Continental Motors TSIO-520-BE User manual

Publication X30570 CHANGE 2
©2011-2013 CONTINENTAL MOTORS, INC. OCT 2013
TSIO-520-BE
CONTINENTAL®AIRCRAFT ENGINE
PERMOLD SERIES
MAINTENANCE
AND
OPERATOR’S MANUAL
TECHNICAL CONTENT ACCEPTED BY THE FAA

A TSIO-520-BE Permold Series Engine Maintenance and Operator’s Manual
CHANGE 2 15 October 2013
Supersedure Notice
This manual revision replaces the front cover and list of effective pages for Publication Part No. X30570, dated
February 1990. Previous editions are obsolete upon release of this manual.
Effective Changes for this Manual
0 ..............February 1990
1 ............ 31 August 2011
2 .......... 15 October 2013
List of Effective Pages
Document Title: TSIO-520-BE Permold Series Engine Maintenance and Operator’s Manual
Publication Number: X30570 Initial Publication Date: February 1990
Page Change Page Change Page Change Page Change
Cover............................ 2
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4-1 thru 4-4................... 0
5-1 thru 5-8................... 0
6-1 thru 6-8................... 0
7-1 thru 7-6................... 0
8-1 thru 8-6................... 0
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10-1 thru 10-12.............0
11-1 thru 11-4 ............... 0
12-1 thru 12-2...............0
13-1 thru 13-15.............0
Published and printed in the U.S.A. by Continental Motors, Inc.
Available exclusively from the publisher: P.O. Box 90, Mobile, AL 36601
Copyright © 2011-2013 Continental Motors, Inc. All rights reserved. This material may not be reprinted, republished, broadcast, or otherwise
altered without the publisher's written permission. This manual is provided without express, statutory, or implied warranties. The publisher will
not be held liable for any damages caused by or alleged to be caused by use, misuse, abuse, or misinterpretation of the contents. Content is
subject to change without notice. Other products and companies mentioned herein may be trademarks of the respective owners.

FORM NO. X30570-1
i
MAINTENANCE AND OPERATOR’S MANUAL
FOR
TSIO-520-BE AIRCRAFT ENGINE
- NOTICE-
The operator must comply with all the instructions contained in this manual in order to assure safe and reliable
engine performance. Failure to comply will be deemed misuse, thereby relieving the engine manufacturer of
responsibility under its warranty.
This manual contains no warranties, either expressed or implied. The information and procedures contained
herein provide the operator with technical information and instructions applicable to safe operation.

CHAPTER INDEX
c~~~ P~e
Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-1
2 Tools and Equipment .................................................. 2-1
3 Detailed Engine Description ............................................. 3-1
4 Engine Specifications and Operating limits . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-1
5 Unpacking, Installation, Testing & Removal .................................. 5-1
6 Normal Operating Procedures ............................................ 6-1
7 Emergency Operating Procedures ......................................... 7-1
8 Abnormal Environmental Conditions ....................................... 8-1
9 Service and Maintenance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9-1
1 O Trouble Shooting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10-1
11 Engine Preservation and Storage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11-1
12 Airworthiness Limitations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12-1
13 Engine Performance and Cruise Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13-1
ii

FIGURE INDEX
Figure No. Page
3- 1 Lubrication System Schematic
3-3
3- 2 Induction and Exhaust System Schematic . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-5
3- 3 Turbocharger Sectional . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-5
3- 4 Ignition Wiring Diagram . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-7
3- 5 Fuel Injection System Schematic . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-7
5- 1 Installation Drawing
5-4
5- 2 Installation Drawing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-5
6- 1 Priming Time Requirement . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-8
13- 1 Sea Level Performance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13-4
13- 2 Constant Speed Sea Level Performance Full Rich Mixture ....................... 13-5
13- 3 Constant Speed Sea Level Performance Best Power Mixture ..................... 13-6
13- 4 Altitude Performance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13- 7
13- 5 Mixture Ratio Curve - 80% 2500 RPM and 32.8" Hg. ADMP ...................... 13-8
13- 6 Mixture Ratio Curve - 75% 2400 RPM and 32.5" Hg. ADMP ...................... 13-9
13- 7 Mixture Ratio Curve - 65% 2300 RPM and 30.0" Hg. ADMP ..................... 13-10
13- 8 Mixture Ratio Curve -
50% 2200 RPM and 25.8" Hg. ADMP
13-11
13- 9 Fuel Flow Vs. Brake Horsepower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13-12
13-10 Metered Fuel Pressure Vs. Fuel Flow ..................................... 13-13
13-11 Fuel Injection Fuel Pump Pressure - PSIA Vs.
% Rated Horsepower - 100°F AVGAS .................................... 13-14
13-12 Fuel Flow Vs. Pressure Drop . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13-15
iii

