Mazda Engine SKYACTIV-G 2.5. Manual — part 15
MECHANICAL
01-10–44
(2) Tighten lower cylinder block installation bolts
A in the order shown in the figure using the
following procedure:
Tightening procedure
Step 1: 38—42 N·m {3.9—4.2 kgf·m, 29—30
ft·lbf}
Step 2: Loosen all the bolts (until bolts are
torque-free).
Step 3: 30—34 N·m {3.1—3.4 kgf·m, 23—25
ft·lbf}
Step 4: 57.5—62.5°
(3) Tighten the lower cylinder block installation
bolts B in the order shown in the figure.
Tightening torque
19—25 N·m {2.0—2.5 kgf·m, 15—18 ft·lbf}
6. After verifying that silicone sealant protrudes to
the rear oil seal press-in part, wipe away the
excess silicone sealant.
• If silicone sealant does not protrude to the
rear oil seal press-in part, remove the lower
cylinder block and apply silicone sealant
again.
Piston Pin Assembly Note
1. Apply clean engine oil to the piston pin.
2. Insert the piston pin to the piston and connecting rod.
Note
• When assembling the piston to the connecting rod, each one can be assembled in either direction.
Snap Ring Assembly Note
Caution
• Do not compress the outer diameter of the snap ring more than necessary when assembling the
snap ring (20.66 mm {0.8134 in} or less).
1. Insert a new snap ring using a thin plier.
3
7
10
6
2
4
8
9
5
1
ENGINE
FRONT
A
A
A
A
A
A
A
A
A
A
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8
9
5
1
3
7
10
6
2
4
B
B
B
B
B
B
B
B
B
B
ENGINE
FRONT
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MECHANICAL
01-10–45
01-10
Piston Ring Assembly Note
Note
• It is not required to position the end gap between the top ring and second ring.
1. Assemble the oil ring so that the end gap of each
oil ring rail does not overlap as shown in the
figure.
2. Assemble so that the identification paint marks on
the top and second rings are visible to the right
side of each end gap.
Note
• If there are no identification paint marks on
the top and second rings, place the ring with
the bigger inner circumference at the top as
shown in the figure.
30
°
30
°
PISTON PIN AXIS
LOWER OIL RING RAIL
UPPER OIL RING RAIL
OIL RING SPACER
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TOP RING
END GAP
IDENTIFICATION PAINT MARK
SECOND RING
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TOP RING
NOTCH
NOTCH
SECOND RING
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MECHANICAL
01-10–46
Connecting Rod Bearing Assembly Note
Caution
• If a connecting rod bearing is reused, assemble it to the same position and in the direction as
before removal to prevent engine damage due to seizure or burning of the bearing.
• To prevent engine damage due to seizure or burning of the bearing, apply engine oil to the sliding
part when assembling.
1. Apply engine oil to the connecting rod bearings.
2. Align the positioning tab of the connecting rod
bearing with the positioning groove of the
connecting rod and connecting rod cap, and
assemble the bearings.
Piston, Connecting Rod Assembly Note
1. Insert the piston into the cylinder with the mark on
top of the piston facing the intake side.
INSTALLED
CONNECTING ROD
BEARING
CONNECTING ROD CAP
TAB
GROOVE
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6TN
G
2
ENGINE
FRONT
EX
IN
MARKED
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MECHANICAL
01-10–47
01-10
Connecting Rod Cap Assembly Note
Caution
• When assembling the connecting rod caps, align the broken, rough faces of the connecting rods
and connecting rod caps.
• If the following condition is met, replace the connecting rod cap bolts.
—
Length exceeds maximum
specification
Standard connecting rod cap bolt length
43.7—44.3 mm {1.73—1.74 in}
Maximum connecting rod cap bolt length
45.0 mm {1.77 in}
1. Position so that the broken, rough faces of the
connecting rods and connecting rod caps are
aligned exactly, and assemble the connecting rod
caps.
2. Tighten the connecting rod cap bolts in the
following two steps.
Tightening procedure
Step 1: 26—32 N·m {2.7—3.2 kgf·m, 20—23 ft·lbf}
Step 2: 80—100°
Pilot Bearing Assembly Note
1. Install new pilot bearing to the specified position
using the following tools.
Tool
Snap-on brand millimeter size bushing
driver set (A160M) adapter A160M7 (20—
22 mm {0.79—0.86 in})
• Use the adapter with the 20 mm {0.79 in}
side of the A160M7 (20—22 mm {0.79—
0.86 in}) facing the pilot bearing side.
Substitution tool
Outer diameter: 21 mm {0.83 in}
Inner diameter: 19 mm {0.75 in}
Standard pilot bearing position
Distance A of pilot bearing from crankshaft
end: 1.5—2.5 mm {0.060—0.098 in}
End Of Sie
L
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PILOT BEARING
A
CRANKSHAFT
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