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Piper Lance II User Manual
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LANCE
II
SERVICE
MANUAL
2-19.
TAXIING.
Before
attempting
to
taxi
the
airplane,
ground
personnel
should
be
checked
out
by
a
qualified
pilot
or
other
responsible
person.
Engine
starting
and
shut-down
procedures
should
be
covered
as
well.
When
it
is
ascertained
that
the
propeller
back
blast
and
taxi
areas
are
clear,
apply
power
to
start
the
taxi
roll
and
perform
the
following
checks:
a.
Taxi
forward
a
few
feet
and
apply
brakes
to
determine
their
effectiveness.
b.
Taxi
with
propeller
set
in
low
pitch,
high
RPM
setting.
c.
While
taxiing,
make
slight
turns
to
ascertain
the
effectiveness
of
steering.
d.
Observe
wing
clearances
when
taxiing
near
buildings
or
other
stationary
objects.
If
possible,
station
a
guide
outside
the
airplane
to
observe.
e.
When
taxiing
on
uneven
ground,
look
for
holes
and
ruts.
f.
Do
not
operate
the
engine
at
high
RPM
when
running
up
or
taxiing
over
ground
containing
loose
stones,
gravel
or
any
loose
material
that
may
cause
damage
to
the
propeller
blades.
2-20.
EXTERNAL
POWER
RECEPTACLE.
2-21.
OPERATION
OF
EXTERNAL
POWER
RECEPTACLE.
The
external
power
receptacle
is
located
on
the
left
side
of
the
nose
section
just
aft
of
the
engine
cowling.
When
using
external
power
for
starting
or
operation
of
any
of
the
airplane's
equipment,
the
following
procedure
should
be
followed:
Turn
the
master
switch
OFF
and
turn
all
electrical
equipment
OFF.
Connect
the
RED
lead
of
the
PEP
kit
jumper
cable
to
the
POSITIVE
(+)
terminal
of
an
external
12-volt
battery
and
the
BLACK
lead
to
the
NEGATIVE
(-)
terminal.
Insert
the
plug
of
the
jumper
cable
into
the
socket
located
on
the
fuselage.
Note
that
when
the
plug
is
inserted,
the
electrical
system
is
ON.
Proceed
with
the
normal
starting
technique.
After
the
engine
has
started,
reduce
power
to
the
lowest
possible
RPM,
to
reduce
sparking,
and
disconnect
the
jumper
cable
from
the
aircraft.
Turn
the
master
switch
ON
and
check
the
alternator
ammeter
for
an
indication
of
output.
DO
NOT
ATTEMPT
FLIGHT
IF
THERE
IS
NO
INDICATION
OF
ALTERNATOR
OUTPUT.
If
aircraft
battery
is
weak,
charging
current
will
be
high.
DO
NOT
TAKE
OFF
until
charging
current
falls
below
20
amps.
NOTE
For
all
normal
operations
using
the
PEP
jumper
cables,
the
master
switch
should
be
OFF,
but
it
is
possible
to
use
the
ships
battery
in
parallel
by
turning
the
master
switch
ON.
This
will
give
longer
cranking
capabilities,
but
will
not
increase
the
amperage.
CAUTION:
Care
should
be
exercised
because
if
the
ships
battery
has
been
depleted,
the
external
power
supply
can
be
reduced
to
the
level
of
the
ships
battery.
This
can
be
tested
by
turning
the
master
switch
ON
momentarily
while
the
starter
is
engaged.
If
cranking
speed
increases,
the
ships
battery
is
at
a
higher
level
than
the
external
power
supply.
When
the
engine
is
firing
evenly,
advance
the
throttle
to
800
RPM.
If
oil
pressure
is
not
indicated
within
thirty
seconds,
stop
the
engine
and
determine
the
trouble.
In
cold
weather
it
will
take
a
few
seconds
longer
to
get
an
oil
pressure
indication.
If
the
engine
has
failed
to
start,
refer
to
the
Lycoming
Operating
Handbook,
Engine
Troubles
and
Their
Remedies.
Starter
manufacturers
recommended
that
cranking
periods
be
limited
to
thirty
seconds
with
a
two
minute
rest
between
cranking
periods.
Longer
cranking
periods
will
shorten
the
life
of
the
starter.
Issued:
1/3/78
1C1
HANDLING
AND
SERVICING
48
50
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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