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1 Sheet of 0 Printout: (yd) ENGINE DATA MTU Project No. No. Index Unit 2V4000G63 Chargeair coolant teperature Rawwater inlet teperature DATARELEVANT ENGINE DESIGN CONFIGURATION Fuelconsuption optiized X 2 Exhausteissions optiized (liit values see Exhaust Eissions, Chapter 2) 47 "TALuft" (Geran cleanair standard) Coplies with: Regulations for stationary power plants in France (arrêté du Juillet 997) Coplies with: US EPA, regulation for nonroad engines (40 CFR 89 Tier ) Coplies with: US EPA regulations for nonroad engines (40 CFR 89 Tier ) NOx20% Coplies with: US EPA regulations for nonroad engines (40 CFR 89 Tier ) NOx40% Coplies with: US EPA, regulation for nonroad engines (40 CFR 89 Tier 2 ) Engine rated speed switchable (500/800 rp) Engine with sequential turbocharging (turbochargers with cutin/cutout control) Engine without sequential turbocharging (turbochargers without cutin/cutout control). POWERRELATED DATA (power ratings are net brake power to ISO 3046) X Engine rated speed A rp Mean piston speed /s Continuous power ISO 3046 (0% overload capability) (design power DIN 6280, ISO 8528) A kw Fuel stop power ISO 3046 A kw Mean effective pressure (MEP) (Continuous power ISO 3046) Mean effective pressure (MEP) (Fuel stop power ISO 3046) 2. GENERAL CONDITIONS (for axiu power) bar 22.0 bar 24.2 Intake air depression (new filter) A 5 2 Intake air depression, ax. L 50 3 Exhaust back pressure A 30 4 Exhaust back pressure, ax. L 85 5 Fuel teperature at fuel feed connection R 0 Fuel teperature at fuel feed connection, ax. L 8 Fuel teperature at fuel feed connection, in. L 3. CONSUMPTION Specific fuel consuption (be) 00 % CP (+ 5 %; EN 590; 42.8 MJ/kg) Specific fuel consuption (be) 75 % CP (+ 5 %; EN 590; 42.8 MJ/kg) Specific fuel consuption (be) 50 % CP (+ 5 %; EN 590; 42.8 MJ/kg) G g/kwh 93 R g/kwh 94 R g/kwh 20 X = Applicable = Not applicable N = Not yet defined value Z = See notes provided after "ENGINE DATA"

2 Sheet 2 of 0 Printout: (yd) ENGINE DATA MTU Project No. No. Index Unit 2V4000G63 Chargeair coolant teperature Rawwater inlet teperature Specific fuel consuption (be) % CP (+ 5 %; EN 590; 42.8 MJ/kg) Specific fuel consuption (be) FSP (+ 5 %; EN 590; 42.8 MJ/kg) R g/kwh 228 R g/kwh Noload fuel consuption R kg/h Lube oil consuption after 00 h of operation (B = fuel consuption per hour) Lube oil consuption after 00 h of operation, ax. (B = fuel consuption per hour) 4. MODELRELATED DATA (basic design) R % of B 0.3 L % of B.0 3 Engine with exhaust turbocharger (ETC) and intercooler X 4 Exhaust piping, noncooled X 5 Exhaust piping, liquidcooled 33 Working ethod: fourcycle, diesel, singleacting X 34 Cobustion ethod: direct injection X 36 Cooling syste: conditioned water X 37 Direction of rotation: c.c.w. (facing driving end) X 6 Nuber of cylinders 2 7 Cylinder configuration: V angle degrees 90 0 Bore 70 Stroke 20 2 Displaceent, cylinder liter Displaceent, total liter Copression ratio Cylinder heads: singlecylinder X 4 Cylinder liners: wet, replaceable X 42 Piston design: coposite piston 49 Piston design: solidskirt piston X 24 Nuber of inlet valves, per cylinder 2 Nuber of exhaust valves, per cylinder 2 5 Nuber of turbochargers 4 8 Nuber of intercoolers 28 Standard flywheel housing flange (engine ain PTO) SAE Static bending oent at standard flywheel housing flange, ax. Dynaic bending oent at standard flywheel housing flange, ax. L kn 5 L kn Flywheel interface DISC 2 46 Engine ass diagra, drawing No. 47 Engine ass diagra, drawing No. (cont.) 5. COMBUSTION AIR / EXHAUST GAS 8 Chargeair pressure before cylinder CP R bar abs Chargeair pressure before cylinder FSP R bar abs Cobustion air volue flow CP R ³/s.8 0 Cobustion air volue flow FSP R ³/s 2.0 Exhaust volue flow (at exhaust teperature) CP R ³/s 4.5 X = Applicable = Not applicable N = Not yet defined value Z = See notes provided after "ENGINE DATA"

