length CHRYSLER VOYAGER 1996 User Guide
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Page 574 of 1938

kit 6680. Pull on the wire to remove the terminal
from the connector (Fig. 14) (Fig. 15).
(5) Reset the terminal locking tang, if it has one.
(6) Insert the removed wire in the same cavity on
the repair connector.
(7) Repeat steps four through six for each wire in
the connector, being sure that all wires are inserted
into the proper cavities. For additional connector pin-
out identification, refer to the wiring diagrams.
(8) Insert the connector locking wedge into the
repaired connector, if required.
(9)
Connect connector to its mating half/component.
(10) Connect battery and test all affected systems.
CONNECTOR AND TERMINAL REPLACEMENT
(1) Disconnect battery.
(2) Disconnect the connector (that is to be
repaired) from its mating half/component.
(3) Cut off the existing wire connector directly
behind the insulator. Remove six inches of tape from
the harness.
(4) Stagger cut all wires on the harness side at
1/2 inch intervals (Fig. 16).(5) Remove 1 inch of insulation from each wire on
the harness side.
(6) Stagger cut the matching wires on the repair
connector assembly in the opposite order as was done
on the harness side of the repair. Allow extra length
for soldered connections. Check that the overall
length is the same as the original (Fig. 16).
(7) Remove 1 inch of insulation from each wire.
(8) Place a piece of heat shrink tubing over one
side of the wire. Be sure the tubing will be long
enough to cover and seal the entire repair area.
(9) Spread the strands of the wire apart on each
part of the exposed wires.
(10) Push the two ends of wire together until the
strands of wire are close to the insulation.
(11) Twist the wires together.
(12) Solder the connection together using rosin
core type solder only.Do not use acid core solder.
(13) Center the heat shrink tubing over the joint
and heat using a heat gun. Heat the joint until the
tubing is tightly sealed and sealant comes out of both
ends of the tubing
(14) Repeat steps 8 through 13 for each wire.
(15) Re-tape the wire harness starting 1-1/2 inches
behind the connector and 2 inches past the repair.
(16) Re-connect the repaired connector.
(17) Connect the battery, and test all affected sys-
tems.
TERMINAL/CONNECTOR REPAIR- AUGAT
CONNECTORS
(1) Disconnect battery.
(2) Disconnect the connector from its mating half/
component.
(3) Push down on the yellow connector locking tab
to release the terminals (Fig. 17).
(4) Using special tool 6932, push the terminal to
remove it from the connector (Fig. 18).
Fig. 14 Terminal Removal
Fig. 15 Terminal Removal Using Special Tool
Fig. 16 Stagger Cutting Wires
8W - 01 - 12 8W-01 GENERAL INFORMATIONNS/GS
SERVICE PROCEDURES (Continued)
Page 575 of 1938

(5) Repair or replace the connector or terminal as
necessary.
(6) When re-assembling the connector, the locking
wedge must be placed in the locked position to pre-
vent terminal push out.
TERMINAL REPLACEMENT
(1) Disconnect battery.
(2) Disconnect the connector being repaired from
its mating half. Remove connector locking wedge, if
required (Fig. 19).
(3) Remove connector locking wedge, if required
(Fig. 19).
(4) Position the connector locking finger away from
the terminal using the proper pick from special tool
kit 6680. Pull on the wire to remove the terminal
from the connector (Fig. 20) (Fig. 21).
(5) Cut the wire 6 inches from the back of the con-
nector.
(6) Remove 1 inch of insulation from the wire on
the harness side.(7) Select a wire from the terminal repair assem-
bly that best matches the color wire being repaired.
(8) Cut the repair wire to the proper length and
remove 1 inch of insulation.
