Caterpillar Motor

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Product News Market Marine Propulsion Application Commercial Vessels Description Building on the durability and reliability of the C280 engine platform, Caterpillar is pleased to offer the EPA Tier 2 compliant C280 engine line. The core components are the same as the existing C280, including the latest in EUI fuel system capabilities and state-of-the-art ADEM™ A3 Electronic Control Unit (ECU) features. Caterpillar ® products continue to deliver more available power while delivering outstanding fuel efficiency. You can also count on long maintenance intervals and worldwide Caterpillar parts and service availability. For C280 Tier 2 Auxiliary and Diesel Electric Propulsion (DEP) ratings information please refer to LEXM8386. Availability Order board will open on June 18 2008. Pricing Information Refer to the U.S. EPA Tier 2 ratings on the C280MARL outline in the On-line Price List. General Comments All previous ratings for the C280-6 through C280-16 propulsion engines are now available as EPA Tier 2 and IMO compliant engines. The ratings have remained the same but some combustion characteristics have changed. As such, it is important to follow the oil change intervals as documented in the appropriate maintenance manuals. Due to changed combustion characteristics do not assume that Tier 2 engines will have the same oil change intervals as previous C280 or 3600 engines. A new Scheduled Oil Sampling (S•O•S SM ) analysis must be done to determine actual oil change intervals. Note: C280 ratings require 32°C SCAC temperature at standard ambient conditions. Cat ® C280 Marine Propulsion Engine — EPA Tier 2 Compliant Marine Power Systems July 2008 LEXM8385-01 1 of 40 Information contained in this publication may be considered confidential. Discretion is recommended when distributing. Materials and specifications are subject to change without notice. ©2008 Caterpillar CAT, CATERPILLAR, their respective logos, ADEM, S•O•S, “Caterpillar Yellow” and the POWER EDGE trade dress, All rights reserved. as well as corporate and product identity used herein, are trademarks of Caterpillar and may not be used without permission. Printed in U.S.A.

Transcript of Caterpillar Motor

Page 1: Caterpillar Motor

Product News

Market Marine Propulsion

Application Commercial Vessels

Description Building on the durability and reliability of the C280 engineplatform, Caterpillar is pleased to offer the EPA Tier 2compliant C280 engine line. The core components are thesame as the existing C280, including the latest in EUI fuelsystem capabilities and state-of-the-art ADEM™ A3Electronic Control Unit (ECU) features. Caterpillar®

products continue to deliver more available power whiledelivering outstanding fuel efficiency. You can also counton long maintenance intervals and worldwide Caterpillarparts and service availability.

For C280 Tier 2 Auxiliary and Diesel Electric Propulsion(DEP) ratings information please refer to LEXM8386.

Availability Order board will open on June 18 2008.

Pricing Information Refer to the U.S. EPA Tier 2 ratings on the C280MARLoutline in the On-line Price List.

General Comments All previous ratings for the C280-6 through C280-16propulsion engines are now available as EPA Tier 2 andIMO compliant engines. The ratings have remained thesame but some combustion characteristics have changed.As such, it is important to follow the oil change intervals asdocumented in the appropriate maintenance manuals. Dueto changed combustion characteristics do not assume thatTier 2 engines will have the same oil change intervals asprevious C280 or 3600 engines. A new Scheduled OilSampling (S•O•SSM) analysis must be done to determineactual oil change intervals.

NNoottee:: C280 ratings require 32°C SCAC temperature at standardambient conditions.

Cat® C280 Marine PropulsionEngine — EPA Tier 2 Compliant

Marine Power Systems July 2008

LEXM8385-01 1 of 40

Information contained in this publication may be considered confidential. Discretionis recommended when distributing. Materials and specifications are subject to change without notice. ©2008 CaterpillarCAT, CATERPILLAR, their respective logos, ADEM, S•O•S, “Caterpillar Yellow” and the POWER EDGE trade dress, All rights reserved. as well as corporate and product identity used herein, are trademarks of Caterpillar and may not be used without permission. Printed in U.S.A.

Page 2: Caterpillar Motor

PRODUCT NEWS –C280 MARINE PROPULSION ENGINE T2 COMPLIANT

LEXM8385-01 2 of 40

Features and BenefitsA3 ECUAdvantages:

• CAN J1939 data link

• Waterproof connectors

• Maintenance-free

• Backup ECU for redundant governing

Electronic Advantages:

• Load feedback

• Programmable droop

• Adjustable gain

• Adjustable fuel/air ratio control

• Histograms of engine operation

• Cat Messenger display presents diagnosticsand other engine parameters

Data Advantages through J1939 Link:

• Engine speed

• Boost pressure

• Throttle position

• Fuel consumption rate

• Inlet manifold temperature

• Diagnostic codes and events

• Configuration

• Desired engine speed

• Battery voltage

• Engine load

• Lifetime totals — engine hours, fuel burned,idle fuel, idle hours

• Trip totals — average fuel rate, idle fuel, idlehours, engine hours, fuel burned, trip reset

Customer Interface PanelAdvantages:

• Interfaces with standard Cat® MarineMonitoring System (PLC in Price List)

• Provides visual indication of ECUfunctionality

• Accepts 4 — 20 mA or PWM remote throttlespeed input

• Marine alarm and protection

Electronic Unit InjectorsAdvantages:

• “Drop-in” installation

• No threaded fuel connections

• High pressure inside injector only

• Does not require double wall fuel lines orleak collection device

• Injector synchronization not required

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LEXM8385-01 3 of 40

PRODUCT NEWS –C280 MARINE PROPULSION ENGINE T2 COMPLIANT

C280 Marine Reference Chart

Engine ApplicationRating Rating Rating Per. # Spec Sheet Feature(mhp) (bkW) (bhp) rpm Rating (DM****) (LEHM****) Codes

C280-6 Propulsion 2352 1730 2320 900 CSR 8389 7087 C280M20

C280-6 Propulsion 2515 1850 2481 1000 CSR 8390 7088 C280M20

C280-6 Propulsion 2583 1900 2548 900 MCR 8391 7089 C280M20

C280-6 Propulsion 2760 2030 2722 1000 MCR 8392 7090 C280M20

C280-8 Propulsion 3127 2300 3084 900 CSR 8397 7095 C280M21

C280-8 Propulsion 3345 2460 3299 1000 CSR 8398 7096 C280M21

C280-8 Propulsion 3440 2530 3393 900 MCR 8399 7097 C280M21

C280-8 Propulsion 3684 2710 3634 1000 MCR 8400 7098 C280M21

C280-12 Propulsion 4704 3460 4640 900 CSR 8405 7103 C280M22

C280-12 Propulsion 5031 3700 4962 1000 CSR 8406 7104 C280M22

C280-12 Propulsion 5167 3800 5096 900 MCR 8407 7105 C280M22

C280-12 Propulsion 5520 4060 5444 1000 MCR 8408 7106 C280M22

C280-16 Propulsion 6255 4600 6169 900 CSR 8413 7111 C280M23

C280-16 Propulsion 6690 4920 6598 1000 CSR 8414 7112 C280M23

C280-16 Propulsion 6879 5060 6785 900 MCR 8415 7113 C280M23

C280-16 Propulsion 7369 5420 7268 1000 MCR 8416 7114 C280M23

Propulsion

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Product Description

PRODUCT NEWS –C280 MARINE PROPULSION ENGINE T2 COMPLIANT

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In-line 6 & 8 4-Stroke-Cycle-Diesel Vee 12 & 16 4-Stroke-Cycle-DieselEmissions . . . . . . . . . . . . . . . . IMO, EPA Tier 2Displacement — L (cu in)

6 Cylinder . . . . . . . . . . . . . . . . . . . 111 (6,773)8 Cylinder . . . . . . . . . . . . . . . . . . . 148 (9,031)12 Cylinder . . . . . . . . . . . . . . . . . 222 (13,546)16 Cylinder . . . . . . . . . . . . . . . . . 296 (18,062)

Bore — mm (in). . . . . . . . . . . . . . . . . 280 (11.0)Stroke — mm (in) . . . . . . . . . . . . . . . 300 (11.8)Aspiration . . . . . . . . Turbocharged-AftercooledGovernor . . . . . . . . . . . . . . . . . . . . . . . Electronic

Engine Weight, net dry (approx.) — kg (lb)6 Cylinder . . . . . . . . . . . . . . . 15,682 (34,574)8 Cylinder . . . . . . . . . . . . . . . 19,000 (41,800)12 Cylinder . . . . . . . . . . . . . . 25,980 (57,276)16 Cylinder . . . . . . . . . . . . . . 28,500 (62,832)

Refill Capacities — L (gal)Cooling System (engine and expansion tank)

6 Cylinder . . . . . . . . . . 900-1075 (238-284)8 Cylinder . . . . . . . . . 1030-1205 (272-318)12 Cylinder . . . . . . . . 1400-1575 (370-416)16 Cylinder . . . . . . . . 1660-1835 (439-485)

Lube Oil System (shallow sump)6 Cylinder . . . . . . . . . . . . . . . . . . . 697 (184)8 Cylinder . . . . . . . . . . . . . . . . . . . 760 (201)12 Cylinder . . . . . . . . . . . . . . . . . . 910 (240)16 Cylinder . . . . . . . . . . . . . . . . . 1057 (279)

Oil Change Interval — hrs 6 Cylinder . . . . . . . . . . . . . . . . . . . . . . . . . 10258 Cylinder . . . . . . . . . . . . . . . . . . . . . . . . . . 92512 Cylinder . . . . . . . . . . . . . . . . . . . . . . . . . 75016 Cylinder . . . . . . . . . . . . . . . . . . . . . . . . . 600

Rotation(from flywheel end) . . . . . . Counterclockwise

Dimensions (drawing)6 CylinderDrawing Number. . . . . . . . . . . . . . . . . 277-7716Overall Length — mm (in.) . . . . . 4011 (157.9)

From front to rear face of block . . . . . . . N/AFrom front to end of flywheel housing . . N/A

Overall Width — mm (in.). . . . . . . 1796 (70.7)From crankshaft centerline

to left side . . . . . . . . . . . . . . . . . . . 922 (36.3)From crankshaft centerline

to right side. . . . . . . . . . . . . . . . . . 874 (34.4)

Overall Height — mm (in.) . . . . 2734 (107.6)From crankshaft centerline

to top of engine . . . . . . . . . . . . . 1893 (74.5)From crankshaft centerline

to bottom of oil pan . . . . . . . . . . 841 (33.1)

8 CylinderDrawing Number. . . . . . . . . . . . . . . . . 277-7717Overall Length — mm (in.) . . . . 4958 (195.2)

From front to rearface of block . . . . . . . . . . . . . . 4081 (160.7)

From front to end offlywheel housing . . . . . . . . . . 4357 (171.5)

Overall Width — mm (in.). . . . . . . 1804 (71.0)From crankshaft centerline

to left side. . . . . . . . . . . . . . . . . . . 931 (36.6)From crankshaft centerline

to right side . . . . . . . . . . . . . . . . . 874 (34.4)

Overall Height — mm (in.) . . . . . 2648 (104.2)From crankshaft centerline

to top of engine . . . . . . . . . . . . . 1806 (71.1)From crankshaft centerline

to bottom of oil pan . . . . . . . . . . 842 (33.2)

12 CylinderDrawing Number. . . . . . . . . . . . . . . . . 277-7718Overall Length — mm (in.). . . . . 4612 (181.6)

From front to rear facof block . . . . . . . . . . . . . . . . . . 3658 (144.0)

From front to end offlywheel housing . . . . . . . . . . 4136 (162.9)

Overall Width — mm (in.). . . . . . . 2022 (79.6)From crankshaft centerline

to left side. . . . . . . . . . . . . . . . . . 1164 (45.8)From crankshaft centerline

to right side . . . . . . . . . . . . . . . . . . 858 (33.8)

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Product Description (continued)

PRODUCT NEWS –C280 MARINE PROPULSION ENGINE T2 COMPLIANT

Overall Height — mm (in.) . . . . . 3404 (134.0)From crankshaft centerline

to top of engine . . . . . . . . . . . . . . 2429 (95.6)From crankshaft centerline

to bottom of oil pan . . . . . . . . . . . 976 (38.4)

16 CylinderDrawing Number. . . . . . . . . . . . . . . . . 277-7719Overall Length — mm (in.). . . . . 5685 (223.8)

From front to rear face of block . . . . . . . . N/AFrom front to end of flywheel housing . . N/A

Overall Width — mm (in.). . . . . . . 2038 (80.2)From crankshaft centerline

to left side. . . . . . . . . . . . . . . . . . . 1173 (46.2)From crankshaft centerline

to right side . . . . . . . . . . . . . . . . . . 865 (34.1)