3 Sheet 3 of 0 Printout: (yd) ENGINE DATA MTU Project No. No. Index Unit 2V4000G63 Chargeair coolant teperature Rawwater inlet teperature Exhaust volue flow (at exhaust teperature) FSP R ³/s Exhaust teperature after turbocharger CP R Exhaust teperature after turbocharger FSP R HEAT DISSIPATION 5 Heat dissipated by engine coolant CP with oil heat, without chargeair heat R kw Heat dissipated by engine coolant FSP with oil heat, without chargeair heat R kw Chargeair heat dissipation CP R kw Chargeair heat dissipation FSP R kw Heat dissipated by return fuel flow CP R kw 0 32 Heat dissipated by return fuel flow FSP R kw 33 Radiation and convection heat, engine CP R kw Radiation and convection heat, engine FSP R kw COOLANT SYSTEM (highteperature circuit) Coolant teperature 7 A 00 (at engine outlet to cooling equipent) 57 Coolant teperature differential after/before engine, R 8 fro 58 Coolant teperature differential after/before engine, to R 0 23 Coolant teperature differential after/before engine L 2 20 Coolant teperature after engine, alar R 02 2 Coolant teperature after engine, shutdown L 04 Coolant antifreeze content, ax. L % Cooling equipent: coolant flow rate A ³/h Coolant pup: inlet pressure, in. L bar Coolant pup: inlet pressure, ax. L bar.5 4 Pressure loss in offengine cooling syste, ax. L bar Breather valve (expansion tank) opening pressure (excess pressure) Breather valve (expansion tank) opening pressure (depression) R bar.0 R bar Cooling equipent: height above engine, ax. L 5 53 Cooling equipent: operating pressure A bar Coolant level in expansion tank, below in. alar Coolant level in expansion tank, below in. shutdown L L X 50 Therostat, starts to open R COOLANT SYSTEM (lowteperature circuit) 9 Coolant teperature before intercooler (at engine inlet fro cooling equipent) A 4 Coolant teperature before intercooler, alar R 75 6 Coolant teperature before intercooler, shutdown L 54 Coolant teperature differential after/before intercooler, in. Coolant teperature differential after/before intercooler, ax. L 9 L X = Applicable = Not applicable N = Not yet defined value Z = See notes provided after "ENGINE DATA"

4 Sheet 4 of 0 Printout: (yd) ENGINE DATA MTU Project No. No. Index Unit 2V4000G63 Chargeair coolant teperature Rawwater inlet teperature Coolant antifreeze content, ax. L % 50 7 Chargeair teperature after intercooler, ax. L Teperature differential between intake air and chargeair coolant before intercooler Teperature differential between intake air and chargeair coolant before intercooler, ax. Chargeair teperature after intercooler, ax. for copliance with "TALuft" at CP A K 30 L K 22 L 20 Cooling equipent: coolant flow rate A ³/h 30 2 Intercooler: coolant flow rate R ³/h Coolant pup: inlet pressure, in. L bar 0.5 Coolant pup: inlet pressure, ax. L bar.5 29 Pressure loss in offengine cooling syste, ax. L bar Cooling equipent: height above engine, ax. L Breather valve (expansion tank) opening pressure (excess pressure) Breather valve (expansion tank) opening pressure (depression) R bar.0 R bar Cooling equipent: operating pressure A bar Coolant level in expansion tank, below in. alar Coolant level in expansion tank, below in. shutdown L L X 39 Therostat, starts to open R LUBE OIL SYSTEM Lube oil operating tep. before engine, fro R 88 2 Lube oil operating tep. before engine, to R 98 5 Lube oil teperature before engine, alar R 99 6 Lube oil teperature before engine, shutdown L 0 8 Lube oil operating press. bef. engine, fro R bar Lube oil operating press. bef. engine, to R bar Lube oil pressure before engine, alar R bar Lube oil pressure before engine, shutdown L bar Lube oil fine filter (ain circuit): nuber of units Lube oil fine filter (ain circuit): nuber of eleents per unit Lube oil fine filter (ain circuit): particle retention Lube oil fine filter (ain circuit): pressure differential, ax.. FUEL SYSTEM Fuel pressure at fuel feed connection, in. (when engine is starting) Fuel pressure at fuel feed connection, ax. (when engine is starting) Fuel pressure at fuel feed connection, ax. (peranent) 5 R 0.02 L bar.5 L bar 0. L bar.5 L bar Fuel supply flow, ax. R liter/in 2 X = Applicable = Not applicable N = Not yet defined value Z = See notes provided after "ENGINE DATA"

