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Rating: M1 - 325hp (242kW) @ 2100 RPM Application:Marine Model: 6090SFM75 Designed/Calibrated to meet: Certified by: • EPA Commercial Marine Tier 2 • IMO MARPOL Annex VI Compliant • NRMM (97/68/EC), as amended Ref: Engine Emission Label 16-Sep-12 All values at rated speed, power, and standard conditions, per SAE J1995 unless otherwise noted. Engine Performance Curves September 2012 Performance Curve: 6090SFM75_A 6090 - Marine ENGINE PERFORMANCE CURVE PowerTech TM 9.0L Engine REFERENCE CONDITIONS Air Intake Restriction......................................................................12 in.H 2 O (3 kPa) Exhaust Back Pressure................................................................ 30 in.H 2 O (7.5 kPa) Rated speed and power Gross power guaranteed within ±5% at SAE J1995 and ISO 3046 J1995 and ISO 3046 conditions: 77 ˚F (25 ˚C) air inlet temperature 29.31 in.Hg (99 kPa) barometric pressure 104 ˚F (40 ˚C) fuel inlet temperature 0.853 fuel specific gravity @ 60 ˚F (15.5 ˚C) Ambient air temperature is defined to be the temperature of ambient air close to operating vessel that is not influenced in any manner by operating characteristics of the vessel (free field temp). Conversion factors: Power: kW = hp x 0.746 Fuel: 1 gal = 7.1 lb, 1 L = 0.85 kg Torque: N·m = lb-ft x 1.356 All values from currently available data. Subject to manufacturing and measurement variations and to change without notice. Actual performance is subject to application and operation conditions outside of John Deere control. 0 8 15 23 30 38 45 53 61 0 2 4 6 8 10 12 14 16 900 1100 1300 1500 1700 1900 2100 Fuel - L/hr Fuel - gal/hr Engine Speed - RPM Propeller Fuel 0 37 75 112 149 186 224 261 0 50 100 150 200 250 300 350 900 1100 1300 1500 1700 1900 2100 Power - kW Power - hp 475 610 746 881 1017 1152 1288 1423 1559 350 450 550 650 750 850 950 1050 1150 900 1100 1300 1500 1700 1900 2100 Torque - Nm Torque - lb-ft Crankshaft 1065 lb-ft (1444 Nm) Crankshaft Propeller Power Notes: M1: The M1 rating is for marine propulsion applications that may operate up to 24 hours per day at uninterrupted full power and have load factors* greater than 65 percent. Possible applications: Line hauls tugs and towboats, fish and shrimp trawlers/draggers, and displacement hull fishing boats.
20

ENGINE PERFORMANCE CURVE - John Deere€¦ · Fuel System Air Intake System ECU Description Engine Air Flow 19.1 m3/min 674.5 ft3/min Fuel Injection Pump Intake Manifold Pressure

Apr 13, 2018

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Page 1: ENGINE PERFORMANCE CURVE - John Deere€¦ · Fuel System Air Intake System ECU Description Engine Air Flow 19.1 m3/min 674.5 ft3/min Fuel Injection Pump Intake Manifold Pressure

Rating: M1 - 325hp (242kW) @ 2100 RPM

Application:Marine Model: 6090SFM75

REFERENCE CONDITIONS

Air Intake Restriction…………………………………………………………………. 12 in.H2O (3 kPa)

Exhaust Back Pressure………………………………………………………… 30 in.H2O (7.5 kPa)

Rated speed and power

J1995 and ISO 3046 conditions:

77 ˚F (25 ˚C) air inlet temperature

29.31 in.Hg (99 kPa) barometer

104 ˚F (40 ˚C) fuel inlet temperature

0.853 fuel specific gravity @ 60 ˚F (15.5 ˚C)

Conversion factors:

Power: kW = hp x 0.746

Torque: N·m = lb-ft x 1.356

Designed/Calibrated to meet: Certified by:

• EPA Commercial Marine Tier 2

• IMO MARPOL Annex VI Compliant

• NRMM (97/68/EC), as amended

Ref: Engine Emission Label 16-Sep-12

All values at rated speed, power, and standard conditions, per SAE J1995 unless otherwise noted.

Engine Performance Curves September 2012

Performance Curve: 6090SFM75_A

6090 - Marine

ENGINE PERFORMANCE CURVE

PowerTechTM

9.0L Engine

REFERENCE CONDITIONS Air Intake Restriction......................................................................12 in.H2O (3 kPa) Exhaust Back Pressure................................................................ 30 in.H2O (7.5 kPa) Rated speed and power Gross power guaranteed within ±5% at SAE J1995 and ISO 3046 J1995 and ISO 3046 conditions: 77 ˚F (25 ˚C) air inlet temperature

29.31 in.Hg (99 kPa) barometric pressure 104 ˚F (40 ˚C) fuel inlet temperature 0.853 fuel specific gravity @ 60 ˚F (15.5 ˚C) Ambient air temperature is defined to be the temperature of ambient air close to operating vessel that is not influenced in any manner by operating characteristics of the vessel (free field temp). Conversion factors: Power: kW = hp x 0.746 Fuel: 1 gal = 7.1 lb, 1 L = 0.85 kg Torque: N·m = lb-ft x 1.356 All values from currently available data. Subject to manufacturing and measurement variations and to change without notice. Actual performance is subject to application and operation conditions outside of John Deere control.

0

8

15

23

30

38

45

53

61

0

2

4

6

8

10

12

14

16

900 1100 1300 1500 1700 1900 2100

Fu

el -

L/

hr

Fu

el -

gal/

hr

Engine Speed - RPM

Propeller Fuel

0

37

75

112

149

186

224

261

0

50

100

150

200

250

300

350

900 1100 1300 1500 1700 1900 2100

Po

wer -

kW

Po

wer -

hp

475

610

746

881

1017

1152

1288

1423

1559

350

450

550

650

750

850

950

1050

1150

900 1100 1300 1500 1700 1900 2100

To

rq

ue -

Nm

To

rq

ue -

lb

-ft

Crankshaft

1065 lb-ft (1444 Nm)

Crankshaft

Propeller Power

Notes:

M1: The M1 rating is for marine propulsion applications that may operate up to 24

hours per day at uninterrupted full power and have load factors* greater than 65 percent.

Possible applications: Line hauls tugs and towboats, fish and shrimp

trawlers/draggers, and displacement hull fishing boats.

Page 2: ENGINE PERFORMANCE CURVE - John Deere€¦ · Fuel System Air Intake System ECU Description Engine Air Flow 19.1 m3/min 674.5 ft3/min Fuel Injection Pump Intake Manifold Pressure

General Data Physical Data Model Length to rear face of block 1293 mm 50.9 in

Number of Cylinders Length maximum 1714 mm 67.5 in

Bore 118.4 mm 4.66 in Width maximum 975 mm 38.4 in

Stroke 136 mm 5.35 in Height, crank centerline to top 662 mm 26.1 in

Displacement 9.0 L 549 in3 Height, crank centerline to bottom 320 mm 320 in

Compression Ratio Weight, with oil, no coolant (includes engine, flywheel

Valves per Cylinder, Intake/Exhaust housing, flywheel, and electronics)

Combustion System Center of Gravity Location, X-axis From Rear Face 404 mm 15.9 in

Firing Order of Block

Engine Type Center of Gravity Location, Y-axis Right of Crankshaft -24 mm -0.9 in

Aspiration Center of Gravity Location, Z-axis Above Crankshaft 133 mm 5.2 in

Aftercooling System Max. Allowable Static Bending Moment At Rear Face

Engine Crankcase Vent System of Flywheel Housing with 5-G Load

Thrust Bearing Load Limit, Forward Continuous 8.6 kN 1933 lbf

Cooling System* Thrust Bearing Load Limit, Forward Intermittent 13 kN 2923 lbf

Total Engine to Seawater Heat Rejection** 196 kW 11156 BTU/min Thrust Bearing Load Limit, Rearward Continuous 4 kN 899 lbf

Aftercooler Heat Rejection 42.3 kW 2408 BTU/min Thrust Bearing Load Limit, Rearward Intermittent 6 kN 1349 lbf

Coolant Flow 371 L/min 98 gal/min

Thermostat Start to Open 82 ˚C 180 ˚F Electrical System Thermostat Fully Open 94 ˚C 202 ˚F Min. Recommended Battery Capacity, 12V @32 ˚F (0 ˚C) 1100 amps

Min. Coolant Fill Rate 12 L/min 3.2 gal/min Min. Recommended Battery Capacity, 24V @32 ˚F (0 ˚C) 750 amps

Min. Pressure Cap 110.3 kPa 16 psi Starter Rolling Current, 12V @32 ˚F (0 ˚C) amps

Max. External Coolant Restriction 40 kPa 5.8 psi Starter Rolling Current, 24V @32 ˚F (0 ˚C) amps

Normal Operation Max Top Tank Temperature 100 ˚C 212 ˚F Min. Voltage at ECU during Cranking, 12V volts

≤ 5% of Total Operating Time Top Min. Voltage at ECU during Cranking, 24V volts

Tank Temperature Max. Allowable Start Circuit Resistance, 12V ohms

Absolute Max Top Tank Temperature 110 ˚C 230 ˚F Max. Allowable Start Circuit Resistance, 24V ohms

Recommended Fuel Cooler 15 kW 826 BTU/min Recommended Starter Cable, 12V 100"

Engine Radiated Heat 28 kW 1600 BTU/min Recommended Starter Cable, 24V 100"

Recommended Starter Cable, 12V 200"

Recommended Starter Cable, 24V 200"

Electrical Component Maximum Temperature Limit 125 ˚C 257 ˚F

* The cooling system should be capable of typical at ambient up to the maximum

conditions in which the vessel will operate.