Overall Height — mm (in.) . . . . . 3406 (134.1)From crankshaft centerline

to top of engine . . . . . . . . . . . . . . 2429 (95.6)From crankshaft centerline

to bottom of oil pan . . . . . . . . . . . 977 (38.5)

Engineering Model6 Cylinder . . . . . . . . . . . . . . . . . . . . . . . . . E9708 Cylinder . . . . . . . . . . . . . . . . . . . . . . . . . E97112 Cylinder . . . . . . . . . . . . . . . . . . . . . . . . E97216 Cylinder . . . . . . . . . . . . . . . . . . . . . . . . E973

Serial Number Prefix6 Cylinder . . . . . . . . . . . . . . . . . . . . . . . . . SCB8 Cylinder . . . . . . . . . . . . . . . . . . . . . . . . . PKA12 Cylinder . . . . . . . . . . . . . . . . . . . . . . . . . TSJ16 Cylinder . . . . . . . . . . . . . . . . . . . . . . . . NKB

Performance Numbers6 Cylinder

2320 bhp . . . . . . . . . . . . . . . . . . . . . DM83892481 bhp . . . . . . . . . . . . . . . . . . . . . DM83902548 bhp . . . . . . . . . . . . . . . . . . . . . DM83912722 bhp . . . . . . . . . . . . . . . . . . . . . DM8392

8 Cylinder3084 bhp . . . . . . . . . . . . . . . . . . . . . DM83973299 bhp . . . . . . . . . . . . . . . . . . . . . DM83983393 bhp . . . . . . . . . . . . . . . . . . . . . DM83993634 bhp . . . . . . . . . . . . . . . . . . . . . DM8400

12 Cylinder4640 bhp . . . . . . . . . . . . . . . . . . . . . DM84054962 bhp . . . . . . . . . . . . . . . . . . . . . DM84065096 bhp . . . . . . . . . . . . . . . . . . . . . DM84075444 bhp . . . . . . . . . . . . . . . . . . . . . DM8408

16 Cylinder6169 bhp . . . . . . . . . . . . . . . . . . . . . DM84136598 bhp . . . . . . . . . . . . . . . . . . . . . DM84146785 bhp . . . . . . . . . . . . . . . . . . . . . DM84157268 bhp . . . . . . . . . . . . . . . . . . . . . DM8416

Basic Engine Arrangement6 Cylinder . . . . . . . . . . . . . . . . . . . . . 297-25498 Cylinder . . . . . . . . . . . . . . . . . . . . . 297-255012 Cylinder . . . . . . . . . . . . . . . . . . . . 297-255116 Cylinder . . . . . . . . . . . . . . . . . . . . 297-2552

Service InformationParts Book . . . . . . . . . . . . . . . . . . . . . SEBP3600Service Manual

6/8 Cylinder . . . . . . . . . . . . . . . . . KENR685312/16 Cylinder . . . . . . . . . . . . . . . RENR5080

Operation & MaintenanceManual . . . . . . . . . . . . . . . . . . . . . . SEBU7876

Specifications . . . . . . . . . . . . . . . . . . RENR5082Systems Operation Test

& Adjustment . . . . . . . . . . . . . . . . RENR5083Disassembly and Assembly

6/8 Cylinder. . . . . . . . . . . . . . . . . . RENR508512/16 Cylinder . . . . . . . . . . . . . . . KENR6071

Electronic Troubleshooting . . . . . . RENR5084Schematic. . . . . . . RENR5086 &RENR5087A

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Intake and Exhaust SystemCharge air cooler, air inlet shutoff, high flowturbocharger, dry manifold with soft or hardshielding

Basic Engine ArrangementIn-line engine (vee engine for 12 and 16cylinder) with one-piece grey iron cylinderblock, individual cylinder heads with fourintake/exhaust valves, right- or left-handservice side available

Control SystemDual Caterpillar® A3 ECU with electronic unitinjector fuel system, rigid wiring harness (10 amp, 24 volt power required to drive ECU)

Cooling SystemSingle or combined system, engine mountedfreshwater and seawater pumps, engine coolantwater drains

Fuel SystemEngine operates on MDO; fuel injectionsystem consists of engine-driven fuel transferpump and an electronic unit injector for eachcylinder, engine-mounted duplex fuel filters,and flexible connections

Lube Oil SystemTop-mounted crankcase breather, twocentrifugal oil filters with single shutoff (threefilters for 12 and 16 cylinder), gear-drivenpump, duplex oil filter, crankcase explosionrelief, oil filler and dipstick

Monitoring, Alarm, and Safety ControlSystemAlarms and shutdowns provided as required bymarine society for unmanned machineryspaces. Marine Monitoring System II [listed asProgrammable Logic Control (PLC) in thePrice List] or Engine Control Panel areavailable; systems include temperature,pressure, and speed sensors; optional: oil mistdetector or particle detector available; cylinderpressure relieve valves (for cold weatheroperation) available for 16 cylinder engines

ECU FunctionsKey-switch, desired engine speed,programmable low idle, SAE J1939 data link,Cat data link, Messenger (displays engine data, diagnostics, etc.), diagnostics, generalalarm, programmable parameters (system,application, and tattletales), Caterpillar ETservice tool interface, remote shutdown,shutdown notify, load feedback, overspeedshutdown, overspeed verify, engine powercorrection, bollard pull test

GeneralFour lifting eyes mounted to cylinder heads,Caterpillar yellow paint, parts books andmaintenance manuals, shrink wrap

Optional Supplied EquipmentTorsional coupling, fresh water heat exchanger,fuel cooler, expansion tank, emergency pumpsand connections, jacket water heater, flexibleconnections, and anti-vibration isolators

Standard Equipment

PRODUCT NEWS –C280 MARINE PROPULSION ENGINE T2 COMPLIANT

Page 7: Caterpillar Motor

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PRODUCT NEWS –C280 MARINE PROPULSION ENGINE T2 COMPLIANT

Competitive InformationC280-6

Caterpillar C280-6 MAN L28/32 Wartsila 26 6L26

Power — bhp 2320 2481 2548 2722 1970 2300 2626 2955 2530 2650 2650 2775

Power — bkW 1730 1850 1900 2030 1470 1715 1960 2205 1860 1950 1950 2040

Engine Speed — rpm 900 1000 900 1000 775 775 775 775 900 900 1000 1000

BSFC — g/kW-hr 194 203 194 200 N/A N/A

SFOC — g/kW-hr 190 198 190 196 188 182-184(without pumps)

Configuration I-6 I-6 I-6

Bore — mm/in 280 x 11.0 280 x 11.02 260 x 10.2

Stroke — mm/in 300 x 11.8 320 x 12.6 320 x 12.6

Displacement — L 111 118 138 158 177 102

Fuel System Electronic Unit Injection N/A N/A

Weight — kg 15 682 19 000 21 000 23 500 26 500 18 000

Weight — lbs 34,574 41,800 46,200 51,700 58,300 39,690

Power Density — bkW/kg .110 .118 .121 .129 .077 .082 .083 .083 .103 .108 .108 .113

Dimensions — mm4340 x 4750 x 6290 x 6770 x

(L x W x H)4011 x 1796 x 2734 1732 x 1732 x 1732 x 1844 x 4212 x 1815 x 2664

3186 3186 3186 3242

C280-8

Caterpillar C280-8EMD

MAN L27/3812-710G7B 16-710G7B

Power — bhp 3084 3299 3393 3634 3000 3525 3191 3648

Power — bkW 2300 2460 2530 2710 2240 2628 2380 2720

Engine Speed — rpm 900 1000 900 1000 900 800 800 800

BSFC — g/kW-hr 188 197 188 197 N/A N/A

SFOC — g/kW-hr 184 193 184 193 N/A 182(without pumps)

Configuration I-8 Vee 12 Vee 16 I-7 I-7

Bore — mm/in 280 x 11.0 230 x 9.06 270 x 10.6

Stroke — mm/in 300 x 11.8 279 x 11.0 380 x 15.0

Displacement — L 148 139 185 139 174

Fuel System Electronic Unit Injection N/A N/A

Weight — kg 19 000 N/A 33 500 37 000

Weight — lbs 41,800 N/A 73,855 81,571

Power Density — bkW/kg .121 .129 .133 .143 N/A .071 .074

Dimensions — mm 4407 x 1370 5960 x 1370(L x W x H)

4958 x 1804 x 2648 N/Ax 3595 x 3565

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PRODUCT NEWS –C280 MARINE PROPULSION ENGINE T2 COMPLIANT

LEXM8385-01 8 of 40

C280-12

Caterpillar EMD WartsilaC280-12 20-710G7B 26 12V26

Power — bhp 4640 4962 5096 5444 4400 5000 5060 5300 5300 5545

Power — bkW 3460 3700 3800 4060 3310 3730 3720 3900 3900 4080

Engine Speed — rpm 900 1000 900 1000 800 900 900 900 1000 1000

BSFC — g/kW-hr 194 203 194 200 N/A N/A

SFOC — g/kW-hr 190 198 190 196 N/A 186-192(without pumps)

Configuration Vee 12 Vee 20 Vee 12

Bore — mm/in 280 x 11.0 N/A 260 x 320

Stroke — mm/in 300 x 11.8 N/A 10.2 x 12.6

Displacement — L 222 N/A 204

Fuel System Electronic Unit Injection N/A N/A

Weight — kg 25 980 N/A 30 500

Weight — lbs 57,276 N/A 67,250

Power Density — bkW/kg .133 .142 .146 .156 N/A .122 .128 .128 .134

Dimensions — mm 5124 x 2474 x 3298(L x W x H)

4612 x 2022 x 3404 N/A

Competitive Information

C280-16

Caterpillar WartsilaC280-16 26 16V26

Power — bhp 6169 6598 6785 7268 6745 7070 7070 7395

Power — bkW 4600 4920 5060 5420 4960 5200 5200 5440

Engine Speed — rpm 900 1000 900 1000 900 900 1000 1000

BSFC — g/kW-hr 188 197 188 197 N/A

SFOC — g/kW-hr 184 193 184 193 182-184(without pumps)

Configuration Vee 16 Vee 16

Bore — mm/in 280 x 11.0 260 x 10.2

Stroke — mm/in 300 x 11.8 320 x 12.6

Displacement — L 296 272

Fuel System Electronic Unit Injection N/A

Weight — kg 28 500 37 000

Weight — lbs 62,832 81,400

Power Density — bkW/kg .161 .173 .178 .190 .141 .148 .148 .153

Dimensions — mm(L x W x H)

5685 x 2038 x 3406 5964 x 2474 x 3274

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PRODUCT NEWS –C280 MARINE PROPULSION ENGINE T2 COMPLIANT

Performance Data

C280-6 DIESEL ENGINE TECHNICAL DATA

:GNITAR ENIGNE009:)MPR( DEEPS DETAR Marine CSR

RATED POWER1 (bkW): 1730 CERTIFICATION5: IMO/EPA MARINE TIER IIBMEP @ 100% LOAD (kPa): 2082 TURBOCHARGER PART #: 157-5514

ID:NOITSUBMOC1:31:OITAR NOISSERPMOC

AFTERCOOLER WATER (oC): etallitsiD:EPYT LEUF23

JACKET WATER OUTLET (oC): YRD:DLOFINAM TSUAHXE09IUE:METSYS NOITINGI MEAN PISTON SPEED (m/s): 9

FIRING PRESSURE, MAXIMUM (kPa):

Engine Performance

ZONE LIMIT DATA ZONE LIMIT DATA

Fuel Boost Air hxE hxEtsooBleuFhxEhxE hxEEngine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhSpeed Power g ewoPdeepS/m ucpmeTobruT/m ucaPketaR/ r lb/ Rate in Hg- Flow4 Turbo Temp Flow

rpm bkW kW-hr L/hr Gaug rh-phphbmprnimCCniMe gal/hr Gauge cfm F F cfm

4803141713019406571.411543.002320095.0739735553.1715523.2340120371009Curve A 850 1634 209 407.1 264 164.7 559 389 361.6 Curve A 850 2191 0.344 107.5 78 5815 1039 733 12771

2491157796018425375.001243.026020081.8333146756.8415425.08380283510085770173822115944265.39933.043910571.5037445063.7219023.4536022441057239686882115182339.46443.042310073.6914649067.971119.542902789007127569886110722422.65053.082110560.2610841363.46289.212212148056896499827117581810.84753.04490060.3312843366.25069.181712407006617336872118051214.93463.00670552.5012648067.24244.94112276505514722778201691172.03763.07750056.771143559.33524.411322034005

PROPELLER DEMAND DATA PROPELLER DEMAND DATAFuel Boost Air hxE hxEtsooBleuFhxEhxE hxE

Engine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhOptimum Speed Power g/ Rate kPa cu m/ Turbo Temp cu m/ Optimum Speed Power lb/ Rate in Hg- Flow4 Turbo Temp Flow

Load rpm bkW kW-hr L/hr Gauge Min C C min Load rpm bhp hp-hr gal/hr Gauge cfm F F cfm

5072131721011985574.501453.088020098.9538735458.6613520.9935127551009(Curve P1) 850 1312 215 335.4 207 137.5 543 393 303.7 (Curve P1) 850 1759 0.353 88.6 61 4857 1010 740 10724

864867771017173447.27843.066410088.9323147452.5018413.5721124901008476620804010682131.06943.080210570.9818240650.183015.722212109057113511864018522126.94453.02890074.0513343659.36178.781512337007012449771013181414.04063.07870562.9113247453.15849.2519127850564723247459174191.23463.09160067.295932157.14136.1211221640067842856468402158.42563.07740554.078432641.43810.49222553055478116565779938.81863.08530051.354922042.82011.17322762005

Heat Rejection @ 100% Load and 25o C Air)65301(281) nim/utB (WkrelooC liO ebuL)02022(783) nim/utB (WkretaW tekcaJ)47492(815) nim/utB (WkrelooCretfA)05816(7801) nim/utB (WkretaW waR ot noitcejeR taeH latoT

Exhaust Gas2 kW ( Btu/min ) 1321 ( 75165 ))3984(68) nim/utB (WknoitaidaR

Notes1 Ratings are based on ISO 3046/1 and SAEJ1995 Jan 90 standard reference conditions of 100 kPa, 25o C, and 30% relative humidity at the stated aftercooler water temperature.