Fig. 17 Augat Connector Repair
Fig. 18 Using Special Tool 6932
Fig. 19 Connector Locking Wedge Tab (Typical)
Fig. 20 Terminal Removal
Fig. 21 Terminal Removal Using Special Tool
NS/GS8W-01 GENERAL INFORMATION 8W - 01 - 13
SERVICE PROCEDURES (Continued)
Page 1064 of 1938

2.4L ENGINE
INDEX
page page
DESCRIPTION AND OPERATION
ENGINE COMPONENTS.................. 15
ENGINE IDENTIFICATION................. 14
ENGINE LUBRICATION SYSTEM............ 14
DIAGNOSIS AND TESTING
CHECKING ENGINE OIL PRESSURE......... 16
SERVICE PROCEDURES
CRANKSHAFT END PLAY................. 20
FITTING CONNECTING ROD BEARINGS..... 18
FITTING MAIN BEARINGS................. 19
FITTING PISTON RINGS.................. 16
FITTING PISTONS....................... 16
VALVE SERVICE RECONDITION............ 21
REMOVAL AND INSTALLATION
BALANCE SHAFTS CARRIER ASSEMBLY..... 30
CAMSHAFT FOLLOWER.................. 30
CAMSHAFT OIL SEALÐFRONT............. 41
CAMSHAFT............................ 28
CRANKSHAFT OIL SEALÐFRONT........... 42
CRANKSHAFT OIL SEALÐREAR............ 43
CRANKSHAFT.......................... 46
CYLINDER HEAD COVER................. 28
CYLINDER HEAD........................ 34
ENGINE ASSEMBLY...................... 26
ENGINE MOUNTÐFRONT................. 23
ENGINE MOUNTÐLEFT.................. 24
ENGINE MOUNTÐREAR.................. 25
ENGINE MOUNTÐRIGHT................. 24HYDRAULIC LASH ADJUSTER.............. 33
OILFILTER ............................ 47
OILPAN ............................... 45
OIL PUMP............................. 47
PISTON AND CONNECTING ROD........... 49
STRUCTURAL COLLAR................... 25
TIMING BELT COVER.................... 37
TIMING BELT TENSIONER ASSEMBLY....... 40
TIMING BELT........................... 37
VALVE SPRINGS AND
VALVE SEALS IN VEHICLE............... 33
VALVES AND VALVE SPRINGS............. 35
VIBRATION DAMPER.................... 36
DISASSEMBLY AND ASSEMBLY
OIL PUMP............................. 50
CLEANING AND INSPECTION
OIL PUMP............................. 52
CRANKSHAFT.......................... 52
CYLINDER BLOCK....................... 54
CYLINDER HEAD........................ 51
VALVE AND VALVE SPRING................ 51
ADJUSTMENTS
ENGINE MOUNTS....................... 54
SPECIFICATIONS
2.4L ENGINE........................... 55
TORQUE CHART 2.4L.................... 57
SPECIAL TOOLS
2.4L ENGINE........................... 58
DESCRIPTION AND OPERATION
ENGINE IDENTIFICATION
The engine identification number is located on the
rear of the cylinder block (Fig. 1).
ENGINE LUBRICATION SYSTEM
OIL PAN
A structural die cast aluminum oil pan provides
lower engine protection as well as serving as the
engine oil reservoir. Oil pan is attached to block and
sealed with a gasket. The oil pickup tube has a
strainer and cover.
PRESSURE LUBRICATION
Oil drawn up through the pickup tube is pressur-
ized by the pump and routed through the full flow fil-
ter to the main oil gallery running the length of thecylinder block. Oil pickup, pump and check valve pro-
vide oil flow to the main oil gallery.
MAIN/ROD BEARINGS
A diagonal hole in each bulkhead feeds oil to each
main bearing. Drilled passages within the crankshaft
route oil from main bearing journals to connecting
rod journals.
CAMSHAFT/HYDRAULIC LASH ADJUSTERS
A vertical hole at the number five bulkhead routes
pressurized oil through a restrictor up past a cylin-
der head bolt to an oil gallery running the length of
the cylinder head. The camshaft journals are par-
tially slotted to allow a predetermined amount of
pressurized oil to pass into the bearing cap cavities
with small holes directed to spray lubricate the cam-
shaft lobes.
