MTU Friedrichshafen

Technical Sales Documentation MTU Project No. - ENGINE DATA - Printout: (y-m-d) 2003-04-10 Sheet 1

No. Index Unit 12V2000G23

Application Group 3B MTU data code 13 Intake air temperature C 25 Charge-air coolant temperature C --- Barometric pressure mbar 1000 Site altitude above sea level m 100 Raw-water inlet temperature C ---

Explanation: A = Design Value N = Not yet defined value G = Guaranteed value - = Not applicable CP = Ref.value: Continuous power R = Guideline value X = Applicable FSP = Ref.value: Fuel stop power L = Limit value, up to which the engine can be operated, Z = See notes provided after "ENGINE DATA" without change (e.g. of power setting).

0. DATA-RELEVANT ENGINE DESIGN CONFIGURATION

1 Fuel-consumption optimized X

2 Exhaust-emissions optimized --- (limit values see Exhaust Emissions, Chapt. 21)

16 Complies with: TA-Luft (Edition 1986) --- (German clean-air standard)

17 Complies with: --- Regulation for stationary power plants in France (arrt du 25 Juillet 1997)

18 Complies with: --- US EPA, regulation for non-road mobile machinery (40 CFR 89 - stage I -)

25 Complies with: --- US EPA, regulation for non-road mobile machinery (40 CFR 89 - stage II -)

8 Engine rated speed switchable (1500/1800 rpm) ---

12 Engine with sequential turbocharging --- (exhaust turbochargers with cut-in/cut-out control)

13 Engine without sequential turbocharging X (exhaust turbochargers without cut-in/cut-out control)

31 Engine with air charge air cooling X

32 Engine with water charge air cooling (external) ---

1. POWER-RELATED DATA (power ratings are net brake power to ISO 3046)

1 Engine rated speed A 1500 1/min

3 Mean piston speed 7.5 m/s

4 Continuous power ISO 3046 (10% overload CP A 565 kW cap., design power DIN 6280, ISO 8528)

5 Fuel stop power ISO 3046 FSP A 622 kW

8 Mean effective pressure (MEP) CP 18.9 bar

9 Mean effective pressure (MEP) FSP 20.8 bar

2. GENERAL CONDITIONS (for max. power)

1 Intake air depression (new filter) (design) A 15 mbar

2 Intake air depression (limit value) L 30 mbar

3 Exhaust backpressure (design) A 30 mbar

4 Exhaust backpressure (limit value) L 50 mbar

5 Fuel temperature at fuel feed connection R 25 C

3. CONSUMPTION

17 Specific fuel consumption (be) 100% CP G 197 g/kWh (+5%; EN 590; 42.8MJ/kg)

18 Specific fuel consumption (be) 75% CP R 198 g/kWh (+5%; EN 590; 42.8MJ/kg)

19 Specific fuel consumption (be) 50% CP R 205 g/kWh (+5%; EN 590; 42.8MJ/kg)

20 Specific fuel consumption (be) 25% CP R 234 g/kWh (+5%; EN 590; 42.8MJ/kg)

21 Specific fuel consumption (be) FSP R 197 g/kWh (+5%; EN 590; 42.8MJ/kg)

73 No-load fuel consumption R 14 kg/h

MTU Friedrichshafen

Technical Sales Documentation MTU Project No. - ENGINE DATA - Printout: (y-m-d) 2003-04-10 Sheet 2

No. Index Unit 12V2000G23

Application Group 3B MTU data code 13 Intake air temperature C 25 Charge-air coolant temperature C --- Barometric pressure mbar 1000 Site altitude above sea level m 100 Raw-water inlet temperature C ---

Explanation: A = Design Value N = Not yet defined value G = Guaranteed value - = Not applicable CP = Ref.value: Continuous power R = Guideline value X = Applicable FSP = Ref.value: Fuel stop power L = Limit value, up to which the engine can be operated, Z = See notes provided after "ENGINE DATA" without change (e.g. of power setting).

