Piston SUZUKI SWIFT 2000 1.G SF310 Service Owner's Manual

6A1
ENGINE MECHANICAL (G13B, 1-CAM 16-VALVES ENGINE) 6A1-1
SECTION 6A1
ENGINE MECHANICAL
(G13B, 1-CAM 16-VALVES ENGINE)
WARNING:
For vehicles equipped with Supplement Restraint (Air Bag) System:

Service on and around the air bag system components or wiring must be performed only by an autho-
rized SUZUKI dealer. Refer to “Air Bag System Components and Wiring Location View” under “Gener-
al Description” in air bag system section in order to confirm whether you are performing service on
or near the air bag system components or wiring. Please observe all WARNINGS and “Service Precau-
tions” under “On-Vehicle Service” in air bag system section before performing service on or around
the air bag system components or wiring. Failure to follow WARNINGS could result in unintentional
activation of the system or could render the system inoperative. Either or these two conditions may
result in severe injury.

Technical service work must be started at least 90 seconds after the ignition switch is turned to the
“LOCK” position and the negative cable is disconnected from the battery. Otherwise, the system may
be activated by reserve energy in the Sensing and Diagnostic Module (SDM).
CONTENTS
GENERAL DESCRIPTION6A1- 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Engine6A1- 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Engine Lubrication6A1- 3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Cylinder Block6A1- 4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Crankshaft and Main Bearings 6A1- 4. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Pistons, Rings, Piston Pins and Connecting Rods 6A1- 4. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Cylinder Head and Value Train 6A1- 4. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
ON VEHICLE SERVICE6A1- 5 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Compression Check6A1- 5 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Engine Vacuum Check6A1- 6 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Oil Pressure Check6A1- 7 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Valve Lash (Clearance)6A1- 9 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Air Cleaner Element6A1-11 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Air Cleaner Outlet Hose6A1-12 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Cylinder Head Cover6A1-13 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Throttle Body and Intake Manifold 6A1-14. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Exhaust Manifold6A1-17 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Timing Belt and Belt Tensioner 6A1-19. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Oil Pan and Oil Pump Strainer 6A1-25. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Oil Pump6A1-28 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Rocker Arms, Rocker Arm Shaft and Camshaft 6A1-33. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Valves and Cylinder Head6A1-41 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Piston, Piston Rings, Connecting Rods and Cylinders 6A1-54. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
UNIT REPAIR OVERHAUL6A1-64 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Engine Assembly6A1-64 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Main Bearings, Crankshaft and Cylinder Block 6A1-68. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
SPECIAL TOOLS6A1-80 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
REQUIRED SERVICE MATERIALS6A1-81 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
TIGHTENING TORQUE SPECIFICATIONS6A1-82 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
NOTE:
For what each abbreviation stands for (i.e., full term), refer to SECTION 0A.

ENGINE MECHANICAL (G13B, 1-CAM 16-VALVES ENGINE) 6A1-3
ENGINE LUBRICATION
The oil pump is of a trochoid type, and mounted on crankshaft at crankshaft pulley side.
Oil is drawn up through oil pump strainer and passed through pump to oil filter.
The filtered oil flows into two paths in cylinder block. In one path, oil reaches crankshaft journal bearings.
Oil from crankshaft journal bearings is supplied to connecting rod bearings by means of intersecting passages
drilled in crankshaft, and then injected from a small hole provided on big end of connecting rod to lubricate piston,
rings, and cylinder wall.
In another path, oil goes up to cylinder head and lubricates camshaft journals, rocker arms, camshaft, etc., passing
through oil gallery in rocker arm shaft.
An oil relief valve is provided on oil pump. This valve starts relieving oil pressure when the pressure comes over
about 400 kPa (4.0 kg / cm
2, 56.9 psi). Relieved oil drains back to oil pan.

1. Rocker arm shaft
2. Rocker arm (EX)
3. Intake valve
4. Exhaust valve5. Rocker arm (IN)
6. Camshaft
7. Clip
8. PivotEx In
CYLINDER BLOCK
The cylinder block is made of cast aluminum alloy and
has 4 cylinders arranged “In-Line”. A cylindrical cast
iron sleeve is installed in each cylinder.
CRANKSHAFT AND MAIN
BEARINGS
A monoblock casting crankshaft is supported by
5 main bearings which are of precision insert type.
Four crank pins on the crankshaft are positioned 180
apart.
PISTONS, RINGS, PISTON PINS AND
CONNECTING RODS
The piston is cast aluminum alloy, and has two com-
pression rings and one oil ring.
Among two compression rings (top and 2nd rings),
the outer surface of the top ring is treated with hard
chromium for improvement in abrasion resistance.
The oil ring consists of two rails and one spacer. The
piston pin is offset 0.5 mm towards the major thrust
side.This allows a gradual change in thrust pressure
against the cylinder wall as the piston travels its path.
Pins, made of chromium steel, have a floating fit in the
pistons and in the connecting rods. The connecting
rods are made of forged steel, and the rod bearings
are of precision insert type.
CYLINDER HEAD AND VALVE TRAIN
The cylinder head is made of aluminum casting. The
supporting part of the camshaft is an independent cap
type. The combustion chamber has 4 valves and uses
the center plug type pent roof shape for higher intake
and exhaust efficiency.
As the intake side rocker arm is end pivot type, it
swings according to the camshaft movement to open
and close the intake valve.
On the other hand, the exhaust side rocker arm is see-
saw type. It swings with the rocker arm shaft as its
supporting point and according to the camshaft
movement to open and close the exhaust valve.
6A1-4 ENGINE MECHANICAL (G13B, 1-CAM 16-VALVES ENGINE)