5 Sheet 5 of 0 Printout: (yd) ENGINE DATA MTU Project No. No. Index Unit 2V4000G63 Chargeair coolant teperature Rawwater inlet teperature Fuel return flow, ax. R liter/in 5 0 Fuel pressure at return connection on engine, ax. L bar Fuel teperature differential before/after engine R 4 38 Fuel teperature after highpressure pup, alar L Fuel teperature after highpressure pup, shutdown L 5 Fuel prefilter: nuber of units A 6 Fuel prefilter: nuber of eleents per unit A 7 Fuel prefilter: particle retention A 8 Fuel fine filter (ain circuit): nuber of units A 9 Fuel fine filter (ain circuit): nuber of eleents per unit A 20 Fuel fine filter (ain circuit): particle retention A Fuel fine filter (ain circuit): pressure differential, ax. L bar.0 2. GENERAL OPERATING DATA 2 Cold start capability: air teperature (w/o starting aid, w/o preheating) (case A) Additional condition (to case A): engine coolant teperature R 0 R 0 3 Additional condition (to case A): lube oil teperature R 0 4 Additional condition (to case A): lube oil viscosity R SAE Cold start capability: air teperature (w/o starting aid, w/ preheating) (case C) Additional condition (to case C): engine coolant teperature R 0 R 40 Additional condition (to case C): lube oil teperature R 0 2 Additional condition (to case C): lube oil viscosity R SAE 5W Cold start capability: air teperature (w/ starting aid, w/ preheating) (case D) Additional condition (to case D): engine coolant teperature R 5 R 40 5 Additional condition (to case D): lube oil teperature R 5 6 Additional condition (to case D): lube oil viscosity R SAE 0W40 2 Coolant preheating, heater perforance (standard) R kw 9 22 Coolant preheating, preheating teperature (in.) R Breakaway torque (without driven achinery) coolant teperature +5 R N 650 Breakaway torque (without driven achinery) 30 coolant teperature +40 Cranking torque at firing speed (without driven 29 achinery) coolant teperature +5 Cranking torque at firing speed (without driven 3 achinery) coolant teperature +40 Starting is blocked if the engine coolant teperature is 96 below R N 300 R N 900 R N Runup period to rated speed (with driven achinery) (* at general conditions) R s 6 37 High idling speed, ax. (static) L rp Liit speed for overspeed alar / eergency shutdown L rp 750 X = Applicable = Not applicable N = Not yet defined value Z = See notes provided after "ENGINE DATA"