61 Lube oil consumption after 100h operation, R 0.5 % of B average (B = fuel consumption per hour)

62 Lube oil consumption after 100h operation, L 1.0 % of B maximal (B = fuel consumption per hour)

4. MODEL-RELATED DATA (basic design)

3 Engine with exhaust turbocharging (ETC) X and charge air cooling (CAC)

4 Exhaust piping, non-cooled X

5 Exhaust piping, liquid-cooled ---

33 Working method: four-cycle, diesel, single-acting X

34 Combustion method: direct injection X

36 Cooling system: conditioned water X

37 Direction of rotation: c.c.w. (facing driving end) X

6 Number of cylinders 12

7 Cylinder configuration: V angle 90 degree

10 Bore 130 mm

11 Stroke 150 mm

12 Displacement, cylinder 1.99 liter

13 Displacement, total 23.88 liter

14 Compression ratio 16

40 Cylinder heads: single-cylinder X

41 Cylinder liners: wet, replaceable X

24 Number of inlet valves, per cylinder 2

25 Number of exhaust valves, per cylinder 2

15 Number of turbochargers 2

18 Number of intercoolers 1

28 Standard flywheel housing flange 0 SAE (engine main PTO)

43 Flywheel interface 18" DISC

46 Engine mass diagram, drawing No. N

47 Engine mass diagram, drawing No. (cont.) N

5. COMBUSTION AIR / EXHAUST GAS

8 Charge air pressure before CP R 2.5 bar abs cylinder (abs.)

27 Charge air pressure before FSP R N bar abs cylinder (abs.)

9 Combustion air volume flow CP R 0.7 m3/s

10 Combustion air volume flow FSP R N m3/s

11 Exhaust volume flow (at exhaust temp.) CP R 2.0 m3/s

12 Exhaust volume flow (at exhaust temp.) FSP R N m3/s

15 Exhaust temperature after turbocharger CP R 585 C

16 Exhaust temperature after turbocharger FSP R N C

MTU Friedrichshafen

Technical Sales Documentation MTU Project No. - ENGINE DATA - Printout: (y-m-d) 2003-04-10 Sheet 3

No. Index Unit 12V2000G23

Application Group 3B MTU data code 13 Intake air temperature C 25 Charge-air coolant temperature C --- Barometric pressure mbar 1000 Site altitude above sea level m 100 Raw-water inlet temperature C ---

Explanation: A = Design Value N = Not yet defined value G = Guaranteed value - = Not applicable CP = Ref.value: Continuous power R = Guideline value X = Applicable FSP = Ref.value: Fuel stop power L = Limit value, up to which the engine can be operated, Z = See notes provided after "ENGINE DATA" without change (e.g. of power setting).

