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Bergen Engines

C25:33L9

Main Engine 4-Stroke · Main Engines (4-Stroke)

Technical data from manufacturer or class sources · not yet verified by a person
3,375 kWPower
9Cylinders
250 mmBore
330 mmStroke
1,000 rpmMCR RPM

The Bergen C25:33L9 is a medium‑speed, 4‑stroke, 9‑cylinder diesel/dual‑fuel main engine delivering up to 3 375 kW at 1 000 rpm, known for its flexible fuel capability (MDO/HFO/LNG) and extended service intervals.

Specifications

Technical data.reference — unverified

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Bmep25 bar @ 750 rpm (Propulsion), 26 bar @ 720 rpm (Genset)
SFOC (100% MCR)171-177 g/kWh (MDO basis, varies by cylinders)
SFOC (85% MCR)173-175 g/kWh
Lube Oil Consumption0.5 g/kWh
Mean Piston Speed11.2 m/s (@ 750 rpm), 10.8 m/s (@ 720 rpm)
Dry Weight L6P42,400 kg
Dry Weight L8P53,500 kg
Dry Weight L9P56,400 kg
Dry Weight V12P71,867 kg
Genset Weight L6A48,300 kg (engine only)
Genset Weight L8A60,600 kg (engine only)
Genset Weight L9A62,400 kg (engine only)
Engine Type4-stroke, turbocharged with 2-stage charge air cooler
Service IntervalsExtended up to 25,000 hours
IMO ComplianceTier II (standard), Tier III (with SCR)
Electrical Output L6 50Hz3,515 kW genset
Electrical Output L8 50Hz4,690 kW genset
Electrical Output L9 50Hz5,285 kW genset
Electrical Output V12 60Hz6,750 kW genset
Electrical Output V12 50Hz7,050 kW genset
Max Cont Rating (kW)3,000 kW
Manufacturer documentation

Images from manufacturer documentation.

Photos, drawings and page previews from this model’s datasheet or catalog.

“The Bergen C25:33L has a compact footprint and excellent power-toweight ratio, making it ideal for vessels requiring reliable, responsive power in tight spaces. Silent resilient mounting ensures…”

Bergen Engines C25:33L9 – Photo (ae1f026d279c_S1-1 S. 1)
Photo · ae1f026d279c_S1-1 · S. 1
Bergen Engines C25:33L9 – Drawing (ae1f026d279c_S1-1 S. 1)
Drawing · ae1f026d279c_S1-1 · S. 1
Source: Bergen Engines C25:33L9 datasheet, p. 1
Inspection

Inspector Detail

Common issues

  • Gas admission valve wear or leakage in dual-fuel (gas) operating mode
  • Pilot fuel injector wear affecting ignition reliability in gas mode
  • Turbocharger fouling reducing available boost
  • Cylinder liner and piston ring wear over extended running
  • Knock/detonation sensor drift requiring recalibration in gas mode
  • Exhaust valve seat wear
  • Charge air cooler fouling

Inspection checklist

  • Borescope inspect cylinder liners and piston crowns for wear/deposits
  • Function test gas admission valves and gas safety shut-off valves where fitted
  • Check pilot fuel injector condition and spray pattern
  • Verify knock sensor calibration and detonation protection function in gas mode
  • Inspect turbocharger bearings and check boost trend
  • Check main and big-end bearing clearance at scheduled overhaul
  • Take crankshaft deflection readings
  • Sample lube oil for TBN, soot and wear metal trend
  • Check gas fuel piping and ventilation/gas detection system in the engine room

Service intervals

Lube oil analysisevery 250-500 hours per PMS
Gas detection system function testper class/IGF code requirement, typically at defined survey intervals
Pilot injector servicecondition-based, commonly reviewed in the 2,000-4,000 hour range
Major overhaul (liners/bearings)typically in the 20,000-30,000 hour range for medium-speed dual-fuel engines of this class - confirm against Bergen's schedule for the C25:33

Typical wear limits

Piston ring end gaptypically in the 0.8-1.6 mm range for this bore class (250 mm) - confirm against Bergen's own manual before condemning
Main/big-end bearing clearancecheck against the manufacturer's cold-clearance table rather than a generic figure
Exhaust valve seat recessiontrack trend at each inspection against the manufacturer's limit

Ranges are typical for this design class. Always confirm against the manufacturer documentation for your serial number.

Critical spares

  • Cylinder liner
  • Piston ring set
  • Pilot fuel injector
  • Gas admission valve
  • Exhaust valve
  • Main bearing shells
  • Big-end bearing shells
  • Turbocharger repair kit

Safety

  • Crankcase explosion risk - oil mist detector must be functional and tested regularly
  • Gas fuel system leak risk in dual-fuel operation - gas detection and ventilation per IGF/class rules must be verified working
  • High-pressure pilot fuel system
  • Hot surfaces at exhaust and turbocharger
  • Starting air system leak/fire risk

Class survey

Continuous Survey Machinery candidate. For dual-fuel operation, class also requires periodic testing of the gas fuel safety system (double-wall piping integrity, gas detection, ventilation) in addition to standard crankshaft deflection and bearing condition checks.

Estimated lifetime: Medium-speed dual-fuel engines of this class typically see major overhaul intervals in the 20,000-30,000 running hour range, with total service life extending well beyond that across multiple overhaul cycles.

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