Page 200 of 2189

lllustrated Index
I runricate att internal parts with engine oil during reassembly'
NOTE:
o Apply liquid gaskettothe mating surfaces ofthe right side cover and oil pumpcase before installingthem'
. Use liquid gasket, part No 08718-0001 or08718-0003'
. Clean the oil pan gasket mating surfaces betore installing the oil pan
81642 engine:
DRAIN BOLT44 N,m {4.5 kgf'm,33 lbt'ft)
6 x 1.0 mm'11 N.m (1.1 kgI'm,
I tbl.ft)
OIL PANReter to page 7 27when installing.
6 r 1.O mm12 N.m t1.2 kgl'm, 8 7 lbf'lt)
OIL PAN GASKET
BUFFLE PLA
12 x 1.0 mm103 N.m {10.5 kgf'm,
76 tbr.ft)
6 x 1.0 mm11 N.m (1 .1 kgf.m,
8 tbI.fr)
GASKETReplace.FLYWHEEL(M/TI
12 x 1.0 mm
74 N.m (7.5
kof.m, 54 lbf'ft)
1^c{Eb\%^ t*^
*o"rr^--(Wffi
oa*,trto2,.w
FLYWHEEL COVER
IM/T)
DRIVE PLATECOVER (AiT)
11 x 1.5 mm76 N.m (7.9 kgf'm, 56 lbf'ft)
Apply engine oil to the bolt
threads.NOTE: After torqurngeach cap, turn crankshaft
to check for binding.
MAIN EEARING CAP
MAIN BEARINGSSelection, page 7_10
NOTE: New main bearings musl
be selected bY matching crank
and block identification markrngs
CRANKSHAFTInstallation, Page 7'23
OIL JET BOLT16 N.m 11.6 kgf'm, 12 lbl'ft)
OIL JETInspection, Page 8_10
Check for cracks
6x1.0mm11 N.m {1.1 kgf'm, I lbf'ft}
CRANKSHAFT OIL SEAL
Installation,pagesl 22 andl 29
Replace-
DOWEL PINOIL PUMPOverhaul, page 8-'l1Removal/lnspection,page 8-13.Apply liquid gasket
to mating surlace.RIGHT SIDE COVERApply liquid gasket
to mating surface.
THRUST WASHERS8 x 1.25 mm24 N.m {2.4 kgf.m, 17 lbf'ft)Grooved sides face outward
NOTE: Thrusr washer thickness
is tixed and must not be changed
by grinding or shimming
O-RINGReplace
CRANKSHAFT SEAL11 N.m {1.1 kgf'm, lnstallation, pages 7'29 and I 14
a lbt.ltl Heplace. (cont'd)
d#*
Page 201 of 2189