Typical operation is defined as the average load sustainable in the vessel over 10 min.

** Reference 32 ˚C Sea Water Temperature

All values at rated speed, power, and standard conditions, per SAE J1995 unless otherwise noted.

Engine Performance Curves 6090 - Marine Sheet 2 - September 2012

100-110 ˚C ˚F212-230

Performance Curve: 6090SFM75_A

#2

#0000 or 2#00

#0

500

300

#00

6

10

0.002

0.0012

6

16.0:123491066

Engine Installation Criteria

6090SFM75

2/2

Direct injection

kg lb

600 lb-ftNm

1-5-3-6-2-4

In line, 4 Cycle

Turbocharged and Aftercooled

Seawater cooled814

Closed

Page 3: ENGINE PERFORMANCE CURVE - John Deere€¦ · Fuel System Air Intake System ECU Description Engine Air Flow 19.1 m3/min 674.5 ft3/min Fuel Injection Pump Intake Manifold Pressure

Fuel System Air Intake System ECU Description Engine Air Flow 19.1 m

3/min 674.5 ft

3/min

Fuel Injection Pump Intake Manifold Pressure 133 kPa 19.3 psi

Governor Type Manifold Air Temperature 40.4 ˚C 105 ˚F

Volumetric Fuel Consumption 56 L/hr 14.8 gal/hr Maximum Manifold Air Temperature 67 ˚C 153 ˚F

Mass Fuel Consumption 47.6 kg/hr 105 lb/hr Max. Allowable Temperature Rise, Ambient

Total Fuel Volumetric Flow 251 L/hr 66.3 gal/hr Air to Engine Inlet

Total Fuel Mass Flow 213 kg/hr 470 lb/hr Max. Air Intake Restriction, Clean Air Cleaner 3 kPa 12 in.H2O

Max. Fuel Inlet Restriction* 20 kPa 80 in.H2O Max. Air Intake Restriction, Dirty Air Cleaner 6.25 kPa 25 in.H2O

Max. Fuel Inlet Pressure 20 kPa 80 in.H2O Min. Ventilation Area 0.117 m2 182 in

2

Max Fuel Return Pressure 20 kPa 80 in.H2O

Max. Fuel Height Above Transfer Pump 2.4 m 7.9 ft Performance Data Max. Leak-off Return Height 2.4 m 7.9 ft Rated Power 242 kW 325 hp

Max. Fuel Inlet Height Above Fuel Tank Supply 2.4 m 7.9 ft Rated Speed 2100 RPM

Normal Operation Fuel Temperature 40 ˚C 104 ˚F Peak Torque Speed 1600 RPM

Max. Fuel Inlet Temperature 100 ˚C 212 ˚F Low Idle Speed 650 RPM

Min. Recommended Fuel Line Inside Diameter 8.53 mm 0.34 in Rated Torque 1100 Nm 812 ft-lb

Min. Recommended Fuel Line Size 6 (-) AN Peak Torque 1444 Nm 1065 ft-lb

Primary Fuel Filter 10 mic BMEP, Rated 1537 kPa 223 psi

Secondary Fuel Filter 2 mic Rated Pferdestärke (metric hp) 329 ps

Front Drive Capacity, Intermittent 550 Nm 406 lb-ft

Lubrication System Front Drive Capacity, Continuous 468 Nm 345 lb-ft

Oil Pressure at Rated Speed 284 kPa 41 psi

Oil Pressure at Low Idle (800rpm)** 136 kPa 20 psi Exhaust System Max. Crankcase Pressure 2 kPa 8 in.H2O Exhaust Flow 42.5 m

3/min 1501 ft

3/min

Maximum Installed Angle, Front Down 0 deg Exhaust Flow @ gas STP 20.4 m3/min 720 ft

3/min

12 deg Exhaust Temperature 395 ˚C 743 ˚F

20 deg Max. Allowable Exhaust Restriction 7.5 kPa 30 in.H2O

30 deg Max. Shear on Turbocharger Exhaust Outlet 11 kg 24.3 lb

Max. Bending Moment on Turbocharger Exhaust

Seawater Pump System Outlet

Seawater Pump Flow 323 L/min 85 gal/min Min. Exhaust Pipe Diameter, Dry 114.3 mm 4.5 in

Max. Suction Lift 3 m 9.8 ft Min. Exhaust Pipe Diameter, Wet 127 mm 5.0 in

Max. Outlet Pressure 140 kPa 20 psi

Max. Inlet Restriction 30 kPa 4 psi

* With clean filters

** With John Deere Plus-50 IITM

15w-40, not applicable with break in oil.

*** With 1932 option

All values at rated speed, power, and standard conditions, per SAE J1995 unless otherwise noted.

Sheet 2 - September 2012 Engine Performance Curves 6090 - Marine Sheet 3 - September 2012

Engine Angularity Limits Any Direction, Intermittent***

Engine Angularity Limits Any Direction, Continuous***

Maximum Installed Angle, Front Up

7 Nm 15.4 lb-ft

Performance Curve: 6090SFM75_A

Electronic

HPCR

˚C 30 ˚F

Engine Installation Criteria

L14

17

Page 4: ENGINE PERFORMANCE CURVE - John Deere€¦ · Fuel System Air Intake System ECU Description Engine Air Flow 19.1 m3/min 674.5 ft3/min Fuel Injection Pump Intake Manifold Pressure

Engine Performance Data Table

RPM kW hp Nm lb-ft kW hp L/hr gal/hr g/kW-hr

2100 243 325 1103 814 243 325 56.3 14.9 197

2000 242 325 1156 853 210 281 48.3 12.8 196

1900 242 325 1218 898 180 241 42.7 11.3 202

1800 242 325 1284 947 153 205 36.4 9.6 203

1700 242 324 1359 1002 129 173 30.9 8.2 204

1600 242 324 1444 1065 107 144 25.6 6.8 203

1500 213 286 1356 1000 88 119 21.3 5.6 205

1400 178 239 1217 897 72 96 17.7 4.7 210

1300 136 182 995 734 58 77 14.6 3.9 216

1200 106 142 845 623 45 61 11.4 3.0 214

1100 84 112 725 535 35 47 8.9 2.4 218

1000 68 91 645 475 26 35 7.0 1.8 226

* Theoretical 3.0 exponent propeller curve , measured at flywheel

All values at rated speed, power, and standard conditions, per SAE J1995 unless otherwise noted.

Sheet 3 - September 2012 Engine Performance Curves Sheet 4 - September 20126090 - Marine

Performance Curve: 6090SFM75_A

* Prop Power * Prop Fuel * Prop BSFCEngine Speed Crank Power Crank Torque

Engine Installation Criteria

Page 5: ENGINE PERFORMANCE CURVE - John Deere€¦ · Fuel System Air Intake System ECU Description Engine Air Flow 19.1 m3/min 674.5 ft3/min Fuel Injection Pump Intake Manifold Pressure

Rating: M2 - 375hp (280kW) @ 2200 RPM

Application:Marine Model: 6090SFM75

REFERENCE CONDITIONS

Air Intake Restriction…………………………………………………………………. 12 in.H2O (3 kPa)

Exhaust Back Pressure………………………………………………………… 30 in.H2O (7.5 kPa)

Rated speed and power

J1995 and ISO 3046 conditions:

77 ˚F (25 ˚C) air inlet temperature

29.31 in.Hg (99 kPa) barometer

104 ˚F (40 ˚C) fuel inlet temperature

0.853 fuel specific gravity @ 60 ˚F (15.5 ˚C)

Conversion factors:

Power: kW = hp x 0.746

Torque: N·m = lb-ft x 1.356

Designed/Calibrated to meet: Certified by:

• EPA Commercial Marine Tier 2

• IMO MARPOL Annex VI Compliant

• NRMM (97/68/EC), as amended

Ref: Engine Emission Label 16-Sep-12

All values at rated speed, power, and standard conditions, per SAE J1995 unless otherwise noted.

