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Piper Lance II User Manual
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LANCE
II
SERVICE
MANUAL
1.
Loosen
rotor
holding
tool
and
move
the
rotor
back
a
few
degrees;
then
move
it
forward.
Both
lights
should
go
out
to
indicate
opening
of
the
main
breakers
when
the
timing
pointer
is
indicating
within
the
width
of
the
"L"
mark
and
the
red
painted
teeth
are
centered
in
timing
windows.
m.
If
breaker
timing
is
not
correct,
loosen
cam
securing
screw
(refer
to
Figure
8-16)
and
unseat
main
breaker
cam
from
taper.
Using
1
1-3031
Retaining
Ring
Pliers
inserted
in
holes
in
cam,
rotate
main
breaker
cam
in
direction
of
rotation
until
left
main
breaker
points
just
open
and
press
cam
onto
taper.
Install
and
torque
cam
retaining
screw
from
21
to
25
inch
pounds.
NOTE
Refer
to
Lycoming
Service
Instructions
No.
1400
for
recommended
replacement
of
old
cam
retaining
screw
with
new
self-locking
cam
retaining
screw.
n.
Loosen
rotor
holding
tool
to
turn
rotating
magnet
back
a
few
degrees;
then
turn
rotating
magnet
in
normal
direction
of
rotation.
Timing
light
should
go
out
when
timing
pointer
is
aligned
with
"L"
("E"
gap)
mark.
Lock
rotating
magnet
in
position
where
points
just
open.
o.
Loosen
right
main
breaker
securing
screws
and
position
breaker
so
cam
follower
is
pressed
against
cam
with
points
closed.
Tighten
contact
assembly
securing
screws
to
prevent
contact
assembly
from
bouncing
back
when
moved.
Using
a
small
mallet
and
drift,
tap
right
breaker
in
until
points
just
open.
p.
Turn
rotating
magnet
back
a
few
degrees;
then
turn
rotating
magnet
in
normal
direction
of
rotation.
Both
timing
lights
should
go
out
within
one
degree
or
half
the
width
of
"L"
mark
on
rotor.
If
breakers
are
not
properly
synchronized,
reset
right
breaker.
q.
Check
right
main
breaker
contact
for
0.016
.004
inch
point
opening
and
torque
right
breaker
contact
securing
screws
to
20-25
inch-pounds.
If
point
opening
is
out
of
limits,
repeat
timing
procedure
setting
left
main
breaker
opening
at
.016
.002
inch.
If
right
contacts
open
beyond
.020
inch,
set
left
contacts
closer
to
.018
inch.
If
right
contacts
open
less
than
.012
inch,
set
left
contacts
closer
to
.014
inch.
r.
Using
timing
light,
recheck
timing
to
insure
main
breakers
open
with
one-half
the
width
of
"L"
mark
and
that
retard
breaker
opens
at
correct
degree
setting.
Using
a
wire
feeler
gauge,
check
left
main
breaker
for
.016
.002
inch
point
opening
and
right
main
breaker
and
retard
breaker
for
.016
.004
inch
point
opening.
NOTE
If
correct
breaker
timing
cannot
be
achieved,
remove
magneto
and
have
it
overhauled.
s.
Check
capacitors
for
looseness
in
the
magneto
cover
of
the
harness
assembly
and
for
any
physical
damage.
The
capacitors
should
be
checked
for
capacitance,
series
resistance
and
leakage.
Capacitance
should
be
0.34
to
0.41
microfarads.
The
use
of
a
Bendix
condenser
tester,
part
number
11-1767-1,
-2
or
-3
or
equivalent
will
simplify
this
test.
Replace
defective
capacitors
and
torque
securing
nut
to
60-70
inch-pounds.
NOTE
Spring
in
capacitor
outlet
may
cause
an
indication
of
a
short
to
ground
if
adapter
lead
is
not
used.
(Refer
to
Paragraph
8-30,
Step
c,
Note.)
POWER
PLANT
Revised:
10/3/80
2B9
320
322
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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