lllustrated Index
(cont'dl
I Luoricate att internal parts with engine oil during reassembly.
NOTE:
' Apply liquid gasket to the mating surfaces ofthe rightside coverand oil pumpcase before installingthem.. Use liquid gasket, part No. 08718 - 0001 or 087,18 _ OOO3.. Clean the oil pan gasket mating surfaces before installing it.
D16Y7 engine:6 x 1.0 mm12 N.m (1.2 kgt.m.8.7 tbf.tr)DRAIN BOLT44 N.m {4.5 kgt.m.33 tbt.ttl
,(
I
I
OIL PAN GASKETFLYWHEEL COVERIM/T)6x 1.0 mm12 N.m ('l .2 kgt.m, 8.7 tbt.trl
OIL PANRefer to page 7-27
Apply liquid gasker tothese points.
Replace.
WASHERReplace.12 x '1.0 mm118 N.m{12.0 kgt.m, 87 tbf.tr}
11 x 1.5 mm51 N.m15.2 kgl.m,38lbtftl
Apply engine oilto the boltthreads.NOTE: After torquingeach cap, turn the crankshaftto check for binding.
MAIN BEARINGSSelection, page 7-10
MAIN BEARING CAP
CRANKSHAFTInstallation, page 7 23
NOTE: New main bearings mustbe selected by matching crankand block identification markings.
6 r 1.0 mm11 N.m {1.1
6 x 1.0 mm11 N.m 11.1
ksI.m, 8 lbt.ft)
OIL SCREEN
kgt.m, 8 lbf.trl
Check for cracks.
CRANKSHAFT OIL SEALInstallation,pages 1 22 a^d 7-29
\:eprace'
GASKETReplace.
6 x 1.O mm11 N.m {1.1 kgt.m,8 rbt.frl
RIGHT SIDE COVERApply liquid gasker1o matrng surface,
OIL PUMPOverhaul, page 8-12Bemoval/lnspection,page 8-13
DOWEL PIN
WASHERSGrooved sides face outward.NOTE: Thrust washer thicknessis fixed and must not be changedby grinding or shimming.
CRANKSHAFT SEAL
l.j"Ji:l"^ pages z.2e --.S)
Replace.
6 x 1.0 mm11 N.m {1.18 tbt.fr)
7-4
BREATHING PORT COVERMOUNT BOLTS6 x 1.0 mm11 N.m {1.1 kgt.m, 8 tbf.fr}Apply liquid gasker tothe boh threads.
DOWEL PIN
Page 203 of 2189

lllustrated Index
(cont'd)
NOTE: New rod bearings must be selected by matching connecting rod assembly and crankshaft(see page 7,11).identification markings
Lubricate all internal parts with engine oil duringreassembtv.
PISTON INSTALLATION DIRECTION:
EXHAUST
4\/=\6\z\
\e/!rqrf/
INTAKE
PISTON RINGSReplacement. page 7-20Measurement, pages 7 20 andj-21Alignment, page 7-21
PISTON PINRemoval, page 7,17Installation, page 7-18Inspection, page 7,19
CONNECTING RODEnd play, page 7-8Selection, page 7,18
CONNECTING RODBEARINGSClearance, page 7 11Selection, page 7-11
CONNECTING ROD BEARING CAPInstallation, page 7-23NOTE: lnstall caps so thebearing recess is on thesame side as the recessin the rod.
PISTONInspectron, page 7-15NOTE: Betore removing the piston, inspect thetop of the cylinder bore for carbon build-up orridge. Bemove ridge if necessary, page 7-13
ENGINE BLOCKCylinder bore inspection, page 7-16Warpage inspection, page 7,'16Cylinder bore honing, page 7,17
Inspect top of each cylinder borefor carbon build-up or ridgebefore removing piston.Remove ridge if necessary, page 7-13
CONNECTING ROD CAP NUT816A2 €ngin6:9 x 0.75 mm{0 N.m (4.1 kgt m, 30 tbf.ftlD16Y5, Dl6Y7. D16Y8 engines:8 x 0.75 mm3l N.m {3.2 kg{.m,23 tbt.fr)Apply engine oiltothe bolt threads.NOTE: After torquing each bearingcap, rotate crankshaft tocheck for binding.
7-6
Page 207 of 2189

Main Bearing
Selection
CAUTION: lf the codes are indecipherable because of anaccumulation of dirt and dust, do not scrub them with a
wire brush or scraper. Clean them only with solvent ol
deiergent.
Crankshaft Bore Code Location
81642 engine:
Letters have been stamped on the end of the block as acode for the size of each of the 5 main journal bores.
Use them, and the numbers or bars stamped on the
crank {codes for main journal size), to choose the correct
beaflngs.
Main JournalCode Locations {Nombers or Barc)
Eearing ldentificationColor code rson lhe edge ofthe bear ng.Larger crank bore
acD
-----------""' Smallerbeanngtlhrcker)
9""1B':""
Alack
Black
Alue
7-10
\
D16Y5, D16Y7, D16Y8 engines:
Letters have been stamped on the end of the block as acode for the size of each of the 5 main journal bores.
Use them, and the numbers stamped on the crankshaft(codes for main journal size), to choose the correct bear-
Ings.
Main Journal Code Location (Numbers)
\
Color codeon theedge ofthe bearing-
Ldrger crank bore
Smaller bea ng {th'cker)
lr-l
t#lt+,tlf l 4 tlf '- 't
Smaller Smallermaan bearingjournal {thicker)
RedPinkGreen
PinkGreenBrown
GreenBrownBlack
GreenBrownBlackElue
I
Bearing ldentification
BcD
Page 211 of 2189