Engine Performance Curves September 20126090 - Marine

Performance Curve: 6090SFM75_B

ENGINE PERFORMANCE CURVE

PowerTechTM

9.0L Engine

REFERENCE CONDITIONS Air Intake Restriction......................................................................12 in.H2O (3 kPa) Exhaust Back Pressure................................................................ 30 in.H2O (7.5 kPa) Rated speed and power Gross power guaranteed within ±5% at SAE J1995 and ISO 3046 J1995 and ISO 3046 conditions: 77 ˚F (25 ˚C) air inlet temperature

29.31 in.Hg (99 kPa) barometric pressure 104 ˚F (40 ˚C) fuel inlet temperature 0.853 fuel specific gravity @ 60 ˚F (15.5 ˚C) Ambient air temperature is defined to be the temperature of ambient air close to operating vessel that is not influenced in any manner by operating characteristics of the vessel (free field temp). Conversion factors: Power: kW = hp x 0.746 Fuel: 1 gal = 7.1 lb, 1 L = 0.85 kg Torque: N·m = lb-ft x 1.356 All values from currently available data. Subject to manufacturing and measurement variations and to change without notice. Actual performance is subject to application and operation conditions outside of John Deere control.

0

11

23

34

45

57

0

3

6

9

12

15

18

900 1100 1300 1500 1700 1900 2100 2300

Fu

el -

L/

hr

Fu

el -

gal/

hr

Engine Speed - RPM

Propeller Fuel

0

56

112

168

224

280

336

0

75

150

225

300

375

450

900 1100 1300 1500 1700 1900 2100 2300

Po

wer -

kW

Po

wer -

hp

475

746

1017

1288

1559

1830

350

550

750

950

1150

1350

900 1100 1300 1500 1700 1900 2100 2300

To

rq

ue -

Nm

To

rq

ue -

lb

-ft Crankshaft

1160 lb-ft (1573 Nm)

Crankshaft

Propeller Power

Notes:

M2: The M2 rating is for marine propulsion applications that typically operate

between 3,000-5,000 hours per year and have load factors up to 65 percent. This rating is for applications that are in continuous use and use full power for no more than 16 hours of each 24 hours of operation. The remaining time of operation is at or below cruising speed.

Possible applications: Short-range tugs and towboats long-range ferryboats,

large passenger vessels and offshore displacement hull fishing boats

Page 6: ENGINE PERFORMANCE CURVE - John Deere€¦ · Fuel System Air Intake System ECU Description Engine Air Flow 19.1 m3/min 674.5 ft3/min Fuel Injection Pump Intake Manifold Pressure

General Data Physical Data Model Length to rear face of block 1293 mm 50.9 in

Number of Cylinders Length maximum 1714 mm 67.5 in

Bore 118.4 mm 4.66 in Width maximum 975 mm 38.4 in

Stroke 136 mm 5.35 in Height, crank centerline to top 662 mm 26.1 in

Displacement 9.0 L 549 in3 Height, crank centerline to bottom 320 mm 320 in

Compression Ratio Weight, with oil, no coolant (includes engine, flywheel

Valves per Cylinder, Intake/Exhaust housing, flywheel, and electronics)

Combustion System Center of Gravity Location, X-axis From Rear Face 404 mm 15.9 in

Firing Order of Block

Engine Type Center of Gravity Location, Y-axis Right of Crankshaft -24 mm -0.9 in

Aspiration Center of Gravity Location, Z-axis Above Crankshaft 133 mm 5.2 in

Aftercooling System Max. Allowable Static Bending Moment At Rear Face

Engine Crankcase Vent System of Flywheel Housing with 5-G Load

Thrust Bearing Load Limit, Forward Continuous 8.6 kN 1933 lbf

Cooling System* Thrust Bearing Load Limit, Forward Intermittent 13 kN 2923 lbf

Total Engine to Seawater Heat Rejection** 226.5 kW 12892 BTU/min Thrust Bearing Load Limit, Rearward Continuous 4 kN 899 lbf

Aftercooler Heat Rejection 58.8 kW 3347 BTU/min Thrust Bearing Load Limit, Rearward Intermittent 6 kN 1349 lbf

Coolant Flow 390 L/min 103 gal/min

Thermostat Start to Open 82 ˚C 180 ˚F Electrical System Thermostat Fully Open 94 ˚C 202 ˚F Min. Recommended Battery Capacity, 12V @32 ˚F (0 ˚C) 1100 amps

Min. Coolant Fill Rate 12 L/min 3.2 gal/min Min. Recommended Battery Capacity, 24V @32 ˚F (0 ˚C) 750 amps

Min. Pressure Cap 110.3 kPa 16 psi Starter Rolling Current, 12V @32 ˚F (0 ˚C) amps

Max. External Coolant Restriction 40 kPa 5.8 psi Starter Rolling Current, 24V @32 ˚F (0 ˚C) amps

Normal Operation Max Top Tank Temperature 100 ˚C 212 ˚F Min. Voltage at ECU during Cranking, 12V volts

≤ 5% of Total Operating Time Top Min. Voltage at ECU during Cranking, 24V volts

Tank Temperature Max. Allowable Start Circuit Resistance, 12V ohms

Absolute Max Top Tank Temperature 110 ˚C 230 ˚F Max. Allowable Start Circuit Resistance, 24V ohms

Recommended Fuel Cooler 14 kW 792 BTU/min Recommended Starter Cable, 12V 100"

Engine Radiated Heat 32 kW 1829 BTU/min Recommended Starter Cable, 24V 100"

Recommended Starter Cable, 12V 200"

Recommended Starter Cable, 24V 200"

Electrical Component Maximum Temperature Limit 125 ˚C 257 ˚F

* The cooling system should be capable of typical at ambient up to the maximum

conditions in which the vessel will operate.

Typical operation is defined as the average load sustainable in the vessel over 10 min.

** Reference 32 ˚C Sea Water Temperature

All values at rated speed, power, and standard conditions, per SAE J1995 unless otherwise noted.

Engine Performance Curves 6090 - Marine Sheet 2 - September 2012

#2

#0000 or 2#00

#0

Performance Curve: 6090SFM75_B

0.0012

#00

6

10

600

0.002

Nm lb-ft

500

300

16.0:11066 2349

2/2kg lb

Engine Installation Criteria

6090SFM75

6

100-110 ˚C 212-230 ˚F

1-5-3-6-2-4

Direct injection

In line, 4 Cycle

Turbocharged and Aftercooled

Seawater cooled814

Closed

Page 7: ENGINE PERFORMANCE CURVE - John Deere€¦ · Fuel System Air Intake System ECU Description Engine Air Flow 19.1 m3/min 674.5 ft3/min Fuel Injection Pump Intake Manifold Pressure

Fuel System Air Intake System ECU Description Engine Air Flow 22.7 m

3/min 801.6 ft

3/min

Fuel Injection Pump Intake Manifold Pressure 169.7 kPa 24.6 psi

Governor Type Manifold Air Temperature 42 ˚C 108 ˚F

Volumetric Fuel Consumption 64 L/hr 16.9 gal/hr Maximum Manifold Air Temperature 67 ˚C 153 ˚F

Mass Fuel Consumption 54.4 kg/hr 120 lb/hr Max. Allowable Temperature Rise, Ambient

Total Fuel Volumetric Flow 251 L/hr 66.3 gal/hr Air to Engine Inlet

Total Fuel Mass Flow 213 kg/hr 470 lb/hr Max. Air Intake Restriction, Clean Air Cleaner 3 kPa 12 in.H2O

Max. Fuel Inlet Restriction* 20 kPa 80 in.H2O Max. Air Intake Restriction, Dirty Air Cleaner 6.25 kPa 25 in.H2O

Max. Fuel Inlet Pressure 20 kPa 80 in.H2O Min. Ventilation Area 0.14 m2 216 in

2

Max Fuel Return Pressure 20 kPa 80 in.H2O

Max. Fuel Height Above Transfer Pump 2.4 m 7.9 ft Performance Data Max. Leak-off Return Height 2.4 m 7.9 ft Rated Power 280 kW 375 hp

Max. Fuel Inlet Height Above Fuel Tank Supply 2.4 m 7.9 ft Rated Speed 2200 RPM

Normal Operation Fuel Temperature 40 ˚C 104 ˚F Peak Torque Speed 1700 RPM

Max. Fuel Inlet Temperature 100 ˚C 212 ˚F Low Idle Speed 650 RPM

Min. Recommended Fuel Line Inside Diameter 8.53 mm 0.34 in Rated Torque 1215 Nm 896 ft-lb

Min. Recommended Fuel Line Size 6 (-) AN Peak Torque 1573 Nm 1160 ft-lb

Primary Fuel Filter 10 mic BMEP, Rated 1697 kPa 246 psi

Secondary Fuel Filter 2 mic Rated Pferdestärke (metric hp) 329 ps

Front Drive Capacity, Intermittent 550 Nm 406 lb-ft

Lubrication System Front Drive Capacity, Continuous 468 Nm 345 lb-ft

Oil Pressure at Rated Speed 284 kPa 41 psi

Oil Pressure at Low Idle (800rpm)** 136 kPa 20 psi Exhaust System Max. Crankcase Pressure 2 kPa 8 in.H2O Exhaust Flow 49 m

3/min 1730 ft

3/min

Maximum Installed Angle, Front Down 0 deg Exhaust Flow @ gas STP 24.3 m3/min 858 ft

3/min

12 deg Exhaust Temperature 371 ˚C 700 ˚F

20 deg Max. Allowable Exhaust Restriction 7.5 kPa 30 in.H2O

30 deg Max. Shear on Turbocharger Exhaust Outlet 11 kg 24.3 lb

Max. Bending Moment on Turbocharger Exhaust

Seawater Pump System Outlet

Seawater Pump Flow 338 L/min 89 gal/min Min. Exhaust Pipe Diameter, Dry 114.3 mm 4.5 in

Max. Suction Lift 3 m 9.8 ft Min. Exhaust Pipe Diameter, Wet 127 mm 5.0 in

Max. Outlet Pressure 140 kPa 20 psi

Max. Inlet Restriction 30 kPa 4 psi

* With clean filters

** With John Deere Plus-50 IITM

15w-40, not applicable with break in oil.