9 - 14 2.4L ENGINENS
Page 1066 of 1938

sealing and a chrome plated taper faced intermediate
ring for additional cylinder pressure control. There
are also standard oil control rings.
CYLINDER HEAD:Features a Dual Over Head
Camshaft (DOHC) 4 valves per cylinder cross flow
design. The valves are arranged in two inline banks,
with the ports of the bank of two intake valves per
cylinder facing toward the radiator side of engine
and ports of the bank of two exhaust valves per cyl-
inder facing toward the dash panel. Incorporates
powder metal valve guides and seats. Integral oil gal-
leys within the cylinder head supplies oil to the
hydraulic lash adjusters, camshaft and valve mecha-
nisms.
CAMSHAFTS:The nodular iron camshafts have
six bearing journals and 2 cam lobes per cylinder.
Flanges at the rear journals control camshaft end
play. Provision for cam position sensor is located on
the intake camshaft at the rear of cylinder head. A
hydrodynamic oil seal is used for oil control at the
front of the camshaft.
VALVES:4 valves per cylinder are actuated by
roller cam followers which pivot on stationary
hydraulic lash adjusters. All valves have 6 mm diam-
eter chrome plated valve stems. The valve sizes are
34.8 mm (1.370 inch.) diameter intake valves and
30.5 mm (1.20 inch.) diameter exhaust valves. Viton
rubber valve stem seals are integral with the spring
seats. Valve springs, spring retainers, and locks are
conventional.
INTAKE MANIFOLD:The intake manifold is a
two piece aluminum casting, attached to the cylinder
head with ten screws. This long branch fan design
enhances low and midspeed torque, while minimizing
undesirable inlet noise.
EXHAUST MANIFOLD:The exhaust manifold is
made of cast iron for strength and high tempera-
tures.
ENGINE LUBRICATION:Refer to Group 0
Lubrication and Maintenance for recommended oil to
be used in various engine application. System is full
flow filtration, pressure feed type. The oil pump is
mounted in the front engine cover and driven by the
crankshaft. Pressurized oil is then routed through
the main oil gallery, running the length of the cylin-
der block, supplying main and rod bearings with fur-
ther routing. Pistons are lubricated from rod bearing
throw off and lubricating slots on the connecting rod
assemblies. Camshaft and valve mechanisms are
lubricated from a full length cylinder head oil gallery
supplied from the crankcase main oil gallery.DIAGNOSIS AND TESTING
CHECKING ENGINE OIL PRESSURE
(1) Remove oil pressure sending unit and install
gauge assembly C-3292.
(2) Run engine until thermostat opens.
CAUTION: If oil pressure is 0 at idle, Do Not Run
engine at 3000 RPM
(3) Oil Pressure:Curb Idle25 kPa (4 psi) mini-
mum3000 RPM170/550 kPa (25/80 psi).
(4) If oil pressure is 0 at idle. Shut off engine,
check for pressure relief valve stuck open or a
clogged oil pickup screen.
SERVICE PROCEDURES
FITTING PISTONS
Piston and cylinder wall must be clean and dry.
Piston diameter should be measured 90 degrees to
piston pin about 14 mm (9/16 inch.) from the bottom
of the skirt as shown in (Fig. 3). Cylinder bores
should be measured halfway down the cylinder bore
and transverse to the engine crankshaft center line
shown in (Fig. 2). Refer to Cylinder Bore and Piston
Specification Chart.
Correct piston to bore clearance must be estab-
lished in order to assure quiet and economical oper-
ation.
Chrysler engines use pistons designed specifically
for each engine model. Clearance and sizing locations
vary with respect to engine model.
NOTE: Pistons and cylinder bores should be mea-
sured at normal room temperature, 70ÉF (21ÉC).
