Install
the
filler
plug
finger
tight
and
extend
and
compress
the
strut
two
or
three
times
to
remove
air
from
the
housing.
5.
Remove
the
filler
plug,
raise
the
strut
to
full
compression
and
fill
with
fluid
if
needed.
6.
Apply
thread
lubricant
(Parker
6PB)
to
the
threads
of
the
filler
plug.
Reinstall
the
filler
plug
and
torque
to
45
foot-pounds.
e.
With
the
airplane
still
on
jacks,
compress
and
extend
the
gear
strut
several
times
to
ascertain
that
the
strut
actuates
freely.
The
weight
of
the
gear
fork
and
wheel
should
extend
the
strut.
f.
Clean
off
overflow
of
fluid
and
inflate
the
strut
as
described
in
Paragraph
2-41.
g.
Check
that
fluid
is
not
leaking
around
the
strut
piston
at
the
bottom
of
the
housing.
2-41.
INFLATING
OLEO
STRUTS.
After
making
certain
that
an
oleo
strut
has
sufficient
fluid,
attach
a
strut
pump
to
the
air
valve
and
inflate
the
oleo
strut.
The
strut
should
be
inflated
until
the
correct
inches
of
piston
is
exposed
with
normal
static
load
(empty
weight
of
airplane
plus
full
fuel
and
oil)
on
the
gears.
(Refer
to
Paragraph
2-39.)
Rock
the
airplane
several
times
to
ascertain
that
the
gear
settles
back
to
the
correct
strut
position.
(If
a
strut
pump
is
not
available,
the
airplane
may
be
raised
and
line
pressure
from
a
high
pressure
air
system
used.
Lower
the
airplane
and
while
rocking
it,
let
air
from
the
valve
to
bring
the
strut
down
to
the
proper
extension.)
Before
capping
the
valve,
check
for
valve
core
leakage.
Issued:
1/3/78
HANDLING
AND
SERVICING
1C8
55
57
Table of Contents
Table of Contents
3
Schematic Diagram of RSA Fuel Injection System
7
Electrical Symbols
11
Landing Gear
13
Scope of Manual
13
Brake System
14
Flight Controls
14
Fuel System
14
Instrument and Autopilot System
14
Section II Handling and Servicing
15
Handling and Servicing
15
Dimensions
17
Serial Number Plate
17
Ia17
17
Station Reference Lines
17
Tools and Test Equipment
25
Torque Requirements
25
Installation of Flexible Hose Assemblies
31
Ground Handling
45
General
45
Leveling
46
Mooring
47
Parking
48
Taxiing
49
External Power Receptacle
49
Fuel System
50
1C2
50
Filling Fuel Tanks
50
Draining Fuel System
51
Servicing
50
General
50
Brake System
51
Servicing Brake System
51
Filling Brake Cylinder Reservoir
51
Draining Brake System
51
Hydraulic System
54
Servicing Hydraulic System
54
1C6
54
Servicing Hydraulic Pump Reservoir
54
Landing Gear System
54
Servicing Landing Gear
54
Inspection
77
Sectionv Surfacecontrols
131
Wing
131
Surface Controls
132
Description
132
Introduction
132
Control Column Assembly
138
Removal of Control Column Assembly
138
Aileron Controls
139
Removal of Aileron Control Cables
139
Installation of Aileron Control Cables
140
Removal of Aileron Bellcrank Assembly
142
Installation of Aileron Bellcrank Assembly
143
Rigging and Adjustment of Aileron Controls
143
Stabilator Controls
147
Removal of Stabilator Control Cables
147
Installation of Stabilator Control Cables
148
Rigging and Adjustment of Stabilator Controls
149
Stabilator Trim Controls
153
Removal of Stabilator Trim Assembly (Forward)
153
Installation of Stabilator Trim Assembly
154
Removal of Stabilator Trim Controls (Aft)
155
Installation of Stabilator Trim Controls (Aft)
155
Rigging and Adjustment of Stabilator Trim
155
Rudder and Steering Pedal Assembly
156
Installation of Rudder and Steering Pedal Assembly
157
Rudder Controls
159
Removal of Rudder Control Cables
159
Installation of Rudder Control Cables
160
Rigging and Adjustment of Rudder Controls
162
Rudder Trim Controls
162
Removal of Rudder Trim Controls
162
Sectionvi Hydraulic System
181
Description
181
Hydraulic System
181
Assembly of Hydraulic Pump
192
Installation of Hydraulic Pump
193
Gear Back-Up Extender Actuator Assembly
193
Removal of Gear Back-Up Extender Actuator Assembly
193
Installation of Gear Back-Up Extender Actuator Assembly
194
Check and Adjustment of Gear Back-Up Extender Actuator
196
Nose Gear Actuating Cylinder
199
Removal of Nose Gear Actuating Cylinder
199
Disassembly of Nose Gear Actuating Cylinder
200
Cleaning, Inspection and Repair of Nose Gear Actuating Cylinder
201
Assembly of Nose Gear Actuating Cylinder
201
Installation of Nose Gear Actuating Cylinder
201
Main Gear Actuating Cylinder