6. HEAT DISSIPATION

15 Heat dissipated by engine coolant, CP R 275 kW with oil heat, without charge air heat

16 Heat dissipated by engine coolant, FSP R N kW with oil heat, without charge air heat

26 Charge-air heat dissipation CP R 95 kW

27 Charge-air heat dissipation FSP R N kW

33 Radiation and convection heat, engine CP R 40 kW

34 Radiation and convection heat, engine FSP R N kW

7. COOLANT SYSTEM (high-temperature circuit)

17 Coolant temperature A 95 C (at engine outlet to cooling equipment)

20 Coolant temperature after engine, alarm R 97 C

21 Coolant temperature after engine, shutdown L 102 C

25 Coolant antifreeze content, L 50 % max. permissible

30 Cooling equipment: coolant flow rate A 49 m3/h

35 Coolant pump: inlet pressure, min. L 0.4 bar

36 Coolant pump: inlet pressure, max. L 1.52 bar

41 Pressure loss in off-engine cooling system, L 0.7 bar max. permissible

72 Pressure loss in off-engine cooling system L 0.55 bar min. required

47 Breather valve (expansion tank) R N bar opening pressure (excess pressure)

48 Breather valve (expansion tank) R N bar opening pressure (depression)

49 Pressure in complete cooling system, L N bar max. permissible

54 Cooling equipment: height above engine L 15.2 m max. permissible

53 Cooling equipment: design pressure A 2.2 bar

73 Coolant level in expansion tank, L --- below min. alarm

74 Coolant level in expansion tank, L X below min. shutdown

10. LUBE OIL SYSTEM

1 Lube oil operating temp. before engine, from R 88 C

2 Lube oil operating temp. before engine, to R 98 C

5 Lube oil temperature before engine, alarm R 103 C

6 Lube oil temperature before engine, shutdown L --- C

8 Lube oil operating press. bef. engine, from R 6.2 bar

9 Lube oil operating press. bef. engine, to R 7.5 bar

10 Lube oil pressure before engine, R 4.4 bar alarm

11 Lube oil pressure before engine, L 3.9 bar shutdown

MTU Friedrichshafen

Technical Sales Documentation MTU Project No. - ENGINE DATA - Printout: (y-m-d) 2003-04-10 Sheet 4

No. Index Unit 12V2000G23

Application Group 3B MTU data code 13 Intake air temperature C 25 Charge-air coolant temperature C --- Barometric pressure mbar 1000 Site altitude above sea level m 100 Raw-water inlet temperature C ---

Explanation: A = Design Value N = Not yet defined value G = Guaranteed value - = Not applicable CP = Ref.value: Continuous power R = Guideline value X = Applicable FSP = Ref.value: Fuel stop power L = Limit value, up to which the engine can be operated, Z = See notes provided after "ENGINE DATA" without change (e.g. of power setting).

19 Lube oil fine filter (main circuit): 1 number of units

20 Lube oil fine filter (main circuit): 2 number of elements per unit

21 Lube oil fine filter (main circuit): R 0.009 mm particle retention

32 Lube oil fine filter (main circuit): L 0.8 bar pressure differential, max. permissible (limit value)

11. FUEL SYSTEM

1 Fuel pressure at supply connection on engine L -0.3 bar (when engine is starting), min. admissible

2 Fuel pressure at supply connection on engine L +0.5 bar (when engine is starting), max. admissible

37 Fuel supply flow, max. R 7.5 liter/min

8 Return fuel flow, max. R 3.5 liter/min

10 Fuel pressure at return connection on engine, L 0.5 bar max. permissible

15 Fuel prefilter: A --- number of units

16 Fuel prefilter: A --- elements per unit

17 Fuel prefilter: A --- mm particle retention

18 Fuel fine filter (main circuit): A 1 number of units

19 Fuel fine filter (main circuit): A 1 elements per unit

20 Fuel fine filter (main circuit): A 0.005 mm particle retention

21 Fuel fine filter (main circuit): L 1.0 bar pressure differential max. permissible (limit value)

12. GENERAL OPERATING DATA

1 Cold start capability, air temperature R 0** C (w/o starting aid, w/o preheating) (case A)

2 Side condition (to case A): R N C Engine coolant temperature

3 Side condition (to case A): R +10** C Lube oil temperature

4 Side condition (to case A): R 30** SAE Lube oil viscosity

9 Cold start capability, air temperature R -10** C (w/o starting aid, w/ preheating) (case C)

10 Side condition (to case C): R +40** C Engine coolant temperature

11 Side condition (to case C): R -5** C Lube oil temperature

12 Side condition (to case C): R 10W30 SAE Lube oil viscosity

21 Coolant preheating, R 3 kW heater performance (standard)

MTU Friedrichshafen

Technical Sales Documentation MTU Project No. - ENGINE DATA - Printout: (y-m-d) 2003-04-10 Sheet 5

No. Index Unit 12V2000G23

Application Group 3B MTU data code 13 Intake air temperature C 25 Charge-air coolant temperature C --- Barometric pressure mbar 1000 Site altitude above sea level m 100 Raw-water inlet temperature C ---

Explanation: A = Design Value N = Not yet defined value G = Guaranteed value - = Not applicable CP = Ref.value: Continuous power R = Guideline value X = Applicable FSP = Ref.value: Fuel stop power L = Limit value, up to which the engine can be operated, Z = See notes provided after "ENGINE DATA" without change (e.g. of power setting).