FITTING PISTON RINGS
(1) Wipe cylinder bore clean. Insert ring and push
down with piston to ensure it is square in bore. The
ring gap measurement must be made with the ring
positioning at least 12 mm (0.50 inch) from bottom of
cylinder bore. Check gap with feeler gauge (Fig. 4).
Refer to specification in Piston Ring Specification
Chart.
(2) Check piston ring to groove side clearance (Fig.
5). Refer to specification in Piston Ring Specification
Chart.
9 - 16 2.4L ENGINENS
DESCRIPTION AND OPERATION (Continued)
Page 1071 of 1938

OPTIONAL CRANKSHAFT END PLAY CHECK
(1) Move crankshaft all the way to the rear of its
travel using a lever inserted between a main bearing
cap and a crankshaft cheek, using care not to dam-
age any bearing surface.DO NOTloosen main bear-
ing cap.
(2) Use a feeler gauge between number three
thrust bearing and machined crankshaft surface to
determine end play.
VALVE SERVICE RECONDITION
VALVE REMOVAL
(1) With cylinder head removed, compress valve
springs using Special Tool C-3422-B or equivalent.
(2) Remove valve retaining locks, valve spring
retainers, valve stem seals and valve springs.
(3) Before removing valves,remove any burrs
from valve stem lock grooves to prevent dam-
age to the valve guides.Identify valves to insure
installation in original location.
VALVE INSPECTION
(1) Clean valves thoroughly and discard burned,
warped and cracked valves.
(2) Measure valve stems for wear. Measure stem
about 60 mm beneath the valve lock grooves.
(3) If valve stems are worn more than 0.05 mm
(0.002 in.), replace valve.
VALVE GUIDES
(1) Remove carbon and varnish deposits from
inside of valve guides with a reliable guide cleaner.
(2) Using a small hole gauge and a micrometer,
measure valve guides in 3 places top, middle and bot-
tom (Fig. 15). Refer to Valve Guide Specification
Chart. Replace guides if they are not within specifi-
cation.
(3) Check valve guide height (Fig. 16).
TESTING VALVE SPRINGS
(1) Whenever valves have been removed for inspec-
tion, reconditioning or replacement, valve springs
should be tested. As an example, the compression
length of the spring to be tested is 33.34 mm (1 5/16inches). Turn tool table until surface is in line with
the 33.34 mm (1 5/16 in.) mark on the threaded stud
and the zero mark on the front. Place spring over
stud on the table and lift compressing lever to set
tone device (Fig. 17). Pull on torque wrench until
ping is heard. Take reading on torque wrench at this
instant. Multiply this reading by two. This will give
the spring load at test length. Fractional measure-
ments are indicated on the table for finer adjust-
ments. Discard the springs that do not meet
specifications. The Following specifications apply to
both intake and exhaust valve springs;
²Valve Closed Nominal TensionÐ 76 lbs. @ 38.0
mm (1.50 in.)
²Valve Open Nominal TensionÐ 136 lbs. @ 29.75
mm (1.17 in.)
(2) Inspect each valve spring for squareness with a
steel square and surface plate, test springs from both
ends. If the spring is more than 1.5 mm (1/16 inch)
out of square, install a new spring.
REFACING VALVES AND VALVE SEATS
(1) The intake and exhaust valve seats and valve
face have a 45 and a 45 1/2 degree angles.
Fig. 15 Checking Wear on Valve GuideÐTypical
VALVE GUIDE SPECIFICATION CHART
Valve Guide Diameter
Intake and
Exhaust Valve:5.975 - 6.000 mm
(0.2352 - 0.2362 in.)
Valve Guide Clearance
New Service
Limit
Intake Valve: 0.048 - 0.066 mm
(0.0018 - 0.0025 in.)
0.25 mm
(0.010 in.)
Exhaust Valve: 0.0736 - 0.094 mm
(0.0029 - 0.0037 in.)