2 Exhaust Heat rejection is based on fuel LHV and is not normally recoverable in total

4 Air flows are shown for 25oC air inlet to the turbocharger and 32oC cooling water to the charge air cooler.

DM8389-00 1/16/07

3 At 100% load with pumps +/- 3%. Performance and fuel consumption are based on 35 API, 16oC fuel having a lower heating value of 42,780 kJ/kg used at 29oC with a density of 838.9 g/liter.

5 This engine's exhaust emissions are in compliance with the INTERNATIONAL MARINE ORGANIZATION'S (IMO) standard as described in REGULATION 13 of ANNEX VI of MARPOL 73/78 and ISO 8178 for measuring HC, CO, PM, and NOx.

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Page 10: Caterpillar Motor

PRODUCT NEWS –C280 MARINE PROPULSION ENGINE T2 COMPLIANT

C280-6 DIESEL ENGINE TECHNICAL DATA

:GNITAR ENIGNE0001:)MPR( DEEPS DETAR Marine CSR

RATED POWER1 (bkW): 1850 CERTIFICATION5: IMO/EPA MARINE TIER IIBMEP @ 100% LOAD (kPa): 2003 TURBOCHARGER PART #: 189-4427

ID:NOITSUBMOC1:31:OITAR NOISSERPMOC

AFTERCOOLER WATER (oC): etallitsiD:EPYT LEUF23

JACKET WATER OUTLET (oC): YRD:DLOFINAM TSUAHXE09IUE:METSYS NOITINGI MEAN PISTON SPEED (m/s): 10

FIRING PRESSURE, MAXIMUM (kPa):

Engine Performance

ZONE LIMIT DATA ZONE LIMIT DATA

Fuel Boost Air hxE hxEtsooBleuFhxEhxE hxEEngine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhSpeed Power g ewoPdeepS/m ucpmeTobruT/m ucaPketaR/ r lb/ Rate in Hg- Flow4 Turbo Temp Flow

rpm bkW kW-hr L/hr Gaug rh-phphbmprnimCCniMe gal/hr Gauge cfm F F cfm

401413071896856171.121243.0184200014.9933737255.6818327.85480205810001Curve A 910 1683 214 429.4 234 160.3 543 388 352.2 Curve A 910 2257 0.352 113.4 69 5662 1009 730 12438

2180166771018674854.101833.080120582.6038047450.5315912.483502275105843776289998423333.27143.098410080.9121447350.290119.372702011100892666483792472320.16443.044210577.7812543256.77972.13290282905785157381496412715.94743.09990071.6417445058.06654.78111254700719548580598781510.44943.04880360.0319540152.35945.66121295603678145683499961415.24753.05380066.8113646051.84742.16171232600640639680390641112.53963.01760051.2015649944.14735.331422005005

PROPELLER DEMAND DATA PROPELLER DEMAND DATAFuel Boost Air hxE hxEtsooBleuFhxEhxE hxE

Engine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhOptimum Speed Power g/ Rate kPa cu m/ Turbo Temp cu m/ Optimum Speed Power lb/ Rate in Hg- Flow4 Turbo Temp Flow

Load rpm bkW kW-hr L/hr Gauge Min C C min Load rpm bhp hp-hr gal/hr Gauge cfm F F cfm

825218967591785561.211253.0332200017.4530734152.6610227.42441256610001(Curve P1) 910 1255 217 324.6 157 123.2 512 395 273.4 (Curve P1) 910 1683 0.357 85.7 47 4351 954 743 9654

61772970598333139.86253.017310585.8122240155.495018.062412320105887466085292772223.65643.034110084.3810346945.87474.31201225800803250973885622611.74153.02490571.8411243741.46353.87131220705796442771587691218.83653.06670075.6211145547.55140.7416121750079113127297034187.82163.08550363.883832245.04727.8019126140361672286927113167.52473.02840062.871637831.73123.797220630062112165316231140.51773.09720058.954923231.23418.65922802005

Heat Rejection @ 100% Load and 25o C Air)80611(402) nim/utB (WkrelooC liO ebuL)49312(673) nim/utB (WkretaW tekcaJ)74523(275) nim/utB (WkrelooCretfA)94556(2511) nim/utB (WkretaW waR ot noitcejeR taeH latoT

Exhaust Gas2 kW ( Btu/min ) 1480 ( 84212 ))8715(19) nim/utB (WknoitaidaR

Notes1 Ratings are based on ISO 3046/1 and SAEJ1995 Jan 90 standard reference conditions of 100 kPa, 25o C, and 30% relative humidity at the stated aftercooler water temperature.

2 Exhaust Heat rejection is based on fuel LHV and is not normally recoverable in total

4 Air flows are shown for 25oC air inlet to the turbocharger and 32oC cooling water to the charge air cooler.

DM8390-00 1/16/07

3 At 100% load with pumps +/- 3%. Performance and fuel consumption are based on 35 API, 16oC fuel having a lower heating value of 42,780 kJ/kg used at 29oC with a density of 838.9 g/liter.

5 This engine's exhaust emissions are in compliance with the INTERNATIONAL MARINE ORGANIZATION'S (IMO) standard as described in REGULATION 13 of ANNEX VI of MARPOL 73/78 and ISO 8178 for measuring HC, CO, PM, and NOx.

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LEXM8385-01 10 of 40

Performance Data

Page 11: Caterpillar Motor

PRODUCT NEWS –C280 MARINE PROPULSION ENGINE T2 COMPLIANT

LEXM8385-01 11 of 40

Performance Data

C280-6 DIESEL ENGINE TECHNICAL DATA

:GNITAR ENIGNE009:)MPR( DEEPS DETAR Marine MCR

RATED POWER1 (bkW): 1900 CERTIFICATION5: IMO/EPA MARINE TIER IIBMEP @ 100% LOAD (kPa): 2286 TURBOCHARGER PART #: 157-5514

ID:NOITSUBMOC1:31:OITAR NOISSERPMOC

AFTERCOOLER WATER (oC): etallitsiD:EPYT LEUF23

JACKET WATER OUTLET (oC): YRD:DLOFINAM TSUAHXE09IUE:METSYS NOITINGI MEAN PISTON SPEED (m/s): 9

FIRING PRESSURE, MAXIMUM (kPa):

Engine Performance

ZONE LIMIT DATA ZONE LIMIT DATA

Fuel Boost Air hxE hxEtsooBleuFhxEhxE hxEEngine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhSpeed Power g ewoPdeepS/m ucpmeTobruT/m ucaPketaR/ r lb/ Rate in Hg- Flow4 Turbo Temp Flow

rpm bkW kW-hr L/hr Gaug rh-phphbmprnimCCniMe gal/hr Gauge cfm F F cfm

5943132754014816974.121433.084520091.2834833651.5716628.9543020091009Curve A 850 1794 205 438.4 268 167.7 561 386 366.9 Curve A 850 2406 0.338 115.7 79 5921 1042 727 12957

7512166747019635370.901833.056220082.4438049750.2517427.21450298610082811183853114564366.101633.032120576.6138443168.1314129.4834023851057386758884119703830.27243.057410075.7124740262.789217.2728020011007380661968117732728.95743.070210563.2711941463.76094.622112009056600552920210491022.15653.001010068.1416940569.45769.391612357006069329846110751412.24463.03180551.2118749265.44746.95112260605542926089601042185.23963.07160058.280346751.53829.221422064005

PROPELLER DEMAND DATA PROPELLER DEMAND DATAFuel Boost Air hxE hxEtsooBleuFhxEhxE hxE

Engine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhOptimum Speed Power g/ Rate kPa cu m/ Turbo Temp cu m/ Optimum Speed Power lb/ Rate in Hg- Flow4 Turbo Temp Flow

Load rpm bkW kW-hr L/hr Gauge Min C C min Load rpm bhp hp-hr gal/hr Gauge cfm F F cfm

3682121761015695572.801053.066120092.4638737459.8615528.9043125161009(Curve P1) 850 1361 215 347.9 219 143.0 547 393 315.7 (Curve P1) 850 1824 0.353 91.8 65 5052 1016 739 11149

608877732010683743.57743.012510084.9424141553.9018511.5821124311008709670884019492231.26743.035210576.5911345655.389011.532112539057774591895013132222.15353.091010071.5517341755.56570.491412067007533450843010581517.14953.06180568.2210347554.25151.85181280605627337573797941012.33363.02460065.593043254.24339.5211229740069552476488122167.52563.04940555.277533746.43024.792229630551291575477700134.91763.01730054.452032145.82116.37322772005

Heat Rejection @ 100% Load and 25o C Air)57801(191) nim/utB (WkrelooC liO ebuL)03912(583) nim/utB (WkretaW tekcaJ)59403(635) nim/utB (WkrelooCretfA)00336(2111) nim/utB (WkretaW waR ot noitcejeR taeH latoT

Exhaust Gas2 kW ( Btu/min ) 1379 ( 78465 ))5325(29) nim/utB (WknoitaidaR

Notes1 Ratings are based on ISO 3046/1 and SAEJ1995 Jan 90 standard reference conditions of 100 kPa, 25o C, and 30% relative humidity at the stated aftercooler water temperature.

2 Exhaust Heat rejection is based on fuel LHV and is not normally recoverable in total

4 Air flows are shown for 25oC air inlet to the turbocharger and 32oC cooling water to the charge air cooler.

DM8391-00 1/16/07

3 At 100% load with pumps +/- 3%. Performance and fuel consumption are based on 35 API, 16oC fuel having a lower heating value of 42,780 kJ/kg used at 29oC with a density of 838.9 g/liter.

5 This engine's exhaust emissions are in compliance with the INTERNATIONAL MARINE ORGANIZATION'S (IMO) standard as described in REGULATION 13 of ANNEX VI of MARPOL 73/78 and ISO 8178 for measuring HC, CO, PM, and NOx.