*** With 1932 option

All values at rated speed, power, and standard conditions, per SAE J1995 unless otherwise noted.

Sheet 2 - September 2012 Engine Performance Curves 6090 - Marine Sheet 3 - September 2012

7 Nm 15.4 lb-ft

Performance Curve: 6090SFM75_B

Engine Angularity Limits Any Direction, Continuous***

Engine Angularity Limits Any Direction, Intermittent***

Maximum Installed Angle, Front Up

17 ˚C 30 ˚F

Engine Installation Criteria

L14

Electronic

HPCR

Page 8: ENGINE PERFORMANCE CURVE - John Deere€¦ · Fuel System Air Intake System ECU Description Engine Air Flow 19.1 m3/min 674.5 ft3/min Fuel Injection Pump Intake Manifold Pressure

Engine Performance Data Table

RPM kW hp Nm lb-ft kW hp L/hr gal/hr g/kW-hr

2200 279 375 1213 895 279 375 64 17 194

2100 280 375 1273 939 243 326 56 15 196

2000 280 375 1337 986 210 282 49 13 199

1900 280 375 1407 1038 180 241 42 11 198

1800 280 375 1485 1095 153 205 36 10 200

1700 280 376 1573 1160 129 173 31 8 202

1600 257 344 1532 1130 107 144 26 7 203

1500 213 286 1356 1000 89 119 21 6 204

1400 179 240 1220 900 72 97 18 5 209

1300 136 182 996 734 58 77 15 4 214

1200 106 142 845 623 45 61 11 3 214

1100 84 112 726 535 35 47 9 2 215

1000 67 89 636 469 26 35 7 2 225

* Theoretical 3.0 exponent propeller curve , measured at flywheel

All values at rated speed, power, and standard conditions, per SAE J1995 unless otherwise noted.

Sheet 3 - September 2012 Engine Performance Curves Sheet 4 - September 20126090 - Marine

Performance Curve: 6090SFM75_B

Engine Speed Crank Power Crank Torque

Engine Installation Criteria

* Prop Power * Prop Fuel * Prop BSFC

Page 9: ENGINE PERFORMANCE CURVE - John Deere€¦ · Fuel System Air Intake System ECU Description Engine Air Flow 19.1 m3/min 674.5 ft3/min Fuel Injection Pump Intake Manifold Pressure

Rating: M3 - 425hp (317kW) @ 2300 RPM

Application:Marine Model: 6090SFM75

REFERENCE CONDITIONS

Air Intake Restriction…………………………………………………………………. 12 in.H2O (3 kPa)

Exhaust Back Pressure………………………………………………………… 30 in.H2O (7.5 kPa)

Rated speed and power

J1995 and ISO 3046 conditions:

77 ˚F (25 ˚C) air inlet temperature

29.31 in.Hg (99 kPa) barometer

104 ˚F (40 ˚C) fuel inlet temperature

0.853 fuel specific gravity @ 60 ˚F (15.5 ˚C)

Conversion factors:

Power: kW = hp x 0.746

Fuel: 1 gal = 7.1 lb, 1 L = 0.85 kg

Torque: N·m = lb-ft x 1.356

Designed/Calibrated to meet: Certified by:

• EPA Commercial Marine Tier 2

• IMO MARPOL Annex VI Compliant

• NRMM (97/68/EC), as amended

Ref: Engine Emission Label 16-Sep-12

All values at rated speed, power, and standard conditions, per SAE J1995 unless otherwise noted.

Engine Performance Curves September 20126090 - Marine

Performance Curve: 6090SFM75_C

ENGINE PERFORMANCE CURVE

PowerTechTM

9.0L Engine

REFERENCE CONDITIONS Air Intake Restriction......................................................................12 in.H2O (3 kPa) Exhaust Back Pressure................................................................ 30 in.H2O (7.5 kPa) Rated speed and power Gross power guaranteed within ±5% at SAE J1995 and ISO 3046 J1995 and ISO 3046 conditions: 77 ˚F (25 ˚C) air inlet temperature

29.31 in.Hg (99 kPa) barometric pressure 104 ˚F (40 ˚C) fuel inlet temperature 0.853 fuel specific gravity @ 60 ˚F (15.5 ˚C) Ambient air temperature is defined to be the temperature of ambient air close to operating vessel that is not influenced in any manner by operating characteristics of the vessel (free field temp). Conversion factors: Power: kW = hp x 0.746 Fuel: 1 gal = 7.1 lb, 1 L = 0.85 kg Torque: N·m = lb-ft x 1.356 All values from currently available data. Subject to manufacturing and measurement variations and to change without notice. Actual performance is subject to application and operation conditions outside of John Deere control.

0

19

38

57

75

94

0

5

10

15

20

25

900 1100 1300 1500 1700 1900 2100 2300

Fu

el -

L/

hr

Fu

el -

gal/

hr

Engine Speed - RPM

Propeller Fuel

0

75

149

224

298

373

0

100

200

300

400

500

900 1100 1300 1500 1700 1900 2100 2300

Po

wer -

kW

Po

wer -

hp

475

746

1017

1288

1559

1830

350

550

750

950

1150

1350

900 1100 1300 1500 1700 1900 2100 2300

To

rq

ue -

Nm

To

rq

ue -

lb

-ft

Crankshaft

1267 lb-ft (1718 Nm)

Crankshaft

Propeller Power

Notes:

M3: The M3 rating is for marine propulsion applications that typically operate between

2,000-4,000 hours per year and have load factors up to 50 percent. This rating is for applications that use full power for no more than 4 hours out of each 12 hours of operation. The remaining time of operation is at or below cruising speed.

Possible applications: Coastal fishing boats offshore crew boats, research boats.

Short range ferryboats and dinner cruise boats.

Page 10: ENGINE PERFORMANCE CURVE - John Deere€¦ · Fuel System Air Intake System ECU Description Engine Air Flow 19.1 m3/min 674.5 ft3/min Fuel Injection Pump Intake Manifold Pressure

General Data Physical Data Model Length to rear face of block 1293 mm 50.9 in

Number of Cylinders Length maximum 1714 mm 67.5 in

Bore 118.4 mm 4.66 in Width maximum 975 mm 38.4 in

Stroke 136 mm 5.35 in Height, crank centerline to top 662 mm 26.1 in

Displacement 9.0 L 549 in3 Height, crank centerline to bottom 320 mm 320 in

Compression Ratio Weight, with oil, no coolant (includes engine, flywheel

Valves per Cylinder, Intake/Exhaust housing, flywheel, and electronics)

Combustion System Center of Gravity Location, X-axis From Rear Face 404 mm 15.9 in

Firing Order of Block

Engine Type Center of Gravity Location, Y-axis Right of Crankshaft -24 mm -0.9 in

Aspiration Center of Gravity Location, Z-axis Above Crankshaft 133 mm 5.2 in

Aftercooling System Max. Allowable Static Bending Moment At Rear Face

Engine Crankcase Vent System of Flywheel Housing with 5-G Load

Thrust Bearing Load Limit, Forward Continuous 8.6 kN 1933 lbf

Cooling System* Thrust Bearing Load Limit, Forward Intermittent 13 kN 2923 lbf

Total Engine to Seawater Heat Rejection** 264 kW 15027 BTU/min Thrust Bearing Load Limit, Rearward Continuous 4 kN 899 lbf

Aftercooler Heat Rejection 79.6 kW 4531 BTU/min Thrust Bearing Load Limit, Rearward Intermittent 6 kN 1349 lbf

Coolant Flow 409 L/min 108 gal/min

Thermostat Start to Open 82 ˚C 180 ˚F Electrical System Thermostat Fully Open 94 ˚C 202 ˚F Min. Recommended Battery Capacity, 12V @32 ˚F (0 ˚C) 1100 amps

