A B C D E F G H J K L M N P R S

L-08067-28 ITEM PART NO. REQ'D NAME

1 4406.3
[173.5 ]
11
4243.4 4417.8 5422.6
[167.1 ] [173.9 ] [213.5 ]

2296.9
[90.4 ]
2 39
18 6

1745
3
[68.7 ]
E

1475
3210.6 [58.1 ]
[126.4]

4 H

12 A

Z
5 698.7
[27.5 ] 1

482.4
[19.0 ]

386
[15.2 ]
14
6 200.9
[7.9 ]
64.6 5
[2.5 ]
0 CRANKSHAFT
120 [.0 ]
[4.7 ]

7 D

437
[17.2 ]

589.7
[23.2 ]

2
8

899
[35.4 ]

35 15 L M B 20 C
PRICE CODE:
9 2313 P2716J2
[91.1]
454 145 115 81.6 366.1 4087.5 4999.2 5092.7 5238.7
[17.9 ] [5.7 ] [4.5 ] [3.2 ] [14.4 ] [160.9 ] [196.8 ] [200.5 ] [206.2 ]

0 REFERENCE NOTES:
[.0 ] RIGHT SIDE VIEW
REAR FACE 1. OVERALL LENGTH OF ENGINE: 6056.0 [238.4]
OF OVERALL WIDTH OF ENGINE: 2322.6 [91.4]
10 CRANKCASE OVERALL HEIGHT OF ENGINE: 3210.6 [126.4]

ECO 157701
REV NO 106
UNLESS OTHERWISE SPECIFIED: DIMENSIONS ARE IN MILLIMETERS.
MACHINE DIMENSION TOLERANCE STANDARD -
SURFACE FINISH STANDARD -
DIMENSIONING AND TOLERANCING STANDARD - ASME Y14.5M, LATEST VERSION.
FABRICATION TOLERANCES -
MATERIAL: - REF. L-08092-26
11
HEAT TREATMENT:
-
NAME:
157701 01-15 SEE SHEET 2 & 3. THIS PRINT IS PROVIDED ON A RESTRICTED BASIS NOT TO BE USED
INSTALLATION
IN ANY WAY DETRIMENTAL TO THE INTEREST OF WAUKESHA ENGINE DIVISION.
MODELS C.C.
157535 12-14 SUPERSEDED BY L-08067-30. DRAWING
16V275GL+ -
157534 12-14 UPDATED CONNECTION DIMENSIONS, SEE ECO AND SHEETS 2 AND 3.
157101 07-14 ADDED PRICE CODE. SEE SHEETS 2 - 5 FOR CHANGES. FILE PART NO.
12 156928 04-14 SEE SHEET 3 FOR CHANGES L-08067-28
155229 01-13 RELEASED. SUPERSEDES L-08067-26.
DR: MAO DATE: 01-15-13APP:
CHK: RHN DATE: 01-31-13APP:
CJN DATE:
DATE:
01-31-13
D SHT. 1 OF 5 SCALE: 0.100
 A B C D E F G H J K L M N P R S
L-08067-28 ITEM PART NO. REQ'D NAME

12X 0.75-10UNC-2B
1 40 MIN. A 692.15 B.C.
11 6 [27.25 ]
18

5422.6 4499.8 4417.8 4243.4 12X 30 $

[213.5 ] [177.2 ] [173.9 ] [167.1 ]

2
15 $
+0.13
733.42
-0
+.005
[ 28.9 ]
-.000
2306.1
[90.8 ]

3
7 115
[4.5 ]

6.4
1745 A [.3]
[68.7 ] K
SECTION A-A
4
FLYWHEEL DETAIL
1475
1450.1
[58.1 ]
[57.1 ]

37
37
5 SEE DETAIL
VIEW 12

AA
747.5
36 [29.4 ]
6
5

386
[15.2 ]

R
200.9 38
[7.9 ]
7
22.7 0 CRANKSHAFT
[.9 ] [.0 ]
120
208.1
[4.7 ] DETAIL PRECHAMBER
175.4
[8.2 ]
[6.9 ] FUEL MANIFOLD
SCALE 0.150
8
437
[17.2 ] 14

589.7
[23.2 ]
16
603.2
[23.7 ]
9 899
[35.4 ]

2 38 G U 20 10 F 17 L Q N 15 35
REFERENCE NOTES:

