Home
Piper
Aircrafts
Lance II
Piper Lance II User Manual
4
of 1
of 1 rating
568 pages
Give review
Manual
Specs
To Next Page
To Next Page
To Previous Page
To Previous Page
Loading...
LANCE
II
SERVICE
MANUAL
Locating
and
repairing
the
trouble
early
will
usually
result
in
savings
to
the
customer
both
in
time
and
additional
troubles
that
too
often
result
from
neglect.
A
Performance
Test
of
the
system
is
the
only
positive
way
in
which
the
complete
system
can
be
checked
for
efficient
operation.
The
air
conditioning
system
should
be
given
this
test
before
work
is
begun
on
the
system
whenever
possible,
however,
if
the
system
is
completely
inoperative,
repairs
must
be
performed
before
the
system
can
be
properly
tested.
The
test
can
uncover
further
work
that
must
be
performed
before
the
system
is
brought
to
its
full
operating
efficiency.
The
Performance
Test
should
always
be
performed
after
repair
work
has
been
done
and
before
the
aircraft
is
released
to
the
customer.
The
serviceman
performing
this
test
carefully
will
insure
that
the
repairs
have
been
properly
performed
and
that
the
system
will
operate
satisfactorily.
The
Performance
Test
when
properly
performed
includes
a
thorough
examination
of
the
outside
of
the
system
as
well
as
the
inside.
Many
related
parts
are
overlooked
because
it
is
felt
they
are
of
no
bearing
on
the
operating
efficiency
of
the
unit.
For
this
reason,
a
thorough
visual
inspection
of
the
complete
system
should
be
performed,
followed
by
an
operating
inspection
of
the
system.
14-5.
SPECIAL
SERVICING
PROCEDURES.
The
air
conditioning
system
should
be
serviced
by
a
qualified
shop
with
trained
personnel.
The
following
procedures
and
precautions
should
be
observed.
The
efficiency
of
this
system
depends
upon
the
pressure-temperature
relationship
of
pure
refrigerant.
As
long
as
the
system
contains
only
pure
refrigerant
plus
a
specified
amount
of
compressor
oil
(which
is
mixed
with
the
refrigerant),
it
is
considered
to
be
chemically
stable.
Foreign
materials
within
the
system
will
affect
the
chemical
stability,
contaminate
the
system,
and
decrease
its
efficiency.
I.
GENERAL
REFRIGERATION
SYSTEM
PROCEDURES.
A.
REFRIGERANT
SAFETY
PRECAUTIONS.
1.
Refrigerant
12
(commonly
known
as
R-12
or
"Freon"
12)
is
odorless
and
colorless
in
either
the
liquid
or
gaseous
state.
R-1
2
for
charging
refrigeration
systems
is
supplied
in
pressurized
containers
(approx.
70
psi
at
70
F)
in
liquid
form.
Since
this
material
is
essentially
inert
at
room
temperatures
the
dangers
are
primarily
associated
with
the
pressure
and
the
refrigeration
effects
of
the
release
and
subsequent
evaporation
of
this
pressurized
liquid.
2.
Wear
suitable
eye
protection
when
handling
R-12
due
to
the
possibility
of
freezing
of
the
eye
if
contacted
by
escaping
liquid
refrigerant.
If
liquid
R-l
2
does
strike
the
eye,
the
following
actions
should
be
taken:
a.
DO
NOT
RUB
THE
EYE.
b.
Splash
large
quantities
of
cool
water
into
the
eye
to
raise
the
temperature.
c.
Tape
on
an
eye
patch
to
avoid
the
possibility
of
dirt
entering
the
eye.
d.
Rush
to
a
physician
or
hospital
for
immediate
professional
aid.
e.
DO
NOT
ATTEMPT
TO
TREAT
IT
YOURSELF.
3.
If
liquid
R-12
strikes
the
skin
frostbite
can
occur.
Treat
with
cool
water
and
protect
with
petroleum
jelly.
4.
Do
not
discharge
large
quantities
of
R-12
into
closed
rooms.
It
may
displace
most
of
the
air
in
the
room
and
this
could
cause
oxygen
starvation.
Gaseous
R-l
2
is
heavier
than
air
and
flows
to
the
bottom
of
a
container.
Issued:
1/3/78
ACCESSORIES
AND
UTILTIES
2J22
525
527
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
Based on 1 rating
Ask a question
Give review
Questions and Answers:
Need help?
Do you have a question about the Piper Lance II and is the answer not in the manual?
Ask a question
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
Related product manuals
Piper Cherokee Arrow II
189 pages
Piper CHEROKEE WARRIOR II
282 pages
Piper SARATOGA II HP PA-32R-301
470 pages
Piper Dakota
616 pages
Piper COMANCHE
61 pages
Piper PA-28-180
80 pages
Piper Warrior III
1104 pages
Piper Cherokee 140
62 pages
Piper CHEROKEE 180
73 pages
Piper CHEROKEE 180 C
80 pages
Piper Arrow PA-28R-201
470 pages
Piper Cherokee SIX 300
854 pages