The information in this manual is not all inclusive and
cannot take into account all unique situations. Note that
some illustrations are typical and may not reflect the
exact arrangement of every component installed on a
specific chassis.
The information, specifications, and illustrations in this
publication are based on information that was current at
the time of publication.
No part of this publication may be reproduced, stored in a
retrieval system, or be transmitted in any form by any
means including electronic, mechanical, photocopying,
recording, or otherwise without prior written permission
of Mack Trucks, Inc.
Page ii
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SAFETY INFORMATION
SAFETY INFORMATION
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SAFETY INFORMATION
Advisory Labels
Cautionary signal words (Danger-Warning-Caution) may appear in various locations throughout this
manual. Information accented by one of these signal words must be observed to minimize the risk of
personal injury to service personnel, or the possibility of improper service methods which may damage
the vehicle or render it unsafe. Additional Notes and Service Hints are utilized to emphasize areas of
procedural importance and provide suggestions for ease of repair. The following definitions indicate the
use of these advisory labels as they appear throughout the manual:
Directs attention to unsafe practices which could result in damage to equipment and
possible subsequent personal injury or death if proper precautions are not taken.
Directs attention to unsafe practices which could result in personal injury or
death if proper precautions are not taken.
Directs attention to unsafe practices and/or existing hazards which will result
in personal injury or death if proper precautions are not taken.
An operating procedure, practice, condition, etc., which is essential to emphasize.
A helpful suggestion which will make it quicker and/or easier to perform a certain
procedure, while possibly reducing overhaul cost.
Page iv
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Service Procedures and Tool Usage
Anyone using a service procedure or tool not recommended in this manual must first satisfy himself
thoroughly that neither his safety nor vehicle safety will be jeopardized by the service method he selects.
Individuals deviating in any manner from the instructions provided assume all risks of consequential
personal injury or damage to equipment involved.
Also note that particular service procedures may require the use of a special tool(s) designed for a
specific purpose. These special tools must be used in the manner described, whenever specified in the
instructions.
1. Before starting a vehicle, always be seated in the driver’s seat, place the
transmission in neutral, be sure that parking brakes are set, and disengage
the clutch.
SAFETY INFORMATION
2. Before working on a vehicle, place the transmission in neutral, set the
parking brakes, and block the wheels.
3. Before towing the vehicle, place the transmission in neutral and lift the rear
wheels off the ground, or disconnect the driveline to avoid damage to the
transmission during towing.
REMEMBER,
SAFETY . . . IS NO ACCIDENT!
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SAFETY INFORMATION
Mack Trucks, Inc. cannot anticipate every
possible occurrence that may involve a potential
hazard. Accidents can be avoided by recognizing
potentially hazardous situations and taking
necessary precautions. Performing service
procedures correctly is critical to technician safety
and safe, reliable vehicle operation.
The following list of general shop safety practices
can help technicians avoid potentially hazardous
situations and reduce the risk of personal injury.
DO NOT perform any services, maintenance
procedures or lubrications until this manual has
been read and understood.
앫Perform all service work on a flat, level
surface. Block wheels to prevent vehicle
from rolling.
앫DO NOT wear loose fitting or torn clothing.
Remove any jewelry before servicing
vehicle.
앫ALWAYS wear safety glasses and protective
shoes. Avoid injury by being aware of sharp
corners and jagged edges.
앫Use hoists or jacks to lift or move heavy
objects.
앫NEVER run engine indoors unless exhaust
fumes are adequately vented to the outside.
앫Be aware of hot surfaces. Allow engine to
cool sufficiently before performing any
service or tests in the vicinity of the engine.
앫Keep work area clean and orderly. Clean up
any spilled oil, grease, fuel, hydraulic fluid,
etc.
앫Only use tools that are in good condition,
and always use accurately calibrated torque
wrenches to tighten all fasteners to their
specified torques. In instances where
procedures require the use of special tools
which are designed for a specific purpose,
use only in the manner described in the
instructions.
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EXPLANATION OF NUMERICAL CODE
EXPLANATION OF NUMERICAL CODE
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EXPLANATION OF NUMERICAL CODE
EXPLANATION OF 3-DIGIT
NUMERICAL CODE
The organization of MACK service manuals has
been upgraded to standardize manual content
according to a reference system based on
component identification. The new reference
system will help link the information contained in
this publication with related information included
in other MACK service/warranty publications,
such as associated service bulletins, warranty
manuals, and the TS477 Service Labor Time
Standards Manual.
The system is based on a numerical code
first digit of which identifies the general
component grouping as listed here:
GROUP 000 — INSPECTIONS
GROUP 100 — CHASSIS
GROUP 200 — ENGINE
GROUP 300 — CLUTCH, TRANSMISSION,
TRANSFER CASE AND PTO
, the
GROUP 400 — STEERING, AXLES, WHEELS
AND TIRES, DRIVELINE
GROUP 500 — BRAKES, AUXILIARY
SYSTEMS
GROUP 600 — CAB, TRUCK BODY
GROUP 700 — ELECTRICAL
The second two digits of the 3-digit code
are used to identify the system, assembly or
subassembly, as appropriate, within each of
the groupings. The codes applicable to this
publication are shown at the TOP OF EACH
PAGE and at SECTION HEADINGS, as
necessary, and may also appear in the TABLE
OF CONTENTS, to guide you to specific
component information.
Additionally, a two-character alpha code (i.e.
[NV] RINGS, PISTON) is shown with each
operation. This alpha code, in combination with
the three-digit Group number, identifies the
specific assembly, subassembly or part, and
directly relates to the first five positions of the
operation code listed in the Service Labor Time
Standards Manual, TS477.
Examples:
Base Operation
Cylinder Block Moving Parts
Rings, Piston
MACK E7
Replace (one piston)
212NV2J53
200976a
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ABOUT THIS MANUAL
ABOUT THIS MANUAL
Page ix
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ABOUT THIS MANUAL
CHANGES FROM THE
EXISTING E7 MANUAL
Mack Trucks, Inc. has made many major
improvements to this E7 Service Manual, with
changes to both content and organization. The
specifications have been revised to reflect
changes and improvements in E7 engines.
All specifications and torque values are given in
English and metric measurements. Torque
values are also included in the text, eliminating
the need to refer to the Fits and Limits chart each
time a specified torque value is required. The
Special Tools list has been revised to include new
special tools. Warnings, cautions, notes and
service hints help the technician service the
engine safely and efficiently.
The ENGINE DISASSEMBLY section shows how
to remove components in an order that requires
the least amount of handling. It includes brief
component descriptions and information needed
to properly service that component.
The BENCH PROCEDURES section guides the
technician in disassembly, cleaning, inspection
and assembly of each component. It also helps in
determining if the part is serviceable or should be
replaced. This section alerts the user to
component upgrades and helps the technician to
decide whether to use the latest available parts or
reinstall existing parts. Precise descriptions aid in
component identification.
The ENGINE ASSEMBLY section includes stepby-step procedures for reassembling the engine.
This helps to ensure proper installation and
longer service life.
The SETUP AND ADJUSTMENTS section has
the latest setup information, complete with charts
showing necessary data for adjusting all E7
engine models. Engines perform best and
conserve fuel most efficiently when adjusted
properly.
Two additional sections are included as guides
for removing and reinstalling the engine. Both
sections are generic in nature. E7 engine
installation procedures vary from one vehicle
style to another. These procedures are intended
as a checklist to remind the technician of all
necessary tasks.
While troubleshooting procedures are similar for
most diesel engines, this manual includes only
those that pertain to the E7 engine. The
TROUBLESHOOTING section contains
questions to help the technician consider all
possible problem sources.
This service manual has been revised to include
all applicable active service bulletins and service
letters since publication of the earlier E7 Service
Manual (October 1992).
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TABLE OF CONTENTS
TABLE OF CONTENTS
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This manual is intended to assist the technician
in properly overhauling MACK E7 engines. The
manual is divided into nine major sections.
Working on the E7 engine is not difficult, but like
most present-day precision equipment, it requires
proper tools and knowledge.
The overhaul procedures are separated into three
sections: engine disassembly, bench procedures
and engine assembly. Each section contains
detailed procedures that must be followed in the
order specified. If a step calls for a procedure that
has already been described earlier in the manual,
you will be referred to the section where the
original procedure appeared. This manual covers
the overhaul of an engine once it is removed from
the vehicle, but also gives instructions for
removing the engine from a nonspecified chassis.
The new E7 is the most fuel-efficient diesel
engine MACK has ever produced. This engine
provides higher horsepower ratings, better fuel
economy, increased durability and improved
serviceability. In addition, the E7 still easily meets
all applicable emissions standards. All this,
coupled with the latest manufacturing techniques
and equipment, makes the new E7 the highestquality MACK engine ever made.
Externally, all E7 engine models look the same.
However, Mack Trucks, Inc. has made many
major internal design changes to comply with
current and future EPA emission standards. To
properly identify the E7 engine model year, refer
to the engine information plate and the following
pages of this section for additional engine plate
information.
200600a
Figure 1 — 3/4 View E7, Front, Left
Page 1-2
3/4 VIEW E7
200333a
Figure 2 — 3/4 View E7, Front, Right
5-101.bk Page 3 Friday, March 17, 2006 11:05 AM
200 GENERAL INFORMATION
ENGINE MODEL
IDENTIFICATION
Engine Information Plate
All engines are identified by an engine
information plate located on the front valve cover
of the engine. This plate indicates the engine’s
11GBA number, emission standards, serial
number and various engine adjustments. The
engine is also identified by the serial number
stamped into the cylinder block above the timing
cover on early engines, or on the pad just to the
rear of the air compressor on later engines.
For some current MACK engines, the engine
information plate also includes pertinent
emissions characteristics of NO
unique to that engine.
A given MACK engine may meet federal emission
regulations in 49 states (excluding California) or
an engine may meet emission regulations of all
50 states (including California). To determine
which regulations a given engine meets, refer to
the engine information plate. If the engine plate
has a series of dashes in the long upper-left
block, and two dashes in the CALIF. FAMILY
block, the engine does not meet California
regulations.
and particulates
x
Figure 3 — Engine Information Plates
New Engine Information Plate
The following explanations are provided to aid in
interpreting some of the key information found on
the new engine information plate (effective late
1996). Refer to Figure 1-4.
Block 1 — U.S. EPA Regulations
앫An “X” in block one means the engine meets
United States EPA regulations for the year
stamped in block No. four.
앫Two dashes in block one indicates the
engine does not meet United States EPA
regulations for the year stamped in block
No. four. This is only permissible with certain
export engines. All domestic engines will
have an “X” in block one.
Block 2 — California Regulations
앫An “X” in block two indicates the engine
meets California emissions regulations for
the year stamped in block No. four. This
engine is referred to as a “50-state” engine
and can be sold in any state throughout the
U.S.
앫Two dashes stamped in block two means
the engine does not meet California
emissions regulations. If an engine has an
“X” in block one and two dashes in block
two, it is referred to as a “49-state” engine,
meaning it is not certified for sale in
California.
Page 1-3
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200 GENERAL INFORMATION
Block 3 — ADR Regulations
앫An “X” in block three means the engine has
been certified to meet Australian emissions
regulations.
앫Two dashes in block three means the engine
does not meet Australian emissions
regulations.
Block 4 — Model Year
앫The four-digit numeral stamped in block four
represents the year in which the engine was
certified.
Block 5 — Federal Family
앫A two-digit numeral stamped in block five
denotes the Federal Family to which the
engine belongs, for emissions certification
purposes.
앫All domestic engines will have a two-digit
Federal Family number in block five.
Block 6 — California Family
앫If the engine meets California emissions
regulations, the same two-digit numeral
stamped in the Federal Family block is
stamped in the California block.
앫If the engine does not meet California
emissions regulations, there will be two
dashes in block six.
Block 7 — Initial Injection Timing
앫Block seven indicates the initial setting for
E7 injection timing.
앫E7 EUP (E-Tech™) engines do not have an
initial injection timing, as this is controlled
electronically. E-Tech™ engines have “NA”
stamped in block seven.
Block 8 — Engine Brake
앫This block is only used when the engine is
equipped with a Jake Brake. The stamping
in this block indicates the Jake Brake slavepiston lash setting.
Page 1-4
Figure 4 — Engine Information Plate
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LUBRICANTS AND SEALANTS
200 GENERAL INFORMATION
Use only the following recommended sealing
compounds and lubricants.
All genuine MACK cylinder head gaskets are
precoated and do not require any type of sealing
compound. Before installing new gaskets,
degrease both gasket sealing surfaces to avoid
leaks.