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Page 12: Caterpillar Motor

PRODUCT NEWS –C280 MARINE PROPULSION ENGINE T2 COMPLIANT

LEXM8385-01 12 of 40

C280-6 DIESEL ENGINE TECHNICAL DATA

:GNITAR ENIGNE0001:)MPR( DEEPS DETAR Marine MCR

RATED POWER1 (bkW): 2030 CERTIFICATION5: IMO/EPA MARINE TIER IIBMEP @ 100% LOAD (kPa): 2198 TURBOCHARGER PART #: 189-4427

ID:NOITSUBMOC1:31:OITAR NOISSERPMOC

AFTERCOOLER WATER (oC): etallitsiD:EPYT LEUF23

JACKET WATER OUTLET (oC): YRD:DLOFINAM TSUAHXE09IUE:METSYS NOITINGI MEAN PISTON SPEED (m/s): 10

FIRING PRESSURE, MAXIMUM (kPa):

Engine Performance

ZONE LIMIT DATA ZONE LIMIT DATA

Fuel Boost Air hxE hxEtsooBleuFhxEhxE hxEEngine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhSpeed Power g ewoPdeepS/m ucpmeTobruT/m ucaPketaR/ r lb/ Rate in Hg- Flow4 Turbo Temp Flow

rpm bkW kW-hr L/hr Gaug rh-phphbmprnimCCniMe gal/hr Gauge cfm F F cfm

5464141760015676576.131933.0227200017.4149731456.1914525.89460203020001Curve A 910 1847 209 460.2 248 167.1 559 390 368.5 Curve A 910 2477 0.344 121.5 73 5901 1038 734 13013

8251136792016905462.011433.041320584.6236044553.4416125.7143025271058783882804017153738.87333.036610085.7322440656.995216.8922020421008841706820011292724.76143.088310574.2020649357.28294.552702530105700752685795232026.45443.031110074.1611644258.56668.60290203800720942885797691619.74743.08690368.8312744257.55556.18111222703623649883798481517.54453.05090062.1316743253.25150.37151257600670142981499361110.73273.07960053.6118745054.64731.041622025005

PROPELLER DEMAND DATA PROPELLER DEMAND DATAFuel Boost Air hxE hxEtsooBleuFhxEhxE hxE

Engine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhOptimum Speed Power g/ Rate kPa cu m/ Turbo Temp cu m/ Optimum Speed Power lb/ Rate in Hg- Flow4 Turbo Temp Flow

Load rpm bkW kW-hr L/hr Gauge Min C C min Load rpm bhp hp-hr gal/hr Gauge cfm F F cfm

467212076690695667.511153.0513200014.1632739158.8613222.83431262710001(Curve P1) 910 1301 206 319.4 165 124.1 516 394 274.6 (Curve P1) 910 1744 0.339 84.3 49 4381 961 741 9699

07873977597933334.17253.012410589.2223244152.690114.072412060105883460186392472320.95943.058110083.2812342056.77873.32221248800864351088985922711.84643.06790574.1517241840.56653.28101282705725443879687391316.14763.04970071.6217145649.45344.7513222950075233727387025185.92753.09750362.496837140.34826.1117122340368692196927104152.62763.00050061.486637837.93811.993223730063042865016182148.51283.09820050.868921233.63217.95232612005

Heat Rejection @ 100% Load and 25o C Air)36021(212) nim/utB (WkrelooC liO ebuL)47822(204) nim/utB (WkretaW tekcaJ)08843(316) nim/utB (WkrelooCretfA)61896(7221) nim/utB (WkretaW waR ot noitcejeR taeH latoT

Exhaust Gas2 kW ( Btu/min ) 1228 ( 69873 ))3365(99) nim/utB (WknoitaidaR

Notes1 Ratings are based on ISO 3046/1 and SAEJ1995 Jan 90 standard reference conditions of 100 kPa, 25o C, and 30% relative humidity at the stated aftercooler water temperature.

2 Exhaust Heat rejection is based on fuel LHV and is not normally recoverable in total

4 Air flows are shown for 25oC air inlet to the turbocharger and 32oC cooling water to the charge air cooler.

DM8392-00 1/16/07

3 At 100% load with pumps +/- 3%. Performance and fuel consumption are based on 35 API, 16oC fuel having a lower heating value of 42,780 kJ/kg used at 29oC with a density of 838.9 g/liter.

5 This engine's exhaust emissions are in compliance with the INTERNATIONAL MARINE ORGANIZATION'S (IMO) standard as described in REGULATION 13 of ANNEX VI of MARPOL 73/78 and ISO 8178 for measuring HC, CO, PM, and NOx.

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Performance Data

Page 13: Caterpillar Motor

PRODUCT NEWS –C280 MARINE PROPULSION ENGINE T2 COMPLIANT

LEXM8385-01 13 of 40

Performance Data

C280-8 DIESEL ENGINE TECHNICAL DATA

:GNITAR ENIGNE009:)MPR( DEEPS DETAR Marine CSR

RATED POWER1 (bkW): 2300 CERTIFICATION5: IMO/EPA MARINE TIER IIBMEP @ 100% LOAD (kPa): 2076 TURBOCHARGER PART #: 284-8280

ID:NOITSUBMOC1:31:OITAR NOISSERPMOC

AFTERCOOLER WATER (oC): etallitsiD:EPYT LEUF23

JACKET WATER OUTLET (oC): YRD:DLOFINAM TSUAHXE09IUE:METSYS NOITINGI MEAN PISTON SPEED (m/s): 9

FIRING PRESSURE, MAXIMUM (kPa):

Engine Performance

ZONE LIMIT DATA ZONE LIMIT DATA

Fuel Boost Air hxE hxEtsooBleuFhxEhxE hxEEngine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhSpeed Power g ewoPdeepS/m ucpmeTobruT/m ucaPketaR/ r lb/ Rate in Hg- Flow4 Turbo Temp Flow

rpm bkW kW-hr L/hr Gaug rh-phphbmprnimCCniMe gal/hr Gauge cfm F F cfm

2378178690019888870.051143.048030094.0354633457.1525622.8657020032009Curve A 850 2172 209 540.3 260 240.9 543 367 510.3 Curve A 850 2913 0.344 142.7 77 8508 1009 693 18020

6207110701013897473.431443.024720081.2842733451.6220525.8059024402008715413072890976260.811223.007520571.1143738253.2919029.6446917191057534010572693964730.18533.089610075.5929937159.2314217.603302662100726087085893543325.56333.008310563.8221340358.79771.8422029201056084634850016962510.45343.030110065.3810540453.67055.402902228006838515840014142017.74453.05490553.5615540454.86536.08151250705534446580001328173.04953.07870058.5218548356.15427.251812785005

PROPELLER DEMAND DATA PROPELLER DEMAND DATAFuel Boost Air hxE hxEtsooBleuFhxEhxE hxE

Engine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhOptimum Speed Power g/ Rate kPa cu m/ Turbo Temp cu m/ Optimum Speed Power lb/ Rate in Hg- Flow4 Turbo Temp Flow

Load rpm bkW kW-hr L/hr Gauge Min C C min Load rpm bhp hp-hr gal/hr Gauge cfm F F cfm

648716764899558572.931253.067720093.5058539254.2423523.7254120702009(Curve P1) 850 1744 210 437.2 213 210.3 500 348 430.8 (Curve P1) 850 2338 0.346 115.4 63 7428 932 658 15214

085216664090016942.49933.005910082.6532535847.2717617.6536024541008691014072096774530.77633.060610577.8823733842.5319116.192402891105791289470290073423.36043.060310077.2328933948.401186.93260247900742561871397582517.15743.064010567.4816140059.08150.6911120870563215377309852294.14353.02280061.5411144849.36138.6514123160065704127957878141.23653.04360554.5113834042.35416.1216122740556203156037584131.42553.06740057.584438831.2493.19612553005

Heat Rejection @ 100% Load and 25o C Air)07731(242) nim/utB (WkrelooC liO ebuL)04572(484) nim/utB (WkretaW tekcaJ)92662(864) nim/utB (WkrelooCretfA)93976(4911) nim/utB (WkretaW waR ot noitcejeR taeH latoT

Exhaust Gas2 kW ( Btu/min ) 1804 ( 102648 ))7846(411) nim/utB (WknoitaidaR

Notes1 Ratings are based on ISO 3046/1 and SAEJ1995 Jan 90 standard reference conditions of 100 kPa, 25o C, and 30% relative humidity at the stated aftercooler water temperature.

2 Exhaust Heat rejection is based on fuel LHV and is not normally recoverable in total

4 Air flows are shown for 25oC air inlet to the turbocharger and 32oC cooling water to the charge air cooler.

DM8397-00 1/16/07

3 At 100% load with pumps +/- 3%. Performance and fuel consumption are based on 35 API, 16oC fuel having a lower heating value of 42,780 kJ/kg used at 29oC with a density of 838.9 g/liter.

5 This engine's exhaust emissions are in compliance with the INTERNATIONAL MARINE ORGANIZATION'S (IMO) standard as described in REGULATION 13 of ANNEX VI of MARPOL 73/78 and ISO 8178 for measuring HC, CO, PM, and NOx.

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Page 14: Caterpillar Motor

PRODUCT NEWS –C280 MARINE PROPULSION ENGINE T2 COMPLIANT

C280-8 DIESEL ENGINE TECHNICAL DATA

:GNITAR ENIGNE0001:)MPR( DEEPS DETAR Marine CSR

RATED POWER1 (bkW): 2460 CERTIFICATION5: IMO/EPA MARINE TIER IIBMEP @ 100% LOAD (kPa): 1998 TURBOCHARGER PART #: 284-8276

ID:NOITSUBMOC1:31:OITAR NOISSERPMOC

AFTERCOOLER WATER (oC): etallitsiD:EPYT LEUF23

JACKET WATER INLET (oC): YRD:DLOFINAM TSUAHXE09IUE:METSYS NOITINGI MEAN PISTON SPEED (m/s): 10

FIRING PRESSURE, MAXIMUM (kPa):

Engine Performance

ZONE LIMIT DATA ZONE LIMIT DATA

Fuel Boost Air hxE hxEtsooBleuFhxEhxE hxEEngine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhSpeed Power g/ Rate kPa cu m/ Turbo Temp cu m/ Speed Power lb/ Rate in Hg- Flow4 Turbo Temp Flow

rpm bkW kW-hr L/hr Gaug rh-phphbmprnimCCniMe gal/hr Gauge cfm F F cfm

1000 2460 213 624.4 268 274.1 543 375 587.4 1000 3299 0.351 164.9 79 9680 1010 707 20743Curve A 950 2337 212 589.8 258 263.3 541 368 557.9 Curve A 950 3134 0.349 155.7 76 9297 1006 694 19702

910 2239 211 562.6 243 247.8 544 374 530.6 910 3002 0.347 148.5 72 8751 1011 706 18739850 2091 210 523.3 213 216.7 562 405 487.0 850 2804 0.346 138.2 63 7652 1043 762 17200800 1474 212 372.7 115 139.6 584 466 343.0 800 1976 0.349 98.4 34 4929 1082 872 12112750 1212 217 313.7 77 105.2 615 509 274.5 750 1625 0.357 82.8 23 3717 1138 948 9693700 950 223 252.1 47 78.5 628 536 212.2 700 1274 0.367 66.6 14 2772 1163 996 7494630 760 227 205.8 29 59.5 634 545 163.2 630 1019 0.374 54.3 9 2101 1172 1013 5762600 741 229 202.1 26 55.4 654 561 155.3 600 994 0.377 53.4 8 1956 1210 1042 5484500 532 236 149.8 12 38.9 616 523 104.3 500 714 0.389 39.6 4 1375 1141 973 3685

PROPELLER DEMAND DATA PROPELLER DEMAND DATAFuel Boost Air hxE hxEtsooBleuFhxEhxE hxE

Engine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhOptimum Speed Power g/ Rate kPa cu m/ Turbo Temp cu m/ Optimum Speed Power lb/ Rate in Hg- Flow4 Turbo Temp Flow

Load rpm bkW kW-hr L/hr Gauge Min C C min Load rpm bhp hp-hr gal/hr Gauge cfm F F cfm

1000 2214 215 567.6 247 268.3 523 361 562.0 1000 2969 0.354 149.9 73 9474 973 683 19847(Curve P1) 950 1898 216 489.1 204 230.7 524 378 495.6 (Curve P1) 950 2546 0.356 129.1 60 8148 974 712 17502

910 1668 214 425.5 160 192.2 529 402 428.8 910 2237 0.352 112.3 47 6787 983 756 15143850 1360 214 347.2 104 140.8 550 446 335.6 850 1823 0.353 91.7 31 4974 1022 835 11853800 1134 218 294.7 71 109.1 571 479 272.9 800 1520 0.359 77.8 21 3854 1060 895 9638750 934 222 247.0 48 85.5 585 501 220.5 750 1253 0.365 65.2 14 3019 1085 935 7789700 759 225 203.6 31 68.0 579 501 175.5 700 1018 0.370 53.8 9 2400 1074 934 6198630 554 229 150.8 16 50.6 528 458 123.4 630 742 0.376 39.8 5 1788 982 857 4360600 478 230 131.3 11 44.9 496 429 105.1 600 641 0.379 34.7 3 1586 924 805 3711500 277 237 78.2 3 31.7 370 320 62.3 500 371 0.390 20.6 1 1119 698 607 2199

Heat Rejection @ 100% Load and 25o C Air)02451(172) nim/utB (WkrelooC liO ebuL)39382(994) nim/utB (WkretaW tekcaJ)91653(626) nim/utB (WkrelooCretfA)23497(6931) nim/utB (WkretaW waR ot noitcejeR taeH latoT

Exhaust Gas2 kW ( Btu/min ) 2056 ( 116986 ))3117(521) nim/utB (WknoitaidaR

Notes1 Ratings are based on ISO 3046/1 and SAEJ1995 Jan 90 standard reference conditions of 100 kPa, 25o C, and 30% relative humidity at the stated aftercooler water temperature.

