This is a four-stroke-cycle diesel engine that consists of four cylinders installed in line with four valves each. This turbocompressor liquid-cooled engine is provided with the reducing gear having the reduction ratio i = 1.69:1. The following embedded systems improve its performance:

  • COMMON RAIL direct injection system
  • all-electronic engine and propeller control system
  • wet-sump lubrication system

CENTURION 2.0 S engines are approved by the European Aviation Safety Agency (EASA) and Federal Aviation Administration (FAA). CENTURION 2.0 S has EASA and FAA supplemental type certificate for the following aircraft models: Cessna-172 and Piper PA28. Diamond Aircraft Industries also installs CENTURION 2.0 S engines into its aircraft, models DA40 TDI, DA42 Twin Star, while Apex Aircraft installs them into Robin DR400 models.

Engine description

  • Price in the «AerojetBaltic» service center, Vilnius – 59,800 €. The price includes the engine, installation works and aircraft flight calibration.
  • Replacement terms: not less than 35 days

Engine description

Operation principle Turbodiesel
Cylinders and their pattern 4 in line
Valves DOHC
Injection Direct injection
Cooling liquid
Lubrication Wet-sump system
Electronics Full digital engine controller (FADEC)
Propeller transmission Reducing gear with the clutch embedded (reducing ratio i = 1:1.69)
Propeller 3-bladed, from mechanical transmission, hydraulic, controllable pitch (MTV-6 series)
Cubic capacity 1.991 cm³ (121.5
Cylinder diameter 83 mm (3.26 in)
Piston stroke 92 mm (3.62 in)
Compression 18:1
Dimensions (WxLxH) 778 x 816 x 636 mm (30.63 x 32.12 x 25.04 in)
Weight (empty, with units) 134 kg (295.4 lbs)

Engine characteristics

Maximum output up to 2000 m/td> 114 kW (155 hp)
Maximum permanent output 114 kW (155 hp)
Economical rating 97 kW (132 hp)
Recommended load 75%
Propeller torque 473 Nm (349
Propeller torque (economical) 410 Nm (302 ft. lb.)
Propeller revolutions on takeoff 2300 rpm
Economical propeller revolutions 2000 rpm
Test over-speed propeller revolutions 2660 rmp
Engine revolutions on takeoff 3890 rmp
Economical engine revolutions 3380 rmp
Test over-speed engine revolutions 4500 rmp
Fuel consumption at cruise speed 18-22 l/h (4,7-5.8 gal/hr)
Specific fuel consumption 220 g/kWh (0.36 lb/hphr)
Electrical system
Electrical system FADEC
Voltage 28 V, optional 14 V
Generator 1680 W, optional 1260 W
Current / Voltage 60 A, optional 90 A
Compact engine display 0,3 kg (0,66 lbs)

Working fluids

Certified fuel Diesel (EN 590), TS-1 Kerosene, Jet A, Jet A-1
Suitable fuel Diesel (EN 590), TS-1 Kerosene, Jet A, Jet A-1, JP-5, DEF STAN 91-86, JP-8, DEF STAN 91-91, JP-8+100, Chines Jet Fuel No 3
Oil Shell Helix Ultra 5W30; Shell Helix Ultra 5W40; AeroShell Oil Diesel 10W-40; AeroShell Oil Diesel Ultra
Cooling fluid 50% Вода; 50% BASF Glysantin; G48/ Glysantin; Protect Plus
Reducing gear oil Shell EP 75W90 API GL-4


Life 1200 hours
Type certificate EASA, FAA, in 60 countries
Supplemental type certificates Cessna 172, Piper PA-28 Diamond DA40, DA42, Robin DR400

Aircraft characteristics

Cessna 172

Piper PA-28

Takeoff distance at height 300 m 235 m (771 ft) 165 m (540 ft)
Takeoff distance (avoiding 15-meter obstacles) 402 m (1,319 ft) 328 m (1,076 ft)
Climbing, near ground 3.9 m/s (767 ft/min) 5 m/s (990 ft/min)
Climbing at the height of 3000 m/td> 3.3 m/s (654 ft/min) 4.2 m/s (830ft/min)
Maximum speed at the height of 3000 m 246 km/h (133 KTAS) 246 km/h (133 KTAS)
Расход дизеля 3000 м, 110 KTAS 18.11 l/h (4.78 gal/hr) 18.11/h (4.78 gal/hr)
Diesel fuel consumption 3000 m, 110 KTAS: 1642 km (887 NM) 1513 km (817 NM)
Flight distance at the height of 3000 m, with standard drums 2550 km (1,377 NM) -