LocationSealant or Lubricant
Cup plugs/threaded plugsLoctite 277 or equivalent/Teflon thread sealer
Injection nozzle holder inserts (upper and lower end)Loctite 620
Camshaft gear assemblyLoctite 609
Timing gear cover
Timing event marker with jam nut
Oil filter sealing gasketClean engine oil
Holding metal parts in place
Valve stems
Engine parts, fasteners (sides and threads), and washersClean engine oil
Cylinder sleeve upper crevice seal (on sleeve)Ethylene glycol or propylene glycol
Cylinder sleeve seat
Oil cooler assemblyPermatex gasket sealer
Oil cooler assembly O-ringDrydene No. 4000
O-rings (except as noted)MACK O-ring lubricant part No. 243SX41
Chassis-mounted charge air cooling system (core sealing)
Engine oil pressure sensor
Intake manifold temperature sensor
Coolant temperature sensor
Coolant level sensor
Fuel injection pump actuator connector
Fuel injection pump driven gear access cover
Econovance
Crankshaft flange and wear ringLoctite 609
Turbocharger mounting nutsFel Pro C5A
drive coupling bolt threadsLoctite 242
MACK Silastic (RTV Silicone Adhesive Sealant)
part No. 342SX32
MACK MG-C grease or petroleum jelly (Vaseline)
MACK Silastic (RTV Silicone Adhesive Sealant) part
No. 342SX32
Dow Corning No. 1200 primer, Dow Corning RTV 734
adhesive (clear), and naphtha solvent or equivalent
Sealing compound on threads
O-ring lube Lubrizol No. OS-50044 or equivalent
Page 1-5
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200 GENERAL INFORMATION
OVERHAUL PART
REPLACEMENT
Use genuine MACK parts at all times. Parts that
are typically replaced during an engine overhaul
are listed below:
앫Gaskets and seals
앫Bearings and bushings
앫Pistons (aluminum) and piston rings
앫Cylinder sleeves
앫Cylinder block cup plugs and cylinder head
cup plugs
앫Connecting rod capscrews
Steel top pistons should not be replaced without
first inspecting them for excessive wear or other
damage. Clean, inspect and measure pistons to
determine need for replacement.
Page 1-6
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200 SPECIFICATIONS
SPECIFICATIONS
Page 2-1
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200 SPECIFICATIONS
SPECIFICATIONS
higher horsepower ratings and future emission
standards. These changes require increased
displacement, higher peak cylinder pressures
Improved Design
Compared to earlier designs, the E7 engines
include improvements required to accommodate
and a superior engine cooling system. This was
all accomplished without a substantial change in
engine weight.
Engine General Specifications
CharacteristicDescription
Weight (wet*)2300 lbs. (1043.3 kg)
Weight (dry)2210 lbs. (1002.5 kg)
Displacement 728 cu. in. (12L)
Bore and stroke4-7/8 x 6-1/2 in. (123.83 x 165.10 mm)
Engine oil capacity33.5 qts. (32L)
Coolant capacity13 qts. (12.3L)
Compression ratio16.5:1 (up to 375 hp); 15.3:1 (375 hp and above)
Fasteners and threadsMetric and English
*Wet includes oil and coolant
Engine Features
ComponentDescription
Cylinder blockAlloyed gray cast iron
Main bearing capsDuctile iron, intermediate supported with buttress screws to prevent bulkhead
movement
Flywheel housingStandard — Aluminum, standard SAE No. 1, precision doweled
Optional — Ductile iron
Cylinder sleevesWet/dry, replaceable, centrifugally cast, alloyed cast iron
Cylinder sleeve sealTeflon-coated AFLAS/EPDM, intolerant of oil (use glycol for installation
Cylinder headsAlloy gray cast iron; four valves per cylinder, two cylinder heads per engine
Cylinder head gaskets
— BodyNonasbestos material with a steel core (two per engine)
— Fire ringSteel, six per engine
Piston assemblyRefer to Tune-Up Specifications manual.
Pistons (1989–1990)Aluminum alloy, Ni-resist insert top two grooves, steel insert third groove, oval
Pistons (1991 and later)Two-piece, top crown material steel, aluminum alloy skirt, three-ring piston
Piston rings (1989–1990)
— CompressionChrome, three per cylinder
— Oil controlChrome, one per cylinder
Piston rings (1991 and later)
— CompressionPlasma, top ring; chrome, second ring
— Oil control Chrome, one per cylinder
Piston pinsFull-floating, 2.25 inch (5.72 cm) diameter, full-pressure lubrication through
lubricant)
and roll burnished pin bores, continuous oil cooling
rifle-drilled holes in connecting rods
Page 2-2
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Engine Features (Cont.)
ComponentDescription
Connecting rodsForged steel, I-beam with tapered pin end, 35-degree cap angle, 10.4 inches
CrankshaftDrop-forged, medium carbon steel, elotherm hardened journals and fillets, eight
Bearings
— MainSteel-backed, lead-tin overlay
— RodSteel-backed, lead-tin overlay deltawall
Vibration damperViscous fluid filled
CamshaftCarbon steel, carburized journals and lobes, gear driven
Valves
— Inlet30-degree face angle (before November 1996), 20-degree face angle
— Exhaust30-degree face angle, poppet with positive rotator, two per cylinder
multiple plunger, flange mounted, gear driven, with variable timing by
Econovance
Page 2-3
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200 SPECIFICATIONS
Good Shop Practice — Fasteners
For additional information on tune-up
specifications for 1992 and 1993 E7 V-MAC
engines, refer to 1992 MACK Engine Tune-Up
Specifications No. 5-304ID92 and V-MAC
Service Manual No. 8-201. For information on
1993 V-MAC E7 engine, refer to 1993 MACK
Engine Tune-Up Specifications No. 5-305ID93.
All 1992 engine models use 1991 injection
nozzles except 1992 EM7-300 V-MAC with
20-degree Econovance, No. 710GB51AM. 1992
EM7-300 models with 20-degree Econovance
use nozzle holder assembly No. 736GB343P4
and nozzle tip No. 114GC325P3. 1992 EM7-300
V-MAC models with 10-degree Econovance, No.
710GB416CM, use 1991 EM7-300 V-MAC
injection nozzles.
Make sure that all components are clean and free
from foreign material or corrosion. Use suitable
tools and assembly procedures to prevent
permanent damage to the engine components.
Metric fasteners are used on the E7 engine with a
few exceptions. The exceptions are fasteners
with English threads, as noted in the charts that
follow.
Patchlock/Hyloc fasteners follow the same
guidelines as standard fasteners.
A calibrated manual torque wrench is required to
tighten the fasteners listed in the charts. Threads,
washers and underhead of screws or washer
face of nuts should be lubricated with engine oil,
unless otherwise specified.
Some designs require individual consideration
and may deviate from torque guidelines in this
manual.
Performance Specifications (Oil Pressure and Intake Manifold Temperature)
*Dependent on outside air temperature and vehicle speed.
Outside air
temperature
——
Full Load
(Peak Torque rpm)
100–140°F*
(38–60°C)
Page 2-4
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200 SPECIFICATIONS
FASTENER TORQUE
Fastener Selection and Installation
Selection and correct installation of threaded
fasteners are essential parts of any assembly or
rebuild procedure. Fasteners hold much of a
vehicle together. If a fastener fails to do its job
properly, it can cause a minor problem such as a
loose mirror, or a large problem, such as loss of
steering control.
Because there are so many styles of fasteners, in
various sizes and quality grades, a mechanic
must have a working familiarity with the fasteners
commonly used in vehicles. Only in this way can
the correct selection and installation of the proper
fastener be ensured. Each fastener is intended to
do a particular job, and is selected by the vehicle
manufacturer for its suitability for that job.
Proper installation is as important as the selection
of the correct fastener. Improperly installing a
correct fastener is just as bad as using an
incorrect one. Undertightening and overtightening
both result in an improperly installed fastener.
When threaded fasteners are tightened, a slight
stretching of the fastener occurs, and it is this
stretching that binds the assembly together. If too
little tightening occurs, the slight stretching does
not happen, and the joint is not clamped securely.
If too much tightening occurs, the fastener will be
excessively stretched, causing narrowing of the
fastener and possibly breaking. Correct and
consistent use of a torque wrench ensures the
fasteners are properly tightened, and clamping
the pieces of the assembly together.
Figure 2-1 — Fastener Grading System
Page 2-5
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200 SPECIFICATIONS
Fastener Sizes and Types
The first and most important fact that the
mechanic must know about a fastener is whether
it is a U.S. (Inch System) or a metric thread. Next,
the size of the fastener, which is usually
determined by the diameter of the shank, the
length of the fastener, which is usually measured
from the bottom of the head to the end of the
thread, and the pitch of the threads.
The pitch of U.S. (Inch System) fasteners is
measured by determining the number of threads
per inch. The two pitches commonly used in
vehicles are coarse thread, officially called
Unified National Coarse (UNC), and fine thread,
officially called Unified National Fine (UNF).
The pitch of metric fasteners is measured by
determining the millimeters per thread. For
example, a bolt with 0.8 pitch would have 125
complete threads in a 100-millimeter section
(100 mm divided by 125 threads equals 0.8), and
a bolt with 1.0 pitch would have 100 threads in a
100-millimeter section. Pitch may be measured
directly, using a ruler and counting the threads.
Also, thread pitch gauges are available for both
U.S. and metric threads, which make it easy to
check the pitch of a fastener.
In the U.S. system, a typical designation would
be: 7/16-20 x 1. This describes a bolt that is
7/16 inch in diameter, has 20 threads per inch,
and is one inch long. The metric system is similar.
A typical metric designation would be: 10 x 0.8 x
25 mm. This describes a bolt that is 10 mm in
diameter, has a thread pitch of 0.8 (0.8 mm per
thread), and is 25 mm long.
Figure 2-2 — Fastener Dimensions
Figure 2-3 — Flanged Capscrew
Page 2-6
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TORQUE SPECIFICATIONS
This section includes specifications for torquing all critical and standard non-critical fasteners.
Torque Specifications for Critical Fasteners (Cont.)
200 SPECIFICATIONS
Description
Oil fill hole cover screw1520
Oil filler/tube drain-to-block screw1520
Oil filter bracket-to-cylinder block screw6081
Oil filter valve plunger spring cap100136
Oil pan-to-cylinder block screw3041
Oil pump driven gear retaining nut6081
Oil pump-to-cylinder block mounting screw4054
Oil pump housing cover screw1520
Oil pump inlet fitting-to-pump assembly screw3547
Oil pump pressure relief valve cap80109
Piston cooling nozzle screw1520
Rocker arm adjusting screw nut4054
Rocker arm bracket-to-cylinder head screw4054
Rocker arm shaft locating screw23 a31
Timing gear cover and front support bracket-to-cylinder block screw7095
Timing gear cover-to-cylinder block screw4054
Timing hole cover screw4054
Timing indicator screw1520
Torque drive hub retaining capscrew1520
Transmission-to-flywheel housing screw4054
Turbo oil inlet screw1520
Turbo oil drain screw1520
Turbo-to-exhaust manifold stud nut4054
Valve yoke screw locknut3345
Vibration damper hub-to-crank screw360488
Vibration damper-to-hub screw4561
V-MAC components:
Control valve mounting capscrews1520
Drive hub retaining capscrew150203
Econovance mounting capscrews4054
Econovance drive coupling bolt150203
Injection pump mounting capscrews4054
Injection pump access cover capscrews3041
Injection pump driven gear capscrews4054
Link-to-support bracket capscrews4054
a
English threads.
b
V-MAC applications.
Lb-FtN•m
Torque
Page 2-9
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200 SPECIFICATIONS
Torque Specifications for Critical Fasteners (Cont.)
Description
V-MAC components (cont.)
Lower support bracket-to-cylinder block capscrews4054
Upper support bracket-to-injection pump capscrews1520
Timing event marker (TEM)2230
V-MAC 7-pin pump connector1520
Bracket-to-block capscrews4054
Hose clamp screw1520
RPM/TDC (engine position) sensor (jam nut)1520
MPH (road speed) sensor (jam nut)1520
Engine oil pressure sensor68
Intake manifold temperature sensor2331
Coolant temperature sensor2331
Coolant level sensor2331
Bulkhead connector (jackscrew)57
V-MAC module connector (jackscrew)23
V-MAC ELAB valve terminal nut34
Fuel injection pump actuator connector1520
Electrical equipment panel mounting leg hardware68
Electrical equipment panel accessory studs23
Timing solenoid to Econovance (four bolts)1520
Water manifold screw2534
Water pump cover-to-water pump housing screw1520
Water pump shaft locknut90122
Water pump-to-cylinder block screw6081
a
English threads.
b
V-MAC applications.
Lb-FtN•m
Torque
Torque Specifications for Hose Clamps
Hose Clamps
Lb-InN•m
SAE J536 Type F
Air inlet systems384
Water or coolant systems283
Oil drain systems283
Hi-torque heavy-duty worm clamp809
T-bolt type hose clamp506
NOTE: The band of any hose clamp in all installations should be a minimum of 0.090 inch (2.290 mm) from the end of the hose
and must be clear of tube bead.
Page 2-10
Torque
5-101.bk Page 11 Friday, March 17, 2006 11:05 AM
Torque Specifications for Pipe Plugs
200 SPECIFICATIONS
Pipe Plugs
1/8 NPT68
1/4 NPT1824.4
3/8 NPT2331
1/2 NPT2331
3/4 NPT2838
1 NPT4358
1-1/2 NPT75102
NOTE: All pipe plugs which are not new plugs with preapplied thread sealer must be sealed using Loctite
sealant with Teflon or equivalent.
Lb-FtN•m
Torque Specifications for Non-Critical Fasteners
PROPERTY CLASS 8.8
Size (mm)Pitch
60.7568
61.0068
81.001520
81.251419
101.253041
101.502838
121.255575
121.755068
141.5086117
142.0080109
161.50133180
162.00124168
181.50193262
182.50172233
201.50270366
202.50244331
221.50365495
222.50332450
242.00459622
243.00421571
272.00666903
273.00618838
302.009281258
Tightening Torques
Lb-FtN•m
Torque
®
PST pipe thread
Page 2-11
5-101.bk Page 12 Friday, March 17, 2006 11:05 AM
200 SPECIFICATIONS
Torque Specifications for Non-Critical Fasteners (Cont.)
PROPERTY CLASS 8.8 (Cont.)