2313 1. DIMENSION TAKEN FROM THE CUSTOMER CONNECTION

[91.1] BOLT SURFACE OF THE FLYWHEEL.
5602 5238.7 5092.7 4479.1 4265.1 4087.5 3126.6 366.1 81.6 145 277.6 454
[220.6 ] [206.2 ] [200.5 ] [176.3 ] [167.9 ] [160.9 ] [123.1 ] [14.4 ] [3.2 ] 0 [5.7 ] [10.9 ] [17.9 ]
10 [.0 ] SEE NOTE 1
LEFT SIDE VIEW REAR FACE
OF ECO 157701
CRANKCASE
REV NO 106
UNLESS OTHERWISE SPECIFIED: DIMENSIONS ARE IN MILLIMETERS.
MACHINE DIMENSION TOLERANCE STANDARD -
SURFACE FINISH STANDARD -
DIMENSIONING AND TOLERANCING STANDARD - ASME Y14.5M, LATEST VERSION.
FABRICATION TOLERANCES -
MATERIAL: - REF. L-08092-26
11
HEAT TREATMENT:
-
NAME:
157701 01-15 REVISED. SEE ECO. THIS PRINT IS PROVIDED ON A RESTRICTED BASIS NOT TO BE USED
INSTALLATION
IN ANY WAY DETRIMENTAL TO THE INTEREST OF WAUKESHA ENGINE DIVISION.
MODELS C.C.
157535 12-14 SEE SHEET 1. DRAWING
16V275GL+ -
157534 12-14 UPDATED CONNECTION DIMENSIONS, SEE ECO AND SHEETS 1 & 3.
157101 07-14 ADDED PRECHAMBER FUEL MANIFOLD DETAIL. SEE SHEETS 1, 3 - 5. FILE PART NO.
12 156928 04-14 SEE SHEET 3 FOR CHANGES L-08067-28
155229 01-13 RELEASED. SUPERSEDES L-08067-26.
DR: MAO DATE: 01-15-13APP:
CHK: RHN DATE: 01-31-13APP:
CJN DATE:
DATE:
01-31-13
D SHT. 2 OF 5 SCALE: 0.100
 A B C D E F G H J K L M N P R S
L-08067-28 ITEM PART NO. REQ'D NAME

1 5

198 187
[7.8 ] [7.4 ] 569
[22.4 ] 125
2 534.1 [4.9 ]
W Y [21.0 ] 32
11 11 39
496.4
[19.5 ]
30
25

2306.1
[90.8 ] A 31
3 24 629
2225.1
[87.6 ] [24.8 ]
6
23
6
2
1838.3
7 [72.4 ]
4
0 7
[.0 ] 4

DETAIL JACKET/AUX WATER

SCALE 0.150 DETAIL A
SCALE 0.200 3

5
12
S
1126.9
1099.2
[44.4 ]
[43.3 ]
12 L
SEE DETAIL A
A
0 37
6 747.5 [.0 ] 532
[29.4 ] 698.7 [20.9 ]
[27.5 ] I
AA 26
L
482.4 27
T [19.0 ]
386 386
[15.2 ] [15.2 ]
7 28
154.5 200.9
14 29
[6.1 ] [7.9 ]
17
22.7
22.7 0 CRANKSHAFT 0 [.9 ]
[.9 ] [.0 ] [.0 ]
120
[4.7 ] 64.6 17
175.4 [2.5 ]
8 [6.9 ] 120 208.1
[4.7 ] 5 [8.2 ]
38
603.2
15 [23.7 ]
14 480 480
[18.9 ] [18.9 ]

19 589.7
9 [23.2 ]
9 755.2
785
[29.7 ]
[30.9 ] 834.3
[32.8 ]
804
[31.7 ] 883.6 8 2
15 16 13 21 [34.8 ]

951.5 858.9 808.1 753.4 640 239.4 19 0 35 239.4 493.6 640

22 [37.5 ] [33.8 ] [31.8 ] [29.7 ] [25.2 ] [9.4 ] [.7 ] [.0 ] [1.4 ] [9.4 ] [19.4 ] [25.2 ]
10 1035.3 1012.7 894 869.5 399.7 198.7 0 19 115 282 768.7 869.5 1012.7 0 35 271.3
[40.8 ] [39.9 ] [35.2 ] [34.2 ] [15.7 ] [7.8 ] [.0 ] [.7 ] [4.5 ] [11.1 ] [30.3 ] [34.2 ] [39.9 ] [.0 ] [1.4 ] [10.7 ]
FRONT VIEW 157701
DETAIL PRELUBE PUMP
ECO