2 Exhaust Heat rejection is based on fuel LHV and is not normally recoverable in total

4 Air flows are shown for 25oC air inlet to the turbocharger and 32oC cooling water to the charge air cooler.

DM8398-01 2/5/08

3 At 100% load with pumps +/- 3%. Performance and fuel consumption are based on 35 API, 16oC fuel having a lower heating value of 42,780 kJ/kg used at 29oC with a density of 838.9 g/liter.

5 This engine's exhaust emissions are in compliance with the INTERNATIONAL MARINE ORGANIZATION'S (IMO) standard as described in REGULATION 13 of ANNEX VI of MARPOL 73/78 and ISO 8178 for measuring HC, CO, PM, and NOx.

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LEXM8385-01 14 of 40

Performance Data

Page 15: Caterpillar Motor

PRODUCT NEWS –C280 MARINE PROPULSION ENGINE T2 COMPLIANT

LEXM8385-01 15 of 40

Performance Data

C280-8 DIESEL ENGINE TECHNICAL DATA

:GNITAR ENIGNE009:)MPR( DEEPS DETAR Marine MCR

RATED POWER1 (bkW): 2530 CERTIFICATION5: IMO/EPA MARINE TIER IIBMEP @ 100% LOAD (kPa): 2283 TURBOCHARGER PART #: 284-8280

ID:NOITSUBMOC1:31:OITAR NOISSERPMOC

AFTERCOOLER WATER (oC): etallitsiD:EPYT LEUF23

JACKET WATER OUTLET (oC): YRD:DLOFINAM TSUAHXE09IUE:METSYS NOITINGI MEAN PISTON SPEED (m/s): 9

FIRING PRESSURE, MAXIMUM (kPa):

Engine Performance

ZONE LIMIT DATA ZONE LIMIT DATA

Fuel Boost Air hxE hxEtsooBleuFhxEhxE hxEEngine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhSpeed Power g ewoPdeepS/m ucpmeTobruT/m ucaPketaR/ r lb/ Rate in Hg- Flow4 Turbo Temp Flow

rpm bkW kW-hr L/hr Gaug rh-phphbmprnimCCniMe gal/hr Gauge cfm F F cfm

8779179682016929487.261633.039330090.0650734552.3624823.6164020352009Curve A 850 2389 203 577.3 273 248.6 550 369 528.3 Curve A 850 3204 0.334 152.4 81 8779 1022 696 18657

6757189651011628878.241233.061030087.7940736459.3322629.04520294220082465150740014037961.921023.072820579.2444730458.6023321.9845918012057072117377694215349.88823.000910071.9132939151.5414417.6339917141007770940860018983920.57623.041610560.7529241454.011991.4828914021056163746874019003020.36433.022310064.8022644652.58667.832302689006712628838013052311.55253.079010550.6712744859.07346.80241281805521843092601309196.44953.01780052.6314842759.35929.861812056005

PROPELLER DEMAND DATA PROPELLER DEMAND DATAFuel Boost Air hxE hxEtsooBleuFhxEhxE hxE

Engine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhOptimum Speed Power g/ Rate kPa cu m/ Turbo Temp cu m/ Optimum Speed Power lb/ Rate in Hg- Flow4 Turbo Temp Flow

Load rpm bkW kW-hr L/hr Gauge Min C C min Load rpm bhp hp-hr gal/hr Gauge cfm F F cfm

601814768897968670.341843.048820097.2157531353.6428527.1451121512009(Curve P1) 850 1812 211 455.8 224 217.2 508 350 446.5 (Curve P1) 850 2430 0.347 120.3 66 7670 946 662 15767

189211667097136258.79933.062020086.7630536849.8715716.0736021151008155011078095594839.97633.096610578.8922736843.0417214.203402542105749481574297183525.56933.075310075.0420045941.801681.842602210100711766879396292615.35543.078010560.0919144059.28455.20201201805690350873196232019.24253.05580063.0515149849.56433.2614127360066973037658827133.43663.08560555.7018838549.84119.9212221940559303046727305135.62573.05940051.688336835.2492.001822963005

Heat Rejection @ 100% Load and 25o C Air)38441(552) nim/utB (WkrelooC liO ebuL)78192(315) nim/utB (WkretaW tekcaJ)74704(617) nim/utB (WkrelooCretfA)81448(4841) nim/utB (WkretaW waR ot noitcejeR taeH latoT

Exhaust Gas2 kW ( Btu/min ) 1947 ( 110784 ))9996(321) nim/utB (WknoitaidaR

Notes1 Ratings are based on ISO 3046/1 and SAEJ1995 Jan 90 standard reference conditions of 100 kPa, 25o C, and 30% relative humidity at the stated aftercooler water temperature.

2 Exhaust Heat rejection is based on fuel LHV and is not normally recoverable in total

4 Air flows are shown for 25oC air inlet to the turbocharger and 32oC cooling water to the charge air cooler.

DM8399-00 1/16/07

3 At 100% load with pumps +/- 3%. Performance and fuel consumption are based on 35 API, 16oC fuel having a lower heating value of 42,780 kJ/kg used at 29oC with a density of 838.9 g/liter.

5 This engine's exhaust emissions are in compliance with the INTERNATIONAL MARINE ORGANIZATION'S (IMO) standard as described in REGULATION 13 of ANNEX VI of MARPOL 73/78 and ISO 8178 for measuring HC, CO, PM, and NOx.

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Page 16: Caterpillar Motor

PRODUCT NEWS –C280 MARINE PROPULSION ENGINE T2 COMPLIANT

LEXM8385-01 16 of 40

Performance Data

C280-8 DIESEL ENGINE TECHNICAL DATA

:GNITAR ENIGNE0001:)MPR( DEEPS DETAR Marine MCR

RATED POWER1 (bkW): 2710 CERTIFICATION5: IMO/EPA MARINE TIER IIBMEP @ 100% LOAD (kPa): 2201 TURBOCHARGER PART #: 284-8276

ID:NOITSUBMOC1:31:OITAR NOISSERPMOC

AFTERCOOLER WATER (oC): etallitsiD:EPYT LEUF23

JACKET WATER INLET (oC): YRD:DLOFINAM TSUAHXE09IUE:METSYS NOITINGI MEAN PISTON SPEED (m/s): 10

FIRING PRESSURE, MAXIMUM (kPa):

Engine Performance

ZONE LIMIT DATA ZONE LIMIT DATA

Fuel Boost Air hxE hxEtsooBleuFhxEhxE hxEEngine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhSpeed Power g/ Rate kPa cu m/ Turbo Temp cu m/ Speed Power lb/ Rate in Hg- Flow4 Turbo Temp Flow

rpm bkW kW-hr L/hr Gaug rh-phphbmprnimCCniMe gal/hr Gauge cfm F F cfm

1000 2710 213 688.1 289 287.5 563 386 627.7 1000 3634 0.351 181.7 86 10153 1045 727 22168Curve A 950 2574 210 643.6 286 274.1 553 370 583.9 Curve A 950 3452 0.345 169.9 85 9680 1027 699 20620

910 2466 208 611.3 272 257.4 554 375 552.3 910 3307 0.342 161.4 81 9091 1029 707 19505850 2303 206 566.8 240 225.4 575 409 509.9 850 3089 0.340 149.7 71 7959 1066 768 18009800 1651 211 414.5 140 157.0 586 457 380.8 800 2214 0.347 109.4 41 5545 1086 855 13448750 1361 214 347.1 94 116.5 623 506 302.8 750 1824 0.352 91.7 28 4114 1153 944 10692700 1053 221 277.6 57 84.7 646 545 231.8 700 1412 0.364 73.3 17 2992 1195 1012 8187630 806 227 218.0 32 61.6 653 560 172.1 630 1081 0.373 57.6 9 2174 1207 1040 6077600 779 229 212.4 29 57.0 674 577 162.8 600 1045 0.376 56.1 8 2011 1245 1071 5750500 579 236 163.0 14 40.3 661 560 113.3 500 777 0.389 43.0 4 1423 1221 1040 4002

PROPELLER DEMAND DATA PROPELLER DEMAND DATAFuel Boost Air hxE hxEtsooBleuFhxEhxE hxE

Engine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhOptimum Speed Power g/ Rate kPa cu m/ Turbo Temp cu m/ Optimum Speed Power lb/ Rate in Hg- Flow4 Turbo Temp Flow

Load rpm bkW kW-hr L/hr Gauge Min C C min Load rpm bhp hp-hr gal/hr Gauge cfm F F cfm

1000 2304 213 586.2 254 270.7 528 365 570.5 1000 3090 0.351 154.8 75 9560 983 689 20146(Curve P1) 950 1975 215 507.3 215 238.8 527 376 511.3 (Curve P1) 950 2649 0.355 133.9 64 8431 980 708 18058

910 1736 214 442.5 171 200.3 531 398 444.6 910 2328 0.352 116.8 51 7075 987 749 15700850 1415 214 360.1 112 146.7 551 443 348.1 850 1897 0.352 95.1 33 5179 1024 830 12295800 1180 217 305.5 77 113.0 574 479 282.4 800 1582 0.358 80.6 23 3991 1066 894 9973750 972 221 256.4 51 88.0 591 505 228.0 750 1303 0.364 67.7 15 3108 1096 940 8052700 790 225 211.5 33 69.6 589 509 181.5 700 1060 0.370 55.9 10 2458 1092 947 6410630 576 228 156.8 17 51.6 541 469 127.8 630 773 0.376 41.4 5 1822 1006 877 4512600 498 230 136.4 12 45.7 509 440 108.7 600 667 0.379 36.0 4 1614 947 825 3840500 288 237 81.3 3 31.9 381 329 63.8 500 386 0.390 21.5 1 1128 718 624 2252

Heat Rejection @ 100% Load and 25o C Air)54161(482) nim/utB (WkrelooC liO ebuL)13503(735) nim/utB (WkretaW tekcaJ)92205(388) nim/utB (WkrelooCretfA)50969(3071) nim/utB (WkretaW waR ot noitcejeR taeH latoT

Exhaust Gas2 kW ( Btu/min ) 2272 ( 129277 ))5977(731) nim/utB (WknoitaidaR

Notes1 Ratings are based on ISO 3046/1 and SAEJ1995 Jan 90 standard reference conditions of 100 kPa, 25o C, and 30% relative humidity at the stated aftercooler water temperature.

2 Exhaust Heat rejection is based on fuel LHV and is not normally recoverable in total

4 Air flows are shown for 25oC air inlet to the turbocharger and 32oC cooling water to the charge air cooler.

DM8400-01 2/5/08

3 At 100% load with pumps +/- 3%. Performance and fuel consumption are based on 35 API, 16oC fuel having a lower heating value of 42,780 kJ/kg used at 29oC with a density of 838.9 g/liter.

5 This engine's exhaust emissions are in compliance with the INTERNATIONAL MARINE ORGANIZATION'S (IMO) standard as described in REGULATION 13 of ANNEX VI of MARPOL 73/78 and ISO 8178 for measuring HC, CO, PM, and NOx.