Size (mm)Pitch
303.508381136
332.0012501695
333.5011401546
363.0015512103
364.0014651986
PROPERTY CLASS 9.8
Size (mm)Pitch
60.75710
61.0068
81.001622
81.251520
101.253345
101.503142
121.255980
121.755473
141.5094127
142.0087118
161.50144195
162.00135183
181.50210285
182.50187254
201.50293397
202.50264358
221.50395536
222.50360488
242.00498675
243.00456618
272.00722979
273.00669907
302.0010051363
303.509081231
332.0013551837
333.5012351674
363.0016812279
364.0015872152
Tightening Torques
Lb-FtN•m
Tightening Torques
Lb-FtN•m
Page 2-12
5-101.bk Page 13 Friday, March 17, 2006 11:05 AM
Torque Specifications for Non-Critical Fasteners (Cont.)
PROPERTY CLASS 10.9
200 SPECIFICATIONS
Size (mm)Pitch
60.75912
61.00811
81.002129
81.252027
101.254257
101.504054
121.2576103
121.756994
141.50120163
142.00111151
161.50184250
162.00172233
181.50268363
182.50239324
201.50374507
202.50337457
221.50505685
222.50460624
242.00636862
243.00583790
272.009221250
273.008551159
302.0012841741
303.5011591571
332.0017302346
333.5015782140
363.0021462910
364.0020272748
Tightening Torques
Lb-FtN•m
Page 2-13
SECT2.FR5 Page 14 Tuesday, March 21, 2006 12:43 PM
200 SPECIFICATIONS
FITS AND LIMITS
The specifications listed are for new parts. Good judgement, experience and sound shop practice must
be used when determining whether to reuse or replace service parts.
Fits and Limits
Component
AUXILIARY DRIVESHAFT (CAPTURED THRUST WASHER)
Shaft bushing — presized ID (front and rear)2.064–2.068 in.52.426–52.527 mm
— presized OD (front and rear)2.3140–2.3155 in.58.7756–58.8137 mm
— bore in block (front and rear)2.311–2.312 in.58.699–58.725 mm
— press fit in bore (front and rear)0.002–0.0045 in.0.0518–0.1143 mm
Shaft end play0.003–0.012 in.0.076–0.305 mm
Shaft journal to bushing (front and rear)0.0020–0.0072 in.0.0508–0.1829 mm
Shaft journal diameter OD (front and rear)2.061–2.062 in.52.349–52.375 mm
Oil pump driving gear ID (press fit)1.6255–1.6250 in.41.2877–41.2750 mm
Auxiliary shaft oil pump drive journal1.6278–1.6272 in.41.3461–41.3309 mm
Air compressor drive sprocket (press fit)1.1250–1.242 in.28.575–31.547 mm
Auxiliary shaft air compressor sprocket journal1.1272–1.1268 in.28.6309–28.6207 mm
CAMSHAFT
Bushing — presized ID (No. 1 through No. 7)2.693–2.692 in.68.402–68.377 mm
— free OD (No. 1 through No. 7)2.8785–2.8765 in.73.1139–73.0631 mm
— bore in block (No. 1 through No. 7)2.874–2.873 in.73.000–72.974 mm
— press fit in bore (No. 1 through No. 7)0.0025–0.0055 in.0.0635–0.1397 mm
End play0.003–0.012 in.0.076–0.305 mm
Journal diameter (No. 1 through No. 7)2.6895–2.6885 in.68.3133–68.2879 mm
Journal-to-bushing clearance (No. 1 through No. 7)0.002–0.004 in.0.051–0.102 mm
Camshaft gear bore ID1.8758–1.8750 in.47.6453–47.6250 mm
Camshaft gear journal (press fit)1.8784–1.8779 in.47.7114–47.6987 mm
Camshaft gear driving injection pump drive (press fit)1.8135–1.8125 in.46.0629–46.0375 mm
Camshaft gear driving journal1.8159–1.8153 in.46.1239–46.1086 mm
CONNECTING ROD
Length between centers10.4375 in.26.5113 cm
Cap angle35 degrees
Bore for bushing2.4355–2.4345 in.61.8617–61.8363 mm
Burnish bushing to2.2305–2.2275 in.56.6547–56.5785 mm
Finish bore to2.2504–2.2500 in.57.1602–57.1500 mm
Crankpin bore diameter — as bored3.4305–3.4297 in.87.1347–87.1144 mm
— reassembled3.4309–3.4294 in.87.1449–87.1068 mm
Bearing ID in place2.9993–3.0013 in.76.1822–76.2330 mm
Journal clearance0.0012–0.0054 in.0.0305–0.1372 mm
Standard Size or Fit
EnglishMetric
Page 2-14
SECT2.FR5 Page 15 Tuesday, March 21, 2006 12:43 PM
Fits and Limits (Cont.)
200 SPECIFICATIONS
Component
CONNECTING ROD (CONT.)
Side clearance0.007–0.014 in.0.1778–0.3556 mm
Twist within 12 inches (30.48 cm)0.010 in.0.254 mm
Bend within 12 inches (30.48 cm)0.004 in.0.1016 mm
CRANKSHAFT
Crankpin journal OD3.248–3.247 in.82.4992–82.4738 mm
End play at No. 4 main0.004–0.013 in.0.1016–0.3302 mm
Main journal OD4.4974–4.4964 in.114.2340–114.2086 mm
Journal out-of-round or taper (maximum diameter)0.00035 in. 0.00889 mm
Max. Runout at No. 4 journal (shaft supported on No. 1 and No. 7)0.007 in.0.178 mm
CYLINDER BLOCK
Deck flatness0.002 in.0.0508 mm
Dowel pin holes (flywheel housing to block mounting)0.6237–0.6247 in.15.8420–15.8674 mm
Cylinder bore in block— upper5.501–5.500 in.139.725–139.970 mm
— lower5.1266–5.1250 in.130.2156–130.1750 mm
Cylinder bore out-of-round or taper on diameter
For service block only — maximum on reboring block:
0.001 inch (0.0254 mm).
Sleeve, flange channel depth above block deck (do not measure
from top of bead)
Sleeve OD at upper pilot diameter5.5040–5.5030 in.139.8016–139.7762 mm
Sleeve bead for fire ring — protrusion above sleeve channel0.0067–0.010 in.0.1702–0.2540 mm
Sleeve in bore — upper press fit0.004–0.002 in.0.1016–0.0508 mm
— lower loose fit0.0029–0.0003 in.0.0737–0.0076 mm
Sleeve ID installed STD — minimum4.8755 in.123.8377 mm
— maximum4.877 in.123.8758 mm
Main bearing bore in block4.818–4.817 in.122.3772–122.3518 mm
Main bearing-to-crankshaft journal clearance0.0022–0.0056 in.0.0559–0.1422 mm
Main bearing ID in place4.502–4.4996 in.104.3508–114.2898 mm
Valve lifter bore0.6865–0.6875 in.17.4371–17.4625 mm
Valve lifter shank diameter0.6855–0.6860 in.17.4117–17.4244 mm
Valve lifter OD1.380–1.385 in.35.052–35.179 mm
Valve lifter to bore clearance0.0005–0.0020 in.0.0127–0.0508 mm
NOTE: Extension of the cylinder sleeve above the cylinder block deck can vary under the same head, as long as all are
within the 0.022–0.027 inch specification.
CYLINDER HEAD
Alignment across exhaust ports0.005 in.0.127 mm
Deck flatness over 18 in. (45.72 cm)0.0015 in.0.0381 mm
Overall height6.391–6.397 in.162.331–162.484 mm
0.004 in. max.0.1016 mm
0.022–0.027 in0.5588–0.6858 mm
Standard Size or Fit
EnglishMetric
Page 2-15
5-101.bk Page 16 Friday, March 17, 2006 11:05 AM
Fits and Limits (Cont.)
200 SPECIFICATIONS
Component
CYLINDER HEAD (CONT.)
Injection nozzle holder insert to bore fit — upper and intermediate0.001–0.003 in. tight0.0254–0.0762 mm
— lower0.0015–.004 in. tight0.0381–0.1016 mm
Injection nozzle holder insert bore — upper and intermediate bore0.9360–0.9375 in.23.7744–23.8125 mm
— bottom bore0.904–0.906 in.22.962–23.012 mm
Injection nozzle holder insert OD— upper and intermediate0.9390–0.9385 in.23.8506–23.8379 mm
— lower 1/2 inch (12.7 mm)0.9080–0.9075 in.23.0632–23.0505 mm
Fire ring groove — width0.030–0.036 in.0.762–0.914 mm
— depth0.005–0.013 in.0.127–0.330 mm
— ID5.137–5.139 in.130.479–130.531 mm
Valve guide OD0.6886–0.6881 in.17.4904–17.4777 mm
Valve guide ream ID (after installation)
inlet and exhaust (used with 3/8 valve stem)
Top end of valve guide to valve spring seat0.959 ± 0.040 in.24.359 ± 1.016 mm
Valve guide bore in head0.686–0.687 in.17.424–17.450 mm
Valve guide to bore (press fit)0.0011–0.0026 in.0.0279–0.0660 mm
Valve guide extension (fire deck to top of guide)5.24 ± 0.03 in.113.096 ± 0.762 mm
Yoke guide pin OD0.4389–0.4392 in.11.1481–11.1557 mm
Yoke guide pin installed height1.848–1.918 in.46.939–48.717 mm
Valve seat width — exhaust
— inlet
Valve seat insert face angle
Before November 1996— inlet and exhaust30° – 0
November 1996 and later — inlet20° 30' ± 15'
— exhaust30° – 0'/+30'
Valve seat width runout0.001 in. F.I.M.0.0254 mm
Valve seat insert counterbore diameter— exhaust1.6875–1.6885 in.42.8625–42.8879 mm
— inlet1.8285–1.8295 in.46.4439–46.4693 mm
Valve seat OD — exhaust1.692–1.693 in.42.977–43.002 mm
— inlet1.831–1.832 in.46.507–46.533 mm
Valve seat insert press fit in head — exhaust0.0035–0.0055 in.0.0889–0.1397 mm
— inlet0.0015–0.0035 in.0.0381–0.0889 mm
Valve seat counterbore depth— exhaust0.372–0.376 in.9.449–9.550 mm
— inlet0.360–0.364 in.9.144–9.246 mm
0.3745–0.3755 in.9.5123–9.5377 mm
0.051–0.081 or
1/16 ± 1/64 in.
0.051–0.081 or
1/16 ± 1/64 in.
Standard Size or Fit
EnglishMetric
1.295–2.057 mm or
1.588 ± 0.397 mm
1.295–2.057 mm or
1.588 ± 0.397 mm
'/+30'
Page 2-16
5-101.bk Page 17 Friday, March 17, 2006 11:05 AM
Fits and Limits (Cont.)
200 SPECIFICATIONS
Component
FLYWHEEL AND HOUSING
Dowel pins
Hole in flywheel housing — LH for round pin0.6259–0.6263 in.15.8979–15.9080 mm
— RH for diamond pin0.6831–0.6835 in.17.3507–17.3609 mm
— RH for blade pin
Pin OD — LH round pin0.6251–0.6253 in.15.8775–15.8826 mm
— RH diamond pin
— RH blade pin
Cylinder block end0.6251–0.6253 in.15.8775–15.8826 mm
Flywheel housing end0.6820–0.6825 in.17.3228–17.3355 mm
Crankshaft seal mounting bore6.748–6.752 in.171.3992–171.5008 mm
Flywheel housing transmission mounting face runout0.008 in. T.I.R.*0.2032 mm*
Flywheel housing transmission pilot bore runout0.010 in. T.I.R.*0.254 mm*
Flywheel housing rear seal bore runout0.009 in. T.I.R.*0.2286 mm*
Starter motor mounting bore3.625–3.629 in.92.075–92.117 mm
* Must be held relative to main bearing bores. Check runout with an alignment bar installed through the cylinder block main
bearing bores.
OIL PUMP
Gear-to-cover end clearance0.0035–0.0060 in.0.0889–0.1524 mm
Gear-to-cavity side clearance0.0030–0.0045 in.0.0762–0.1143 mm
Gear backlash in pump0.0235–0.0295 in.0.5969–0.7493 mm
Oil pump drive gear-to-oil pump driven gear backlash0.0072–0.0138 in.0.1829–0.3505 mm
Relief valve spring, free length6.38 in.162.052 mm
Spring pressure when compressed to 5.56 inches (14.12 cm)63 lbs.28.6 kg
Ring groove service limit over 0.120 inch pins (3.048 mm)
Top groove4.912 in.124.765 mm
PISTON RINGS
Piston ring end gap — when checked in 4.875 gauge diameter
Compression rings — No. 349GC31010.016–0.028 in.0.406–0.711 mm
Compression rings — No. 349GC31020.013–0.025 in.0.330–0.635 mm
Oil control ring — No. 350GC3400.013–0.028 in.0.330–0.711 mm
Piston ring side clearance (new)0.0016–0.0030 in.0.0406–0.0762 mm
Piston ring side clearance (used)Maximum 0.0045 in.Maximum 0.1143 mm
NOTE: Refer to MACK branch or distributor for specifications for piston ring part numbers not listed above.
NOTE: For every 0.001 in. (0.0254 mm) increase in gauge diameter, ring gap will increase by 0.003 in. (0.076 mm).