22 Coolant preheating, R 32 C preheating temperature (min.)

28 Breakaway torque (without driven machinery) R 580* Nm coolant temperature +5C

30 Breakaway torque (without driven machinery) R 330* Nm coolant temperature +40C

29 Cranking torque at firing speed (without R 380* Nm driven machinery) coolant temp. +5C

31 Cranking torque at firing speed (without R 305* Nm driven machinery) coolant temp. +40C

96 Starting is blocked if the engine coolant 5 C temperature is below

37 High idle speed, max. permissible L 1600 1/min (static)

38 Limit speed for overspeed L 1800 1/min alarm/emergency shutdown

42 Firing speed, from R 100 1/min

43 Firing speed, to R 120 1/min

44 Engine coolant temperature before starting L 60 C full-load operation, recommended min. (for emergency/standby sets with coolant preheating: at least the preheating temperature)

48 Recommended minimum continuous load R 20 %

49 Extended low or no-load operation possible X (consultation required)

50 Engine mass moment of inertia R 1.12 kgm2 (without flywheel)

51 Engine mass moment of inertia R 4.22 kgm2 (with standard flywheel)

52 Standard flywheel mass moment of inertia R 3.10 kgm2

69 Speed droop R 0 % (with electronic governor) adjustable from

70 Speed droop R 4 % (with electronic governor) adjustable to

95 Number of starter ring-gear teeth on engine 160 flywheel

13. STARTING (electric)

1 Starter, rated power R 6.7 kW (make BOSCH) (standard design)

2 Starter, rated voltage R 24 V= (standard design)

4 Starter, power requirement max. R 1860 A (make BOSCH)

5 Starter, power requirement at firing speed R 800 A (make BOSCH)

6 Recommended battery capacity A N Ah/20h (automotive starter battery, DIN 72311)

10 Recommended battery capacity from A N Ah/20h (automotive starter battery, DIN 72311)

11 Recommended battery capacity to A N Ah/20h (automotvie starter battery, DIN 72311)

MTU Friedrichshafen

Technical Sales Documentation MTU Project No. - ENGINE DATA - Printout: (y-m-d) 2003-04-10 Sheet 6

No. Index Unit 12V2000G23

Application Group 3B MTU data code 13 Intake air temperature C 25 Charge-air coolant temperature C --- Barometric pressure mbar 1000 Site altitude above sea level m 100 Raw-water inlet temperature C ---

Explanation: A = Design Value N = Not yet defined value G = Guaranteed value - = Not applicable CP = Ref.value: Continuous power R = Guideline value X = Applicable FSP = Ref.value: Fuel stop power L = Limit value, up to which the engine can be operated, Z = See notes provided after "ENGINE DATA" without change (e.g. of power setting).

7 Recommended battery capacity A N Ah/ 5h (NiCd battery)

8 Recommended battery capacity A N Ah/ 5h (NiCd battery, VDE 0108)

16 Start attempt duration (guideline value) R --- sec (engine preheated)

17 Start attempt duration (guideline value) R --- sec (engine not preheated)

18 Start attempt duration (limit value) L 6 sec

15. STARTING (pneumatic starter)

5 Starting air pressure before starter motor R N bar (min. operating value)

6 Starting air pressure before starter motor R N bar (max. operating value)

7 Starting air pressure before starter motor L N bar (min. limit value)

8 Starting air pressure before starter motor L N bar (max. limit value)

18 Start attempt duration (guideline value) R N sec (engine preheated)

19 Start attempt duration (guideline value) R N sec (engine not preheated)

20 Start attempt duration (limit value) L N sec

21 Air consumption / start attempt R N mn3

(engine preheated)

22 Air consumption / start attempt R N mn3

(engine not preheated)

23 Starting air tank for 3 start attempts R N liter (max. 40 bar tank pressure) (engine preheated)

24 Starting air tank for 3 start attempts R N liter (max. 30 bar tank pressure) (engine preheated)

25 Starting air tank for 6 start attempts R N liter (max. 40 bar tank pressure) (engine preheated)

26 Starting air tank for 6 start attempts R N liter (max. 30 bar tank pressure) (engine preheated)

27 Starting air tank for 10 start attempts R N liter (max. 40 bar tank pressure) (engine preheated)

28 Starting air tank for 10 start attempts R N liter (max. 30 bar tank pressure) (engine preheated)

29 Starting air tank for 3 start attempts R N liter (max. 40 bar tank pressure) (engine not preheated)

30 Starting air tank for 3 start attempts R N liter (max. 30 bar tank pressure) (engine not preheated)

31 Starting air tank for 6 start attempts R N liter (max. 40 bar tank pressure) (engine not preheated)

MTU Friedrichshafen

Technical Sales Documentation MTU Project No. - ENGINE DATA - Printout: (y-m-d) 2003-04-10 Sheet 7