6 Sheet 6 of 0 Printout: (yd) ENGINE DATA MTU Project No. No. Index Unit 2V4000G63 Chargeair coolant teperature Rawwater inlet teperature Firing speed, fro R rp Firing speed, to R rp Engine coolant teperature before starting fullload operation, recoended in. (for eergency/standby sets with coolant preheating: at least the preheating teperature) L Miniu continuous load R % Engine ass oent of inertia (without flywheel) Engine ass oent of inertia (with standard flywheel) Load application sequence (st load stage) (seconds after start coand) (* at additonal conditions) Load application sequence (2nd load stage) (seconds after start coand) (* at additional conditions) Load application sequence (3rd load stage) (seconds after start coand) (* at additional conditions) Load application sequence (st load stage) (% of engine continuous power) (* at additional conditions) Load application sequence (2nd load stage) (% of engine continuous power) (* at additional conditions) Load application sequence (3rd load stage) (% of engine continuous power) (* at additional conditions) Additional conditions*: engine preheated, transient speed droop ax. 0 %, plant ass oent of inertia, in. R kg² 9.7 R kg² 9.95 R s R s R s R % R % R % R kg² 69 Speed droop (with electronic governor) adjustable, fro R % 0 70 Speed droop (with electronic governor) adjustable, to R % 0 95 Nuber of starter ringgear teeth on engine flywheel STARTING (electric) 2 Starter, rated power (ake DELCO) (standard design) R kw 2 Starter, rated voltage (standard design) R V= 24 4 Starter, power requireent ax. (ake DELCO) R A 5 Starter, power requireent at firing speed (ake DELCO) R A 6 Start attept duration (engine preheated) R s 3 7 Start attept duration (engine not preheated) R s N 8 Start attept duration, ax. L s STARTING (pneuatic/oil pressure starter) 5 Starting air pressure before starter otor, in. R bar 8 6 Starting air pressure before starter otor, ax. R bar 0 7 Starting air pressure before starter otor, in. L bar 8 8 Starting air pressure before starter otor, ax. L bar 0 8 Start attept duration (engine preheated) R s 3 9 Start attept duration (engine not preheated) R s 5 X = Applicable = Not applicable N = Not yet defined value Z = See notes provided after "ENGINE DATA"

7 Sheet 7 of 0 Printout: (yd) ENGINE DATA MTU Project No. No. Index Unit 2V4000G63 Chargeair coolant teperature Rawwater inlet teperature Start attept duration, ax. L s 2 Air consuption / start attept (engine preheated) R ^3n Starting air tank for 3 start attepts (ax. 40 bar) (engine preheated) Starting air tank for 3 start attepts (ax. 30 bar) (engine preheated) Starting air tank for 6 start attepts (ax. 40 bar) (engine preheated) Starting air tank for 6 start attepts (ax. 30 bar) (engine preheated) Starting air tank for 0 start attepts (ax. 40 bar) (engine preheated) Starting air tank for 0 start attepts (ax. 30 bar) (engine preheated) R liter 45 R liter 60 R liter 90 R liter 20 R liter 50 R liter INCLINATIONS STANDARD OIL SYSTEM (ref.: waterline) Longitudinal inclination, continuous ax. driving end down Longitudinal inclination, teporary ax. driving end down Longitudinal inclination, continuous ax. driving end up Longitudinal inclination, teporary ax. driving end up Transverse inclination, continuous ax. Transverse inclination, teporary ax. Longitudinal inclination, continuous ax. driving end down Longitudinal inclination, teporary ax. driving end down Longitudinal inclination, continuous ax. driving end up Longitudinal inclination, teporary ax. driving end up Transverse inclination, continuous ax Transverse inclination, teporary ax. 8. CAPACITIES Engine coolant capacity (without cooling equipent) R liter 60 0 Intercooler coolant capacity R liter 40 Onengine fuel capacity R liter 7 4 Engine oil capacity, initial filling (standard oil syste) R liter 260 X = Applicable = Not applicable N = Not yet defined value Z = See notes provided after "ENGINE DATA"