INTENTIONALLY
LEFT
BLANK
iv

Section
1-1
1-2
1-3
1-4
CHAPTER 1
INTRODUCTION
Section Index
Page
Scope..... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-2
Related Publications . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-3
Abbreviations and Glossary of Terms . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-4
Manual Revisions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-6
1-1

INTRODUCTION
1-1 SCOPE
Recommendations, cautions and warnings regarding operation of this engine are not intended to
impose undue restrictions, but are inserted to enable the pilot to obtain maximum performance from
the engine commensurate with safety and efficiency. Abuse, misuse,
or neglect of any piece of
equipment can cause eventual failure. In the case of
an aircraft engine it should be obvious that a
failure may have disastrous consequences. Failure
to obseive the instructions contained in this
manual constitutes unauthorized operation in areas unexplored during development
of the engine,
or in areas which experience
has proved to be undesirable or detrimental.
Notes, Cautions and Warnings are included throughout this manual, Application is as follows:
NOTE
... Special interest information which may facilitate the operation of equipment.
CAUTION ... Information issued to emphasize certain instructions or to prevent possible damage
to engine or accessories.
WARNING ... Information which, if disregarded, may result in severe damage to or
destruction of the engine or endangerment to personnel.
1-2

1-2 RELATED PUBLICATIONS
I. Engine Manuals:
A Overhaul Manual for TSI0-520-BE Series Aircraft Engine. Form No. X30574A.
8. Illustrated Parts Catalog for TSI0-520-BE Series Aircraft Engine. Form No. X30576A.
C. Teledyne Continental Motors Aircraft Engine Service Bulletins.
D. Fuel Injection Manual. Form X30593A.
The above publications can be ordered through your Teledyne Continental Motors Distributor
or ordered directly, if prepaid, from:
Teledyne Continental Motors
Aircraft Products
P. 0. Box 90
Mobile, AL 36601
Attn: Accounts Receivable
For price information see TCM Optional and Current Publications Service Bulletins.
II. Accessory Manuals:
A. Magnetos
B. Starter Motor
C. Alternator
Service Manual
Teledyne Continental Motors
Aircraft Products
P. 0. Box 90
Mobile, AL 36601
Attn: Accounts Receivable
Teledyne Continental Motors
Aircraft Products
P. 0. Box 90
Mobile, AL 36601
Attn: Accounts Receivable
Alternator Service Instructions
Form X30531-3
Teledyne Continental Motors
Aircraft Products
P. 0. Box 90
Mobile, AL 36601
Attn: Accounts Receivable
1-3