Fig. 16 Valve Guide Height
NS2.4L ENGINE 9 - 21
SERVICE PROCEDURES (Continued)
Page 1072 of 1938

(2) Inspect the remaining margin after the valves
are refaced (Fig. 18). Intake valves with less than 1.2
mm (3/64 inch.) margin and Exhaust valves with less
than 0.9 mm (1/32 inch.) margin should be discarded.
(3) When refacing valve seats, it is important that
the correct size valve guide pilot be used for reseat-
ing stones. A true and complete surface must be
obtained.
(4) Measure the concentricity of valve seat and
valve guide using a valve seat runout dial indicator.
Total runout should not exceed. 0.051 mm (0.002
inch.) (total indicator reading).
(5) Inspect the valve seat with Prussian blue to
determine where the valve contacts the seat. To do
this, coat valve seatLIGHTLYwith Prussian blue
then set valve in place. Rotate the valve with light
pressure. If the blue is transferred to the center of
valve face, contact is satisfactory. If the blue is trans-
ferred to top edge of the valve face, lower valve seat
with a 15 degrees stone. If the blue is transferred to
the bottom edge of valve face raise valve seat with a
65 degrees stone.²Intake valve seat diameter is 34.37 34.63 mm
(1.158 1.363 inch.)
²Exhaust valve seat diameter is 29.37 29.63 mm
(1.156 1.166 inch.)
(6) Valve seats which are worn or burned can be
reworked, provided that correct angle and seat width
are maintained. Otherwise the cylinder head must be
replaced.
(7) When seat is properly positioned the width of
intake and exhaust seats should be 0.9 to 1.3 mm
(0.35 to 0.051 inch.) (Fig. 19).
(8) Check valve tip height dimensions A after
grinding the valve seats or faces (Fig. 20). Grind
valve tip to 47.99 mm (1.889 in.) for exhaust valve
and 48.04 mm (1.891 in.) for intake valve when
installed in the head. The valve tip chamfer may
Fig. 17 Testing Valve Springs
Intake and Exhaust Valves
VALVE SPECIFICATION CHART
Face Angle
Intake and Exhaust: 44.5É-45É
Head Diameter
Intake: 34.67 - 34.93 mm
(1.364 - 1.375 in.)
Exhaust: 30.37 - 30.63 mm
(1.195 - 1.205 in.)
Length (Overall)
Intake: 112.76 - 113.32 mm
(4.439 - 4.461 in.)
Exhaust: 109.59 - 110.09 mm
(4.314 - 4.334 in.)
Stem Diameter
Intake: 5.934 - 5.952 mm
(0.2337 - 0.2344 in.)
Exhaust: 5.906 - 5.924 mm
(0.2326 - 0.2333 in.)
Valve Margin
Intake: 1.285 - 1.615 mm
(0.050 - 0.063 in.)
Exhaust: 0.985 - 1.315 mm
(0.038 - 0.051 in.)
Fig. 18 Refacing Intake and Exhaust Valves
9 - 22 2.4L ENGINENS
SERVICE PROCEDURES (Continued)
Page 1103 of 1938

between rotors and the straightedge, replace pump
assembly (Fig. 106),ONLYif rotors are in specs.
(8) Inspect oil pressure relief valve plunger for
scoring and free operation in its bore. Small marks
may be removed with 400 grit wet or dry sandpaper.
(9) The relief valve spring has a free length of
approximately 60.7 mm (2.39 inches) it should test
between 18 and 19 pounds when compressed to 40.5
mm (1.60 inches). Replace spring that fails to meet
specifications.
(10) If oil pressure is low and pump is within
specifications, inspect for worn engine bearings or
other reasons for oil pressure loss.