ROCKER ARM
Ratio1.5:1
Hole ID1.1306–1.1326 in.28.7172–28.7680 mm
Hole-to-shaft clearance0.004–0.0015 in.0.1016–0.0381 mm
Shaft OD1.1286–1.1291 in.28.6664–28.6791 mm
Push rod overall length — intake and non-brake exhaust (flat to
cup top)
Push rod overall length — exhaust w/Dynatard (flat to flat)16.353–16.388 in.415.366–416.255 mm
TIMING GEAR COVER
Dowel Pins
Holes in cylinder block (both)0.4987–0.4997 in.12.6670–12.6924 mm
Hole in timing gear cover — RH for round pin0.5005–0.5012 in.12.7127–12.7305 mm
— LH for diamond pin0.5577–0.5584 in.14.1656–14.1834 mm
Pin OD — RH for round pin0.5001–0.5003 in.12.7025–12.7076 mm
— LH for diamond pin, cylinder block end0.5001–0.5003 in.12.7025–12.7076 mm
— LH for diamond pin, timing cover end0.5570–0.5575 in.14.1478–14.1605 mm
Crankshaft seal mounting bore3.9995–4.0025 in.101.5873–101.6635 mm
Seal square to hub0.010 in.0.254 mm
Seal mounting bore-to-crank runout0.015 in. T.I.R.*0.381 mm*
Hydraulic steering pump mounting bore3.2525–3.2545 in.82.6135–82.6643 mm
* Must be held relative to main bearing bores. Check runout with an alignment bar installed through the cylinder block main
bearing bores.
TIMING GEAR
Backlash — injection pump drive gear to injection pump
driven gear
— all other gears0.0013–0.0108 in.0.0330–0.2743 mm
15.751–15.813 in.400.075–401.650 mm
0.0025–0.0095 in.0.0635–0.2413 mm
Standard Size or Fit
EnglishMetric
Page 2-18
5-101.bk Page 19 Friday, March 17, 2006 11:05 AM
Fits and Limits (Cont.)
200 SPECIFICATIONS
Component
TURBOCHARGER
Model S3B (S4D)
Shaft end play0.003–0.006 in.0.0762–0.1524 mm
Bearing radial check (measured at bearings)0.018–0.030 in.0.4572–0.7620 mm
(0.018–0.025) in(0.4572–0.6350 mm)
Model S300, S400
Shaft end play0.003–0.006 in.0.0762–0.1524 mm
Bearing radial check (measured at bearings)0.018–0.029 in.0.4572–0.7366 mm
VALVE
Deck to valve face— inlet+ 0.0425 ± 0.007 in.+1.0795 ± 0.1778 mm
— exhaust (pre-1994)– 0.0414 ± 0.007 in.–1.0516 ± 0.1778 mm
— exhaust (Pyromet, 1994 and later)– 0.021 ± 0.007 in.–1.5334 ± 0.1778 mm
Stem to guide— inlet0.0015–0.0035 in.0.0381–0.0889 mm
— exhaust0.0025–0.0045 in.0.0635–0.1143 mm
Stem to rocker arm lash (cold static) — inlet0.016 in.0.4064 mm
— exhaust (prior to May 1996)0.024 in.0.6096 mm
— exhaust (May 1996 and later)*0.028 in.0.7112 mm
*Cam part No. 454GC5205
Face runout, inlet and exhaust0.0015 in.0.0381 mm
Seat angle before November 1996 — inlet and exhaust30° + 0
November 1996 and later— inlet20° 30' ± 15'
— exhaust30° + 0'/–30'
Stem OD— inlet (3/8 in.)0.373–0.372 in.9.474–9.449 mm
— exhaust (7/16 in.)0.3720–0.3710 in9.4488–9.4234 mm
VALVE SPRINGS
Free length2.640 in.67.056 mm
Spring pressure — when compressed to 1.435 in. (36.45 mm)142.5–157.5 lbs.64.6–71.4 kg
VALVE SPRINGS (with Jacob combination compression and
exhaust brake)
Free length2.830 in.71.882 mm
Spring pressure — when compressed to 1.5 in. (38.1 mm)190–210 lbs.86.184–95.256 kg
Standard Size or Fit
EnglishMetric
'/–30'
Page 2-19
5-101.bk Page 20 Friday, March 17, 2006 11:05 AM
200 SPECIFICATIONS
METRIC MISMATCH
Certain metric/English fastener thread
combinations are incompatible and may
result in mismatch conditions. These
conditions can cause thread stripping and/or
assembly weaknesses which may lead to
service failure, rendering a vehicle
inoperative or unsafe for operation.
Inch Thread vs. Metric Thread
Fastener Combinations
Contributing to Thread Stripping
The following inch/metric screw and nut (or
tapped hole) combinations can be finger started
(at least two full turns), but will strip if fully
assembled.
Inch ScrewsMetric Nuts
4-40M3 x 0.5
5/16-18M8 x 1.25
*5/16-24M8 x 1.25
3/8-16*M10 x 1.25
*3/8-24*M10 x 1.25
M10 x 1.5
*M10 x 1.0
7/16-14*M12 x 1.25
*7/16-20M12 x 1.75
*M10 x 1.25
*1/2-20M14 x 2
*5/8-18*M16 x 1.5
*7/8-14M24 x 3
*1-12M27 x 3
*Fine thread
Inch NutsMetric Screws
5-40M3 x 0.5
1/4-20M6 x 1.0
*1/4-28M6 x 1.0
*5/16-24*M8 x 1.0
7/16-14M10 x 1.5
7/16-14*M10 x 1.25
7/16-14*M10 x 1.0
1/2-13M12 x 1.75
*1/2-20M12 x 1.75
1/2-13*M12 x 1.5
*1/2-20*M12 x 1.5
1/2-13*M12 x 1.25
9/16-12M14 x 2
*9/16-18*M14 x 1.5
*5/18-18*M16 x 1.5
1-8*M24 x 2
*Fine thread
Page 2-20
5-101.bk Page 21 Friday, March 17, 2006 11:05 AM
200 SPECIFICATIONS
Inch Thread vs. Metric Thread
Fastener Combinations
Contributing to Assembly
Weakness
The following inch/metric screw and nut (or
tapped hole) combinations can be fully tightened,
but the resulting assembly will be 25% to 60%
weaker than required. Service failure of the
assembly is probable.
Inch ScrewsMetric Nuts
*4-48M3 x 0.5
5-40M3.5 x 0.6
6-40M3.5 x 0.6
*8-36M4 x 0.7
*10-32M5 x 0.8
12-24M6 x 1.0
*1/4-28M7 x 1.0
3/8-16M10 x 1.5
7/16-14M12 x 1.75
1/2-13M14 x 2
3/4-10M20 x 2.5
*3/4-16*M20 x 1.5
7/8-9M24 x 3
*Fine thread
Inch NutsMetric Screws
*5-44 M3 x 0.5
*6-40 M3.5 x 0.6
8-32 M4 x 0.7
*8-36 M4 x 0.7
*10-32 M5 x 0.8
12-24 M5 x 0.8
*12-28 M5 x 0.8
*1/2-20 *M12 x 1.25
3/4-10 M18 x 2.5
*3/4-16 *M18 x 1.5
1-8 M24 x 3
*1-12 M24 x 2
*Fine thread
Incompatible Metric vs. Metric
Fastener Systems
Thread mismatch can also result when combining
fasteners from incompatible metric fastener
systems. The resulting faulty thread engagement
typically causes thread stripping and/or assembly
weakness which may lead to service failure.
CONVERSION FACTORS
1 inch = 25.4 millimeters
1 mile = 1.61 kilometers
1 pint (U.S. liquid) = .473 liter
1 quart (U.S. liquid) = .946 liter
1 cubic inch = .01639 liter
1 pound-foot = 1.3558 Newton-meters
1 horsepower = .746 kilowatt
1 pound/square inch = 6.895 kilopascals
1 pound/square inch = 27.6 inches of water/2.04 inches of
mercury
degrees Fahrenheit = (1.8 x degrees Celsius) + 32
1 gallon (U.S. liquid) = .83267 imperial gallon
1 millimeter = .03937 inch
1 kilometer = .6214 mile
1 liter = 2.1134 pints (U.S. liquid)
1 liter = 1.0567 quarts (U.S. liquid)
1 liter = 61.024 cubic inches
1 Newton-meter = .7376 pound-foot
1 kilowatt = 1.34 horsepower
1 kilopascal = .145 pound/square inch
degrees Celsius = .556 x (degrees Fahrenheit – 32)
1 imperial gallon = 1.2009 gallons (U.S. liquid)
000068a
Page 2-21
5-101.bk Page 22 Friday, March 17, 2006 11:05 AM
200 SPECIFICATIONS
SPECIAL TOOLS
Special Tool List
Tool No.Description
814Midget Seal Tool
022001Jacobs Thickness Gauge, 0.060 inch (1.52 mm)
018781Jacobs Thickness Gauge, 0.080 inch (2.03 mm)
014177Jacobs Thickness Gauge, 0.085 inch (2.16 mm)
021327Jacobs Thickness Gauge, 0.100 inch (2.54 mm)
945-6041Connecting Rod Fixture (Sweeney)
HT77136Valve Seat Insert Counterbore
J 21588Injector Gasket Retriever
J 22738-02Universal Spring Tester, Model MST 50
J 23442Piston Ring Compressor
J 2619-01Slide Hammer
J 26589Nozzle Insert Carbon Reamer
J 26637-AThermostat Seal Installer
J 26948Depth Gauge
J 28452Injection Pump Drive Coupling Holder R.B.
J 28452-AInjection Pump Drive Coupling Holder
J 29109 Engine Stand
J 29294-BValve Spring Keeper Remover
J 29296Valve Yoke Guide Pin Installer
J 29297Nozzle Sleeve Installer
J 29510Keystone Piston Ring Groove Gauge
J 29539-15Top Dead Center Indicator Metric Adapter
J 29539-ATop Dead Center (TDC) Indicator
J 29600-C Fire Ring Groove Cutter
J 29880Nozzle Sleeve Extractor
J 34046-ACompression Gauge Adapter Set
J 34046-5Compression Tester Metric Adapter (Used with J 34046-A)
J 34684Cylinder Head Core Plug Installer (13/16 inch)
J 34687Cylinder Head Core Plug Installer (1-1/16 inch)
J 35529Wear Ring and Seal Installer
J 37077Position Sensor
J 37078P7100 Series Injection Pump Holding/Alignment Fixture
J 38500-620APro-Link V-MAC II Diagnostic Cartridge
J 38581Connector, Test Adapter Kit
J 38582Terminal Crimping and Removal Tool Kit
J 38675-CPro-Link 9000 V-MAC Diagnostic Kit
J 38675-DV-MAC I/ITC
J 38740V-MAC Hub Barring Tool
J 38748V-MAC Test Lead, Seven-Pin Connector
J 39200Fluke Model 87 Digital Multi-Meter
J 41443Pro-Link 9000 V-MAC II Diagnostic Kit
Page 2-24
5-101.bk Page 1 Friday, March 17, 2006 11:05 AM
200 ENGINE REMOVAL
ENGINE REMOVAL
Page 3-1
5-101.bk Page 2 Friday, March 17, 2006 11:05 AM
200 ENGINE REMOVAL
GENERAL
Details of the engine removal procedure vary
from one vehicle to another. This section
provides general guidelines for removing the
engine from the vehicle.
Before beginning engine removal, make sure all
equipment is available for use and has been
inspected for safety.
Vehicle Preparation
It is good practice to steam-clean the engine to
remove road grime, grease and oil before starting
work. Steam cleaning the engine and engine area
allows more detailed inspection and improved
workmanship.
Care must be used to keep moisture from
entering the air intake system. If moisture does
enter the system, make sure it is removed (dried
out) before the engine is reinstalled.
3.Using an appropriate filter wrench, remove
the oil filters, fuel filters and coolant
conditioner.
4.Loosen clamps that secure the air intake
tube to the turbocharger and air filter.
Remove the intake tube.
5.If vehicle is equipped with air conditioning:
a.Using A/C refrigerant recovery and
recycling equipment, recover the A/C
system refrigerant.
b.Disconnect the A/C compressor
discharge hose at connection near the
radiator support.
c.Disconnect the A/C line at the
receiver/dryer.
d.Locate and disengage the electrical
connector from binary pressure switch
on the receiver/dryer.
e.Locate and disengage the electrical
connector from the low-pressure cutout
switch in the A/C refrigerant line.
6.Disconnect the upper radiator hose from the
engine coolant outlet fitting.
7.Disconnect the lower radiator hose from the
coolant inlet of the oil cooler assembly.
1.Position vehicle on a flat and level surface in
an area with ample work space in and
around the vehicle. Ensure that a suitable
lifting device is available.
2.Apply the parking brake and block the
vehicle wheels to prevent vehicle from
moving. Observe all safety precautions.
3.Disconnect the battery negative (ground)
cable.
4.Drain the air tanks.
Engine Removal
1.Remove the hood and position it away
from the work area to prevent accidents or
hood damage. Refer to Hood Removal
procedures in the appropriate vehicle
manual.
2.Place a suitable container beneath the
engine and drain engine oil and coolant.
Open the coolant drain valves in the block,
if applicable.
8.Remove the clamps that retain the coolant
overflow tank. Remove tank.
9.Disconnect the chassis-mounted charge air
cooler inlet hose at the cooler.
10. Disconnect the chassis-mounted charge air
cooler outlet hose at the cooler.
11. Locate the engine coolant temperature
sensor and disengage the electrical
connector, if applicable. Remove sensor
harness from the radiator support.
12. Remove fastener from the bracket that
secures the radiator fan air clutch solenoid
valve to the radiator support. Set the
solenoid valve aside.
13. Remove the retaining bolts from the radiator
support rods at the radiator support.