1-3 DEFINITIONS AND ABBREVIATIONS
ABBREVIATIONS/SYMBOLS
TERM
A,B,C
ADMP
Approx.
A.T.C.
Bar.
B.B.C.
B.H.P.
BSFC
B.T.C.
F.A.A.
C.A.R.
c.f.m.
C.G.
C.H.T.
ccw
cw
OF.
EGT
Fig.
Front
ft.
F.T.
FT-LBS
G.P.M.
gms
H20
Hg.
l.D.
in.(")
Hex.
hr.
IN-LBS
Left Side
Lbs.
Lockwire
100LL
Man.
Max.
Min.
30'
N.P.T.
N.C.
N.F.
NRP
OAT
O.D.
oz
Press.
p.s.i.
EXPLANATION
After Bottom Center
Absolute Dry Manifold Pressure
Approximately
After Top Center
Barometric
Before Bottom Center
Brake Horsepower
Brake Specific Fuel Consumption
Before Top Center
Federal Aviation Administration
Civil Air Regulations
Cubic Feet Per Minute
Center of Gravity
Cylinder Head Temperature
Counterclockwise Rotation
Clockwise Rotation
Degrees of Angle
Degrees Fahrenheit
Exhaust Gas Temperature
Figure (Illustration)
Propeller
End
Foot or Feet
Full Throttle
Foot Pounds Torque
Gallons Per Minute
Grams
Water
Mercury
Inside Diameter
Inches
Hexagon
Hour
Inch Pounds Torque
Side on which Nos.
2, 4 and 6 cylinders are located (Rear to Front)
Pounds
Stainless Steel Wire Used To Safety Connections, Etc.
100 Octane Low Lead Fuel
Manifold Manometer
Maximum
Minimum
Thirty Minutes of Angle (60' equals one degree)
National Pipe Thread (tapered)
National Course (thread)
National Fine (thread)
Normal Rated Power
Outside Air Temperature
Outside Diameter
Ounce
Pressure
Pounds Per Square Inch
1-4

PSIA
PSIG
PPH
Rear
Rec.
Right Side
R.P.M.
Std.
TBO
T.D.C.
T.l.T.
Torque
DEFINITIONS
ADMP
Ambient
BHP
BSFC
Cavitation
Cold Soaking
Corrosion
Critical
Attitude
Density Altitude
Pounds
Per Square Inch Absolute
Pounds
Per Square Inch Gage
Pounds Per Hour
Accessory
End of Engine
Recommended
Side on Which Nos.
1, 3 and 5 Cylinder are Located (rear to front)
Revolution Per Minute
Standard
Time Between Overhaul
Top
Dead Center
Turbine Inlet Temperature
Force x Lever Arm (125
ft. -lbs. torque = 125 lbs. force applied one ft.
from bolt center or 62 1 /2 lbs. applied 2 ft. from center, etc.)
Absolute dry manifold pressure, is used in establishing a baseline standard of engine
performance. Manifold pressure is the absolute pressure in the intake manifold;
measured
in inches of mercury.
A term used
to denote a condition of surrounding atmosphere at a particular time. For
example: Ambient Temperature or Ambient Pressure.
Brake Horsepower. The power actually delivered
to the engine propeller shaft. It is
called Brake Horsepower because it was formerly measured by applying a brake to
the power shaft of
an engine. The required effort to brake the engine could be
converted to horsepower -hence: "brake horsepower".
Brake Specific
Fuel Consumption. Fuel Consumption stated in pounds per hour per
brake horsepower. For example,
an engine developing 300 horsepower while burning
150 pounds of fuel per hour, has a BSFC of .5.
Fuel Consumption in PPH
Brake Horsepower
Formation of partial vacuums in a flowing liquid
as a result of the separation of its parts.
Prolonged exposure of an object
to cold temperatures so that its temperature
throughout approaches that of ambient.
Deterioration of a metal surface usually caused by oxidation of the
metal.
The maximum altitude at which a component can operate at 100% capacity. For
example, an engine with a critical altitude of 16,000 feet cannot produce 100% of its
rated manifold pressure above 16,000 feet.
The effective altitude, based on prevailing temperature and pressure, equivalent to
some standard pressure altitude.
Dynamic Condition A term referring
to properties of a body in motion.
EGT
Exhaust gas temperature. Measurement of this gas temperature is sometimes used as
an aid to fuel management.
1-5