Min. Coolant Fill Rate 12 L/min 3.2 gal/min Min. Recommended Battery Capacity, 24V @32 ˚F (0 ˚C) 750 amps

Min. Pressure Cap 110.3 kPa 16 psi Starter Rolling Current, 12V @32 ˚F (0 ˚C) amps

Max. External Coolant Restriction 40 kPa 5.8 psi Starter Rolling Current, 24V @32 ˚F (0 ˚C) amps

Normal Operation Max Top Tank Temperature 100 ˚C 212 ˚F Min. Voltage at ECU during Cranking, 12V volts

≤ 5% of Total Operating Time Top Min. Voltage at ECU during Cranking, 24V volts

Tank Temperature Max. Allowable Start Circuit Resistance, 12V ohms

Absolute Max Top Tank Temperature 110 ˚C 230 ˚F Max. Allowable Start Circuit Resistance, 24V ohms

Recommended Fuel Cooler 13 kW 755 BTU/min Recommended Starter Cable, 12V 100"

Engine Radiated Heat 36 kW 2076 BTU/min Recommended Starter Cable, 24V 100"

Recommended Starter Cable, 12V 200"

Recommended Starter Cable, 24V 200"

Electrical Component Maximum Temperature Limit 125 ˚C 257 ˚F

* The cooling system should be capable of typical at ambient up to the maximum

conditions in which the vessel will operate.

Typical operation is defined as the average load sustainable in the vessel over 10 min.

** Reference 32 ˚C Sea Water Temperature

All values at rated speed, power, and standard conditions, per SAE J1995 unless otherwise noted.

Engine Performance Curves 6090 - Marine Sheet 2 - September 2012

#00

#2

#0000 or 2#00

#0

Performance Curve: 6090SFM75_C

600

0.002

lb-ft

0.0012

16.0:11066 2349

2/2kg lb

Engine Installation Criteria

6090SFM75

6

Direct injection

10

In line, 4 Cycle

Turbocharged and Aftercooled

Seawater cooled814 Nm

Closed

500

100-110 ˚C 212-230 ˚F

1-5-3-6-2-4

300

6

Page 11: ENGINE PERFORMANCE CURVE - John Deere€¦ · Fuel System Air Intake System ECU Description Engine Air Flow 19.1 m3/min 674.5 ft3/min Fuel Injection Pump Intake Manifold Pressure

Fuel System Air Intake System ECU Description Engine Air Flow 27.2 m

3/min 960.6 ft

3/min

Fuel Injection Pump Intake Manifold Pressure 212.2 kPa 30.8 psi

Governor Type Manifold Air Temperature 46.8 ˚C 116 ˚F

Volumetric Fuel Consumption 72.7 L/hr 19.2 gal/hr Maximum Manifold Air Temperature 67 ˚C 153 ˚F

Mass Fuel Consumption 61.8 kg/hr 136 lb/hr Max. Allowable Temperature Rise, Ambient

Total Fuel Volumetric Flow 251 L/hr 66.3 gal/hr Air to Engine Inlet

Total Fuel Mass Flow 213 kg/hr 470 lb/hr Max. Air Intake Restriction, Clean Air Cleaner 3 kPa 12 in.H2O

Max. Fuel Inlet Restriction* 20 kPa 80 in.H2O Max. Air Intake Restriction, Dirty Air Cleaner 6.25 kPa 25 in.H2O

Max. Fuel Inlet Pressure 20 kPa 80 in.H2O Min. Ventilation Area 0.167 m2 259 in

2

Max Fuel Return Pressure 20 kPa 80 in.H2O

Max. Fuel Height Above Transfer Pump 2.4 m 7.9 ft Performance Data Max. Leak-off Return Height 2.4 m 7.9 ft Rated Power 317 kW 425 hp

Max. Fuel Inlet Height Above Fuel Tank Supply 2.4 m 7.9 ft Rated Speed 2300 RPM

Normal Operation Fuel Temperature 40 ˚C 104 ˚F Peak Torque Speed 1700 RPM

Max. Fuel Inlet Temperature 100 ˚C 212 ˚F Low Idle Speed 650 RPM

Min. Recommended Fuel Line Inside Diameter 8.53 mm 0.34 in Rated Torque 1316 Nm 971 ft-lb

Min. Recommended Fuel Line Size 6 (-) AN Peak Torque 1718 Nm 1267 ft-lb

Primary Fuel Filter 10 mic BMEP, Rated 1838 kPa 266 psi

Secondary Fuel Filter 2 mic Rated Pferdestärke (metric hp) 431 ps

Front Drive Capacity, Intermittent 550 Nm 406 lb-ft

Lubrication System Front Drive Capacity, Continuous 468 Nm 345 lb-ft

Oil Pressure at Rated Speed 284 kPa 41 psi

Oil Pressure at Low Idle (800rpm)** 136 kPa 20 psi Exhaust System Max. Crankcase Pressure 2 kPa 8 in.H2O Exhaust Flow 56 m

3/min 1978 ft

3/min

Maximum Installed Angle, Front Down 0 deg Exhaust Flow @ gas STP 28.4 m3/min 1003 ft

3/min

12 deg Exhaust Temperature 360 ˚C 680 ˚F

20 deg Max. Allowable Exhaust Restriction 7.5 kPa 30 in.H2O

30 deg Max. Shear on Turbocharger Exhaust Outlet 11 kg 24.3 lb

Max. Bending Moment on Turbocharger Exhaust

Seawater Pump System Outlet

Seawater Pump Flow 354 L/min 94 gal/min Min. Exhaust Pipe Diameter, Dry 127 mm 5.0 in

Max. Suction Lift 3 m 9.8 ft Min. Exhaust Pipe Diameter, Wet 139.7 mm 5.5 in

Max. Outlet Pressure 140 kPa 20 psi

Max. Inlet Restriction 30 kPa 4 psi

* With clean filters

** With John Deere Plus-50 IITM

15w-40, not applicable with break in oil.

*** With 1932 option

All values at rated speed, power, and standard conditions, per SAE J1995 unless otherwise noted.

Sheet 2 - September 2012 Engine Performance Curves 6090 - Marine Sheet 3 - September 2012

Engine Angularity Limits Any Direction, Intermittent***

7 Nm 15.4 lb-ft

Performance Curve: 6090SFM75_C

Maximum Installed Angle, Front Up

Engine Angularity Limits Any Direction, Continuous***

17 ˚C 30 ˚F

Engine Installation Criteria

L14

Electronic

HPCR

Page 12: ENGINE PERFORMANCE CURVE - John Deere€¦ · Fuel System Air Intake System ECU Description Engine Air Flow 19.1 m3/min 674.5 ft3/min Fuel Injection Pump Intake Manifold Pressure

Engine Performance Data Table

RPM kW hp Nm lb-ft kW hp L/hr gal/hr g/kW-hr

2300 317 425 1315 970 317 425 74 20 200

2200 317 425 1375 1014 277 372 65 17 200

2100 317 425 1441 1063 241 323 56 15 199

2000 317 425 1514 1117 208 279 48 13 197

1900 317 425 1593 1175 179 239 42 11 201

1800 316 424 1677 1237 152 204 36 10 203

1700 306 410 1718 1267 128 172 31 8 205

1600 257 344 1532 1130 107 143 26 7 206

1500 213 286 1356 1000 88 118 22 6 211

1400 178 239 1215 896 71 96 18 5 213

1300 135 182 995 734 57 77 15 4 217

1200 106 142 845 623 45 60 11 3 215

1100 83 112 725 535 35 46 9 2 221

1000 68 91 645 476 26 35 7 2 227

* Theoretical 3.0 exponent propeller curve , measured at flywheel

All values at rated speed, power, and standard conditions, per SAE J1995 unless otherwise noted.

Sheet 3 - September 2012 Engine Performance Curves Sheet 4 - September 20126090 - Marine

Performance Curve: 6090SFM75_C

Engine Speed Crank Power Crank Torque

Engine Installation Criteria

* Prop Power * Prop Fuel * Prop BSFC

Page 13: ENGINE PERFORMANCE CURVE - John Deere€¦ · Fuel System Air Intake System ECU Description Engine Air Flow 19.1 m3/min 674.5 ft3/min Fuel Injection Pump Intake Manifold Pressure

Rating: M4 - 500hp (373kW) @ 2400 RPM

Application:Marine Model: 6090SFM75

REFERENCE CONDITIONS

Air Intake Restriction…………………………………………………………………. 12 in.H2O (3 kPa)

Exhaust Back Pressure………………………………………………………… 30 in.H2O (7.5 kPa)

Rated speed and power

J1995 and ISO 3046 conditions:

77 ˚F (25 ˚C) air inlet temperature

29.31 in.Hg (99 kPa) barometer

104 ˚F (40 ˚C) fuel inlet temperature

0.853 fuel specific gravity @ 60 ˚F (15.5 ˚C)

Conversion factors:

Power: kW = hp x 0.746

Torque: N·m = lb-ft x 1.356

Designed/Calibrated to meet: Certified by:

• EPA Commercial Marine Tier 2

• IMO MARPOL Annex VI Compliant

• NRMM (97/68/EC), as amended

Ref: Engine Emission Label 16-Sep-12

All values at rated speed, power, and standard conditions, per SAE J1995 unless otherwise noted.