Fig. 102 Measuring Outer Rotor Thickness
Fig. 103 Measuring Inner Rotor Thickness
Fig. 104 Measuring Outer Rotor Clearance in
Housing
Fig. 105 Measuring Clearance Between Rotors
Fig. 106 Measuring Clearance Over Rotors
NS2.4L ENGINE 9 - 53
CLEANING AND INSPECTION (Continued)
Page 1104 of 1938

CYLINDER BLOCK
(1) Clean cylinder block thoroughly and check all
core hole plugs for evidence of leaking.
(2) If new core plugs are installed, refer to Engine
Core Plugs outlined in this section.
(3) Examine block and cylinder bores for cracks or
fractures.
CYLINDER BORE INSPECTION
The cylinder walls should be checked for out-of-
round and taper with Tool C119 (Fig. 107). The cyl-
inder bore out-of-round is 0.050 mm (0.002 in.)
maximum and cylinder bore taper is 0.051 mm (0.002
in.) maximum. If the cylinder walls are badly scuffed
or scored, the cylinder block should be replaced, and
new pistons and rings fitted.
Measure the cylinder bore at three levels in direc-
tions A and B (Fig. 107). Top measurement should be
10 mm (3/8 in.) down and bottom measurement
should be 10 mm (3/8 in.) up from bottom of bore.
Refer to Cylinder Bore and Piston Specification
Chart.
ADJUSTMENTS
ENGINE MOUNTS
ENGINE MOUNT INSULATOR ADJUSTMENT
(1) Remove the load on the engine motor mounts
by carefully supporting the engine and transmission
assembly with a floor jack.
(2) Loosen the right engine mount insulator verti-
cal fastener and the fore and aft fasteners, and the
front engine mount bracket to front crossmember
screws.
(3) Pry the engine right or left as required to
achieve the proper drive shaft assembly length. Refer
to Group 2, Suspension and Driveshafts for drive-
shaft identification and related assembly length mea-
suring.
(4) Tighten engine mounts and fasteners in the
following order:
(a) Right engine mount insulator vertical bolts
to 102 N´m (75 ft. lbs.) and the fore and aft bolts to
150 N´m (110 ft. lbs.).
(b) Front engine mount screws to 54 N´m (40 ft.
lbs.) the clearance between the snubbers and the
engine should be 2 mm (0.078 inch.) each side.
(c) Left engine mount through bolt to 75 N´m (55
ft. lbs.).
(5) Recheck driveshaft length.
Fig. 107 Checking Cylinder Bore Size
CYLINDER BORE AND PISTON
SPECIFICATION CHART
Standard Bore Maximum Out-
Of-RoundMaximum-
Taper
87.5 mm 0.051 mm 0.051 mm
(3.445 in.) (0.002 in.) (0.002 in.)
Standard Piston Size
87.450 - 87.468 mm (3.4434 - 3.4441 in.)
Piston To Bore Clearance
0.024 - 0.057 mm (0.0009 - 0.0022 in.)
Measurements taken at Piston Size Location.
9 - 54 2.4L ENGINENS
CLEANING AND INSPECTION (Continued)
Page 1105 of 1938

SPECIFICATIONS
2.4L ENGINE
Type....................In-Line OHV, DOHC
Number of Cylinder.......................4
Bore.....................87.5 mm (3.445 in.)
Stroke....................101 mm (3.976 in.)
Compression Ratio......................9.4:1
Displacement.......2.4 Liters (148 Cubic Inches)
Firing Order.......................1,3,4,2
Compression Pressure...........1172-1551 kPa
(170-225 psi)
Maximum Variation Between Cylinder......25%
Lubrication. . . .Pressure Feed-Full Flow Filtration
(Direct Crankshaft Driven Pump)
Cylinder Block
Cylinder Bore Diameter. . . .87.4924 - 87.5076 mm
(3.4446 - 3.4452 in.)
Out-of-Round (Max.)........0.051 mm (0.002 in.)
Taper (Max.)..............0.051 mm (0.002 in.)
Pistons
Clearance at 14 mm (9/16 in.)