Exhaust Back Opposition to the flow of exhaust gas, primarily caused by the Pressure size and shape
Pressure of the exhaust system. Atmospheric pressure also affects back pressure.
Four Cycle Short for "Four Stroke Cycle". It refers to the four strokes of the piston
in completing
a cycle of engine operation (Intake, Compression, Power
and Exhaust).
Fuel Injection A process of metering fuel into an engine by means other than a carburetor.
Gallery A passageway
in the engine or subcomponent. Generally one through which oil is
directed.
Galling or Scuffing Excessive friction between two
metal surfaces resulting in particles of the softer metal
being torn away
and welded to the harder metal.
Humidity Moisture in the atmosphere. Relative humidity, expressed in percent, is the amount of
moisture (water vapor)
in the air compared with the maximum amount of moisture the
air could contain at a given temperature.
Hydrostatic Lock Inability or restriction of piston rotation at
TDC due to fluid accumulation in excess of
combustion chamber displacement.
Impulse Coupling A mechanical device
used in some magnetos to retard the ignition timing and provide
higher voltage at cranking speeds for starting.
Lean Limit Mixture The leanest mixture approved for any given power condition. It is not necessarily the
leanest mixture at which the engine will continue to operate.
Major Overhaul Per
FAA AC43-11 consists of the complete disassembly of an engine, inspected,
repaired
as necessary, reassembled, tested, and approved for return to service within
the fits
and limits specified by the manufacturer's overhaul data. This should be to new
fits or limits.
The determination as to what fits and limits are used during an engine
overhaul should
be clearly understood by the engine owner at the time the engine is
presented for overhaul. The owner should also be aware of any parts that are replaced,
regardless of condition,
as a result of manufacturer's overhaul data, service bulletin,
or
an airworthiness directive.
Manifold Pressure Pressure measured
in the intake manifold down-stream of the air throttle. Usually
measured
in inches of mercury.
Mixture Mixture ratio.
The proportion of fuel to air used for combustion.
Naturally Aspirated A term
used to describe an engine which obtains induction air by drawing it directly
(Engine) from the atmosph,ere into the cylinder. A non-supercharged engine.
Octane Number
Oil Temperature
Control
Valve
Overboost Valve
Overhead Valves
A rating which describes relative anti-knock (detonation) characteristics of fuel. Fuels
with greater detonation resistance than
100 octane are given performance ratings.
A thermostatic unit
used to divert oil through or around the oil cooler, as necessary,
to maintain oil temperature within desired limits.
A safety device
used on some turbocharged engines to relieve excessive manifold
pressure
in the event of malfunction.
An engine configuration in which the valves are located in the cylinder head itself.
1-6

Performance Rating A rating system used to describe the ability of fuel to with-stand heat and pressure of
combustion as compared with 100 octane fuel. For example, an engine with high com-
pression and high temperature
needs a higher Performance Rated fuel than a low
compression engine. A rating
of 100/130 denotes performance characteristics of lean
(100) and rich (130) miX1ures respectively.
Permold A term used to describe a process by which a crankcase
is made. An engine with a
permold crankcase
has a front, right-hand mounted, gear driven alternator.
Pressure Altitude Altitude, usually expressed
in feet, (using absolute static pressure as a reference)
equivalent to altitude above
the standard sea level reference plane (29.92" Hg.
Standard).
Propeller Load A plot of horsepower, versus
RPM, depicting the power absorption characteristics of
Curve a fixed pitch propeller.
Propeller Pitch The angle between the
mean chord of the propeller and the plane of rotation.
PSIA The absolute thermodynamic pressure measured by the number of pounds -force
exerted on
an area of one square inch.
RAM Increased air pressure due to forward speed.
Rated Power The maximum horsepower at which an engine is approved for operation.
Retard Breaker A device used
in magnetos to delay ignition during cranking. It is used to facilitate
starting.
Rich Limit
The richest fuel/air ratio permitted for a given power condition. It is not necessarily the
richest condition at which the engine
will run.
Rocker Arm A mechanical device used to transfer motion from the pushrod to the valve.
Run Out Eccentricity or wobble of a rotating part.
Sandcast A term used to describe a process by which a crankcase is made. An engine with a
sandcast crankcase
has a belt driven alternator mounted on the left rear accessory
case and a front, right-hand mounted
oil cooler.
Scavenge Pump A pump (especially
an oil pump) to prevent accumulation of liquid in some particular
area.
Sonic Venturi A restriction, especially
in cabin pressurization systems, to limit the flow of air through
a duct.
Standard
Day By general acceptance, a condition of the atmosphere wherein specific amounts of
temperature, pressure, humidity, etc. exist.
Static Condition A term referring to properties of a body at rest.
Sump The lowest part of a system. The main oil sump on a wet sump engine contains the
oil supply.
1-7

