Alternative Repair Procedures
Page9K-t2
Base
Engine Components
DODGE
Turbo Diesel
Thrust Journal/Thrust Surface
Width
Regrinding
Thrust journals can be reground in the same increments and using the same specifications as all other main
journals. The main journal radius may be reground using either the preferred or the optional procedure providing the
thrust surface
width
is not being reground. Then the preferred procedure must be
used.
When
the thrust surface
width
requires regrinding, the main Journal must be reground to the same undersize dimension.
Available Undersize Regrind To
Thrust Journal/Thrust Surface A = Diameter B =
Width
0.50mm
;[.0197inch]
82.500
±
.013mm
[3.2480
±.0005inch]
38.000
+.025mm
[1.4961
±.001 Inch]
1.00mm
[.0394inch]
82.000
±.013mm
[3.2283
±.0005inch]
38.500
±.025mm]
[1.5158
±.001 inch]
®
The thrust surface (C)
is
to be ground on center
within
0.10mm
[.004 inch] and must be perpendicular to the
front
and rear
mains
within
.0015mm
[.00006
inch] per radial Inch on the
thrust area. The surface finish requirement.is .04 micrometer
[16 microinch].
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