Engine Performance Curves September 20126090 - Marine

Performance Curve: 6090SFM75_D

ENGINE PERFORMANCE CURVE

PowerTechTM

9.0L Engine

REFERENCE CONDITIONS Air Intake Restriction......................................................................12 in.H2O (3 kPa) Exhaust Back Pressure................................................................ 30 in.H2O (7.5 kPa) Rated speed and power Gross power guaranteed within ±5% at SAE J1995 and ISO 3046 J1995 and ISO 3046 conditions: 77 ˚F (25 ˚C) air inlet temperature

29.31 in.Hg (99 kPa) barometric pressure 104 ˚F (40 ˚C) fuel inlet temperature 0.853 fuel specific gravity @ 60 ˚F (15.5 ˚C) Ambient air temperature is defined to be the temperature of ambient air close to operating vessel that is not influenced in any manner by operating characteristics of the vessel (free field temp). Conversion factors: Power: kW = hp x 0.746 Fuel: 1 gal = 7.1 lb, 1 L = 0.85 kg Torque: N·m = lb-ft x 1.356 All values from currently available data. Subject to manufacturing and measurement variations and to change without notice. Actual performance is subject to application and operation conditions outside of John Deere control.

0

19

38

57

76

0

5

10

15

20

25

900 1100 1300 1500 1700 1900 2100 2300 2500

Fu

el -

L/

hr

Fu

el -

gal/

hr

Engine Speed - RPM

Propeller Fuel

0

75

149

224

298

373

447

0

100

200

300

400

500

600

900 1100 1300 1500 1700 1900 2100 2300 2500

Po

wer -

kW

Po

wer -

hp

475

746

1017

1288

1559

1830

350

550

750

950

1150

1350

900 1100 1300 1500 1700 1900 2100 2300 2500

To

rq

ue -

Nm

To

rq

ue -

lb

-ft

Crankshaft

1294 lb-ft (1755 Nm)

Crankshaft

Propeller Power

Notes:

M4: The M4 rating is for marine propulsion applications that typically operate between

1,000-3,000 hours per year and have load factors below 40 percent. This rating is for applications that use full power no more than 1 hour out of each 12 hours of operation. The remaining time of operation is at or below cruising speed.

Possible applications: Inshore crew boats, charter fishing boats, pilot boats, dive

boats, and planning hull commercial fishing boats.

Page 14: ENGINE PERFORMANCE CURVE - John Deere€¦ · Fuel System Air Intake System ECU Description Engine Air Flow 19.1 m3/min 674.5 ft3/min Fuel Injection Pump Intake Manifold Pressure

General Data Physical Data Model Length to rear face of block 1293 mm 50.9 in

Number of Cylinders Length maximum 1714 mm 67.5 in

Bore 118.4 mm 4.66 in Width maximum 975 mm 38.4 in

Stroke 136 mm 5.35 in Height, crank centerline to top 662 mm 26.1 in

Displacement 9.0 L 549 in3 Height, crank centerline to bottom 320 mm 320 in

Compression Ratio Weight, with oil, no coolant (includes engine, flywheel

Valves per Cylinder, Intake/Exhaust housing, flywheel, and electronics)

Combustion System Center of Gravity Location, X-axis From Rear Face 404 mm 15.9 in

Firing Order of Block

Engine Type Center of Gravity Location, Y-axis Right of Crankshaft -24 mm -0.9 in

Aspiration Center of Gravity Location, Z-axis Above Crankshaft 133 mm 5.2 in

Aftercooling System Max. Allowable Static Bending Moment At Rear Face

Engine Crankcase Vent System of Flywheel Housing with 5-G Load

Thrust Bearing Load Limit, Forward Continuous 8.6 kN 1933 lbf

Cooling System* Thrust Bearing Load Limit, Forward Intermittent 13 kN 2923 lbf

Total Engine to Seawater Heat Rejection** 317 kW 18044 BTU/min Thrust Bearing Load Limit, Rearward Continuous 4 kN 899 lbf

Aftercooler Heat Rejection 101.3 kW 5766 BTU/min Thrust Bearing Load Limit, Rearward Intermittent 6 kN 1349 lbf

Coolant Flow 425 L/min 112 gal/min

Thermostat Start to Open 82 ˚C 180 ˚F Electrical System

Thermostat Fully Open 94 ˚C 202 ˚F Min. Recommended Battery Capacity, 12V @32 ˚F (0 ˚C) 1100 amps

Min. Coolant Fill Rate 12 L/min 3.2 gal/min Min. Recommended Battery Capacity, 24V @32 ˚F (0 ˚C) 750 amps

Min. Pressure Cap 110.3 kPa 16 psi Starter Rolling Current, 12V @32 ˚F (0 ˚C) amps

Max. External Coolant Restriction 40 kPa 5.8 psi Starter Rolling Current, 24V @32 ˚F (0 ˚C) amps

Normal Operation Max Top Tank Temperature 100 ˚C 212 ˚F Min. Voltage at ECU during Cranking, 12V volts

≤ 5% of Total Operating Time Top Min. Voltage at ECU during Cranking, 24V volts

Tank Temperature Max. Allowable Start Circuit Resistance, 12V ohms

Absolute Max Top Tank Temperature 110 ˚C 230 ˚F Max. Allowable Start Circuit Resistance, 24V ohms

Recommended Fuel Cooler 12 kW 694 BTU/min Recommended Starter Cable, 12V 100"

Engine Radiated Heat 44 kW 2486 BTU/min Recommended Starter Cable, 24V 100"

Recommended Starter Cable, 12V 200"

Recommended Starter Cable, 24V 200"

Electrical Component Maximum Temperature Limit 125 ˚C 257 ˚F

* The cooling system should be capable of typical at ambient up to the maximum

conditions in which the vessel will operate.

Typical operation is defined as the average load sustainable in the vessel over 10 min.

** Reference 32 ˚C Sea Water Temperature

All values at rated speed, power, and standard conditions, per SAE J1995 unless otherwise noted.

Engine Performance Curves 6090 - Marine Sheet 2 - September 2012

#00

#2

#0000 or 2#00

#0

Performance Curve: 6090SFM75_D

600

0.002

lb-ft

0.0012

16.0:11066 2349

2/2kg lb

Engine Installation Criteria

6090SFM75

6

Direct injection

10

In line, 4 Cycle

Turbocharged and Aftercooled

Seawater cooled814 Nm

Closed

500

100-110 ˚C 212-230 ˚F

1-5-3-6-2-4

300

6

Page 15: ENGINE PERFORMANCE CURVE - John Deere€¦ · Fuel System Air Intake System ECU Description Engine Air Flow 19.1 m3/min 674.5 ft3/min Fuel Injection Pump Intake Manifold Pressure

Fuel System Air Intake System ECU Description Engine Air Flow 30.6 m

3/min 1081 ft

3/min

Fuel Injection Pump Intake Manifold Pressure 246 kPa 35.7 psi

Governor Type Manifold Air Temperature 48.7 ˚C 120 ˚F

Volumetric Fuel Consumption 87 L/hr 23.0 gal/hr Maximum Manifold Air Temperature 67 ˚C 153 ˚F

Mass Fuel Consumption 74 kg/hr 163 lb/hr Max. Allowable Temperature Rise, Ambient

Total Fuel Volumetric Flow 251 L/hr 66.3 gal/hr Air to Engine Inlet

Total Fuel Mass Flow 213 kg/hr 470 lb/hr Max. Air Intake Restriction, Clean Air Cleaner 3 kPa 12 in.H2O

Max. Fuel Inlet Restriction* 20 kPa 80 in.H2O Max. Air Intake Restriction, Dirty Air Cleaner 6.25 kPa 25 in.H2O

Max. Fuel Inlet Pressure 20 kPa 80 in.H2O Min. Ventilation Area 0.188 m2 292 in

2

Max Fuel Return Pressure 20 kPa 80 in.H2O

Max. Fuel Height Above Transfer Pump 2.4 m 7.9 ft Performance Data Max. Leak-off Return Height 2.4 m 7.9 ft Rated Power 373 kW 500 hp

Max. Fuel Inlet Height Above Fuel Tank Supply 2.4 m 7.9 ft Rated Speed 2400 RPM

Normal Operation Fuel Temperature 40 ˚C 104 ˚F Peak Torque Speed 1800 RPM

Max. Fuel Inlet Temperature 100 ˚C 212 ˚F Low Idle Speed 650 RPM

Min. Recommended Fuel Line Inside Diameter 8.53 mm 0.34 in Rated Torque 1484 Nm 1095 ft-lb