14. Obtain a lifting device (chain fall or engine
hoist) and support the radiator.
15. Remove the retaining bolts from the radiator
support mounts.
16. Remove the radiator from the vehicle using
a lifting device and an assistant, if required.
Page 3-2
5-101.bk Page 3 Friday, March 17, 2006 11:05 AM
200 ENGINE REMOVAL
17. Disconnect the heater hoses and A/C
refrigerant lines, if applicable, from
connections at the lower dash panel behind
the engine.
18. Disconnect the tube connecting the
turbocharger to the air cleaner assembly.
19. Remove all coolant tubes, ground straps, air
lines, fuel lines, hydraulic hoses or tubes,
throttle linkage and electrical wiring
harnesses that are attached to the engine
and would prevent its removal.
20. Remove the air cleaner assembly, if
required.
21. Remove the exhaust bracket from the
clutch, or the torque converter, flywheel
housing and exhaust clamp at the
turbocharger.
22. Remove power steering hoses and the
reservoir, if applicable.
23. Disconnect any electrical cables or wires still
connected to the starter. Remove three
mounting capscrews from the mounting
flange and remove the starter.
24. Support the transmission with an
appropriate transmission jack.
26. Remove the hood rest crossmember(s), if
applicable.
27. Obtain the appropriate lifting equipment (bar
or chain) and attach to the proper lift points
on the engine.
28. Position and attach the engine hoist to the
lift bar or chain and place tension on the bar
or chain by operating hoist.
29. Remove the clutch linkage and bracket
retaining bolts (manual transmission).
30. Remove torque converter access panel and
remove capscrews that secure the torque
converter to the flywheel (automatic
transmission).
31. Remove the retaining bolts that secure the
engine mounts to the engine.
32. Obtain assistance for removal of the engine.
Remove engine while watching for
obstructions that interfere with its removal
such as engine or chassis components,
brackets, clamps or other parts still attached
to the engine.
33. Refer to the ENGINE DISASSEMBLY
section of this manual for procedures for
mounting the engine on an engine stand.
25. Remove the retaining bolts that secure the
transmission bell housing to the flywheel
housing.
Page 3-3
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NOTES
Page 3-4
5-101.bk Page 1 Friday, March 17, 2006 11:05 AM
200 ENGINE DISASSEMBLY
ENGINE DISASSEMBLY
Page 4-1
5-101.bk Page 2 Friday, March 17, 2006 11:05 AM
200 ENGINE DISASSEMBLY
GENERAL
This section includes step-by-step procedures for
complete disassembly of the MACK E7 engine
upon removal from the vehicle. Major
components are removed as assemblies and
overhauled in the BENCH PROCEDURES
section of this manual.
Failure to follow the sequence of operations listed
below may result in damage to components or
personal injury.
10
1
2
[219 EV] CENTRI-MAX™ AND
SPIN-ON FILTER ELEMENTS
Refer to Figure 4-1.
1. Place a suitable container below the filter
element area to catch any spilled fluids.
Do not apply the filter wrench to any area other
than that labeled WRENCH HERE on the
Centri-Max™ filter housing, or damage to the
Centri-Max™ housing will result.
2. Using a suitable filter wrench, remove the
fuel and oil filter elements. Do not reuse filter
elements. Discard used elements in a
responsible, environmentally safe manner.
3. Loosen drain hose assembly (4) from
Centri-Max™ filter housing assembly by
loosening hose clamp (3) at the
Centri-Max™ housing.
9
8
7
5
Figure 4-1 — Centri-Max™ Housing Removal Studs
1. Studs
2. Seal ring
3. Clamp
4. Drain hose assembly
5. Washers
6. Nuts
7. Adapter
8. O-ring
9. Centri-Max
10. Centri-Max
3
4
5
6
200326a
™ housing
™ element
4. Remove two nuts (6) and two washers (5)
securing hose adapter (7) to studs (1) at the
cylinder block. Discard O-ring (8).
5. Remove drain hose assembly (4).
6. Remove Centri-Max™ housing (9) and
element (10). Discard seal ring (2).
Page 4-2
5-101.bk Page 3 Friday, March 17, 2006 11:05 AM
MOUNTING ENGINE IN STAND
The engine is heavy (approximately 2,300 lbs.
[1043 kg] wet). Stay out from under the engine
when it is being lifted. Failure of the lifting
device could result in serious injury or death.
Make sure to use lifting equipment that is
rated at a capacity greater than the weight of
the engine.
The fuel and oil filter elements, as well as the
Centri-Max™ assembly, must be removed before
mounting the adapter plate to the engine.
200 ENGINE DISASSEMBLY
Engine stand, Kent-Moore tool number J 29109,
and adapter plate J 38048, are recommended to
safely support the engine during disassembly and
assembly procedures.
When servicing an E7 engine with an isolating oil
pan arrangement, avoid using an engine stand
that supports the engine on the oil pan rail while
the oil pan is still installed. Damage to the oil pan,
pan gasket or the isolators may result. If this type
of stand must be used and the oil pan is to remain
installed, support the engine on the pads
provided at each corner of the cylinder block as
shown in Figure 6-56.
Special Tools Required
앫Engine Stand J 29109
앫Adapter Plate J 38048
Refer to Figure 4-2.
1. Using three mounting capscrews (2), secure
adapter plate J 38048 (1) to the left side of
the engine.
2. Secure adapter plate (1) to engine stand
J 29109 (3) with six mounting capscrews (4).
3. Remove lifting device from the engine.
Page 4-3
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200 ENGINE DISASSEMBLY
1
2
3
1. Adapter plate J 38048
2. Capscrews
Figure 4-2 — Mount Engine in Stand
3. Engine stand J 29109
4. Capscrew
4
2
200348a
Page 4-4
5-101.bk Page 5 Friday, March 17, 2006 11:05 AM
200 ENGINE DISASSEMBLY
[271 CB] ALTERNATOR
Refer to Figure 4-3.
1. Loosen adjusting capscrew (2) and
mounting nuts (6).
2. Remove drive belts (1) and tag belts for
reassembly.
3. Disconnect and tag electrical wires by
removing mounting hardware.
4. Remove mounting nuts (6) and washers.
Pull out capscrews (3) and remove
alternator (7).
5. Remove alternator plate (5) by removing
mounting hardware (4).
2
1
3
[215 HB] FAN ASSEMBLY
Refer to Figure 4-4.
1. Loosen eight fan assembly mounting nuts
(2) and capscrews (1).
2. While supporting fan assembly (3), remove
nuts (2) from capscrews (1) and remove fan
assembly.
1
Figure 4-4 — Fan Assembly Removal
2
200350a
3
7
3
6
5
Figure 4-3 — Alternator Removal
1. Drive belt
2. Adjusting capscrew
3. Capscrew
4. Mounting hardware
4
5. Alternator plate
6. Mounting nuts
7. Alternator
200349a
1. Capscrew
2. Nut
3. Fan assembly
Refer to Figure 4-5.
3. If the fan assembly is equipped with a
viscous drive, be sure to store the assembly
either horizontally, with the fan face down
(hub flange up), or vertically, as shown in
Figure 4-5. This will prevent fluid leaking
from the assembly.
Do not store the assembly horizontally with the
fan face up (hub flange down). Fluid in the
viscous drive reservoir can leak out.
Page 4-5
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200 ENGINE DISASSEMBLY
[231 PB] FUEL FILTER
ADAPTER ASSEMBLY
Refer to Figure 4-6
1. Disconnect three fuel lines from fittings (2, 3
and 5) on fuel filter adapter assembly (1).
Tag and cap all lines.
2. Remove three capscrews (4) from the top of
the fuel filter adapter assembly.
3. Remove fuel filter adapter assembly from
the air inlet manifold (7).
Figure 4-5 — Viscous Fan Drive Assembly Storage
Figure 4-6 — Fuel Filter Adapter Assembly Removal
1. Fuel filter adapter
assembly
2. Secondary filter fitting
(out)
3. Secondary filter fitting
(in)
4. Capscrews
5. Primary filter fitting (out)
6. Primary filter fitting (in)
7. Air inlet manifold
8. Mounting flange
Page 4-6
a
5-101.bk Page 7 Friday, March 17, 2006 11:05 AM
200 ENGINE DISASSEMBLY
[215 LD] COOLANT
CONDITIONER ELEMENT
Refer to Figure 4-7.
1. Cut the plastic tie wrap (1) securing coolant
conditioner supply tube (2) to cylinder head
manifold overflow line.
2. Disconnect fittings (3) from both ends of the
coolant conditioner supply tube. Remove
tube (2).
2
1
Refer to Figure 4-8.
3. Place a suitable container below the coolant
filter area to catch any spilled coolant.
4. Using a suitable filter wrench (J 29927 or
equivalent), remove the coolant conditioner
filter element (13). Discard element.
5. Remove coolant conditioner head assembly
(2) from thermostat housing (5) and coolant
manifold (9) by removing mounting
capscrews (1).
6. Remove and discard O-ring (4).
7. Carefully remove and examine the check
valve assembly (3). Examine check valve
assembly by depressing the check ball. If it
resists movement and does not return to its
seat freely, the check valve assembly must
be replaced.
1. Disconnect turbocharger lubrication supply
hose (6) from the oil filter/cooler assembly
(5).
2. Disconnect feed line (2) from the centrifugal
filter housing fitting. Tag and cap line and
fitting.
Unless it is necessary to repair any portion of the
oil cooler or oil filter housing, remove the units as
an assembly. The assembly can be
disassembled later if necessary. Refer to Oil
Cooler Disassembly in the BENCH
PROCEDURES section.
3. Disconnect Centri-Max™ filter breather hose
(1) by sliding hose from fitting. (For MR
chassis Jake Brake applications, remove the
Centri-Max™ breather filter. Clean with
suitable solvent to make sure breather is
clear.)
4. Remove four capscrews (3) securing oil filter
feed assembly (4) to engine block.
Effective with the introduction of the S300 and
S400 model turbochargers (May 1996), a new
style oil inlet line is used. The line is a stainless
steel braided line which replaces the conventional
hose type line and steel oil inlet tube. The new oil
line is connected directly to the threaded oil inlet
port at the turbocharger.
Figure 4-10 — Oil Cooler Removal
1. Centri-Max™ filter breather hose (MR chassis with Jake
Brake uses breather assembly)
2. Feed line
3. Capscrew
Page 4-10
4. Oil filter feed assembly
5. Oil filter/cooler assembly
6. Turbocharger lubrication feed hose
5-101.bk Page 11 Friday, March 17, 2006 11:05 AM
200 ENGINE DISASSEMBLY
[215 SW] WATER PUMP
Refer to Figure 4-11.
1. Disconnect coolant return hose to air
compressor (1) at fitting.
2. Remove three mounting capscrews (3) and
remove water pump (2).
1
3
[214 SD] TURBOCHARGER
Refer to Figure 4-12.
1. Remove two capscrews (3) securing
turbocharger lubrication drain tube (4) to
turbocharger (1).
2. Loosen hose clamp (5) securing drain tube
to oil fill tube. Remove drain tube (4).
3. Remove turbocharger lubrication feed hose
(2).
2
Beginning with May 1996 production, Schwitzer
turbocharger models S300 and S400 replace
models S3B and S4B. Service old with old and
new with new. Also note that with the S300 and
S400 models, a stainless-steel braided oil feed
line is used.
4. Loosen four turbocharger mounting nuts (6)
and remove turbocharger (1).
3
Figure 4-11 — Water Pump Removal
1. Air compressor coolant
return line
2. Water pump
3
200358a
3. Capscrew
Figure 4-12 — Turbocharger Removal
1. Turbocharger
2. Lubrication feed hose
3. Capscrew
4. Lubrication drain tube
5. Clamp
6. Mounting nut
Page 4-11
5-101.bk Page 12 Friday, March 17, 2006 11:05 AM
200 ENGINE DISASSEMBLY
[222 KD] FUEL NOZZLE INLET
TUBE ASSEMBLY
Refer to Figure 4-13.
1. Loosen six tube sleeve nuts (6) at the
injection pump. Be careful to avoid twisting
lines while loosening nuts.
1
11
1
2
3
2
2. Loosen brackets (3 and 5) by removing
retaining hardware.
3. Loosen tube sleeve nuts (1) and tube
clamping screws at the cylinder heads and
remove front (4) and rear (2) tube
assemblies. Cap all lines and fittings to
prevent contaminants from entering the
system.
1
3
1
10
9
8
7
Figure 4-13 — Fuel Inlet Tube Assembly Removal
1. Nozzle fuel inlet tube and sleeve nut
2. Rear fuel inlet tube assembly
3. Bracket/insulator (tube clamp)
4. Front fuel inlet tube assembly
5. Bracket/insulator (tube clamp)
6. Sleeve nut
5
7. Oil filler feed tube
8. Oil filler feed tube bracket
9. Capscrew
10. Exhaust manifold
11. Capscrew
6
4
5
200353a
Page 4-12
5-101.bk Page 13 Friday, March 17, 2006 11:05 AM
200 ENGINE DISASSEMBLY
Refer to Figure 4-14.
4. If necessary, separate fuel inlet tubes (4)
from bracket assembly. Remove nuts (6)
from capscrews (1) and remove clamp plate
(2), insulators (3) and bracket (5).
1
2
3
6
[213 JB] VALVE COVER AND
RISER
If engine is equipped with a Jake Brake®, a riser
is installed under the valve cover. Longer
capscrews are used to secure the valve cover
and riser to the cylinder head.
.
Refer to Figure 4-16.