201
Removal of Main Gear Actuating Cylinder
201
Disassembly of Main Gear Actuating Cylinder
203
Cleaning, Inspection and Repair of Main Gear Actuating Cylinder 1111
203
Assembly of Main Gear Actuating Cylinder
203
Installation of Main Gear Actuating Cylinder
204
Hydraulic Lines
204
Sectionvii Landing Gear and Brake System
219
Description
221
Introduction
221
Landing Gear System
225
Nose Landing Gear System
225
Disassembly of Nose Gear Oleo
225
Cleaning, Inspection and Repair of Nose Gear Oleo
226
Assembly of Nose Gear Oleo
226
Removal of Nose Landing Gear
228
Cleaning, Inspection and Repair of Nose Landing Gear
230
Installation of Nose Landing Gear
230
Adjustment of Nose Landing Gear
236
Alignment of Nose Landing Gear
237
Removal of Nose Gear Door Assembly
238
Cleaning, Inspection and Repair of Nose Gear Door Assembly
239
Installation of Nose Gear Door Assembly
240
Adjustment of Nose Gear Doors
240
Main Landing Gear System
240
Disassembly of Main Gear Oleo
240
Cleaning, Inspection and Repair of Main Gear Oleo
245
Assembly of Main Gearoleo
245
Removal of Main Landing Gear
249
Cleaning, Inspection and Repair of Main Landing Gear
250
Installation of Main Landing Gear
251
Adjustment of Main Landing Gear
252
Alignment of Main Landing Gear
253
Cleaning, Inspection and Repair of Main Gear Door Assembly
256
Installation of Main Gear Door Assembly
256
Troubleshooting
225
Landing Gear Limit Switches
256
Adjustment of Nose Gear up Limit Switch
257
Adjustment of Main Gear down Limit Switch
258
Adjustment of Landing Gear Safety Switch (Squat Switch)
259
Adjustment of Gear Back-Up Extender Actuator Switch
259
Wheel Brake Assembly
269
Brake Master Cylinder (Hand/Parking Brake)
272
Brake Cylinder (10-27) (Toe Brake)
275
Brake Cylinder (1700) (Toe Brake)
275
Brake Cylinder (10-30) (Toe Brake)
278
Fuel System
291
2D12
291
Painted Tooth Centered in Timing Window
292
Timing Mark on Rotor Aligned with Pointer
292
Timing Light Connected to Magneto and Breakers
292
Checking Flyweight to Stop Pin Clearance
292
Checking Impulse Coupling for Magnetization
292
Orientation of Springs in Coupling Body
292
Checking Harness Lead Continuity
292
Checking Harness Lead Insulation Resistance
292
Removing Spring from Lead Assembly
292
Electrical System Troubleshooting
295
Temperature Pressure Chart
295
Aluminum Tubing Torque
295
Compressor Oil Charge
295
Oxygen System Component Limits
295
Propeller Installation
299
Propeller Blade Minor Repair
300
Propeller Governor
303
Engine Installation
306
Adjustment of Engine Controls
308
Fuel Injector
311
Fuel-Air Bleed Nozzle
313
Height of Spring in Distributor Block Tower
314
Contact Points
315
Engine Timing Marks
315
Timing Light Connected to Magneto
317
Timing Marks on Magneto Rotor
318
Cam End View of Magneto
322
Removing Impulse Coupling
323
Stop Pin Installation Dimension
324
Checking Flyweight Axial Wear with Drill Shank
325
Checking Flyweight Radial Wear with Gauge
325
Points of Coupling Body Wear
326
Acceptable and Deformed Coupling Springs
326
Lifting Inner End of Spring
328
Modified Pliers
330
Assembly Tool
331
Using Assembly Tool
331
Ferrule Positioned under Braid
331
Hydraulic System
291
Landing Gear and Brake System
291
1J3
291
Aerofiche Card no
291
Power Plant (Pa-32Rt-300) 2A8 Viiia
291
Power Plant (Pa-32Rt-300T) 2C8
291
Structure
291
Vsurface Controls
291
General/Engine
386
Engine
386
General
386
Airspeed Indicator
403
Troubleshooting
404
Troubleshooting
406
Manifold Pressure Gauge
407
Troubleshooting
407
Tachometer Indicator
407
Troubleshooting
408
Troubleshooting
409
Fuel Pressure Gauge (PA-32RT-300)
409
Troubleshooting
410
Turn and Bank Indicator
411
Troubleshooting
411
Electrical Instruments
412
Fuel Quantity Indicator
412
Troubleshooting
412
Oil Temperature Indicator
413
Electrical System
419
General
420
Index - Electrical System Schematics
422
Ammeter
443
General
455
Electrical System Component Loads
469
Electrical Symbols
487
Electrical Wire Coding
488
Electronics
501
Heating and Ventilating
512
Accessories and Utilities
520
4
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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
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