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Page 17: Caterpillar Motor

PRODUCT NEWS –C280 MARINE PROPULSION ENGINE T2 COMPLIANT

LEXM8385-01 17 of 40

Performance Data

C280-12 DIESEL ENGINE TECHNICAL DATA

:GNITAR ENIGNE009:)MPR( DEEPS DETAR Marine CSR

RATED POWER1 (bkW): 3460 CERTIFICATION5: IMO/EPA MARINE TIER IIBMEP @ 100% LOAD (kPa): 2082 TURBOCHARGER PART #: 157-5514

ID:NOITSUBMOC1:31:OITAR NOISSERPMOC

AFTERCOOLER WATER (oC): etallitsiD:EPYT LEUF23

JACKET WATER OUTLET (oC): YRD:DLOFINAM TSUAHXE09IUE:METSYS NOITINGI MEAN PISTON SPEED (m/s): 9

FIRING PRESSURE, MAXIMUM (kPa):

Engine Performance

ZONE LIMIT DATA ZONE LIMIT DATA

Fuel Boost Air hxE hxEtsooBleuFhxEhxE hxEEngine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhSpeed Power g ewoPdeepS/m ucpmeTobruT/m ucaPketaR/ r lb/ Rate in Hg- Flow4 Turbo Temp Flow

rpm bkW kW-hr L/hr Gaug rh-phphbmprnimCCniMe gal/hr Gauge cfm F F cfm

28452217320159711375.422933.004640095.1278731550.4335423.0586020643009Curve A 850 3268 207 805.3 252 319.8 557 388 701.6 Curve A 850 4382 0.340 212.6 75 11294 1035 731 24778

91232377760121201966.991933.052140085.7562145752.9824329.55760267030089901263802114088953.681833.076830575.7957445063.9421028.50750248820575163156852111455234.921343.074620075.5833647069.6517010.09480247910076031159866117844429.111843.065220561.0230840361.721088.3241122861056743910937118863816.59553.088810067.4623844364.401952.2636128041006814756882115003217.87363.012510551.0123649061.58140.892022431105567452778201983275.06863.035110051.5511144556.76523.922422068005

PROPELLER DEMAND DATA PROPELLER DEMAND DATAFuel Boost Air hxE hxEtsooBleuFhxEhxE hxE

Engine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhOptimum Speed Power g/ Rate kPa cu m/ Turbo Temp cu m/ Optimum Speed Power lb/ Rate in Hg- Flow4 Turbo Temp Flow

Load rpm bkW kW-hr L/hr Gauge Min C C min Load rpm bhp hp-hr gal/hr Gauge cfm F F cfm

89742907500172511270.802943.067140092.2076731454.6232428.7872124113009(Curve P1) 850 2623 212 661.8 200 268.9 544 392 593.3 (Curve P1) 850 3518 0.348 174.7 59 9497 1011 738 20951

8356137732018627244.441543.033920083.8642141558.5023410.74501278120089603110854013065925.911743.071420571.0737243657.851994.25411220810573540121894019344123.89153.056910070.6923345657.521963.2733125641007133869771013853419.97653.037510569.5324247455.101747.20361237110562056347259229297.36163.073210061.4815931157.28034.1429123290065594856368004255.94563.03590553.0418432649.76816.7811221170554473165657199136.73963.06170050.6014922044.65016.241422435005

Heat Rejection @ 100% Load and 25o C Air)29602(463) nim/utB (WkrelooC liO ebuL)08314(727) nim/utB (WkretaW tekcaJ)95745(269) nim/utB (WkrelooCretfA)038611(3502) nim/utB (WkretaW waR ot noitcejeR taeH latoT

Exhaust Gas2 kW ( Btu/min ) 2561 ( 145721 ))6169(961) nim/utB (WknoitaidaR

Notes1 Ratings are based on ISO 3046/1 and SAEJ1995 Jan 90 standard reference conditions of 100 kPa, 25o C, and 30% relative humidity at the stated aftercooler water temperature.

2 Exhaust Heat rejection is based on fuel LHV and is not normally recoverable in total

4 Air flows are shown for 25oC air inlet to the turbocharger and 32oC cooling water to the charge air cooler.

DM8405-00 1/16/07

3 At 100% load with pumps +/- 3%. Performance and fuel consumption are based on 35 API, 16oC fuel having a lower heating value of 42,780 kJ/kg used at 29oC with a density of 838.9 g/liter.

5 This engine's exhaust emissions are in compliance with the INTERNATIONAL MARINE ORGANIZATION'S (IMO) standard as described in REGULATION 13 of ANNEX VI of MARPOL 73/78 and ISO 8178 for measuring HC, CO, PM, and NOx.

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Page 18: Caterpillar Motor

PRODUCT NEWS –C280 MARINE PROPULSION ENGINE T2 COMPLIANT

C280-12 DIESEL ENGINE TECHNICAL DATA

:GNITAR ENIGNE0001:)MPR( DEEPS DETAR Marine CSR

RATED POWER1 (bkW): 3700 CERTIFICATION5: IMO/EPA MARINE TIER IIBMEP @ 100% LOAD (kPa): 2003 TURBOCHARGER PART #: 189-4427

ID:NOITSUBMOC1:31:OITAR NOISSERPMOC

AFTERCOOLER WATER (oC): etallitsiD:EPYT LEUF23

JACKET WATER OUTLET (oC): YRD:DLOFINAM TSUAHXE09IUE:METSYS NOITINGI MEAN PISTON SPEED (m/s): 10

FIRING PRESSURE, MAXIMUM (kPa):

Engine Performance

ZONE LIMIT DATA ZONE LIMIT DATA

Fuel Boost Air hxE hxEtsooBleuFhxEhxE hxEEngine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhSpeed Power g ewoPdeepS/m ucpmeTobruT/m ucaPketaR/ r lb/ Rate in Hg- Flow4 Turbo Temp Flow

rpm bkW kW-hr L/hr Gaug rh-phphbmprnimCCniMe gal/hr Gauge cfm F F cfm

6785250737904021666.732633.0269400017.2374733259.0434227.99840200730001Curve A 910 3366 206 826.6 214 307.2 536 392 678.9 Curve A 910 4514 0.339 218.3 63 10848 997 738 23977

7591233881019719559.891133.071240588.1265448459.9524814.3571024413058384419281990506133.541243.077920081.0143443353.1716014.0558020222008124111182798284227.221643.098420574.3233342257.631476.464012658105758497389394393615.89643.089910076.8627444054.111550.373012094100742385585497933410.09753.076710367.5327547052.69749.043712813103688877680599813317.48653.017610064.3224640153.09548.023612642100643085685298723119.96663.014310055.7223646948.29736.4622220001005

PROPELLER DEMAND DATA PROPELLER DEMAND DATAFuel Boost Air hxE hxEtsooBleuFhxEhxE hxE

Engine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhOptimum Speed Power g/ Rate kPa cu m/ Turbo Temp cu m/ Optimum Speed Power lb/ Rate in Hg- Flow4 Turbo Temp Flow

Load rpm bkW kW-hr L/hr Gauge Min C C min Load rpm bhp hp-hr gal/hr Gauge cfm F F cfm

7025249605916811260.912443.0664400018.3178630159.5330126.92890203330001(Curve P1) 910 2509 210 628.2 145 249.8 508 393 551.8 (Curve P1) 910 3365 0.346 165.9 43 8821 946 739 19488

376510971495976925.631943.024720588.3441245054.291898.6152125402058581312081292665126.111243.068220083.3738244943.061077.2248025071008236019772889464517.39943.048810571.1035142746.131150.553212504105785196674483504119.67253.023510073.9528041548.411834.19241224110079046707477089271.75953.071110365.1815732144.48524.6128123380364575086437247257.05963.05690069.2610630936.77811.2914229170062344955406483245.92073.08550055.5213928135.76216.111522614005

Heat Rejection @ 100% Load and 25o C Air)15412(773) nim/utB (WkrelooC liO ebuL)03134(857) nim/utB (WkretaW tekcaJ)79576(8811) nim/utB (WkrelooCretfA)971231(3232) nim/utB (WkretaW waR ot noitcejeR taeH latoT

Exhaust Gas2 kW ( Btu/min ) 2768 ( 157499 ))58101(971) nim/utB (WknoitaidaR

Notes1 Ratings are based on ISO 3046/1 and SAEJ1995 Jan 90 standard reference conditions of 100 kPa, 25o C, and 30% relative humidity at the stated aftercooler water temperature.

2 Exhaust Heat rejection is based on fuel LHV and is not normally recoverable in total

4 Air flows are shown for 25oC air inlet to the turbocharger and 32oC cooling water to the charge air cooler.

DM8406-00 1/16/07

3 At 100% load with pumps +/- 3%. Performance and fuel consumption are based on 35 API, 16oC fuel having a lower heating value of 42,780 kJ/kg used at 29oC with a density of 838.9 g/liter.

5 This engine's exhaust emissions are in compliance with the INTERNATIONAL MARINE ORGANIZATION'S (IMO) standard as described in REGULATION 13 of ANNEX VI of MARPOL 73/78 and ISO 8178 for measuring HC, CO, PM, and NOx.

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LEXM8385-01 18 of 40

Performance Data

Page 19: Caterpillar Motor

PRODUCT NEWS –C280 MARINE PROPULSION ENGINE T2 COMPLIANT

LEXM8385-01 19 of 40

Performance Data

C280-12 DIESEL ENGINE TECHNICAL DATA

:GNITAR ENIGNE009:)MPR( DEEPS DETAR Marine MCR

RATED POWER1 (bkW): 3800 CERTIFICATION5: IMO/EPA MARINE TIER IIBMEP @ 100% LOAD (kPa): 2286 TURBOCHARGER PART #: 157-5514

ID:NOITSUBMOC1:31:OITAR NOISSERPMOC

AFTERCOOLER WATER (oC): etallitsiD:EPYT LEUF23

JACKET WATER OUTLET (oC): YRD:DLOFINAM TSUAHXE09IUE:METSYS NOITINGI MEAN PISTON SPEED (m/s): 9

FIRING PRESSURE, MAXIMUM (kPa):

Engine Performance

ZONE LIMIT DATA ZONE LIMIT DATA

Fuel Boost Air hxE hxEtsooBleuFhxEhxE hxEEngine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhSpeed Power g ewoPdeepS/m ucpmeTobruT/m ucaPketaR/ r lb/ Rate in Hg- Flow4 Turbo Temp Flow

rpm bkW kW-hr L/hr Gaug rh-phphbmprnimCCniMe gal/hr Gauge cfm F F cfm

08462027530176121775.042133.069050098.9472837555.4431628.0191020083009Curve A 850 3588 203 868.5 260 327.8 557 385 716.6 Curve A 850 4812 0.334 229.3 77 11577 1035 725 25305

65732767170197401172.612533.003540087.2769047757.6929329.81830287330087291224893115909164.202433.064240579.0260545165.7527024.66730266130574315128854116706732.341143.005920075.8242748161.2715214.24570200220073002121908112074624.911743.041420569.9339848362.331881.2541120081056359962920214583022.201553.002020068.1827940561.901660.7836126051006219759856111313412.48363.052610550.4220849267.88648.813122212105544857080701674289.46963.043210055.5611347751.07829.542422029005

PROPELLER DEMAND DATA PROPELLER DEMAND DATAFuel Boost Air hxE hxEtsooBleuFhxEhxE hxE

Engine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhOptimum Speed Power g/ Rate kPa cu m/ Turbo Temp cu m/ Optimum Speed Power lb/ Rate in Hg- Flow4 Turbo Temp Flow

Load rpm bkW kW-hr L/hr Gauge Min C C min Load rpm bhp hp-hr gal/hr Gauge cfm F F cfm

80152017210175611271.412743.013340090.1177734451.0333428.0181120323009(Curve P1) 850 2721 211 685.8 212 279.6 547 392 616.7 (Curve P1) 850 3649 0.348 181.1 63 9875 1017 738 21778

8917157792018457545.941543.024030080.7843144557.3122512.66590296220084253160835017775135.321643.070520579.2830347656.3615018.76401296810579770102836017454226.101053.083020072.5038343758.821379.4832120251007185870853015563517.28553.023610560.3421347555.301051.313612712105689667571792792010.66163.038210067.9813042252.48239.9429127590067905376388334263.15463.09890553.4416533749.86914.4911227370556383575577210230.93863.03470056.8011033140.75117.741422455005

Heat Rejection @ 100% Load and 25o C Air)54712(283) nim/utB (WkrelooC liO ebuL)52834(077) nim/utB (WkretaW tekcaJ)66206(9501) nim/utB (WkrelooCretfA)638521(2122) nim/utB (WkretaW waR ot noitcejeR taeH latoT

Exhaust Gas2 kW ( Btu/min ) 2686 ( 152833 ))65301(281) nim/utB (WknoitaidaR

Notes1 Ratings are based on ISO 3046/1 and SAEJ1995 Jan 90 standard reference conditions of 100 kPa, 25o C, and 30% relative humidity at the stated aftercooler water temperature.

2 Exhaust Heat rejection is based on fuel LHV and is not normally recoverable in total

4 Air flows are shown for 25oC air inlet to the turbocharger and 32oC cooling water to the charge air cooler.

DM8407-00 1/16/07

3 At 100% load with pumps +/- 3%. Performance and fuel consumption are based on 35 API, 16oC fuel having a lower heating value of 42,780 kJ/kg used at 29oC with a density of 838.9 g/liter.

5 This engine's exhaust emissions are in compliance with the INTERNATIONAL MARINE ORGANIZATION'S (IMO) standard as described in REGULATION 13 of ANNEX VI of MARPOL 73/78 and ISO 8178 for measuring HC, CO, PM, and NOx.