Min. Recommended Fuel Line Size 6 (-) AN Peak Torque 1755 Nm 1294 ft-lb

Primary Fuel Filter 10 mic BMEP, Rated 2072 kPa 300 psi

Secondary Fuel Filter 2 mic Rated Pferdestärke (metric hp) 507 ps

Front Drive Capacity, Intermittent 550 Nm 406 lb-ft

Lubrication System Front Drive Capacity, Continuous 468 Nm 345 lb-ft

Oil Pressure at Rated Speed 284 kPa 41 psi

Oil Pressure at Low Idle (800rpm)** 136 kPa 20 psi Exhaust System Max. Crankcase Pressure 2 kPa 8 in.H2O Exhaust Flow 66.2 m

3/min 2338 ft

3/min

Maximum Installed Angle, Front Down 0 deg Exhaust Flow @ gas STP 32.6 m3/min 1151 ft

3/min

12 deg Exhaust Temperature 383 ˚C 721 ˚F

20 deg Max. Allowable Exhaust Restriction 7.5 kPa 30 in.H2O

30 deg Max. Shear on Turbocharger Exhaust Outlet 11 kg 24.3 lb

Max. Bending Moment on Turbocharger Exhaust

Seawater Pump System Outlet

Seawater Pump Flow 369 L/min 97 gal/min Min. Exhaust Pipe Diameter, Dry 127 mm 5.0 in

Max. Suction Lift 3 m 9.8 ft Min. Exhaust Pipe Diameter, Wet 139.7 mm 5.5 in

Max. Outlet Pressure 140 kPa 20 psi

Max. Inlet Restriction 30 kPa 4 psi

* With clean filters

** With John Deere Plus-50 IITM

15w-40, not applicable with break in oil.

*** With 1932 option

All values at rated speed, power, and standard conditions, per SAE J1995 unless otherwise noted.

Sheet 2 - September 2012 Engine Performance Curves 6090 - Marine Sheet 3 - September 2012

Engine Angularity Limits Any Direction, Intermittent***

7 Nm 15.4 lb-ft

Performance Curve: 6090SFM75_D

Maximum Installed Angle, Front Up

Engine Angularity Limits Any Direction, Continuous***

17 ˚C 30 ˚F

Engine Installation Criteria

L14

Electronic

HPCR

Page 16: ENGINE PERFORMANCE CURVE - John Deere€¦ · Fuel System Air Intake System ECU Description Engine Air Flow 19.1 m3/min 674.5 ft3/min Fuel Injection Pump Intake Manifold Pressure

Engine Performance Data Table

RPM kW hp Nm lb-ft kW hp L/hr gal/hr g/kW-hr

2400 373 500 1485 1095 373 500 88 23 202

2300 373 500 1548 1142 328 441 76 20 197

2200 373 500 1618 1193 287 386 67 18 197

2100 373 500 1695 1250 250 335 58 15 196

2000 365 489 1741 1284 216 290 49 13 194

1900 347 466 1745 1287 185 248 42 11 194

1800 331 444 1755 1294 157 211 36 10 197

1700 303 406 1701 1254 133 178 31 8 199

1600 255 343 1525 1125 111 148 26 7 201

1500 213 286 1356 1000 91 122 22 6 205

1400 179 240 1219 899 74 99 18 5 205

1300 135 182 995 734 59 80 14 4 207

1200 106 142 845 623 47 63 11 3 205

1100 84 112 725 535 36 48 9 2 212

1000 66 88 629 464 27 36 7 2 218

* Theoretical 3.0 exponent propeller curve , measured at flywheel

All values at rated speed, power, and standard conditions, per SAE J1995 unless otherwise noted.

Sheet 3 - September 2012 Engine Performance Curves Sheet 4 - September 20126090 - Marine

Performance Curve: 6090SFM75_D

Engine Speed Crank Power Crank Torque

Engine Installation Criteria

* Prop Power * Prop Fuel * Prop BSFC

Page 17: ENGINE PERFORMANCE CURVE - John Deere€¦ · Fuel System Air Intake System ECU Description Engine Air Flow 19.1 m3/min 674.5 ft3/min Fuel Injection Pump Intake Manifold Pressure

Rating: M5 - 550hp (410kW) @ 2500 RPM

Application:Marine Model: 6090SFM75

REFERENCE CONDITIONS

Air Intake Restriction…………………………………………………………………. 12 in.H2O (3 kPa)

Exhaust Back Pressure………………………………………………………… 30 in.H2O (7.5 kPa)

Rated speed and power

J1995 and ISO 3046 conditions:

77 ˚F (25 ˚C) air inlet temperature

29.31 in.Hg (99 kPa) barometer

104 ˚F (40 ˚C) fuel inlet temperature

0.853 fuel specific gravity @ 60 ˚F (15.5 ˚C)

Conversion factors:

Power: kW = hp x 0.746

Fuel: 1 gal = 7.1 lb, 1 L = 0.85 kg

Torque: N·m = lb-ft x 1.356

Designed/Calibrated to meet: Certified by:

• EPA Recreational Marine Tier 2 / RCD (2003/44/EC)

• IMO MARPOL Annex VI Compliant

• NRMM (97/68/EC), as amended

Ref: Engine Emission Label 16-Sep-12

All values at rated speed, power, and standard conditions, per SAE J1995 unless otherwise noted.

Engine Performance Curves September 20126090 - Marine

Performance Curve: 6090SFM75_G

ENGINE PERFORMANCE CURVE

PowerTechTM

9.0L Engine

REFERENCE CONDITIONS Air Intake Restriction......................................................................12 in.H2O (3 kPa) Exhaust Back Pressure................................................................ 30 in.H2O (7.5 kPa) Rated speed and power Gross power guaranteed within ±5% at SAE J1995 and ISO 3046 J1995 and ISO 3046 conditions: 77 ˚F (25 ˚C) air inlet temperature

29.31 in.Hg (99 kPa) barometric pressure 104 ˚F (40 ˚C) fuel inlet temperature 0.853 fuel specific gravity @ 60 ˚F (15.5 ˚C) Ambient air temperature is defined to be the temperature of ambient air close to operating vessel that is not influenced in any manner by operating characteristics of the vessel (free field temp). Conversion factors: Power: kW = hp x 0.746 Fuel: 1 gal = 7.1 lb, 1 L = 0.85 kg Torque: N·m = lb-ft x 1.356 All values from currently available data. Subject to manufacturing and measurement variations and to change without notice. Actual performance is subject to application and operation conditions outside of John Deere control.

0

19

38

57

76

95

114

0

5

10

15

20

25

30

900 1100 1300 1500 1700 1900 2100 2300 2500

Fu

el -

L/

hr

Fu

el -

gal/

hr

Engine Speed - RPM

Propeller Fuel

0

76

151

227

302

378

0

100

200

300

400

500

600

900 1100 1300 1500 1700 1900 2100 2300 2500

Po

wer -

kW

Po

wer -

hp

475

746

1017

1288

1559

1830

2102

350

550

750

950

1150

1350

1550

900 1100 1300 1500 1700 1900 2100 2300 2500

To

rq

ue -

Nm

To

rq

ue -

lb

-ft

Crankshaft

1351 lb-ft (1832 Nm)

Crankshaft

Propeller Power

Notes:

M5: The M5 rating is for marine recreational propulsion applications that

operate between 300-1,000 hours per year and have load factors below 35

percent. This rating is for applications that use full power for no more than 30

minutes out of each 8 hours. The remaining time of operation is at or below

cruising speed.

Possible applications: recreational boats, tactical military vessels and rescue

boats.