No. Index Unit 12V2000G23

Application Group 3B MTU data code 13 Intake air temperature C 25 Charge-air coolant temperature C --- Barometric pressure mbar 1000 Site altitude above sea level m 100 Raw-water inlet temperature C ---

Explanation: A = Design Value N = Not yet defined value G = Guaranteed value - = Not applicable CP = Ref.value: Continuous power R = Guideline value X = Applicable FSP = Ref.value: Fuel stop power L = Limit value, up to which the engine can be operated, Z = See notes provided after "ENGINE DATA" without change (e.g. of power setting).

32 Starting air tank for 6 start attempts R N liter (max. 30 bar tank pressure) (engine not preheated)

33 Starting air tank for 10 start attempts R N liter (max. 40 bar tank pressure) (engine not preheated)

34 Starting air tank for 10 start attempts R N liter (max. 30 bar tank pressure) (engine not preheated)

16. INCLINATIONS STANDARD-OILSYSTEM (ref.: waterline)

15 Longitudinal inclination, continuous max. L 5 degree driving end down (Option: max. operating inclination)

17 Longitudinal inclination, continuous max. L 5 degree driving end up (Option: max. operating inclination)

19 Transverse inclination, continuous max. L 10 degree (Option: max. operating inclination)

18. CAPACITY

1 Engine coolant capacity R 90 liter (without cooling equipment)

11 On-engine fuel capacity R 5 liter

14 Engine oil capacity, initial filling R 77 liter (standard oil system) (Option: max. operating inclinations)

20 Oil change quantity, max. R 74 liter (standard oil system) (Option: max. operating inclinations)

28 Oil pan capacity, dipstick mark min. L 50 liter (standard oil system) (Option: max. operating inclinations)

29 Oil pan capacity, dipstick mark max. L 67 liter (standard oil system) (Option: max. operating inclinations)

19. WEIGHTS / DIMENSIONS

9 Engine weight, dry R 2490 kg (basic engine configuration acc. to scope of supply specification)

10 Engine weight, wet R 2660 kg (basic engine configuration acc. to scope of supply specification)

20. FAN / FAN COOLER

3 Fan, pusher-type X

18 Fan arrangement: vertical above crankshaft X

9 Fan drive, mechanical via V-belt X

13 Fan: speed R N 1/min

19 Standard fan cooler, supplied by MTU, N design and specific data acc. to case A/B/C

21 Fan cooler, designed for: (case A) A N C - ambient temperature

54 Fan cooler, designed for: (case A) A N m - site altitude, max.

22 Fan cooler, designed for: (case A) A N % - coolant antifreeze content, max.

MTU Friedrichshafen

Technical Sales Documentation MTU Project No. - ENGINE DATA - Printout: (y-m-d) 2003-04-10 Sheet 8

No. Index Unit 12V2000G23

Application Group 3B MTU data code 13 Intake air temperature C 25 Charge-air coolant temperature C --- Barometric pressure mbar 1000 Site altitude above sea level m 100 Raw-water inlet temperature C ---

Explanation: A = Design Value N = Not yet defined value G = Guaranteed value - = Not applicable CP = Ref.value: Continuous power R = Guideline value X = Applicable FSP = Ref.value: Fuel stop power L = Limit value, up to which the engine can be operated, Z = See notes provided after "ENGINE DATA" without change (e.g. of power setting).