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Page 20: Caterpillar Motor

PRODUCT NEWS –C280 MARINE PROPULSION ENGINE T2 COMPLIANT

LEXM8385-01 20 of 40

Performance Data

C280-12 DIESEL ENGINE TECHNICAL DATA

:GNITAR ENIGNE0001:)MPR( DEEPS DETAR Marine MCR

RATED POWER1 (bkW): 4060 CERTIFICATION5: IMO/EPA MARINE TIER IIBMEP @ 100% LOAD (kPa): 2198 TURBOCHARGER PART #: 189-4427

ID:NOITSUBMOC1:31:OITAR NOISSERPMOC

AFTERCOOLER WATER (oC): etallitsiD:EPYT LEUF23

JACKET WATER OUTLET (oC): YRD:DLOFINAM TSUAHXE09IUE:METSYS NOITINGI MEAN PISTON SPEED (m/s): 10

FIRING PRESSURE, MAXIMUM (kPa):

Engine Performance

ZONE LIMIT DATA ZONE LIMIT DATA

Fuel Boost Air hxE hxEtsooBleuFhxEhxE hxEEngine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhSpeed Power g ewoPdeepS/m ucpmeTobruT/m ucaPketaR/ r lb/ Rate in Hg- Flow4 Turbo Temp Flow

rpm bkW kW-hr L/hr Gaug rh-phphbmprnimCCniMe gal/hr Gauge cfm F F cfm

6978270779918331479.162833.0444500014.5185736359.8731521.29950206040001Curve A 910 3694 207 911.5 243 335.9 545 390 740.3 Curve A 910 4954 0.341 240.7 72 11861 1013 734 26145

97032167220122201263.812133.072640585.3565040555.9828027.62810215430584737173872012427367.751333.062330080.2947443551.5022122.7952020842008507415689990995722.431933.067720574.6143647356.961093.8056020702057132118580799854917.901643.062220070.8139541250.031565.514012066100773698789594783513.69943.063910369.2720745157.901159.463212444103659887884696453418.19653.001810069.1525748154.001746.743612053100604182987398423116.37073.059310055.0328743050.29639.8725220401005

PROPELLER DEMAND DATA PROPELLER DEMAND DATAFuel Boost Air hxE hxEtsooBleuFhxEhxE hxE

Engine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhOptimum Speed Power g/ Rate kPa cu m/ Turbo Temp cu m/ Optimum Speed Power lb/ Rate in Hg- Flow4 Turbo Temp Flow

Load rpm bkW kW-hr L/hr Gauge Min C C min Load rpm bhp hp-hr gal/hr Gauge cfm F F cfm

9195230736999021369.422143.0926400019.3373737156.2432128.15870225430001(Curve P1) 910 2601 206 638.8 151 253.2 516 398 563.5 (Curve P1) 910 3488 0.339 168.7 45 8941 961 748 19901

852513974596856138.831243.034820581.2343242155.6813016.5258020212058993210187395725228.611643.007320081.1532343054.941574.244012767100824999973092624612.79943.035910575.1826244847.021450.863212654105765381874686363316.18163.088510076.6326142640.301341.90391248110071636037208198281.16073.085110361.0818838249.18825.1325223680363855396747326272.45083.000010061.8517637933.47223.5021326470067964865316305249.13783.09750050.3318923239.07219.021532234005

Heat Rejection @ 100% Load and 25o C Air)98522(793) nim/utB (WkrelooC liO ebuL)19654(308) nim/utB (WkretaW tekcaJ)50957(4331) nim/utB (WkrelooCretfA)581441(4352) nim/utB (WkretaW waR ot noitcejeR taeH latoT

Exhaust Gas2 kW ( Btu/min ) 3097 ( 176219 ))66211(891) nim/utB (WknoitaidaR

Notes1 Ratings are based on ISO 3046/1 and SAEJ1995 Jan 90 standard reference conditions of 100 kPa, 25o C, and 30% relative humidity at the stated aftercooler water temperature.

2 Exhaust Heat rejection is based on fuel LHV and is not normally recoverable in total

4 Air flows are shown for 25oC air inlet to the turbocharger and 32oC cooling water to the charge air cooler.

DM8408-00 1/16/07

3 At 100% load with pumps +/- 3%. Performance and fuel consumption are based on 35 API, 16oC fuel having a lower heating value of 42,780 kJ/kg used at 29oC with a density of 838.9 g/liter.

5 This engine's exhaust emissions are in compliance with the INTERNATIONAL MARINE ORGANIZATION'S (IMO) standard as described in REGULATION 13 of ANNEX VI of MARPOL 73/78 and ISO 8178 for measuring HC, CO, PM, and NOx.

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Page 21: Caterpillar Motor

PRODUCT NEWS –C280 MARINE PROPULSION ENGINE T2 COMPLIANT

LEXM8385-01 21 of 40

Performance Data

C280-16 DIESEL ENGINE TECHNICAL DATA

:GNITAR ENIGNE009:)MPR( DEEPS DETAR Marine CSR

RATED POWER1 (bkW): 4600 CERTIFICATION5: IMO/EPA MARINE TIER IIBMEP @ 100% LOAD (kPa): 2076 TURBOCHARGER PART #: 284-8280

ID:NOITSUBMOC1:31:OITAR NOISSERPMOC

AFTERCOOLER WATER (oC): etallitsiD:EPYT LEUF23

JACKET WATER OUTLET (oC): YRD:DLOFINAM TSUAHXE09IUE:METSYS NOITINGI MEAN PISTON SPEED (m/s): 9

FIRING PRESSURE, MAXIMUM (kPa):

Engine Performance

ZONE LIMIT DATA ZONE LIMIT DATA

Fuel Boost Air hxE hxEtsooBleuFhxEhxE hxEEngine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhSpeed Power g ewoPdeepS/m ucpmeTobruT/m ucaPketaR/ r lb/ Rate in Hg- Flow4 Turbo Temp Flow

rpm bkW kW-hr L/hr Gaug rh-phphbmprnimCCniMe gal/hr Gauge cfm F F cfm

3655346659964271773.282123.096160090.70011535353.8840623.96015910064009Curve A 850 4344 193 999.5 256 467.4 530 357 972.5 Curve A 850 5826 0.318 263.9 76 16506 986 675 34344

6722367609988451271.742613.038450089.3198532356.8343428.53929198040081318220757937131066.132613.014150576.6972734250.3733024.7782913383057721023479594019438.751623.059330079.9655935158.7525116.7958912352007765519972898966120.631643.006720568.0446248257.981272.51501285020561552173800010325419.411663.060220064.5537448351.841743.5342225461006333119489001386499.89763.009810559.0234543456.231136.47332290410558968268999735368.98004.047510053.6421647352.001120.0433424711005

PROPELLER DEMAND DATA PROPELLER DEMAND DATAFuel Boost Air hxE hxEtsooBleuFhxEhxE hxE

Engine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhOptimum Speed Power g/ Rate kPa cu m/ Turbo Temp cu m/ Optimum Speed Power lb/ Rate in Hg- Flow4 Turbo Temp Flow

Load rpm bkW kW-hr L/hr Gauge Min C C min Load rpm bhp hp-hr gal/hr Gauge cfm F F cfm

9144346686919661376.372643.025550096.4791530256.2745424.63010120414009(Curve P1) 850 3488 205 852.3 210 410.2 490 347 839.3 (Curve P1) 850 4677 0.338 225.0 62 14486 914 657 29641

4644226669859811847.681633.099830087.2960530848.6333611.7074028092008058912076983139333.251333.031230571.2652730847.3622119.6752026932057359513476195127227.521833.021620077.1545931943.402570.6745028491007507219778291755311.201243.019020568.9535148948.751547.68380206510560999277698404486.28253.054610069.2821140847.421729.21341272210068397027257166349.36453.076210558.4222830047.301212.2425125490558985946527798228.74253.02590050.7613435830.2881.181412017005

Heat Rejection @ 100% Load and 25o C Air)14572(484) nim/utB (WkrelooC liO ebuL)97055(869) nim/utB (WkretaW tekcaJ)95716(5801) nim/utB (WkrelooCretfA)973441(7352) nim/utB (WkretaW waR ot noitcejeR taeH latoT

Exhaust Gas2 kW ( Btu/min ) 3178 ( 180828 ))02121(312) nim/utB (WknoitaidaR

Notes1 Ratings are based on ISO 3046/1 and SAEJ1995 Jan 90 standard reference conditions of 100 kPa, 25o C, and 30% relative humidity at the stated aftercooler water temperature.

2 Exhaust Heat rejection is based on fuel LHV and is not normally recoverable in total

4 Air flows are shown for 25oC air inlet to the turbocharger and 32oC cooling water to the charge air cooler.

DM8413-00 1/16/07

3 At 100% load with pumps +/- 3%. Performance and fuel consumption are based on 35 API, 16oC fuel having a lower heating value of 42,780 kJ/kg used at 29oC with a density of 838.9 g/liter.

5 This engine's exhaust emissions are in compliance with the INTERNATIONAL MARINE ORGANIZATION'S (IMO) standard as described in REGULATION 13 of ANNEX VI of MARPOL 73/78 and ISO 8178 for measuring HC, CO, PM, and NOx.

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Page 22: Caterpillar Motor

PRODUCT NEWS –C280 MARINE PROPULSION ENGINE T2 COMPLIANT

C280-16 DIESEL ENGINE TECHNICAL DATA

:GNITAR ENIGNE0001:)MPR( DEEPS DETAR Marine CSR

RATED POWER1 (bkW): 4920 CERTIFICATION5: IMO/EPA MARINE TIER IIBMEP @ 100% LOAD (kPa): 1998 TURBOCHARGER PART #: 284-8276

ID:NOITSUBMOC1:31:OITAR NOISSERPMOC

AFTERCOOLER WATER (oC): etallitsiD:EPYT LEUF23

JACKET WATER INLET (oC): YRD:DLOFINAM TSUAHXE09IUE:METSYS NOITINGI MEAN PISTON SPEED (m/s): 10

FIRING PRESSURE, MAXIMUM (kPa):

Engine Performance

ZONE LIMIT DATA ZONE LIMIT DATA

Fuel Boost Air hxE hxEtsooBleuFhxEhxE hxEEngine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhSpeed Power g/ Rate kPa cu m/ Turbo Temp cu m/ Speed Power lb/ Rate in Hg- Flow4 Turbo Temp Flow

rpm bkW kW-hr L/hr Gaug rh-phphbmprnimCCniMe gal/hr Gauge cfm F F cfm

1000 4920 208 1222.0 252 526.1 532 371 1122.2 1000 6598 0.343 322.6 75 18580 989 701 39630Curve A 950 4674 208 1159.8 249 506.3 533 365 1069.1 Curve A 950 6268 0.343 306.2 74 17880 992 689 37754

910 4477 208 1109.4 238 477.3 539 374 1021.4 910 6004 0.342 292.9 70 16855 1002 704 36071850 4182 208 1034.9 209 418.3 563 408 944.9 850 5608 0.342 273.2 62 14771 1045 767 33368800 2947 211 742.4 110 271.9 581 466 668.4 800 3952 0.348 196.0 33 9603 1078 871 23604750 2424 215 622.0 74 206.6 608 504 535.9 750 3251 0.354 164.2 22 7297 1127 940 18925700 1900 221 501.0 46 156.1 620 525 416.4 700 2548 0.364 132.3 13 5512 1148 977 14706630 1520 226 410.1 28 119.7 626 529 321.8 630 2038 0.373 108.3 8 4227 1158 984 11364600 1482 228 403.1 26 111.5 648 545 306.2 600 1987 0.376 106.4 8 3936 1199 1013 10814500 1065 236 299.8 12 77.4 617 509 203.8 500 1428 0.389 79.2 4 2732 1142 948 7196

PROPELLER DEMAND DATA PROPELLER DEMAND DATAFuel Boost Air hxE hxEtsooBleuFhxEhxE hxE

Engine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhOptimum Speed Power g/ Rate kPa cu m/ Turbo Temp cu m/ Optimum Speed Power lb/ Rate in Hg- Flow4 Turbo Temp Flow

Load rpm bkW kW-hr L/hr Gauge Min C C min Load rpm bhp hp-hr gal/hr Gauge cfm F F cfm

1000 4428 210 1108.5 238 508.2 520 365 1070.8 1000 5938 0.346 292.7 71 17946 968 688 37817(Curve P1) 950 3796 212 959.4 197 449.7 523 377 965.0 (Curve P1) 950 5091 0.349 253.3 58 15880 974 710 34077

910 3337 211 839.3 154 372.1 530 402 830.9 910 4475 0.347 221.6 46 13141 986 756 29344850 2719 211 684.0 100 272.9 549 445 649.6 850 3647 0.347 180.6 30 9638 1021 832 22941800 2267 215 581.0 68 211.7 567 475 526.7 800 3040 0.354 153.4 20 7475 1053 887 18602750 1868 219 487.7 45 167.7 577 492 427.5 750 2505 0.361 128.8 13 5922 1071 918 15097700 1519 222 401.9 30 135.4 569 487 343.2 700 2037 0.366 106.1 9 4781 1056 909 12121630 1107 225 297.0 15 101.7 519 443 242.5 630 1485 0.370 78.4 5 3592 967 829 8566600 956 229 261.1 11 90.2 489 415 206.8 600 1283 0.377 68.9 3 3187 913 779 7305500 554 236 155.7 3 63.5 371 311 122.7 500 742 0.389 41.1 1 2241 700 591 4335

Heat Rejection @ 100% Load and 25o C Air)58803(345) nim/utB (WkrelooC liO ebuL)68865(0001) nim/utB (WkretaW tekcaJ)08438(7641) nim/utB (WkrelooCretfA)052171(0103) nim/utB (WkretaW waR ot noitcejeR taeH latoT

Exhaust Gas2 kW ( Btu/min ) 3932 ( 223731 ))72831(342) nim/utB (WknoitaidaR

Notes1 Ratings are based on ISO 3046/1 and SAEJ1995 Jan 90 standard reference conditions of 100 kPa, 25o C, and 30% relative humidity at the stated aftercooler water temperature.