Crankshaft
Inspection
. Clean the crankshaft oil passages with pipe cleaners
or a suitable brush.
. Check the keyway and threads.
Alignment
. Measure runout on all main journals to make
sure the crank is not bent.
. The difference between measurements on eachjournal must not be more than the service limit.
Crankshaft Total Indicated Runout:
Bl6A2 engine:
Standard (Newl: 0.020 mm {0.0008 in} max.
Service Limit: 0.030 mm {0.0012 inl
D16Y5, D15Y7, D15Y8 engines:
Standsrd {New): 0.03 mm (0.001 in} max.
Service Limit; 0.0i1 mm 10.002 in)
Support with lathetype tool or V blocks.
7-14
Out-of-Round and Tapet
. Measure out-of-round at the middle of each rod
and main journal in two places.
a The difference between measurements on eachjournal must not be more than the service limit.
Joulnal Out-of-Round:
81642 engine:
Standard (New): 0.0004 mm {0.0002 in) max.
Service Limit: 0.006 mm {0.0002 in)
Dr6Y5, Dl6Y7, D16Y8 engines:
Standard (Newl: 0.0025 mm (0.0001 inl max.
Service Limh: 0.005 mm (0.0002 inl
round at middle.
. Measure taper at the edges of each rod and mainjournal.
. The difference between measurements on eachjournal must not be more than the service limit.
JournalTaDer:
B16A2 ongine:
Standard lNewl: 0.005 mm (0.0002 inl max.
Service Limit: 0.010 mm (0.00i1 inl
D16Y5, D16Y7, Dl6YB engines:
Standard (New): 0.0025 mm {0.0001 in) max.
Service Limit: 0.005 mm (0.0002 in)
\
Page 212 of 2189

Pistons
Inspection
1.Check the piston for distortion or cracks,
NOTE: lf a cylinder is bored. an oversized piston
must be used.
Measure the piston diameter at a distance A from
bottom of the skirt.
816A2 engino:
A: 15 mm 10.6 in)
D16Y5, D16Y7, D16Y8 engines:
A: 5 mm (0.2 inl
Piston Diameter:
816A2 engine:
Standard lNewl: 80.980 - 80.990 mm
13.1882 - 3.1886 in)
Service Limit: 80.970 mm (3.1878 in)
D16Y5, D16Y7, D16Y8 engines:
Standard {New): 7,f.980 - 7i1.990 mm
|.2.9520 - 2.9521in!
Service Limit: 74.970 mm {2.9516 inl
SKIRT DIAMETER
57-1
3. Calculate the difference between the cylinder bore
diameter (see page 7-16) and the piston diameter.
Piston-to-Cylinder Clsarance
Standard lNewl: 0.010 - 0.0,10 mm
(0.0004 - 0.0016 inl
Servico Limit: 0.05 mm {0.002 in}
lf the clearance is near or exceeds the service limit,
inspect the piston and cylinder block for excessive
wear.
Oversizo Piston Diametor
816A2 ongine:
0.25t 81.23 - 81.21 mm (3.1980 - 3.1984 inl
D16Y5. D16Y7, D16Y8 engines:
O.25t 75.23 - 75.21 mm (2.9618 - 2.9622 in)
0.50: 75.i18 - 75.49 mm {2.9716 - 2.9720 in}
Page 213 of 2189