From Bottom of Skirt.........0.024 - 0.057 mm
(0.0009 - 0.0022 in.)
Weight......................332 - 346 grams
(11.85 - 12.20 oz.)
Top Land Clearance
(Diametrical)................0.614 - 0.664 mm
(0.024 - 0.026 in.)
Piston Length.............60.30 mm (2.374 in.)
Piston Ring Groove Depth
No.1........4.640 - 4.784 mm (0.182 - 0.188 in.)
No.2........4.575 - 4.719 mm (0.180 - 0.185 in.)
No.3........4.097 - 4.236 mm (0.161 - 0.166 in.)
Piston Pins
Clearance in Piston...........0.005 - 0.018 mm
In Rod (Interference)..........0.018 - 0.043 mm
(0.0007 - 0.0017 in.)
Diameter.................21.998 - 22.003 mm
(0.8660 - 0.8662 in.)
End Play.............................None
Length.....................72.75 - 73.25 mm
(2.864 - 2.883 in.)
Piston Ring Gap
Top Compression Ring...........0.25 - 0.51 mm
(0.0098 - 0.020 in.)
2nd Compression Ring...........0.23 - 0.48 mm
(0.009 - 0.018 in.)
Oil Control (Steel Rails).........0.25 - 0.64 mm
(0.0098 - 0.025 in.)
Piston Ring Side Clearance
Top and Second
Compression Rings...........0.030 - 0.080 mm
(0.0011 - 0.0031 in.)Oil Ring (Pack)..............0.012 - 0.178 mm
(0.0004 - 0.0070 in.)
Piston Ring Width
Compression Rings.............1.47 - 1.50 mm
(0.057 - 0.059 in.)
Oil Ring (Pack)................2.72 - 2.88 mm
(0.107 - 0.1133 in.)
Connecting Rod
Bearing Clearance............0.025 - 0.071 mm
(0.0009 - 0.0027 in.)
Piston Pin Bore Diameter......20.96 - 20.98 mm
(0.8252 - 0.8260 in.)
Large End Bore Diameter. . . .53.007 - 52.993 mm
(2.0868 - 2.0863)
Side Clearance..............0.013 - 0.0150 mm
(0.0051 - 0.0150 in.)
Total Weight (Less Bearing).........565.8 grams
(19.96 oz.)
Crankshaft
Connecting Rod
Journal Diameter..........49.984 - 50.000 mm
(1.967 - 1.9685 in.)
Out-of-Round (Max.)......0.0035 mm (0.0001 in.)
Taper (Max.)............0.0038 mm (0.0001 in.)
Main Bearing Diametrical
Clearance No.1-5...........0.018 - 0.058 mm
(0.0007 - 0.0023 in.)
End Play.....................0.09 - 0.24 mm
(0.0035 - 0.0094 in.)
Main Bearing Journals
Diameter.................59.992 - 60.008 mm
(2.361 - 2.3625 in.)
Out-of-Round (Max.)......0.0035 mm (0.0001 in.)
Taper (Max.)...............0.0038 (0.0001 in.)
Hydraulic Lash Adjusters
Body Diameter.............15.901 - 15.913 mm
(0.626 - 0.6264 in.)
Plunger Travel Minimum (Dry)..........3.0 mm
(0.118 in.)
Camshaft
Bearing Bore
Diameters No. 1±6..........26.020 - 26.041 mm
(1.024 - 1.025 in.)
Diametrical Bearing Clearance . .0.069 - 0.071 mm
(0.0027 - 0.003 in.)
End Play...................0.050 - 0.170 mm
(0.0019 - 0.0066 in.)
Bearing Journal
Diameter No. 1±6..........25.951 - 25.970 mm
(1.021 - 1.022 in.)
Lift (Zero Lash) Intake.......8.25 mm (0.324 in.)
Lift (Zero Lash) Exhaust.....6.52 mm (0.256 in.)