8 Sheet 8 of 0 Printout: (yd) ENGINE DATA MTU Project No. No. Index Unit 2V4000G63 Chargeair coolant teperature Rawwater inlet teperature Engine oil capacity, initial filling (standard oil syste) Oil change quantity, ax. (standard oil syste) Oil change quantity, ax. (standard oil syste) Oil pan capacity, dipstick ark in. (standard oil syste) Oil pan capacity, dipstick ark ax. (standard oil syste) Oil pan capacity, dipstick ark in. (standard oil syste) Oil pan capacity, dipstick ark ax. (standard oil syste) 9. WEIGHTS / DIMENSIONS Engine weight, dry (basic engine configuration acc. to scope of supply specification) Engine weight, wet (basic engine configuration acc. to scope of supply specification) 2. EXHAUST EMISSIONS R liter R liter 260 R liter L liter 60 L liter 200 L liter L liter R kg 6200* R kg "TALuft" CP Nitric oxide (NOx) (5% O2) "TALuft" CP Carbon onoxide (CO) (5% O2) "TALuft" CP Unburned hydrocarbons (HC) "TALuft" CP Dust (5% O2) "TALuft" CP Foraldehyde (5% O2) Regulation: stationary power plants in France CP Nitric oxide (NOx) (5% O2) Regulation: stationary power plants in France CP Carbon onoxide (CO) (5% O2) Regulation: stationary power plants in France CP Unburned hydrocarbons (NMHC) Regulation: stationary power plants in France CP Dust / particulates (5% O2) (40 CFR 89 Tier ) Nitric oxide (NOx) (40 CFR 89 Tier ) NOx20% Nitric oxide (NOx) (40 CFR 89 Tier ) NOx40% Nitric oxide (NOx) G g/^3n R g/^3n G g/^3n G g/^3n G g/^3n G g/^3n G g/^3n G g/^3n G g/^3n G g/kwh G g/kwh G g/kwh X = Applicable = Not applicable N = Not yet defined value Z = See notes provided after "ENGINE DATA"

9 Sheet 9 of 0 Printout: (yd) ENGINE DATA MTU Project No. No. Index Unit 2V4000G63 Chargeair coolant teperature Rawwater inlet teperature (40 CFR 89 Tier ) Carbon onoxide (CO) (40 CFR 89 Tier ) Unburned hydrocarbons (HC) (40 CFR 89 Tier ) Particulates (40 CFR 89 Tier 2 ) Nitric oxide (NOx) + unburned hydrocarbons (HC) (40 CFR 89 Tier 2 ) Carbon onoxide (CO) (40 CFR 89 Tier 2 ) Particulates Exhaust volue flow, dry CP (standard conditions) Exhaust ass flow CP (reference conditions) Residual oxygen content (O2) in dry exhaust CP (standard conditions) G g/kwh G g/kwh G g/kwh G g/kwh G g/kwh G g/kwh R ³/h R kg/h 70 R % (vol.) Total cobustion calorific value CP R kw 22. ACOUSTICS Exhaust noise, unsilenced CP (freefield soundpressure level Lp, distance, ISO 6798) Exhaust noise, unsilenced CP Exhaust noise, unsilenced FSP (freefield soundpressure level Lp, distance, ISO 6798) Exhaust noise, unsilenced FSP Exhaust noise, unsilenced FSP (freefield soundpressure level Lp, distance, ISO 6798) Spectru No. Exhaust noise,unsilenced CP Spectru No. Exhaust noise, unsilenced FSP (freefield soundpressure level Lp, distance, ISO 6798) Spectru No. Exhaust noise,unsilenced FSP Spectru No. intake noise (filter) CP (freefield soundpressure level Lp, distance, ISO 6798) intake noise (filter) CP R db(a) 3 R db(a) R db(a) R db(a) e N R db(a) 03 R db(a) 2 X = Applicable = Not applicable N = Not yet defined value Z = See notes provided after "ENGINE DATA"

10 Sheet 0 of 0 Printout: (yd) ENGINE DATA MTU Project No. No. Index Unit 2V4000G63 Chargeair coolant teperature Rawwater inlet teperature intake noise (filter) FSP (freefield soundpressure level Lp, distance, ISO 6798) intake noise (filter) FSP intake noise (filter) CP (freefield soundpressure level Lp, distance, ISO 6798) Spectru No. intake noise (filter) CP Spectru No. intake noise (filter) FSP (freefield soundpressure level Lp, distance, ISO 6798) Spectru No. intake noise (filter) FSP Spectru No. Structure borne noise at engine ounting brackets in vertical direction above resilient engine ounts CP Spectru No. Structure borne noise at engine ounting brackets in vertical direction above resilient engine ounts FSP Spectru No. R db(a) R db(a) 73367e N e 29 Test stand ipedance spectru, Diagra No. 30 Test stand ipedance spectru, Diagra No. (cont.) 23. TBO AND LOAD PROFILE (case A) 5 Maintenance schedule No. 6 Maintenance schedule No. (cont.) X = Applicable = Not applicable N = Not yet defined value Z = See notes provided after "ENGINE DATA"