REAR VIEW REV NO 106

SCALE 0.200 UNLESS OTHERWISE SPECIFIED: DIMENSIONS ARE IN MILLIMETERS.
MACHINE DIMENSION TOLERANCE STANDARD -
SURFACE FINISH STANDARD -
DIMENSIONING AND TOLERANCING STANDARD - ASME Y14.5M, LATEST VERSION.
FABRICATION TOLERANCES -
MATERIAL: - REF. L-08092-26
11
HEAT TREATMENT:
-
NAME:
157701 01-15 SEE SHEET 2 & ECO. THIS PRINT IS PROVIDED ON A RESTRICTED BASIS NOT TO BE USED
INSTALLATION
IN ANY WAY DETRIMENTAL TO THE INTEREST OF WAUKESHA ENGINE DIVISION.
MODELS C.C.
157535 12-14 SEE SHEET 1. DRAWING
16V275GL+ -
157534 12-14 UPDATED CONNECTION DIMENSIONS, SEE ECO AND SHEETS 1 & 2

157101 07-14 ADDED ENGINE ROTATION ON FLYWHEEL AND CONN. 37, 38 & 39 (FRONT VIEW). SEE SHEET 2 & 5. FILE PART NO.
12 156928 04-14 MOVED ELECTRICAL BOX LOCATION TO TOP OF BLOWER MOTOR L-08067-28
155229 01-13 RELEASED. SUPERSEDES L-08067-26
DR: MAO DATE: 01-15-13APP:
CHK: RHN DATE: 01-31-13APP:
CJN DATE:
DATE:
01-31-13
D SHT. 3 OF 5 SCALE: 0.100
 A B C D E F G H J K L M N P R S
L-08067-28
1.00" 1.44" 1.19"
1.31"
1 .94" .94"
A .75"
A .94" A .06"
6.00" A .06"
9.00" 10.00" 7.50"

3.06" 2.44"
5.31" 4.57"
2 6.44" 5.66" 7.31"
4.25" 3.57" 5.00"

8X .75"
7.50" BOLT CIRCLE 4X .75" A
A
SECTION A-A 4.75" BOLT CIRCLE SECTION A-A 8X .88"
8.50" BOLT CIRCLE A SECTION A-A 4X .75"
3 6.00" BOLT CIRCLE A SECTION A-A
4" ANSI 150# FLAT - FACE FLANGE 2" ANSI 150# FLAT - FACE FLANGE 5" ANSI 150# RAISED - FACE FLANGE 3" ANSI 150# RAISED - FACE FLANGE
SCALE 0.380 SCALE 0.250
SCALE 0.250 SCALE 0.380

.88"

.69"
4 A .06"
5.00"

4X .62"
3.88" BOLT CIRCLE
12X 26 [1.02] EQUALLY SPACED 15 $
2.56" 1.95" 2.88"
476.2 [18.75] B.C. 431 11
5 [17.0 ]
L 539.8
[21.3 ]

1132.9
[44.6 ]
A
SECTION A-A

6 863
[34.0 ]
1.5" ANSI 150# RAISED - FACE FLANGE
SCALE 0.500
704
[27.7 ]

361.7 O.D. AC
[14.2 ]
W
7
39 SEE
DETAIL
VIEW 39

125
[4.9 ]
0
2322.6
[.0 ]
[91.4]
8

9 DETAIL AUXILIARY WATER

704
[27.7 ]
AIR BLEED CONNECTION
(TOP OF INTERCOOLER)
863 SCALE 0.150
[34.0 ]
NOTE:

1. FLANGE DIMENSIONS AND TOLERANCES PER

10 ASME/ANSI B16.5 - LATEST REVISION
1189.7
[46.8 ]
0 2313 4243.4 4511 5422.6
[177.6 ]
ECO 157701
[.0 ] [91.1 ] 11 [167.1 ] [213.5 ]
(CRANKCASE REAR) REV NO 106
UNLESS OTHERWISE SPECIFIED:
TOP VIEW
DIMENSIONS ARE IN MILLIMETERS.
MACHINE DIMENSION TOLERANCE STANDARD -
SURFACE FINISH STANDARD -
DIMENSIONING AND TOLERANCING STANDARD - ASME Y14.5M, LATEST VERSION.
FABRICATION TOLERANCES -
MATERIAL: - REF. L-08092-26
11
HEAT TREATMENT:
-
NAME:
157701 01-15 SEE SHEET 2 & 3. THIS PRINT IS PROVIDED ON A RESTRICTED BASIS NOT TO BE USED
INSTALLATION
IN ANY WAY DETRIMENTAL TO THE INTEREST OF WAUKESHA ENGINE DIVISION.
MODELS C.C.
157535 12-14 SEE SHEET 1. DRAWING
16V275GL+ -
157534 12-14 SEE SHEETS 1, 2 & 3.
157101 07-14 ADDED DETAIL VIEW OF AUX. WATER AIR BLEED (R-8). SEE SHEETS 1-3 & 5. FILE PART NO.
12 156928 04-14 SEE SHEET 3 FOR CHANGES L-08067-28
155229 01-13 RELEASED. SUPERSEDES L-08067-26.
DR: MAO DATE: 01-15-13APP:
CHK: RHN DATE: 01-31-13APP:
CJN DATE:
DATE:
01-31-13
D SHT. 4 OF 5 SCALE: 0.100
 A B C D E F G H J K L M N P R S
L-08067-28 ITEM PART NO. REQ'D NAME

ENGINE CONNECTIONS 19. FLYWHEEL - 12X 0.75-10 UNC-2B 1.57 [40] , EQUALLY SPACED AT 27.25 [692.15] B.C.
1 20. AUXILIARY WATER DRAIN - 1.00"-11.5 NPT
1. NATURAL GAS INLET - 2.00" ANSI 150# FLAT - FACE FLANGE

2. AUXILIARY WATER INLET - 4.00" ANSI 150# FLAT - FACE FLANGE

21. OIL PAN OR OIL HEATER CONNECTION - 1.50"-11.5 NPT NOTES:
22. LUBE OIL DRAIN OR OIL HEATER CONNECTION - 1.50"-11.5 NPT 1. ALL ENGINE PIPING FLANGES MUST BE CONNECTED FROM THIS POINT
3. AUXILIARY WATER OUTLET - 4.00" ANSI 150# FLAT - FACE FLANGE
TO THE FACILITY/CUSTOMER PIPING USING A FLEXIBLE CONNECTION.
23. AUXILIARY WATER STATIC LINE - 1.50"-11.5 NPT
4. ENGINE WATER OUTLET - 5.00" ANSI 150# RAISED - FACE FLANGE
2. VENT ALL VALVE EXHAUST PORTS TO A SAFE LOCATION IF COMBUSTIBLE
24. COMPRESSOR COOLING CONNECTION - 2"-11.5 NPT (SEE NOTE 4) GAS IS USED FOR WORKING FLUID.
2 5. ENGINE WATER INLET - 5.00" ANSI 150# RAISED - FACE FLANGE
25. JACKET WATER STATIC LINE - 1.50"-11.5 NPT 3. ALL EXHAUST CONNECTIONS ARE TO BE DONE PER S-08242 (LATEST VERSION).
6. EXHAUST OUTLET - 14" ANSI FLAT - FACED FLANGE
NOTE: EXHAUST SYSTEM MUST SUPPORT ITS OWN WEIGHT BEYOND THIS POINT. 26. LOCAL CONTROL, HARNESS CONNECTION 4. REFERENCE 275GL/GL+ COOLING CIRCUIT SCHEMATIC FOR JACKET WATER CIRCUIT
7. ENGINE AIR INLET - 355.6 [14.00] I.D. (CAN BE ROTATED) AND AUXILIARY WATER CIRCUIT.
27. CUSTOMER INTERFACE, HARNESS CONNECTION
NOTE: AIR INLET SYSTEM MUST SUPPORT ITS OWN WEIGHT BEYOND THIS POINT.
28. EXHAUST THERMOCOUPLES, HARNESS CONNECTION
8. LUBE OIL DRAIN - 1.50"-11.5 NPT