55 Fan: power consumption (case A) R N kW at 1 mbar / 100 Pa duct allowance (pressure and suction sides, total)

56 Fan: power consumption (case A) R N kW at 2 mbar / 200 Pa duct allowance (pressure and suction sides, total)

57 Fan: power consumption (case A) R N kW at 3 mbar / 300 Pa duct allowance (pressure and suction sides, total)

27 Cooling air flow rate (case A) R N m3/s at 1 mbar / 100 Pa duct allowance (pressure and suction sides, total)

28 Cooling air flow rate (case A) R N m3/s at 2 mbar / 200 Pa duct allowance (pressure and suction sides, total)

29 Cooling air flow rate (case A) R N m3/s at 3 mbar / 300 Pa duct allowance (pressure and suction sides, total)

58 Fan: weight (case A) R N kg

59 Fan cooler (incl. Pipework): (case A) R N kg weight, dry

31 Fan cooler: coolant capacity (case A) R N liter

32 Fan cooler, designed for: (case B) A N C - ambient temperature

60 Fan cooler, designed for: (case B) A N m - site altitude, max.

33 Fan cooler, designed for: (case B) A N % - coolant antifreeze content, max.

61 Fan: power consumption (case B) R N kW at 1 mbar / 100 Pa duct allowance (pressure and suction sides, total)

62 Fan: power consumption (case B) R N kW at 2 mbar / 200 Pa duct allowance (pressure and suction sides, total)

63 Fan: power consumption (case B) R N kW at 3 mbar / 300 Pa duct allowance (pressure and suction sides, total)

38 Cooling air flow rate (case B) R N m3/s at 1 mbar / 100 Pa duct allowance (pressure and suction sides, total)

39 Cooling air flow rate (case B) R N m3/s at 2 mbar / 200 Pa duct allowance (pressure and suction sides, total)

40 Cooling air flow rate (case B) R N m3/s at 3 mbar / 300 Pa duct allowance (pressure and suction sides, total)

64 Fan: weight (case B) R N kg

65 Fan cooler (incl. Pipework): (case B) R N kg weight, dry

42 Fan cooler: coolant capacity (case B) R N liter

43 Fan cooler, designed for: (case C) A N C - ambient temperature

66 Fan cooler, designed for: (case C) A N m - site altitude, max.

44 Fan cooler, designed for: (case C) A N % - coolant antifreeze content, max.

MTU Friedrichshafen

Technical Sales Documentation MTU Project No. - ENGINE DATA - Printout: (y-m-d) 2003-04-10 Sheet 9

No. Index Unit 12V2000G23

Application Group 3B MTU data code 13 Intake air temperature C 25 Charge-air coolant temperature C --- Barometric pressure mbar 1000 Site altitude above sea level m 100 Raw-water inlet temperature C ---

Explanation: A = Design Value N = Not yet defined value G = Guaranteed value - = Not applicable CP = Ref.value: Continuous power R = Guideline value X = Applicable FSP = Ref.value: Fuel stop power L = Limit value, up to which the engine can be operated, Z = See notes provided after "ENGINE DATA" without change (e.g. of power setting).

67 Fan: power consumption (case C) R N kW at 1 mbar / 100 Pa duct allowance (pressure and suction sides, total)

68 Fan: power consumption (case C) R N kW at 2 mbar / 200 Pa duct allowance (pressure and suction sides, total)

69 Fan: power consumption (case C) R N kW at 3 mbar / 300 Pa duct allowance (pressure and suction sides, total)

49 Cooling air flow rate (case C) R N m3/s at 1 mbar / 100 Pa duct allowance (pressure and suction sides, total)

50 Cooling air flow rate (case C) R N m3/s at 2 mbar / 200 Pa duct allowance (pressure and suction sides, total)

51 Cooling air flow rate (case C) R N m3/s at 3 mbar / 300 Pa duct allowance (pressure and suction sides, total)

70 Fan: weight (case C) R N kg

71 Fan cooler (incl. Pipework): (case C) R N kg weight, dry

53 Fan cooler: coolant capacity (case C) R N liter

21. EXHAUST EMISSIONS

307 Regulation: TA-Luft (Edition 1986) CP G --- mg/mn3

Nitric oxide (NOx) (5% O2)

308 Regulation: TA-Luft (Edition 1986) CP G --- mg/mn3

Carbon monoxide (CO) (5% O2)

309 Regulation: TA-Luft (Edition 1986) CP G --- mg/mn3

Unburnt hydrocarbons (HC)