Page 18: ENGINE PERFORMANCE CURVE - John Deere€¦ · Fuel System Air Intake System ECU Description Engine Air Flow 19.1 m3/min 674.5 ft3/min Fuel Injection Pump Intake Manifold Pressure

General Data Physical Data Model Length to rear face of block 1293 mm 50.9 in

Number of Cylinders Length maximum 1714 mm 67.5 in

Bore 118.4 mm 4.66 in Width maximum 975 mm 38.4 in

Stroke 136 mm 5.35 in Height, crank centerline to top 662 mm 26.1 in

Displacement 9.0 L 549 in3 Height, crank centerline to bottom 320 mm 320 in

Compression Ratio Weight, with oil, no coolant (includes engine, flywheel

Valves per Cylinder, Intake/Exhaust housing, flywheel, and electronics)

Combustion System Center of Gravity Location, X-axis From Rear Face 404 mm 15.9 in

Firing Order of Block

Engine Type Center of Gravity Location, Y-axis Right of Crankshaft -24 mm -0.9 in

Aspiration Center of Gravity Location, Z-axis Above Crankshaft 133 mm 5.2 in

Aftercooling System Max. Allowable Static Bending Moment At Rear Face

Engine Crankcase Vent System of Flywheel Housing with 5-G Load

Thrust Bearing Load Limit, Forward Continuous 8.6 kN 1933 lbf

Cooling System* Thrust Bearing Load Limit, Forward Intermittent 13 kN 2923 lbf

Total Engine to Seawater Heat Rejection** 357 kW 20320 BTU/min Thrust Bearing Load Limit, Rearward Continuous 4 kN 899 lbf

Aftercooler Heat Rejection 127 kW 7229 BTU/min Thrust Bearing Load Limit, Rearward Intermittent 6 kN 1349 lbf

Coolant Flow 440 L/min 116 gal/min

Thermostat Start to Open 82 ˚C 180 ˚F Electrical System Thermostat Fully Open 94 ˚C 202 ˚F Min. Recommended Battery Capacity, 12V @32 ˚F (0 ˚C) 1100 amps

Min. Coolant Fill Rate 12 L/min 3.2 gal/min Min. Recommended Battery Capacity, 24V @32 ˚F (0 ˚C) 750 amps

Min. Pressure Cap 110.3 kPa 16 psi Starter Rolling Current, 12V @32 ˚F (0 ˚C) amps

Max. External Coolant Restriction 40 kPa 5.8 psi Starter Rolling Current, 24V @32 ˚F (0 ˚C) amps

Normal Operation Max Top Tank Temperature 100 ˚C 212 ˚F Min. Voltage at ECU during Cranking, 12V volts

≤ 5% of Total Operating Time Top Min. Voltage at ECU during Cranking, 24V volts

Tank Temperature Max. Allowable Start Circuit Resistance, 12V ohms

Absolute Max Top Tank Temperature 110 ˚C 230 ˚F Max. Allowable Start Circuit Resistance, 24V ohms

Recommended Fuel Cooler 11 kW 605 BTU/min Recommended Starter Cable, 12V 100"

Engine Radiated Heat 54 kW 3086 BTU/min Recommended Starter Cable, 24V 100"

Recommended Starter Cable, 12V 200"

Recommended Starter Cable, 24V 200"

Electrical Component Maximum Temperature Limit 125 ˚C 257 ˚F

* The cooling system should be capable of typical at ambient up to the maximum

conditions in which the vessel will operate.

Typical operation is defined as the average load sustainable in the vessel over 10 min.

** Reference 32 ˚C Sea Water Temperature

All values at rated speed, power, and standard conditions, per SAE J1995 unless otherwise noted.

Engine Performance Curves 6090 - Marine Sheet 2 - September 2012

#00

#2

#0000 or 2#00

#0

Performance Curve: 6090SFM75_G

600

0.002

lb-ft

0.0012

16.0:11066 2349

2/2kg lb

Engine Installation Criteria

6090SFM75

6

Direct injection

10

In line, 4 Cycle

Turbocharged and Aftercooled

Seawater cooled814 Nm

Closed

500

100-110 ˚C 212-230 ˚F

1-5-3-6-2-4

300

6

Page 19: ENGINE PERFORMANCE CURVE - John Deere€¦ · Fuel System Air Intake System ECU Description Engine Air Flow 19.1 m3/min 674.5 ft3/min Fuel Injection Pump Intake Manifold Pressure

Fuel System Air Intake System ECU Description Engine Air Flow 33.2 m

3/min 1172 ft

3/min

Fuel Injection Pump Intake Manifold Pressure 246 kPa 39.0 psi

Governor Type Manifold Air Temperature 51.5 ˚C 125 ˚F

Volumetric Fuel Consumption 108 L/hr 28.5 gal/hr Maximum Manifold Air Temperature 67 ˚C 152.6 ˚F

Mass Fuel Consumption 91.8 kg/hr 202 lb/hr Max. Allowable Temperature Rise, Ambient

Total Fuel Volumetric Flow 251 L/hr 66.3 gal/hr Air to Engine Inlet

Total Fuel Mass Flow 213 kg/hr 470 lb/hr Max. Air Intake Restriction, Clean Air Cleaner 3 kPa 12 in.H2O

Max. Fuel Inlet Restriction* 20 kPa 80 in.H2O Max. Air Intake Restriction, Dirty Air Cleaner 6.25 kPa 25 in.H2O

Max. Fuel Inlet Pressure 20 kPa 80 in.H2O Min. Ventilation Area 0.204 m2 317 in

2

Max Fuel Return Pressure 20 kPa 80 in.H2O

Max. Fuel Height Above Transfer Pump 2.4 m 7.9 ft Performance Data Max. Leak-off Return Height 2.4 m 7.9 ft Rated Power 410 kW 550 hp

Max. Fuel Inlet Height Above Fuel Tank Supply 2.4 m 7.9 ft Rated Speed 2500 RPM

Normal Operation Fuel Temperature 40 ˚C 104 ˚F Peak Torque Speed 1900 RPM

Max. Fuel Inlet Temperature 100 ˚C 212 ˚F Low Idle Speed 650 RPM

Min. Recommended Fuel Line Inside Diameter 8.53 mm 0.34 in Rated Torque 1566 Nm 1155 ft-lb

Min. Recommended Fuel Line Size 6 (-) AN Peak Torque 1832 Nm 1351 ft-lb

Primary Fuel Filter 10 mic BMEP, Rated 2187 kPa 317 psi

Secondary Fuel Filter 2 mic Rated Pferdestärke (metric hp) 557 ps

Front Drive Capacity, Intermittent 550 Nm 406 lb-ft

Lubrication System Front Drive Capacity, Continuous 468 Nm 345 lb-ft

Oil Pressure at Rated Speed 284 kPa 41 psi

Oil Pressure at Low Idle (800rpm)** 136 kPa 20 psi Exhaust System Max. Crankcase Pressure 2 kPa 8 in.H2O Exhaust Flow 77.7 m

3/min 2744 ft

3/min

Maximum Installed Angle, Front Down 0 deg Exhaust Flow @ gas STP 35.8 m3/min 1264 ft

3/min

12 deg Exhaust Temperature 427 ˚C 800.6 ˚F

20 deg Max. Allowable Exhaust Restriction 7.5 kPa 30 in.H2O

30 deg Max. Shear on Turbocharger Exhaust Outlet 11 kg 24.3 lb

Max. Bending Moment on Turbocharger Exhaust

Seawater Pump System Outlet

Seawater Pump Flow 385 L/min 102 gal/min Min. Exhaust Pipe Diameter, Dry 139.7 mm 5.5 in

Max. Suction Lift 3 m 9.8 ft Min. Exhaust Pipe Diameter, Wet 152.4 mm 6.0 in

Max. Outlet Pressure 140 kPa 20 psi

Max. Inlet Restriction 30 kPa 4 psi

* With clean filters

** With John Deere Plus-50 IITM

15w-40, not applicable with break in oil.

*** With 1932 option

All values at rated speed, power, and standard conditions, per SAE J1995 unless otherwise noted.

Sheet 2 - September 2012 Engine Performance Curves 6090 - Marine Sheet 3 - September 2012

Engine Angularity Limits Any Direction, Intermittent***

7 Nm 15.4 lb-ft

Performance Curve: 6090SFM75_G

Maximum Installed Angle, Front Up

Engine Angularity Limits Any Direction, Continuous***

17 ˚C 30 ˚F

Engine Installation Criteria

L14

Electronic

HPCR

Page 20: ENGINE PERFORMANCE CURVE - John Deere€¦ · Fuel System Air Intake System ECU Description Engine Air Flow 19.1 m3/min 674.5 ft3/min Fuel Injection Pump Intake Manifold Pressure

Engine Performance Data Table

RPM kW hp Nm lb-ft kW hp L/hr gal/hr g/kW-hr

2500 410 550 1566 1155 410 550 108 29 224

2400 410 550 1631 1203 363 486 93 25 218

2300 410 550 1702 1255 319 428 81 21 216

2200 410 550 1780 1313 279 375 69 18 210

2100 400 536 1818 1341 243 326 60 16 210

2000 382 513 1825 1346 210 281 52 14 211

1900 365 489 1832 1351 180 241 45 12 213

1800 342 459 1815 1339 153 205 39 10 217

1700 308 413 1730 1276 129 173 34 9 224

1600 257 344 1532 1130 107 144 29 8 229

1500 213 286 1356 1000 89 119 25 7 240

1400 172 231 1176 867 72 97 20 5 236

1300 135 182 995 734 58 77 16 4 236

1200 106 142 845 623 45 61 13 3 244

1100 84 112 725 535 35 47 10 3 243

1000 68 91 645 476 26 35 8 2 259

* Theoretical 3.0 exponent propeller curve , measured at flywheel

All values at rated speed, power, and standard conditions, per SAE J1995 unless otherwise noted.

Sheet 3 - September 2012 Engine Performance Curves Sheet 4 - September 20126090 - Marine

Performance Curve: 6090SFM75_G

Engine Speed Crank Power Crank Torque

Engine Installation Criteria

* Prop Power * Prop Fuel * Prop BSFC