1. Camshaft allowable turning range - - - By timing mark,
within 90 from “V” mark on head cover on both right
and left.
2. Crankshaft allowable turning range - - - By punch mark,
within 90 from arrow mark on oil pump case on both
right and left.
ENGINE MECHANICAL (G13B, 1-CAM 16-VALVES ENGINE) 6A1-21
CAUTION:

After timing belt is removed, never turn camshaft and
crankshaft independently more than such an extent as
shown in figure. If turned, interference may occur among
piston and valves, and parts related to piston and valves
may be damaged.

Never bend timing belt.
INSPECTION

Inspect timing belt for wear or crack.
Replace it as necessary.

Inspect tensioner for smooth rotation.
INSTALLATION
1) Install tensioner plate to tensioner.
Insert lug (1) of tensioner plate into hole (2) in tensioner.

4. Damper
6A1-22 ENGINE MECHANICAL (G13B, 1-CAM 16-VALVES ENGINE)
2) Install tensioner (2) and tensioner plate (3):
Do not tighten tensioner bolt (1) with wrench yet. Hand tighten
only at this time.
Check to ensure that plate movement in arrow direction as
shown in figure causes tensioner to move in the same direction.
If no associated movement between plate and tensioner occurs,
remove tensioner and plate again and reinsert plate lug into ten-
sioner hole.
3) Check that timing mark (2) on camshaft timing belt pulley is
aligned with “V” mark (1) on cylinder head cover. If not, align two
marks by turning camshaft but be careful not to turn it more than
its allowable turning range which is described on previous page.
4) Check that timing mark (2) on crankshaft timing belt pulley is
aligned with arrow mark (1) on oil pump case. If not, align two
marks by turning crankshaft but be careful not to turn it more
than its allowable turning range which is described on previous
page.
5) Install timing belt and tensioner spring (2).
With two sets of marks aligned and tensioner plate pushed up,
install timing belt on two pulleys in such a way that drive side (1)
of belt is free from any slack.
And then install tensioner spring as shown in figure, and hand-
tighten tensioner stud (3).
NOTE:

When installing timing belt, match arrow mark (
) on
timing belt with rotating direction of crankshaft.

In this state, No. 4 piston is at top dead center of compres-
sion stroke.

1. Top ring
2. 2nd ring
3. Oil ring
4. Piston
5. Connecting rod
6. Connecting rod bearing cap
7. Connecting rod bearing
8. Piston pin
9. Piston pin circlip
10. connecting rod bearing cap nut
: Do not reuse
: Tightening Torque
: Apply engine oil to sliding
: surface of each part.
6
10
6A1-54 ENGINE MECHANICAL (G13B, 1-CAM 16-VALVES ENGINE)
PISTON, PISTON RINGS, CONNECTING RODS AND CYLINDERS
REMOVAL
1) Remove cylinder head from cylinder block as previously out-
lined.
2) Drain engine oil.
3) Remove oil pan and oil pump strainer as previously outlined.
4) Mark cylinder number on all pistons, connecting rods and rod
bearing caps, using silver pencil or quick drying paint.
5) Remove rod bearing caps.
6) Install guide hose (1) over threads of rod bolts. This is to prevent
damage to bearing journal and rod bolt threads when removing
connecting rod.
7) Decarbon top of cylinder bore before removing piston from cylin-
der.
8) Push piston and connecting rod assembly out through the top of
cylinder bore.

ENGINE MECHANICAL (G13B, 1-CAM 16-VALVES ENGINE) 6A1-55
DISASSEMBLY
1) Using piston ring expander, remove two compression rings (Top
and 2nd) and oil ring from piston.
2) Remove piston pin from connecting rod.

Ease out piston pin circlips (1), as shown.

Force piston pin out.
CLEANING
Clean carbon from piston head and ring grooves, using a suitable
tool.