T.D.C. Top Dead Center. The position in which the piston has reached the top of its travel.
A line drawn between the crankshaft rotational axis, through the connecting rod end
axis and the piston pin center would be a straight line. Ignition and valve timing are
stated in terms of degrees before or after TDC.
Thermal Efficiency Regarding engines, the percent of total heat generated which is converted into useful
power.
T.l.T. Turbine Inlet Temperature. The measurement of E.G.T. at the turbocharger turbine inlet.
Torque Twisting moment, or leverage, stated
in pounds -foot (or pounds -inch).
Turbocharger A device used to supply increased amounts of air to an engine induction system.
In
operation, a turbine is driven by engine exhaust gas. In turn, the turbine directly drives
a compressor which pumps air into the engine intake.
Turbo Supercharged A term
used to describe an engine which obtains induction air by drawing it directly
(Engine) from the atmosphere into the Turbocharger Compression Inlet, compressing the air and
routing it to the pressurized induction system.
Vapor Lock
Variable Pressure
Controller
Vernatherm
Valve
Viscosity
Volatility
Volumetric
Efficiency
Wastegate Valve
A condition in which the proper flow of a liquid through a system is disturbed by the
formation of vapor. Any liquid will turn to vapor if heated sufficiently. The amount of
heat required for vaporization will depend
on the pressure exerted on the liquid.
A device used to control the speed, and thus the output of
the turbocharger. It does so
by operating the wastegate which diverts, more or less,
exhaust gas over the turbine.
A thermostatic valve used to divert oil through or around the
oil cooler, as necessary,
to maintain oil temperature within desired limits.
The characteristic of a liquid to resist flowing. Regarding oil, high viscosity refers to
thicker or "heavier" oil while low viscosity oil is thinner. Relative viscosity is indicated
by the specified "weight" of the oil such as 30 "weight" or 50 "weight". Some oils are
specified as multiple-viscosity such as 1 OW30. In such cases, this oil is more stable and
resists the tendency to thin when heated
or thicken when it becomes cold.
The tendency of a liquid to vaporize.
The ability of an engine to fill its cylinders with air compared to their capacity for air
under static conditions. A "naturally aspirated" engine will always have a volumetric
efficiency of slightly less than 100%, whereas superchargers permit volumetric
efficiencies in excess of 100%.
A unit, used on the turbocharged engines, to divert exhaust gas through or around the
turbine,
as necessary, to maintain turbine speed. As more air is demanded by the
engine, due to throttle operation, the compressor must work harder.
In order to
maintain compressor and turbine speed, more exhaust must flow through the turbine.
The wastegate valve closes and causes gas, which would go directly overboard, to
pass through the turbine. The wastegate is usually operated by an actuator which
gets necessary signals from the turbocharger controller.
1-8

1-4 MANUAL REVISIONS
This manual and Teledyne Continental Motors related manuals are current and correct to the best
of Teledyne continental Motors' knowledge
at the time of publication. Any errors, recommended
changes,
or questions should be submitted in writing to:
Department Manager
Technical Publications Department
Teledyne Continental Motors
P. 0. Box 90
Mobile, Alabama
36601
Manuals will be revised and updated as necessary.
Consult Teledyne Continental Motors' Service Bulletin publications for latest technical information
available.
1-9

INTENTIONALLY
LEFT
BLANK
1-10

CHAPTER 2
TOOLS AND EQUIPMENT
Section Index
Section Page
2-1 General Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-2
2-2 Special Tools . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-2
2-1