1. Remove valve covers (3) by removing six
retaining capscrews (4 and 5) from each
cover.
2. Discard seals.
Refer to Figure 4-15.
4
5
3. If a Jake Brake is installed, perform the
following:
4. Support the exhaust manifold and remove
12 mounting capscrews (11) securing the
manifold (10) to cylinder heads.
5. Remove exhaust manifold.
6. Discard gaskets.
34
Figure 4-15 — Control Wire Removal
1. Valve cover
2. Capscrew
3. Control wire
4. Riser housing
Refer to Figure 4-16.
b.Disconnect wires (1) at the actuator
solenoid connector (14).
c.Remove risers (2). Discard seals.
200355a
Page 4-13
5-101.bk Page 14 Friday, March 17, 2006 11:05 AM
200 ENGINE DISASSEMBLY
[213 LP, NV & LH] ROCKER
ARM, VALVE YOKE AND PUSH
ROD
Refer to Figure 4-16.
If equipped with a Jake Brake, perform the
following:
1. Remove three capscrews (6) from each
actuator assembly (15).
2. Remove actuator assemblies from cylinder
heads (one actuator assembly per head).
If a Jake Brake was not installed, there will be six
capscrews per rocker arm assembly. If a Jake
Brake was installed, there will be only three
capscrews per rocker arm assembly remaining.
3. Remove remaining capscrews (13) and
washers (12) from rocker arm shaft brackets
(7). Remove rocker arm assembly (11) from
each head.
1
12
9
13
2
15
14
11
10
3
16
7
7
4
5
6
7
8
4. Remove valve yokes (8) from each pair of
valves by lifting straight up on each yoke.
Tag yokes for reassembly.
5. Remove valve push rods (10) and tag rods
for reassembly.
9
200263a
Figure 4-16 — Valve Cover and Rocker Arm Removal
1. Wire connector
2. Riser
3. Valve cover
4. Short capscrew
5. Long capscrew
6. Actuator capscrew
7. Rocker arm shaft
bracket
8. Valve yoke
9. Head bolt with threaded
hole
10. Push rod
11. Rocker arm assembly
12. Washer
13. Capscrew
14. Connector
15. Actuator assembly
16. Actuator solenoid
Page 4-14
5-101.bk Page 15 Friday, March 17, 2006 11:05 AM
200 ENGINE DISASSEMBLY
[222 KG] NOZZLE HOLDER
Special Tool Required
앫Injection Nozzle Puller J 37093
After removing the nozzles, it is a good practice
to label or tag them for reinstallation into the
same cylinders. After removal, place nozzles on a
clean surface.
Refer to Figure 4-17.
1. Remove nozzle holder retainer (2).
2. Assemble injection nozzle puller J 37093 as
follows:
a.Attach nut (12), bearing (11), spacer
(10) and rubber washer (9) to tool
handle (1).
b.Screw handle (1) in threaded hole of
nozzle holder (5) until rubber washer
(9) is slightly compressed.
3. With tool in position, turn nut (12) clockwise
to draw nozzle holder from cylinder head
nozzle mounting hole (8).
4. Continue turning nut until nozzle holder is
free of insert. Remove nozzle holder and
puller tool as an assembly.
5. Remove nozzle holder gasket (7). The
gasket is manufactured from a special iron
material 0.060 inch (1.524 mm) thick.
1
12
11
10
9
Figure 4-17 — Nozzle Holder Removal
1. Handle
2. Nozzle holder retainer
3. O-ring
4. O-ring
5. Nozzle holder
6. Nozzle
7. Gasket
8. Nozzle mounting hole
9. Rubber washer
10. Spacer
11. Bearing
12. Nut
2
3
4
5
6
7
8
201280a
6. Remove remaining nozzle holders in the
same manner.
Current production nozzle holders do not have
the lower O-ring groove.
Page 4-15
5-101.bk Page 16 Friday, March 17, 2006 11:05 AM
200 ENGINE DISASSEMBLY
[213 EV] CYLINDER HEAD
ASSEMBLY REMOVAL
Refer to Figure 4-18.
1. Remove fuel return tube (3) from between
the cylinder head assemblies (4) by
loosening the tube sleeve nuts from each
end.
Cylinder head assemblies are heavy. Lifting a
cylinder head requires the help of an
assistant or suitable lifting device. Attempting
to lift a cylinder head without assistance may
result in severe personal injury.
2. Remove fuel return line (1) at the front of the
forward cylinder head.
3. Remove cylinder head bolts (2 and 5). Refer
to cylinder head bolt torque sequence chart
in Cylinder Head Installation for location of
bolts, if necessary.
4. Using a suitable lifting device, remove heads
from the engine block.
5. Remove gaskets and six fire rings. Discard
gaskets and fire rings.
1. Fuel return line
2. Bolt
3. Fuel return tube
Page 4-16
Figure 4-18 — Cylinder Heads
4. Cylinder head
5. Bolt with hole in head
5-101.bk Page 17 Friday, March 17, 2006 11:05 AM
200 ENGINE DISASSEMBLY
[212 RB & RH] VIBRATION
DAMPER AND CRANKSHAFT
HUB
Refer to Figure 4-19.
1. Remove six mounting capscrews (4) and
turnover bracket, if equipped.
2. Remove vibration damper (3) and fan belt
drive pulley (1) together.
3. Using a 1-7/16 inch wrench, remove
crankshaft hub capscrew (2).
4. Using a suitable puller such as J 24420-C,
remove the crankshaft hub.
2
1
[261 CK] AIR COMPRESSOR
Refer to Figure 4-20.
Disconnect two coolant lines (1 and 4) from the
air compressor head (2) at the fittings. Tag and
cap lines.
2
1
Figure 4-19 — Vibration Damper Removal
1. Pulley
2. Capscrew
3. Vibration damper
4. Capscrew
3
5
3
Figure 4-20 — Air Compressor Connections
1. Coolant supply line
2. Air compressor head
4
200359a
3. Capscrew
4
200258a
4. Coolant return line
5. Air governor mounting
flange
The air compressor is heavy. Lifting the air
compressor may require the help of an
assistant or suitable lifting device. Attempting
to lift the compressor without such
assistance may result in severe personal
injury.
Page 4-17
5-101.bk Page 18 Friday, March 17, 2006 11:05 AM
200 ENGINE DISASSEMBLY
Refer to Figure 4-21.
1. Remove three mounting capscrews (5)
securing air compressor (1) to auxiliary
driveshaft housing (3).
2. Taking care not to damage or lose the
lubrication oil supply tube (2), remove the air
compressor by pulling it rearward out of the
mounting flange. Discard gasket.
1
2
1. Air compressor
2. Oil supply tube
3. Auxiliary driveshaft
5
4
3
Figure 4-21 — Air Compressor Removal
4. Oil drain openings
5. Capscrew
200360a
Page 4-18
5-101.bk Page 19 Friday, March 17, 2006 11:05 AM
[221 GP] INJECTION PUMP
Refer to Figure 4-22.
1. Disconnect lubrication supply line (6) at both
fittings. Tag and cap fittings.
2. Disconnect fuel lines (1, 3, 4, and 5) at the
fittings. Tag and cap all lines. Remove lines
from the engine by removing clamp retaining
capscrew. Set fuel lines on a clean surface.
If the fuel injection pump does not require
servicing, set pump-to-engine timing before
removal. This will allow ease of installation. Refer
to the SETUP AND ADJUSTMENTS section for
Fuel Injection Pump Fixed Timing Procedure.
200 ENGINE DISASSEMBLY
3. Remove rear support link assembly by
removing mounting hardware (7 and 8),
V-MAC engines only.
4. Mechanically governed engines — Working
from the front of the engine, remove four
capscrews securing the injection pump drive
gear and remove gear. For V-MAC engines,
omit this step and go on to step 5.
5. Remove mounting capscrews securing
pump to adapter.
6. Remove injection pump by moving it away
from mounting flange.
Figure 4-22 — Fuel Line Removal
1. Return from secondary
filter
2. Cylinder head overflow
line
3. Return to tank line
4. Return to secondary
filter
5. Return from primary
filter
6. Lubrication supply line
7. Capscrew
8. Capscrew
Page 4-19
5-101.bk Page 20 Friday, March 17, 2006 11:05 AM
200 ENGINE DISASSEMBLY
[221 CD] ECONOVANCE
V-MAC Equipped Engines
Refer to Figure 4-23.
1. Working from front of engine, remove four
capscrews securing the injection pump drive
gear. Remove gear.
3. Remove the drive coupling (3) by slipping it
off of the splines (6).
3
2
1
Figure 4-24 — Econovance Housing Removal
(Pre-1992 Style Shown)
1. Mounting capscrew
2. Injection pump adapter
3. Drive coupling
4
5
6
4. Capscrew
5. Econovance
6. Splines
[211 NB] OIL PAN
Refer to Figure 4-25.
1. Remove the nuts from the two studs
securing the oil pan to the timing gear cover.
2. Remove the two nuts from the two studs
securing the oil pan to the flywheel housing.
3. Remove the remaining shouldered bolts
securing the oil pan to the pan rails and
remove the oil pan.
200364a
A metal two-piece style drive coupling was
introduced into production on certified E7 V-MAC
engines built after July 1, 1992 — beginning with
serial No. 2P and above. When the Celeron drive
coupling requires replacement, replace the drive
coupling with the updated two-piece style. Older
style shown.
4. Remove the Econovance (5) by removing
four mounting capscrews (4). Rotate shaft to
clear the camshaft gear.
Page 4-20
Oil pans with isolating gaskets are secured with
nuts and shouldered studs at the timing gear
cover and flywheel housing. Refer to Figure 4-25.
5-101.bk Page 21 Friday, March 17, 2006 11:05 AM
200 ENGINE DISASSEMBLY
1. Studs and nuts at timing gear cover
2. Studs and nuts at flywheel housing
Figure 4-25 — Oil Pan Bolt Locations
3. Shouldered bolts along pan rails
Page 4-21
5-101.bk Page 22 Friday, March 17, 2006 11:05 AM
200 ENGINE DISASSEMBLY
[219 MU] OIL PUMP
Refer to Figure 4-26.
If the oil pump must be disassembled for any
reason, it will be easier to loosen the housing
cover retaining capscrews (2), the screen
capscrews (5), the sump capscrews (3), the
cover plate capscrews (9), and the relief valve
cap (8) while the pump is still secured in position.
Do so before loosening the three retaining
capscrews (1).
Remove the oil pump as a unit by removing three
retaining capscrews (1).
5
1
2
1
9
10
2
9
6
4
3
1
3
8
7
6
5
200264a
1. Capscrews
2. Capscrews
3. Capscrews, 12-point
4. Sump
5. Capscrews
Page 4-22
Figure 4-26 — Lubrication Oil Pump
6. Washer
7. Screen
8. Relief valve cap
9. Capscrews
10. Plate
a
5-101.bk Page 23 Friday, March 17, 2006 11:05 AM
200 ENGINE DISASSEMBLY
[211 RP] TIMING GEAR COVER
Do not attempt to remove timing gear cover
without removing oil pan. Doing so may result in
damage to the isolating oil pan gasket.
Refer to Figure 4-27.
1. Remove front engine mount pedestal (4) by
removing six retaining capscrews (7 and 9).
2. Remove auxiliary pump and connecting
hardware, if equipped. Discard O-ring seal.
3. If not equipped with an auxiliary pump,
remove cover (12) and gasket (8) by
removing mounting nuts (10) and
washers (11).
4. Remove the injection pump timing cover
(14) by removing the mounting capscrews (1
and 13). Discard O-ring (2).
5. Remove remaining mounting capscrews
(13) from timing gear cover (3).
2
1
14
13
12
11
10
8
7
9
7
5
6
3
4
200257
Do not damage the timing indicator (5), if
equipped, when removing timing gear cover.
6. Remove timing gear cover. It will be
necessary to pry the cover from the engine
block. Be careful not to damage cover or
block while using sharp tools around
machined surfaces.
2. Using a hub puller such as J 21834-4A,
remove auxiliary driveshaft gear (2) from the
splines (5) on the end of shaft.
1
2
3
4
3. Remove two retaining capscrews (3) from
auxiliary driveshaft captured thrust washer
(4). Remove washer.
2
1
Figure 4-28 — Auxiliary Driveshaft Gear Removal
1. Nut
2. Auxiliary driveshaft gear
3. Capscrew
3
4
5
200361a
4. Captured thrust washer
5. Shaft splines
Refer to Figure 4-29.
5
Figure 4-29 — Auxiliary Driveshaft Removal
1. Rear bushing
2. Front journal
3. Auxiliary driveshaft
4. Rear journal
5. Oil pump drive gear
200362a
[213 CH] CAMSHAFT
Make sure all loose components are secured
to, or removed from, the engine before
rotating engine on the stand. Failure to do so
may result in damage to components or
severe personal injury.
1. Rotate engine so that the deck surface is
downward and the oil pan rail is upward
(engine inverted).
Be very careful to avoid damaging the auxiliary
driveshaft bushings or journals while removing
the shaft.
Remove the auxiliary driveshaft (3) by pulling it
rearward out of the air compressor mounting
flange opening. With engine oil pump in position,
a rotating motion may be necessary to clear the
engine oil pump drive gear (5).
Page 4-24
When engine is rotated, the valve lifters will fall
downward into the push rod holes but will be
captured by their heads. They will be out of the
way for camshaft removal.
Refer to Figure 4-30.
2. Remove the two 12-point capscrews (3) that
retain camshaft thrust washer (1). Camshaft
may have to be rotated slightly to make the
capscrews accessible through openings (2)
in the camshaft drive gear (4).