“a”: 50 mm (1.96 in.)
“b”: 95 mm (3.74 in.)
“a”: 23 mm (0.91 in.)
6A1-56 ENGINE MECHANICAL (G13B, 1-CAM 16-VALVES ENGINE)
INSPECTION
Cylinders

Inspect cylinder walls for scratches, roughness, or ridges which
indicate excessive wear. If cylinder bore is very rough or deeply
scratched, or ridged, rebore cylinder and use oversize piston.

Using a cylinder gauge, measure cylinder bore in thrust and axial
directions at two positions as shown in figure.
If any of the following conditions is noted, rebore cylinder.
1) Cylinder bore dia. exceeds limit.
2) Difference of measurements at two positions exceeds taper lim-
it.
3) Difference between thrust and axial measurements exceeds
out-of-round limit.
Cylinder bore dia. limit: 74.15 mm (2.9196 in.)
Tapper and out-of-round limit: 0.10 mm (0.0039 in.)
NOTE:
If any one of four cylinders has to be rebored, rebore all four
to the same next oversize. This is necessary for the sake of
uniformity and balance.
Pistons

Inspect piston for faults, cracks or other damaged.
Damaged or faulty piston should be replaced.

Piston diameter:
As indicated in figure, piston diameter should be measured at a
position 23 mm (0.91 in.) from piston skirt end in the direction per-
pendicular to piston pin.
Standard73.970 – 73.990 mm
(2.9122 – 2.9130 in.)
Piston
diameterOversize:
0.25 mm
(0.0098 in.)74.220 – 74.230 mm
(2.9220 – 2.9224 in.)
0.50 mm
(0.0196 in.)74.470 –74.480 mm
(2.9319 – 2.9323 in.)

“a”: 23 mm (0.91 in.)
ENGINE MECHANICAL (G13B, 1-CAM 16-VALVES ENGINE) 6A1-57

Piston clearance:
Measure cylinder bore diameter and piston diameter to find their
difference which is piston clearance. Piston clearance should be
within specification as given below. If it is out of specification, re-
bore cylinder and use oversize piston.
Piston clearance: 0.02 – 0.04 mm (0.0008 – 0.0015 in.)
NOTE:
Cylinder bore diameters used here are measured in thrust
direction at two positions.

Ring groove clearance:
Before checking, piston grooves must be clean, dry and free of
carbon.
Fit new piston ring (1) into piston groove, and measure clearance
between ring and ring land by using thickness gauge (2).
If clearance is out of specification, replace piston.
Ring groove clearance:
Top: 0.03 – 0.07 mm (0.0012 – 0.0027 in.)
2nd: 0.02 – 0.06 mm (0.0008 – 0.0023 in.)
Piston Pin

Check piston pin, connecting rod small end bore and piston bore
for wear or damage, paying particular attention to condition of
small end bore bush. If pin, connecting rod small end bore or pis-
ton bore is badly worn or damaged, replace pin, connecting rod
or piston.

Piston pin clearance:
Check piston pin clearance in small end. Replace connecting rod
if its small end is badly worn or damaged or if measured clearance
exceeds limit.
Item
StandardLimit
Piston clearance in
small end0.003 – 0.016 mm
(0.0001 – 0.0006 in.)0.05 mm
(0.0020 in.)
Small-end bore:
19.003 – 19.011 mm (0.7482 – 0.7486 in.)
Piston pin dia.:
18.995 – 19.000 mm (0.7478 – 0.7480 in.)

1. Cylinder block
“a”: 120 mm (4.72 in.)
6A1-58 ENGINE MECHANICAL (G13B, 1-CAM 16-VALVES ENGINE)
Piston Rings
To measure end gap, insert piston ring (3) into cylinder bore and
then measure the gap by using thickness gauge (2).
If measured gap is out of specification, replace ring.
NOTE:
Decarbon and clean top of cylinder bore before inserting pis-
ton ring.
Item
StandardLimit
Piston
Top ring0.15 – 0.30 mm
(0.0059 – 0.0118 in.)0.7 mm
(0.0275 in.)
Piston
ring end
gap
2nd ring0.2 – 0.35 mm
(0.0079 – 0.0137 in.)0.7 mm
(0.0275 in.)
ga
Oil ring0.2 – 0.7 mm
(0.0079 – 0.0275 in.)1.7 mm
(0.0669 in.)
Connecting Rod

Big-end side clearance:
Check big-end of connecting rod for side clearance, with rod fitted
and connected to its crank pin in the normal manner. If measured
clearance is found to exceed its limit, replace connecting rod.
Item
StandardLimit
Big-end side
clearance0.10 – 0.20 mm
(0.0039 – 0.0078 in.)0.35 mm
(0.0137 in.)

Connecting rod alignment:
Mount connecting rod on aligner to check it for bow and twist and,
if limit is exceeded, replace it.
Limit on bow: 0.05 mm (0.0020 in.)
Limit on twist: 0.10 mm (0.0039 in.)