Valve Timing ± Intake Valve
Closes (ABDC)..........................51É
Opens (BTDC)...........................1É
NS2.4L ENGINE 9 - 55
Page 1106 of 1938

Duration.............................232É
Valve Timing ± Exhaust Valve
Closes (ATDC)...........................8É
Opens (BBDC)..........................52É
Duration.............................240É
Valve Timing
Valve Overlap...........................9É
Cylinder Head
Material.....................Cast Aluminum
Gasket Thickness (Compressed)........1.15 mm
(0.045 in.)
Cylinder Head Valve Seat
Angle.................................45É
Runout (Max.).............0.050 mm (0.002 in.)
Width (Finish) Intake and Exhaust. . .0.9 - 1.3 mm
(0.035 - 0.051 in.)
Guide Bore Diameter (Std).......11.0-11.02 mm
(0.4330 - 0.4338 in.)
Finish Guide Bore ID..........5.975 - 6.000 mm
(0.235 - 0.236 in.)
Valves
Face Angle......................44-1/2É - 45É
Head Diameter Intake.........34.67 - 34.93 mm
(1.364 - 1.375 in.)
Head Diameter Exhaust.......30.37 - 30.63 mm
(1.195 - 1.205 in.)
Length±Intake (Overall)......112.76 - 113.32 mm
(4.439 - 4.461 in.)
Length±Exhaust (Overall). . . .109.59 - 110.09 mm
(4.314 - 4.334 in.)
Valve Margin±Intake..........1.285 - 1.615 mm
(0.050 - 0.063 in.)
Valve Margin±Exhaust........0.985 - 1.315 mm
(0.038 - 0.051 in.)
Valve Stem Tip Height±Intake........48.04 mm
(1.891 in.)Valves
Valve Stem Tip Height±Exhaust.......47.99 mm
(1.889 in.)
Stem Diameter±Intake........5.934 - 5.952 mm
(0.234 - 0.234 in.)
Stem Diameter±Exhaust.......5.906 - 5.924 mm
(0.233 - 0.233 in.)
Stem-to-Guide
Clearance±Intake............0.048 - 0.066 mm
(0.0018 - 0.0025 in.)
Stem-to-Guide
Clearance±Exhaust..........0.0736 - 0.094 mm
(0.0029 - 0.0037 in.)
Max. Allowable Stem-to-Guide
Clearance±Intake and Exhaust.......0.025 mm
(0.010 in.)
Valve Springs
Free Length (Approx.).......48.4 mm (1.905 in.)
Spring Tension
(Valve Closed).........338 N620 N @ 38.0 mm
(75.98 lbs.64.5 lbs. @ 1.496 in.)
Spring Tension
(Valve Open).........607 N630 N @ 29.75 mm
(136 lbs.67 @ 1.172 in.)
Number of Coils........................7.82
Wire Diameter.............3.86 mm (0.151 in.)
Installed Spring Height.....38.00 mm (1.496 in.)
Oil Pump
Clearance Over Rotors (Max.). .0.10 mm (0.004 in.)
Cover Out-of-Flat (Max.).....0.025 mm (0.001 in.)
Inner Rotor Thickness (Min.) . .9.40 mm (0.370 in.)
Outer Rotor (Oil Pump)
Clearance (Max.)...........0.39 mm (0.015 in.)
Diameter (Min.)...........79.95 mm (3.148 in.)
Thickness (Min.)............9.40 mm (0.370 in.)
Tip Clearance Between Rotors (Max.). . . .0.20 mm
(0.008 in.)
Oil Pressure
At Curb Idle Speed*.............25kPa(4psi)
At 3000 rpm.........170 - 550 kPa (25 - 80 psi)
CAUTION: * If pressure is ZERO at curb Idle, DO
NOT run engine at 3,000 rpm.
9 - 56 2.4L ENGINENS
SPECIFICATIONS (Continued)