5-101.bk Page 25 Friday, March 17, 2006 11:05 AM
1
200 ENGINE DISASSEMBLY
4. Taking care not to damage camshaft or
bushings, pull camshaft out of the front of
the engine. Carefully guide rear of shaft
through the journals. If shaft does not come
out freely, ensure all valve lifters are clear of
camshaft cams and journals.
2
4
Figure 4-30 — Camshaft Thrust Washer Capscrews
1. Thrust washer
2. Openings
3
200365a
3. Capscrew, 12-point
4. Camshaft drive gear
5. Remove valve lifters.
Valve lifters have established wear patterns and
should be reinstalled in same locations. Label
each valve lifter upon removal and place on a
clean work surface.
[212 NP & LQ] PISTON AND
3
CONNECTING ROD ASSEMBLY
The crankshaft and related components are
heavy, have sharp edges and many possible
pinch points. Always be careful while working
in this area to avoid serious personal injury.
Refer to Figure 4-31.
3. Install the camshaft removal/installation tool
J 41461 (3) in position on the rear segment
of the camshaft (1), securing it with the clip
(2) to the shaft.
1
2
3
200573a
Figure 4-31 — Camshaft Removal/Installation Tool
1. Rear segment of
camshaft
2. Tool retaining clip
3. Camshaft removal/
installation tool
Before removing pistons, connecting rods and
rod caps, ensure they are marked so they can be
reinstalled in the same cylinders from which they
were removed.
Remove connecting rod and piston assemblies in
companion cylinder sets: 1 and 6, 2 and 5, and 3
and 4.
1. Rotate engine stand 90 degrees so that
pistons lie horizontally in the block with top
of pistons and connecting rods accessible.
2. Rotate crankshaft so that pistons 1 and 6
are lowered in the cylinder at least
two inches (51 mm) to allow adequate room
to remove carbon from upper edge of
sleeves.
Page 4-25
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200 ENGINE DISASSEMBLY
Refer to Figure 4-32.
3. Using a sharp knife, carefully remove any
carbon at the top of the sleeves. Remove
any remaining carbon using crocus cloth or
fine sandpaper, then wipe inside of sleeves
with a clean cloth.
Refer to Figure 4-33.
4. Rotate crankshaft so that pistons 1 and 6
are at bottom dead center. Remove
connecting rod capscrews and rod bearing
caps.
Figure 4-32 — Carbon Removal from Cylinder Sleeves
.
Figure 4-33 — Piston and Connecting Rod
Assembly Removal
5. Using a hammer handle, push piston 1 from
the cylinder bore. Remove piston 6 in the
same manner.
6. After removing pistons 1 and 6, rotate
crankshaft so that next set of pistons
(2 and 5) is at bottom dead center.
7. Repeat steps 2 through 6 for removing
piston sets 2 and 5, and 3 and 4.
Page 4-26
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[212 UC] FLYWHEEL
Refer to Figure 4-34.
1. With engine stand rotated so that engine is
inverted (crankshaft horizontal), loosen all
six flywheel retaining capscrews.
2. Remove two of the flywheel retaining
capscrews that are opposite each other.
Install two longer capscrews or studs to
allow flywheel to be safely removed from the
crankshaft.
3. Remove remaining capscrews.
4. Carefully tap flywheel by alternating from
side to side to work it off the aligning dowel
pins.
200 ENGINE DISASSEMBLY
The flywheel is heavy. Lifting the flywheel will
require the help of an assistant or the use of a
suitable lifting device (J 25026-A or
equivalent). Attempting to lift a flywheel
without such assistance may result in severe
personal injury.
Remove flywheel timing pointer, if present, to
avoid damaging the pointer during flywheel
removal.
Figure 4-34 — Flywheel Removal
5. Support the flywheel and remove two guide
capscrews.
6. Using a suitable lifting device such as
J 25026-A, or adequate assistance, remove
flywheel.
Page 4-27
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200 ENGINE DISASSEMBLY
[211 HD] FLYWHEEL HOUSING
Refer to Figure 4-35.
1. Remove eight mounting capscrews (3) from
flywheel housing (2).
2. Remove flywheel housing. It may be
necessary to tap lightly on the housing with
a soft mallet to separate housing from
engine block.
1
1
[211 JA] MAIN BEARING CAP
Before removing main bearing caps, ensure they
are marked so they can be reinstalled on the
same journals. Keep the bearings with the same
cap and tag or mark them to identify the cam side
of the bearings.
Refer to Figure 4-36.
1. Remove eight buttress capscrews (2 and 3).
2. Remove main bearing capscrews (1) from
each of the seven bearing caps (4 and 5).
The center main bearing cap (5) houses the
thrust washers.
3. Position a lady-foot pry bar under the tabs
provided on bearing caps and pry bearing
caps upward. To work them loose, it may be
necessary to tap the bearing caps
alternately from side to side with a soft
mallet.
1
3
Figure 4-35 — Flywheel Housing Removal
1. Capscrew locations
2. Flywheel housing
3. Capscrew
1
2
200366a
Page 4-28
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200 ENGINE DISASSEMBLY
1. Main bearing cap capscrews
2. Buttress capscrews, 80 mm
3. Buttress capscrews, 110 mm
Figure 4-36 — Buttress Capscrew Installation
4. Main bearing caps
5. Center main bearing cap
Page 4-29
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200 ENGINE DISASSEMBLY
[212 HP] CRANKSHAFT
Refer to Figure 4-37.
1. Using a suitable lifting device, secure a sling
or crankshaft support tool around the
crankshaft and lifting device hook. Ensure
crankshaft is evenly balanced when lifted
from the engine block.
2. Lift crankshaft from engine block and store
in a secured stand, or horizontally on
V-blocks.
[219 RV] PISTON COOLING
SPRAY NOZZLE
To avoid damaging spray nozzles, remove them
before removing sleeves.
It is best to use a 10-mm, 6-point socket on a
12-inch extension to remove the nozzle retaining
capscrews.
2. Carefully pull outward on the spray nozzle to
remove it from the block.
3. Remove and discard elastomer seal (1).
Figure 4-37 — Crankshaft Removal
4. Repeat steps 1 through 3 to remove
remaining spray nozzles.
1
Figure 4-38 — Spray Nozzle Removal
1. Elastomer seal
2. Spray nozzle
2
3. Capscrew
3
200613a
Page 4-30
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200 ENGINE DISASSEMBLY
[212 NC] CYLINDER SLEEVE
Special Tool Required
앫Cylinder Liner/Sleeve Puller PT6435
Refer to Figures 39 and 40.
1. Rotate engine in stand so that it is upright
(deck surface upward).
2. Use puller PT6435, or equivalent, to remove
cylinder sleeve (2) from cylinder block (4).
3. Position puller above the sleeve and guide
the puller shaft through the sleeve.
Extreme care must be taken to make sure the
puller shoe is properly aligned in the bottom of
the sleeve to prevent damage to the block.
4. Position puller shoe so that it catches the
lower lip of the sleeve. Ensure that it does
not extend beyond outside edges of the
sleeve so it will not come into contact with
the cylinder block as the sleeve is removed.
6. Remove puller from sleeve.
7. Remove crevice seal (1) from sleeve.
8. Repeat steps 2 through 7 to remove
remaining cylinder sleeves.
1
2
4
3
5. Tighten screw on the puller until sleeve
comes free from cylinder block bore.
Remove shims (3), if installed.
Figure 4-39 — Cylinder Liner/Sleeve Puller PT6435
Figure 4-40 — Sleeve Removal
1. Crevice seal
2. Cylinder sleeve
200614a
3. Shims
4. Cylinder block
Page 4-31
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NOTES
Page 4-32
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200 BENCH PROCEDURES
BENCH PROCEDURES
Page 5-1
5-101.bk Page 2 Friday, March 17, 2006 11:05 AM
200 BENCH PROCEDURES
[211 DB] CYLINDER BLOCK
Cylinder Sleeve Counterbore
SPECIAL TOOLS REQUIRED:
앫Counterbore Tool PT2210
앫Counterbore Cutter Plate PT2210-3A
앫Universal Dial Depth Gauge PT5025
앫Stylus Extension (3-Inch) PT5052-11
앫Hex Key Wrench PT2210-14
INSPECTION AND REPAIR
If the cylinder block deck is resurfaced, the
cylinder sleeve counterbore depth must be recut
to specification. If the cylinder block deck was not
resurfaced but cylinder sleeve counterbore
surface shows excessive pitting or erosion, recut
the counterbore as required.
Use shims to re-establish the correct liner flange
height. Shims are available in the following
thicknesses: 0.002, 0.003, 0.004, 0.008, 0.010,
0.012 and 0.014 inch.
Universal dial depth gauge PT5025, with a 3-inch
stylus extension PT5052-11, is recommended for
measuring the counterbore.
3. Measure and record the counterbore in four
places, 90 degrees apart. Using a depth
gauge with a 3-inch extension, mark the
shallowest point. Subtract the lowest
number from the highest number. This is the
minimum amount to be machined for
cleanup.
SETTING UP COUNTERBORE TOOL PT2210
WITH CUTTER PLATE PT2210-3A
Refer to Figure 5-1.
1. Loosen the two cutter bit hold-down
capscrews (9). Install cutter bit (11) into
cutter plate PT2210-3A (13) by turning the
cutter bit adjuster (10) counterclockwise.
Cutter bit face must be facing a clockwise
rotation cut.
To resurface the cylinder sleeve counterbore
area of the cylinder block, use counterbore
tool PT2210 with counterbore cutter plate
PT2210-3A.
This procedure can be performed either in or out
of the chassis. If performing the procedure in the
chassis, be sure to cover the crankshaft and any
holes in the block to prevent contamination from
machining chips.
Do not cut seats deeper than 4.034 inches
(102.464 mm).
1. Make sure that the top of the deck is clean
and free of burrs. Use a finish mill file and
crocus cloth, if necessary, to create a
smooth, flat surface for positioning the tool.
Do not tighten the cutter bit hold-down cap (12).
The cutter point should not extend beyond the
outer edge of the cutter plate. If the cutter bit
does stick out, damage to the bit will occur when
installing counterbore tool onto cylinder block.
2. Install the cutter plate on the main shaft (15).
Use the large end of hex key wrench
PT2210-14 (18) to hold the cutter plate and
tighten securely. The hole in the side of the
cutter plate accepts the large end of the tool.
Do not allow the cutter bit (11) to touch the
cylinder sleeve bore wall.
2. Using compressed air, thoroughly remove all
debris.
Page 5-2
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200 BENCH PROCEDURES
When the entire block must be counterbored, cut
the deepest bores first. This way, the tool can be
adjusted to the lowest depth and used for all
cylinders, ensuring uniform depth on all cylinder
counterbores.
3. Position the tool in the cylinder bore by
backing the depth-set collars (5 and 16) off
and lowering the cutter plate (13) into the
counterbore to center the tool.
4. Secure the cutter plate to the cylinder block
with four M16 x 2 x 90 hex-head capscrews
(3) and special washers (4) from the
counterbore tool kit PT2210.
5. Cross-torque the capscrews to 30 lb-ft
(41 N폷m) using torque wrench J 24406 or
equivalent.
Lift T-handle (2) slightly (so cutter plate is not in
contact with the counterbore) and rotate the
mainshaft (15) counterclockwise to ensure cutter
plate turns freely without binding. If necessary,
loosen the capscrews and relocate the tool.
It may be necessary to use a flashlight to see the
cutter bit adjusting screw.
11. Using hex key wrench PT2210-14 (18), turn
the cutter bit adjusting screw clockwise until
the cutter bit rests on the counterbore ledge.
12. If the cutter bit will not adjust, adjust the
lower depth-set collar (16) 0.005 inch
(0.127 mm) more and recheck cutter bit
hold-down screws for looseness.
13. Zero the depth-set collars:
a.Back off the lower depth-set collar (16)
and carefully lower the cutter plate (13)
into the bore and allow the cutter to rest
on the counterbore ledge.
b.Rotate both depth-set collars (5 and 16)
down until the bottom collar contacts
the main housing (8).
Do not force the collar beyond this point, as it will
lift the cutter plate and prevent an accurate zero
reading.
6. Using the counterbore tool T-handle (2),
raise the cutter plate approximately 1/2 inch
(12.7 mm) from the counterbore ledge.
7. Using hex key wrench PT2210-14 (18), turn
the cutter bit adjusting screw (10) clockwise
until the cutter bit contacts the counterbore
ledge. Do not touch the counterbore wall.
8. Back off the lower depth-set collar (16) and
lower the cutter plate until the cutter rests on
the ledge.
9. Rotate the lower depth-set collar down until
the collar contacts the main housing.
10. Rotate the collar an additional five
increments: 0.005 inch (0.127 mm). Each
graduation of the collar is one-thousandth
(0.001) of an inch (0.025 mm). This will lift
the cutter bit 0.005 inch (0.127 mm) off the
counterbore ledge, allowing an accurate
setting of the cutter bit.
14. Set the depth of the cut. Determine the final
depth of the cut and back off the top depthset collar accordingly. Each increment on
the depth-set collar increases the depth of
the cut by one-thousandth (0.001) of an inch
(0.025 mm). Tighten the thumbscrew (17) on
the upper collar (5) securely.
