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Piper Lance II User Manual
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NOTE
Throttle
and
mixture
free
play
of
up
to
.30
inches
measured
at
the
point
where
the
control
lever
comes
through
the
quadrant
is
acceptable
providing
the
throttle
or
mixture
arm
at
the
injector
is
held
against
its
stops
when
the
control
lever
is
at
the
full
forward
and
full
aft
positions.
8-17.
INDUCTION
AIR
FILTER.
a.
The
filter
should
be
cleaned
daily
when
operating
in
dusty
conditions.
If
any
holes
or
tears
are
noticed,
the
filter
must
be
replaced
immediately.
b.
Remove
the
filter
element
and
shake
off
loose
dirt
by
rapping
on
a
hard
flat
surface.
being
careful
not
to
damage
or
crease
the
sealing
ends.
CAUTION
Never
wash
the
filter
element
in
any
liquid
or
soak
it
in
oil.
Never
attempt
to
blow
off
dirt
with
compressed
air.
c.
The
filter
housing
can
be
cleaned
by
wiping
with
a
clean
cloth
soaked
in
unleaded
gasoline.
When
the
housing
is
dry,
reinstall
and
seal
the
filter
element.
8-18.
ALTERNATE
AIR
DOOR.
The
alternate
air
door
is
located
on
the
backside
of
the
air
filter
box
which
is
part
of
the
lower
cowl
and
controlled
by
a
lever
mounted
next
to
the
engine
control
quadrant
in
the
cockpit.
The
alternate
air
source
is
taken
off
the
exhaust
stack
assembly.
The
following
should
be
checked
during
inspection:
a.
Check
that
the
air
door
seals
are
tight
and
hinge
is
secure.
b.
Actuate
the
door
to
determine
that
it
is
not
sticking
or
binding
and
the
control
cable
has
free
travel.
c.
Check
that
when
the
air
door
is
fully
opened
and
the
cockpit
control
is
in
the
open
position,
the
cable
has
6
to
8
pounds
tension
when
lever
goes
into
full
open
and
locked
position.
This
insures
positive
seal
in
the
air
box.
(Cable
tension
is
measured
at
the
control
lever
with
a
spring
scale.
Adjust
as
required.)
8-19.
FUEL
INJECTOR.
8-20.
FUEL
INJECTOR
MAINTENANCE.
a.
In
general,
little
attention
is
required
between
injector
overhauls.
However,
it
is
recommended
that
the
following
items
be
checked
during
periodic
inspection
of
the
engine;
torque
all
nuts
to
135-150
inch-pounds.
Seat
pal
type
nuts
finger
tight,
against
plain
nuts,
and
then
tighten
an
additional
1/3
to
1/2
turn.
1.
Check
tightness
and
lock
of
all
nuts
and
screws
which
fasten
the
injector
to
the
engine.
2.
Check
all
fuel
lines
for
tightness
and
evidence
of
leakage.
A
slight
fuel
stain
adjacent
to
the
air
bleed
nozzles
is
not
cause
for
concern.
3.
Check
throttle
and
mixture
control
rod
ends
and
levers
for
tightness
and
lock.
Issued:
1/3/78
POWER
PLANT
2A21
LANCE
II
SERVICE
MANUAL
308
310
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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