Cylinder Block
Inspection
'LMeasure wear and taper in directions X and y at threelevels in each cvlinder as shown.
Cylinder Boro Size
816A2 engine:
Standard (Newl: 81.00 - 81.02 mm
{3.1t|:l - 3.190 intService Limit: 81.07 mm {3.192 in)D16Y5, D16Y7, D16Y8 engines:
Standard lNew): 75.00 - 75.02 mm(2.9s3 - 2.954 in)
Sarvice Limit: 75.07 mm (2.956 in)
Oversize
816A2 engiDe:
0.25t 41.25 - A1.27 mm {3.199 - 3.200 in)D16Y5, D16Y7, D16Y8 Engines:
0.25t 75.25 -15.27 mm (2.9626 - 2.963,0 in)0.50: 75.50 - 75.52 mm 12.9721- 2.9i32 inl
Bore TaDet
Limit: (Difference between first and third measure"ment) 0.05 mm (0.002 inl
7-16
lf the measurements in any cylinder are beyondthe Oversize Bore Service Limit, replace the block.
lf the block is to be rebored. refer to piston Clear-ance Inspection (see page 7-15) after reboring.
NOTE: Scored or scratched cylinder bores must behoned.
Reboring Limit:
Bl642 enginc:
0.25 mm (0.01 in)
Dl6Y5, D16Y7, D16Y8 engin€s:
0.50 mm (0.02 in)
Check the top of the block for warpage,Measure along the edges and across the center asshown.
SURFACES TO BE MEASUREO
Engine Block Warpage:
Bl6A2 engine:
Standard (Now): 0.05 mm {0.002 inl max.Service Limh: 0.08 mm (0.003 in)DtOYs, D16Y7, D16Y8 €nginas:
Standard (N€w): 0.07 mm l0.OO3 inl max.Servica Limit; 0.10 mm {0.00it in)
PRECISION STRAIGHT EDGE
Page 214 of 2189

Cylinder BlockPiston Pins
Bore Honing
1.Measure cylinder bores as shown on page 7-16. lf the
block is to be reused, hone the cylinders and remea-
sure the bores.
Hone cylinder bores with honing oil 8nd a fine (400
grit) stone in a 60 degree cross-hatch pattern.
NOTE:
. Use only a rigid hone with 400 grit or finer stone
such as Sunnen, Ammco, or equivalent.
. Do not use stones lhat are worn or broken.
When honing is complete, thoroughly clean the
engine block of all metal particles. Wash the cylin-
der bores with hot soapY water, then dry and oil
immediately to prevent rusting.
NOTE: Never use solvent. it will only redistribute the
grit on the cylinder walls.
lf scoring or scratches are still present in cylinder
bores after honing to the service limit, rebore the
cylinder block.
NOTE: Some light vertical scoring and scratching is
acceptable if it is not deep enough to catch your fin-
gernail and does not run the full length of the bore.
CYLINOES BLOCK
CYLINDER
NOTE:
. After honing, clean the cylinder thoroughly with
soapy warer.
. Onlv a scored or scratched cylinder bore must be
noneo.
Removal
l. Assemble the special tool as shown.
PISTON BASE HEAD07973 - SBtx)too
ft
PISTON PIN BASE
INSERT01973 - PE00'0)
ptn
NOTEi Us6 a hydraulic press.When pressing the pin in or out.make sure that the recesssdportion of the piston alignswith the lips on the collar.
rg
g\
lj*N*,""
2. Assemble and adjust the length of the piston
driver and shaft to 53 mm (2.1 inl as shown.
PISTON PIN DRIVER HEAD07973 - PE00320
Proat
0
PISTON PINDRIVER SHAFT0t973 - PEqr310
PILOT COLLAR07973 - PE00200
3. Place the piston on the sp€cial tool and press the
pin out with the special tools and a hydraulic press.
Emboss6d mark facing up
7-17