Page 5-3
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1
200 BENCH PROCEDURES
2
5
6
17
16
3
4
7
8
3
9
10
3
4
9
18
3
15
13
14
Figure 5-1 — Counterbore Ledge Tool Installation
4
13
12
11
200328a
1. Cutter plate holder
2. T-handle
3. Capscrews, M16 x 2 x 90
4. Special washers
5. Upper depth-set collar
6. Lower thumbscrew
7. Oil fill tube
8. Main housing
9. Hold-down capscrews
Page 5-4
10. Cutter bit adjuster
11. Cutter bit
12. Hold-down cap
13. Cutter plate
14. Cylinder block
15. Main shaft
16. Lower depth-set collar
17. Upper thumbscrew
18. Hex key wrench
5-101.bk Page 5 Friday, March 17, 2006 11:05 AM
200 BENCH PROCEDURES
CUTTING THE COUNTERBORE
Refer back to Figure 5-1.
1. Fill the oil fill tube (7) with 30W
nondetergent oil to maintain lubrication
during use.
2. Back off the lower depth-set collar (16) two
increments or less, and tighten the
thumbscrew (6) securely.
3. Cut the counterbore by turning the T-handle
clockwise while maintaining constant
downward pressure on the tool. Stop the
handle in a different position to avoid
creating a ridge in the counterbore.
4. Continue backing off the lower depth-set
collar, no more than two graduations per cut.
Check the depth measurement between
each adjustment. Plan to remove 0.001 inch
(0.025 mm) on the final cut to meet the final
predetermined counterbore depth. This
ensures achieving a very fine machined
finish.
[212 CV] AUXILIARY
DRIVESHAFT
Description
All current production engines (effective
February 27, 1992, serial No. 2E1233) are
equipped with a “fast ratio” auxiliary driveshaft
assembly and oil pump assembly. This
arrangement raises oil pump speed to increase
operating oil pressure 25%. Refer to Auxiliary
Driveshaft Installation instructions in the ENGINE
ASSEMBLY section for ratio information.
Do not mix “fast ratio” and “standard ratio”
components. Serious damage may occur.
Inspection
1. Thoroughly clean auxiliary driveshaft.
5. Remove the tool from the cylinder bore.
a.Loosen the two cutter bit hold-down
capscrews (9) and rotate the cutter bit
adjusting screw (10) counterclockwise
until the cutter bit is retracted into the
cutter plate (13).
b.Remove the four machine hold-down
bolts (3) and special washers (4).
c.Remove the tool from the cylinder bore.
6. Follow steps 1 through 5 for the remaining
cylinders.
2. Inspect auxiliary driveshaft journals and gear
teeth for evidence of cracks, pitting, scoring
or severe wear. If any of these conditions
exist, replace the auxiliary driveshaft.
[212 LP] CONNECTING RODS
Description
Refer to Figure 5-2.
Early E7 engine connecting rods were machined
to give rod cap bottoms a contoured appearance.
Since mid-1992, connecting rod caps have had a
flat, machined bottom. The rods are the same in
strength and configuration, with the only
difference being the rod cap bottom surface
machining.
Page 5-5
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200 BENCH PROCEDURES
BEFORE MID 1992
(367GC4243M)
SINCE MID 1992
(367GC4255M)
CONTOUR MACHININGFLAT MACHINING
200282a
Figure 5-2 — Connecting Rod Identification
Refer to Figure 5-3.
A redesigned connecting rod assembly with an
added alignment sleeve feature was introduced
into E7 production engines in April 1995. This
connecting rod assembly has two alignment
sleeves (3), one sleeve in each capscrew hole of
the rod cap (1) to locate and align the cap and rod
thrust faces. These sleeves provide the best
alignment when sleeve gaps are positioned at a
location approximately 90 degrees to the tongue
or groove (2). The sleeve gaps must not be in line
with the tongue or groove.
Figure 5-3 — E7 Connecting Rod with Alignment
1. Rod cap
2. Bearing insert
Sleeves
3. Alignment sleeve
Page 5-6
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During initial production, part numbers were
stamped onto the through hole of the connecting
rod bearing cap. In later production, the part
number was forged into the I-beam of the rod.
Old-style connecting rods (without alignment
sleeves) and new-style connecting rods (with
alignment sleeves) may be intermixed in an
engine. However, the capscrews and alignment
sleeves are not interchangeable between the two
rod assemblies. The alignment sleeves will
physically fit into either of the connecting rod
assemblies, but the sleeve must be used in the
new-style 367GC4267M or M2 connecting rods
ONLY. The capscrews cannot be mixed. The
difference in the thread size between the two
rod assemblies is significant enough that the
14-mm threaded capscrews will not even engage
the 16-mm tapped hole in the old-style
(367GC4255M or M2) rod assemblies. The
16-mm threaded capscrew cannot be assembled
into the 14-mm tapped hole of the new-style
(367GC4267M or M2) connecting rod
assemblies.
It is essential to closely control the weight of
reciprocating parts. MACK E7 connecting rods
fall into two weight classes. Prior to mid-1996
production, the weight classes are identified by
an “M” number (M1 or M2) stamped onto the
connecting rod bearing cap. Effective with mid1996 production, the M2 connecting rod is no
longer stamped with this weight designation. The
M1 weight class rod will continue to be stamped
on the rod cap. When installing a single rod, or
less than a full set, examine removed rod for part
number and M number. Installing parts with the
same weight class is preferred.
200 BENCH PROCEDURES
Special Tools Required
앫Piston Pin Bushing Remover/Installer
J 37717
앫Piston Pin Burnishing Broach J 37718
앫Connecting Rod Fixture 945-6041
Inspection
앫Inspect connecting rods for nicks, cracks,
signs of overheating, bends or twisting that
can cause rod failure.
앫Inspect bolt holes for elongation or pulled
threads.
앫Check mating surfaces between rod and cap
for correct fit.
앫Inspect the crankshaft journal bearing
surface and wrist pin bushing.
If any of the above parts are suspected of being
faulty, replace the connecting rod.
If it is determined that the condition of any part or
component is questionable or is at the limit of
tolerance, throw it out; it may fail or become out of
tolerance after a short time in operation. It is costefficient to replace components when rebuilding.
Always use genuine MACK replacement parts.
Wrist Pin Repair
WRIST PIN BUSHING REMOVAL
If the wrist pin bushing is found to be out of
tolerance, it should be replaced.
Refer to Figure 5-4.
Connecting rods can be weighed to ensure using
proper weight class. Connecting rod weights
for each engine, within each weight class, should
not vary by more than 0.46 ounce (13.04 grams).
The maximum weight difference between the
heaviest possible M2 rod and the lightest
possible M1 rod is 0.83 ounce (23.53 grams).
To replace bushing:
1. Position rod in a press with piston pin
bushing remover/installer J 37717 inserted
into wrist pin bushing.
2. Press bushing out of rod.
Page 5-7
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200 BENCH PROCEDURES
Refer to Figure 5-5.
3. Position rod assembly in press with piston
pin burnishing broach J 37718.
Figure 5-4 — Wrist Pin Bushing Removal
WRIST PIN BUSHING INSTALLATION
The wrist pin bushing has a lubrication hole
through it. This hole MUST be aligned with rifledrilled hole in rod to allow oil flow to wrist pin. If
holes are not aligned, wrist pin, piston, and
connecting rod failure will result.
1. Position rod, bushing and piston pin bushing
remover/installer J 37717 in press, and
press bushing into rod.
2. Align hole in bushing with rifle-drilled hole in
rod.
Make certain that bushing is fully expanded in the
connecting rod bore or it will loosen in service.
Figure 5-5 — Burnishing Wrist Pin Bushing
4. Using a suitable lubricant, press broach
through bushing to expand bushing.
Refer to Figure 5-6.
5. After machining bushing, check connecting
rod for twisting or bending. Use Sweeney
connecting rod fixture 945-6041. Accessory
mandrel and plunger extension assemblies
for various engines are required for use with
this fixture, and are also available from the
Sweeney Company.
Page 5-8
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200 BENCH PROCEDURES
important for engine timing. The flywheel is
mounted to a flange at rear of crankshaft. Two
seals, one at the front and one at the rear,
prevent engine lubricating oil from leaking around
ends of the crankshaft.
Bearing caps are furnished with the crankcase
and support the crankshaft in true alignment.
Webs integral to the crankcase provide upper half
of main bearing supports. Removable caps
provide lower support. Capscrews hold the
caps in position. The bearing caps are not
interchangeable and each has a number stamped
on it which signifies its correct location and
alignment in the crankcase. The caps are
numbered 1 through 7, with No. 1 main bearing
cap in front of engine. The bearing inserts are
precision designed. Bearings are inserted
between the crankshaft and crankcase, and
between the crankshaft and bearing caps. Thrust
flanges to support thrust washers are located at
the center main bearing (No. 4).
200329a
Figure 5-6 — Connecting Rod Fixture
Maximum twist of connecting rod within 12 inches
(30.5 cm) is 0.010 inch (0.254 mm). The
maximum bend of connecting rod within
12 inches (30.5 cm) is 0.004 inch (0.102 mm).
Distances are center to center.
[212 HP] CRANKSHAFT
Description
The crankshaft is fully counterbalanced and
journals are induction-hardened. There are seven
main bearings. Thrust washers located at the
center main bearing (position No. 4) absorb fore
and aft end thrust. Crankshaft extension at
forward end carries the main drive gear, vibration
damper and accessory drive pulleys. The main
drive gear has a shrink fit and the vibration
damper hub has a press fit. The main drive gear
is keyed to the crankshaft and proper assembly is
Extreme care must be taken to guarantee
cleanliness of crankcase, crankshaft, and
bearings during servicing and after service has
been completed. Whenever possible, crankshaft
should be removed when bearings are being
installed in order to clean crankcase thoroughly.
All bearing surfaces must be free of grit and
burrs. Small particles of dust and dirt left between
crankshaft and bearings will cause rapid wear
and scoring of crankshaft journal and inserts. Any
foreign material left between bearings and
crankshaft bearing caps will cause distortion of
bearing and a reduction in operating clearance at
that point. The resulting frictional heat will cause
bearing material to melt away from steel backing
of bearing at that point. Such melted material will
create further hot spots until complete bearing
failure occurs. Anything that interferes with
operating clearance of any bearing, or proper
heat dissipation, affects bearing life. Cleanliness
cannot be overstressed.
Page 5-9
5-101.bk Page 10 Friday, March 17, 2006 11:05 AM
200 BENCH PROCEDURES
Inspection
If crankshaft journals are worn, out of round, or
tapered, order a new crankshaft or exchange kit
through the MACK parts system. New and
exchange crankshafts are available through
MACK distribution centers. When ordering an E7
crankshaft, be sure to note V-MAC or non V-MAC
application, since crankshafts are not the same.
Some crankshafts may have journals which are
0.002 inch (0.0508 mm) undersize. They are
marked by a streak of white paint adjacent to the
journal. Always check journals to ensure using
proper size bearing inserts.
[212 HA] Crankshaft Dowel Pin
Replacement
1. Inspect crankshaft journals for straightness,
out-of-round, taper, and surface finish.
2. Visually check crankshaft for any apparent
cracks, worn journals and damage to
threads, dowel or main drive gear.
3. Magnaflux the crankshaft. This process
requires special equipment and application
methods.
4. Using standard machinist inspection
practice, check crankshaft for straightness.
5. Measure crankshaft journals with a
micrometer. Measure each journal in two
locations, 90 degrees apart, and record
measurements.
6. Check measurements against specifications
in the FITS AND LIMITS section of this
manual.
Crankshaft regrinding by anyone other than Mack
Trucks, Inc. is NOT recommended due to the
tight control required on maintaining geometrical
tolerances, and the hardened characteristics of
the crankshaft journals and journal fillets.
The “diamond” locating dowel pins used for
installing flywheel to crankshaft have been
replaced by blade-style locating dowel pins. The
diamond pins were dual diameter-type pins.
There was a smaller diameter at the round end
than at the diamond end. There are no changes
in the size of the hole in the flywheel. However,
the crankshaft will have larger holes to accept
blade-style pins.
The blade-type dowel pin was introduced in May
1992, starting with serial No. 2K. You must use
the dowel size that is appropriate for the
crankshaft. (Service old with old, and new with
new.)
Effective May 1993, all E7 engine crankshafts are
equipped with flywheel-to-crankshaft dowel
183GC238 installed in the rear flange. Prior to
this date, only V-MAC engine crankshafts had the
183GC238 dowel. Crankshafts in mechanically
governed engines did not have a dowel pin hole
in the rear flange. However, all E7 engine
crankshafts have always had a crankshaft
manufacturing locator hole in the rear flange. This
hole is approximately 1/2 inch (12.7 mm) in
diameter and 3/8 inch (9.52 mm) deep, and is
used only in the manufacturing process.
If the crankshaft is not serviceable, both new and
reground crankshafts are available through the
MACK Parts Distribution Centers.
If crankshaft main journals or rod journals are not
a standard size, be sure to use properly sized
bearing inserts. Bearing inserts are marked with a
“P” which follows the part number, and is
stamped on the back side of the bearing insert.
For example, if a journal is 0.010 inch (0.254 mm)
undersize, a 0.010-inch undersize bearing is
required and will be stamped “P10”.
Page 5-10
The flywheel locating dowel hole — located
directly opposite the manufacturing locator hole —
is approximately 9/16 inch (14.29 mm) in
diameter by 7/8 inch (22.23 mm) deep in
crankshafts made since May 1992 using dowel
183GC238. V-MAC crankshafts made prior to
May 1992 have a flywheel locating dowel hole
1/2 inch (12.7 mm) in diameter by 7/8 inch
(22.23 mm) deep for dowel 183GC221.
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