2-1 GENERAL INFORMATION
The mechanic should be equipped with a complete set of common tools to include a minimum of:
1. Wrenches 1 /4" thru 1"
2. Common and Philister Head Screwdrivers
3. Pliers -Common Dykes, Needle Nose. Duck Bill, Vise Grip.
4. Ratches 1 /4", 3/8", 1 /2" Drive
5. Sockets -1/4" Drive 5/32" thru 1/2" -3/8" Drive 3/8" thru 1" -1/2" Drive 7/16" thru 1-1/4"
6. Sockets (Deepwell) - 1 /2" Drive 7 /16" thru 1"
7. Feeler Gages
8. Leather Mallet
9. Torque Wrenches* (Calibrated) -0-500 In. Lbs. -0-100 Ft. Lbs.
10. Micrometers* (Calibrated)
*Must
be currently calibrated, and the calibration must be traceable to the National Bureau of Standards.
2-2 SPECIAL TOOLS
The specific tools illustrated or similar tools marketing by other manufacturers will be necessary for service
and maintenance of the TSI0-520-BE aircraft engine. The tool illustrations shown on the following pages are
used with the permission of the respective manufacturers.
Most special tools illustrated
in this section are marketed by Burroughs Tool and Equipment Corporation,
2429 North Burdick Street, Kalamazoo, Michigan 49007. A complete catalog of special tools for Teledyne
Continental Motors Aircraft engines can be obtained by writing the Borroughs Tool Company.
The illustrations in this section show only the general appearance of the tools and do not necessarily
correspond to the actual size or shape. Individual illustrations may cover a number of tools with the same
overall design, but with different part numbers.
2-2

COMPANY
A
LC OR
Box 32516
10130 Jones Maltsberger
Rd.
San Antonio, TX 78284
512/349-3771
SPECIAL TOOLS
PROCUREMENT SOURCES
BORROUGHS TOOL AND EQUIP. CORP.
2429
N. Burdick St.
Kalamazoo, Ml 49007-1897
616/345-5163
or 345-2700
Special Tools
CHAMPION SPARK PLUG, CO.
Box 910, 900 Upton Ave.
Toledo, OH 43661
419/535-2461
EASTERN ELECTRONICS, INC.
180 Roberts St.
East Hartford, CT 06108
203/528-9821
FEDERAL
TOOL SUPPLY CO., INC.
10631 Capital
Oak Park, Michigan 48237
800/521-1508 TOLL
FREE
or 313/543-9300
OTC TOOLS & EQUIPMENT
Division of Owatonna Tool Company
Owatonna, Minnesota 55060
507/451-5310
McMASTER-CARR SUPPLY CO.
P.O. Box 4355
Chicago, Illinois 60680
312/833-0300
SNAP ON TOOLS
2611 Commerce Blvd.
Birmingham, Alabama 35210
205 /956-1722
Kell-Strom
Tool Company, Inc.
214 Church St.
Wethersfield, CT 06109
2-3
GENERAL PRODUCT
SUMMARY
Instruments for
Aircraft
Special Tools
Precision Instruments
Measuring Instruments
Precision Tools
Spark Plugs, lgnitors
Oil Filters
Special Tools
Fuel Pressure Test Equipment
Measuring Instruments
Precision Tools
Piston Position Indicators
Printed and Standard Circuits
Precision Inspection
Instruments
Special Tools
Precision Tools
Special Tools
Hydraulic Accessories
Precision Tools
Special Tools
Precision Tools
Special Tools
Ignition Test
Equipment

··NOTICE --
All tools referenced under Sub-section 2-2 Special Tools, are for reference only, not for the purpose of
promoting
or suggesting tools to be purchased from the indicated sources.
(ALR)
(BTC)
(CSPC)
(EEi)
(FTSC)
(OTC)
(MCSC)
{SOT)
(KTC)
=
IDENTIFICATION CODE FOR TOOLS
ALCOA, INC.
BORROUGHS TOOL AND EQUIPMENT CORP.
CHAMPION SPARK PLUG, CO.
EASTERN ELECTRONICS, INC.
FEDERAL TOOL SUPPLY CO., INC.
OTC TOOLS & EQUIPMENT CO.
McMASTER-CARR SUPPLY CO.
SNAP ON TOOLS
KELL-STROM TOOL COMPANY INC.
44 Numbers referenced in the left-hand bottom comer of each picture correspond to the
numbers located in the Special Tool Index.
WARNING
..• Whenever using test equipment, keep equipment and personnel clear of prop
area.