2 Exhaust Heat rejection is based on fuel LHV and is not normally recoverable in total

4 Air flows are shown for 25oC air inlet to the turbocharger and 32oC cooling water to the charge air cooler.

DM8414-01 2/5/08

3 At 100% load with pumps +/- 3%. Performance and fuel consumption are based on 35 API, 16oC fuel having a lower heating value of 42,780 kJ/kg used at 29oC with a density of 838.9 g/liter.

5 This engine's exhaust emissions are in compliance with the INTERNATIONAL MARINE ORGANIZATION'S (IMO) standard as described in REGULATION 13 of ANNEX VI of MARPOL 73/78 and ISO 8178 for measuring HC, CO, PM, and NOx.

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LEXM8385-01 22 of 40

Performance Data

Page 23: Caterpillar Motor

PRODUCT NEWS –C280 MARINE PROPULSION ENGINE T2 COMPLIANT

LEXM8385-01 23 of 40

Performance Data

C280-16 DIESEL ENGINE TECHNICAL DATA

:GNITAR ENIGNE009:)MPR( DEEPS DETAR Marine MCR

RATED POWER1 (bkW): 5060 CERTIFICATION5: IMO/EPA MARINE TIER IIBMEP @ 100% LOAD (kPa): 2283 TURBOCHARGER PART #: 284-8280

ID:NOITSUBMOC1:31:OITAR NOISSERPMOC

AFTERCOOLER WATER (oC): etallitsiD:EPYT LEUF23

JACKET WATER OUTLET (oC): YRD:DLOFINAM TSUAHXE09IUE:METSYS NOITINGI MEAN PISTON SPEED (m/s): 9

FIRING PRESSURE, MAXIMUM (kPa):

Engine Performance

ZONE LIMIT DATA ZONE LIMIT DATA

Fuel Boost Air hxE hxEtsooBleuFhxEhxE hxEEngine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhSpeed Power g ewoPdeepS/m ucpmeTobruT/m ucaPketaR/ r lb/ Rate in Hg- Flow4 Turbo Temp Flow

rpm bkW kW-hr L/hr Gaug rh-phphbmprnimCCniMe gal/hr Gauge cfm F F cfm

8277376679902281280.903913.058760093.86013536359.5156722.07114910605009Curve A 850 4779 197 1122.2 265 487.3 532 356 1014.4 Curve A 850 6408 0.324 296.3 79 17208 990 673 35823

8714398668929161670.672123.023060088.7695630355.8546525.540159189440088001381757951341861.652813.045650570.8781834254.5040321.07939171240579823220895944001148.471323.099730075.9568245154.4827319.16669133820078398148820019367725.151923.092230563.6353749353.612190.47500280420564835105904018985818.721933.044620066.5340150650.761062.484602279100650331200167017094113.511963.049120558.6739350859.831838.63442263610554120155010601226388.29473.034710052.9828651755.201727.1537220031005

PROPELLER DEMAND DATA PROPELLER DEMAND DATAFuel Boost Air hxE hxEtsooBleuFhxEhxE hxE

Engine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhOptimum Speed Power g/ Rate kPa cu m/ Turbo Temp cu m/ Optimum Speed Power lb/ Rate in Hg- Flow4 Turbo Temp Flow

Load rpm bkW kW-hr L/hr Gauge Min C C min Load rpm bhp hp-hr gal/hr Gauge cfm F F cfm

2754384627921071476.772833.096750090.9792432257.1840523.15015022034009(Curve P1) 850 3624 206 889.9 2215 424.8 505 346 868.0 (Curve P1) 850 4860 0.339 235.0 656 15002 941 655 30654

9994244630965321941.291333.025040089.7070434849.9435615.7272021203008563025867091969635.751133.093330577.6753636844.4720215.6951020942057185618471295647422.031633.041720075.9648934944.112181.3944024202007000314774393275415.601443.037120561.8632141051.261745.304902126105607301777019055489.58253.090710066.3924148848.821722.52341257210068337617248183330.86263.071310558.7020830547.59115.7520222890552916586797939237.25473.09890053.5713635242.3896.991722837005

Heat Rejection @ 100% Load and 25o C Air)17982(905) nim/utB (WkrelooC liO ebuL)19385(6201) nim/utB (WkretaW tekcaJ)14967(2531) nim/utB (WkrelooCretfA)303461(8882) nim/utB (WkretaW waR ot noitcejeR taeH latoT

Exhaust Gas2 kW ( Btu/min ) 3391 ( 192948 ))85231(332) nim/utB (WknoitaidaR

Notes1 Ratings are based on ISO 3046/1 and SAEJ1995 Jan 90 standard reference conditions of 100 kPa, 25o C, and 30% relative humidity at the stated aftercooler water temperature.

2 Exhaust Heat rejection is based on fuel LHV and is not normally recoverable in total

4 Air flows are shown for 25oC air inlet to the turbocharger and 32oC cooling water to the charge air cooler.

DM8415-00 1/16/07

3 At 100% load with pumps +/- 3%. Performance and fuel consumption are based on 35 API, 16oC fuel having a lower heating value of 42,780 kJ/kg used at 29oC with a density of 838.9 g/liter.

5 This engine's exhaust emissions are in compliance with the INTERNATIONAL MARINE ORGANIZATION'S (IMO) standard as described in REGULATION 13 of ANNEX VI of MARPOL 73/78 and ISO 8178 for measuring HC, CO, PM, and NOx.

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Page 24: Caterpillar Motor

PRODUCT NEWS –C280 MARINE PROPULSION ENGINE T2 COMPLIANT

LEXM8385-01 24 of 40

Performance Data

C280-16 DIESEL ENGINE TECHNICAL DATA

:GNITAR ENIGNE0001:)MPR( DEEPS DETAR Marine MCR

RATED POWER1 (bkW): 5420 CERTIFICATION5: IMO/EPA MARINE TIER IIBMEP @ 100% LOAD (kPa): 2201 TURBOCHARGER PART #: 284-8276

ID:NOITSUBMOC1:31:OITAR NOISSERPMOC

AFTERCOOLER WATER (oC): etallitsiD:EPYT LEUF23

JACKET WATER INLET (oC): YRD:DLOFINAM TSUAHXE09IUE:METSYS NOITINGI MEAN PISTON SPEED (m/s): 10

FIRING PRESSURE, MAXIMUM (kPa):

Engine Performance

ZONE LIMIT DATA ZONE LIMIT DATA

Fuel Boost Air hxE hxEtsooBleuFhxEhxE hxEEngine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhSpeed Power g/ Rate kPa cu m/ Turbo Temp cu m/ Speed Power lb/ Rate in Hg- Flow4 Turbo Temp Flow

rpm bkW kW-hr L/hr Gaug rh-phphbmprnimCCniMe gal/hr Gauge cfm F F cfm

1000 5420 203 1312.7 271 546.9 543 373 1169.8 1000 7268 0.335 346.6 80 19312 1009 703 41310Curve A 950 5149 203 1245.8 273 528.6 537 361 1110.1 Curve A 950 6905 0.334 328.9 81 18666 999 682 39202

910 4932 203 1193.8 263 499.8 543 370 1064.0 910 6614 0.334 315.2 78 17651 1009 697 37574850 4607 204 1118.7 233 439.9 573 410 996.5 850 6178 0.335 295.4 69 15535 1063 770 35193800 3302 210 827.1 135 306.2 585 460 745.7 800 4428 0.346 218.4 40 10814 1085 859 26333750 2721 213 692.3 92 230.2 619 505 597.4 750 3649 0.351 182.8 27 8130 1146 941 21096700 2105 219 550.7 55 168.5 638 536 456.1 700 2823 0.361 145.4 16 5950 1181 997 16107630 1612 226 434.3 31 123.8 645 545 339.7 630 2162 0.372 114.7 9 4373 1194 1013 11997600 1559 228 423.5 28 114.6 668 561 321.2 600 2090 0.375 111.8 8 4047 1234 1041 11344500 1159 236 326.2 14 80.0 661 545 220.9 500 1554 0.389 86.1 4 2825 1222 1013 7803

PROPELLER DEMAND DATA PROPELLER DEMAND DATAFuel Boost Air hxE hxEtsooBleuFhxEhxE hxE

Engine Cons3 Fuel Press Flow4 Temp to Stack Flow Engine Cons3 Fuel Press Air Temp to Stack ExhOptimum Speed Power g/ Rate kPa cu m/ Turbo Temp cu m/ Optimum Speed Power lb/ Rate in Hg- Flow4 Turbo Temp Flow

Load rpm bkW kW-hr L/hr Gauge Min C C min Load rpm bhp hp-hr gal/hr Gauge cfm F F cfm

1000 4608 208 1142.5 244 510.5 523 367 1080.8 1000 6179 0.342 301.7 72 18030 974 693 38167(Curve P1) 950 3951 210 989.0 207 462.1 526 375 988.5 (Curve P1) 950 5298 0.346 261.1 61 16318 978 707 34910

910 3472 208 861.0 165 387.4 531 398 859.8 910 4657 0.342 227.3 49 13681 988 749 30364850 2830 211 711.8 107 283.9 551 442 673.5 850 3795 0.347 187.9 32 10027 1023 828 23786800 2359 214 601.8 73 219.2 571 475 545.6 800 3164 0.352 158.9 22 7742 1059 887 19267750 1944 218 505.2 49 172.5 584 496 442.1 750 2607 0.359 133.4 15 6091 1083 925 15612700 1581 222 418.3 32 138.6 579 495 355.1 700 2120 0.366 110.4 10 4894 1074 923 12540630 1152 227 311.8 17 103.6 532 453 251.1 630 1545 0.374 82.3 5 3660 990 848 8869600 995 229 271.7 12 91.8 502 426 213.9 600 1335 0.377 71.7 4 3242 936 798 7553500 576 235 161.4 3 63.9 383 320 125.7 500 772 0.387 42.6 1 2257 721 608 4440

Heat Rejection @ 100% Load and 25o C Air)98223(765) nim/utB (WkrelooC liO ebuL)40116(4701) nim/utB (WkretaW tekcaJ)23888(1651) nim/utB (WkrelooCretfA)522281(3023) nim/utB (WkretaW waR ot noitcejeR taeH latoT

Exhaust Gas2 kW ( Btu/min ) 4122 ( 234542 ))80941(262) nim/utB (WknoitaidaR

Notes1 Ratings are based on ISO 3046/1 and SAEJ1995 Jan 90 standard reference conditions of 100 kPa, 25o C, and 30% relative humidity at the stated aftercooler water temperature.

2 Exhaust Heat rejection is based on fuel LHV and is not normally recoverable in total

4 Air flows are shown for 25oC air inlet to the turbocharger and 32oC cooling water to the charge air cooler.

DM8416-01 2/5/08

3 At 100% load with pumps +/- 3%. Performance and fuel consumption are based on 35 API, 16oC fuel having a lower heating value of 42,780 kJ/kg used at 29oC with a density of 838.9 g/liter.

5 This engine's exhaust emissions are in compliance with the INTERNATIONAL MARINE ORGANIZATION'S (IMO) standard as described in REGULATION 13 of ANNEX VI of MARPOL 73/78 and ISO 8178 for measuring HC, CO, PM, and NOx.

17300

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