310 Regulation: TA-Luft (Edition 1986) CP G --- mg/mn3

Dust (5% O2)

366 Regulation: TA-Luft (Edition 1986) CP G --- mg/mn3

Formaldehyde (5% O2)

311 Regulation: stationary power plants in France G --- mg/mn3

Nitric oxide (NOx) (5% O2) CP

312 Regulation: stationary power plants in France G --- mg/mn3

Carbon monoxide (CO) (5% O2) CP

313 Regulation: stationary power plants in France G --- mg/mn3

Unburnt hydrocarbons (NMHC) CP

314 Regulation: stationary power plants in France G --- mg/mn3

Dust / particulates (5% O2) CP

316 Regulation: US EPA "non-road" G --- g/kWh (40 CFR 89 - stage I -) Nitric oxide (NOx)

317 Regulation: US EPA "non-road" G --- g/kWh (40 CFR 89 - stage I -) Carbon monoxide (CO)

318 Regulation: US EPA "non-road" G --- g/kWh (40 CFR 89 - stage I -) Unburnt hydrocarbons (HC)

319 Regulation: US EPA "non-road" G --- g/kWh (40 CFR 89 - stage I -) Particulates

320 Regulation: US EPA "non-road" G --- g/kWh (40 CFR 89 - stage II -) Nitric oxide (NOx) + unburnt hydrocarbons (HC)

MTU Friedrichshafen

Technical Sales Documentation MTU Project No. - ENGINE DATA - Printout: (y-m-d) 2003-04-10 Sheet 10

No. Index Unit 12V2000G23

Application Group 3B MTU data code 13 Intake air temperature C 25 Charge-air coolant temperature C --- Barometric pressure mbar 1000 Site altitude above sea level m 100 Raw-water inlet temperature C ---

Explanation: A = Design Value N = Not yet defined value G = Guaranteed value - = Not applicable CP = Ref.value: Continuous power R = Guideline value X = Applicable FSP = Ref.value: Fuel stop power L = Limit value, up to which the engine can be operated, Z = See notes provided after "ENGINE DATA" without change (e.g. of power setting).

321 Regulation: US EPA "non-road" G --- g/kWh (40 CFR 89 - stage II -) Carbon monoxide (CO)

323 Regulation: US EPA "non-road" G --- g/kWh (40 CFR 89 - stage II -) Particulates

141 Exhaust volume flow, dry CP R N m3/h (standard conditions)

143 Exhaust mass flow CP R N kg/h (reference conditions)

144 Residual oxygen (O2) content CP R N Vol % in dry exhaust (standard conditions)

145 Total combustion calorific value CP R --- kW

37 Smoke index, BOSCH FSP R 0.5

22. ACOUSTICS

101 Exhaust noise, unsilenced CP R N dB(A) (free-field sound pressure level Lp, 1m distance, ISO 6798)

201 Exhaust noise, unsilenced CP R N dB(A) (sound power level LW, ISO 6798)

103 Exhaust noise, unsilenced, Spectrum No. CP N (free-field sound pressure level Lp, 1m distance, ISO 6798)

203 Exhaust noise, unsilenced, Spectrum No. CP N (sound power level LW, ISO 6798)

109 Engine surface noise with attenuated CP R N dB(A) intake noise (filter) (free-field sound pressure level Lp, 1m distance, ISO 6798)

209 Engine surface noise with attenuated CP R N dB(A) intake noise (filter) (sound power level LW, ISO 6798)

111 Engine surface noise, Spectrum No. CP N with atten.intake noise (filter) (free-field sound pressure level Lp, 1m distance, ISO 6798)

211 Engine surface noise, Spectrum No. CP N with attenuated intake noise (filter) (sound power level LW, ISO 6798)

125 Structure borne noise at engine mounting CP N brackets in vertical direction above resilient mounts, spectrum No.

129 Test stand impedance spectrum, N Diagram No.

130 Test stand impedance spectrum, N Diagram No. (cont.)

23. LOAD PROFILE AND TBO (case A)

15 Maintenance schedule no.

16 Maintenance schedule no. (cont.)