3 29. MAIN BEARING THERMOCOUPLES, HARNESS CONNECTION

9. PRELUBE PUMP MOUNTING FLANGE - 4X 12.00 [0.47] ON 5.88 B.C., EQUALLY SPACED
NOTE: MUST CONFORM TO MOTOR FRAME SIZE 182C AND "M" DRIVE CONFIG. 30. MAIN GAS PILOT VALVE INLET - 0.5"-14 NPT (80 PSI MAX.)
10. POWER DISTRIBUTION INTERFACE 31. MAIN GAS PILOT VALVE OUTLET - 0.5"-14 NPT (SEE NOTE 2)
11. JACKET WATER AIR BLEED CONNECTION - 0.50"-14 NPTF 32. MAIN GAS PILOT VALVE OUTLET - 0.25"-18 NPT (SEE NOTE 2)
( 6.35 [0.25] LINE TO JACKET WATER EXPANSION TANK)
33. STARTER PILOT VALVE OUTLET - 0.25"-18 NPT, WITH REMOVABLE MUFFLER
12. AUXILIARY WATER AIR BLEED CONNECTION - 0.50"-14 NPTF
4 ( 6.35 [0.25] LINE TO AUXILIARY WATER EXPANSION TANK) 34. STARTER VALVE SOLENOID OUTLET - 0.25"-18 NPT, WITH REMOVABLE MUFFLER
13. LUBE OIL DRAIN - 1.00"-11.5 NPT, POST FILTER 35. JACKET WATER DRAIN/WATER HEATER INLET - G1-1/2"
5303.2
14. STARTER MOTOR AIR/GAS INLET - 1.50" ANSI 150# RAISED - FACE FLANGE [208.8 ]
36. JACKET WATER HEATER OUTLET - 1.25"-11.5 NPTF
JW OUTLET
15. STARTER MOTOR AIR/GAS OUTLET - 3.00" ANSI 150# RAISED - FACE FLANGE 37. PRE-CHAMBER GAS PRESSURE (GAS) - 0.25"-18 NPT
16. LUBE OIL DRAIN - 1.00"-11.5 NPT - PRE-FILTER 38. INTAKE MANIFOLD PRESSURE (AIR) - 0.25"-18 NPT 5238.7
5 [206.2 ]
17. BREATHER CONNECTION - 101.6 [4.00] O.D. 39. AUXILIARY WATER AIR BLEED CONNECTION - 0.25"-18 NPT (TOP OF INTERCOOLER) JW INLET
(SEE DETAIL VIEW, SHEET 4)
18. LIFTING EYES

8X M39 X 2 10X 37
[1.5 ]

215
6 [8.5]

1280 1140
[50.4] [44.9] ENGINE
8 570 FRONT
[22.4]

215
[8.5]
5249.5
[206.7 ]
AUX OUTLET

10
0 240 700 1160 1620 2080 2540 3000 3460 3920 5092.7
[.0 ] [9.4 ] [27.6 ] [45.7 ] [63.8 ] [81.9 ] [100.0 ] [118.1 ] [136.2 ] [154.3 ] [200.5 ]
AUX INLET ECO 157701
REV NO 106
33 34 BOTTOM VIEW UNLESS OTHERWISE SPECIFIED: DIMENSIONS ARE IN MILLIMETERS.
MACHINE DIMENSION TOLERANCE STANDARD -
SURFACE FINISH STANDARD -
DIMENSIONING AND TOLERANCING STANDARD - ASME Y14.5M, LATEST VERSION.
FABRICATION TOLERANCES -
MATERIAL: - REF. L-08092-26
11
HEAT TREATMENT:
-
NAME:
157701 01-15 SEE SHEET 2 & 3. THIS PRINT IS PROVIDED ON A RESTRICTED BASIS NOT TO BE USED
INSTALLATION
IN ANY WAY DETRIMENTAL TO THE INTEREST OF WAUKESHA ENGINE DIVISION.
MODELS C.C.
157535 12-14 SEE SHEET 1. DRAWING
16V275GL+ -
157534 12-14 SEE SHEETS 1, 2 & 3.
157101 07-14 ADDED ENG. CONNS. 37 & 38 & 39 ON CONN. LIST. SEE SHEETS 1-4. FILE PART NO.
12 156928 04-14 SEE SHEET 3 FOR CHANGES L-08067-28
155229 01-13 RELEASED. SUPERSEDES L-08067-26.
DR: MAO DATE: 01-15-13APP:
CHK: RHN DATE: 01-31-13APP:
CJN DATE:
DATE:
01-31-13
D SHT. 5 OF 5 SCALE: 0.100