Table 6-1. Table of Limits
Continued
CHART
MINIMUM
MAXIMUM
REPLACE-
REF
NO.
DESCRIPTION
INCHES
INCHES
MENT
NO.
(FIGURE)
(MILLIMETERS)
(MILLIMETERS)
MAX
AIR COMPRESSOR ASSEMBLY -
Continued
3
6-38
Crank to pin center ..................
5.124
5.126
(130.1495)
(130.204)
4
6-38
Piston pin bearing width, 2nd, 3rd,
and 4th stage ........................
0.990
1.000
(25.1460)
(25.4000)
5
6-38
Piston pin rod end with, 1st stage
0.760
0.765
(19.3040)
(19.4310)
6
6-38
Piston pin bore, 1st stage ........
1.0005
1.0008
(25.4127)
(25.4203)
Crankshaft
1
6-39
Connecting rod bearing journal
3.746
3.747
(95.1484)
(95.1738)
2
6-39
End bearing journals.................
2.1653
2.1659
(54.9986)
(55.0139)
3
6-39
Oil pump journal ......................
1.499
1.500
(38.0746)
(38.1000)
4
6-39
Oil seal journal .........................
1.374
1.375
(34.8996)
(34.9250)
2, 3
6-39
End bearing journals and oil pump
journal concentricity
0.005TIR
Piston and Pin Subassy, 1st Stage
1
6-40
Piston pin diameter .......................
0.9998
1.0000
0.9988
(25.39492)
(25.40000)
(0.2489)
2
6-40
Piston pin bore diameter ...................
0.9998
1.0002
1.0018
(25.39492)
(25.40508)
(25.44572)
3
6-40
Cylinder Bore Diameter, 1st Stage ....
5.000
5.002
(127.0000)
(127.0508)
Piston and Pin Subassy, 2nd Stage
1
6-41
Piston pin diameter........................
1.0000
1.0003
0.9990
(25.4000)
(25.40762)
(25.3746)
2
6-41
Piston pin bore diameter ...................
1.0001
1.0005
1.0015
(25.40254)
(25.4127)
(25.4381)
6-69
