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 engines are approved by the European Aviation Safety Agency (EASA) and Federal Aviation Administration (FAA). CENTURION 2.0 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 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 – 48,900 €. 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> 99 kW (135 hp)
Maximum permanent output 99 kW (135 hp)
Economical rating 71 kW (97 hp)
Recommended load 75%
Propeller torque 410 Nm (302
Propeller torque (economical) 340 Nm (250 ft. lb.)
Propeller revolutions on takeoff 2300 rpm
Economical propeller revolutions 2000 rpm
Test over-speed propeller revolutions 2660 rpm
Engine revolutions on takeoff 3890 rpm
Economical engine revolutions 3380 rpm
Test over-speed engine revolutions 4500 rpm
Fuel consumption at cruise speed 15-17 l/h (4-4.5 gal/hr)
Specific fuel consumption 214 g/kWh (0.35 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, Chinese 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 1500 hours
Type certificate EASA, FAA, in 60 countries
Supplemental type certificates Cessna 172, Diamond DA40, DA42, Robin DR400, Piper PA-28
Aircraft characteristics
Cessna 172
Piper PA-28
Takeoff distance at height 300 m 228 m (748 ft) 325 m (1,066 ft)
Takeoff distance (avoiding 15-meter obstacles) 472 m (1,548 ft) 538 m (1,765 ft)
Climbing, near ground 3.5 m/s (690 ft/min) 3 m/s (609 ft/min)
Climbing at the height of 3000 m 2.8 m/s (560 ft/min) 2.4 m/s (455 ft/min)
Maximum speed at the height of 3000 m 240 km/h (129 KTAS) 233 km/h (126 KTAS)
Diesel fuel consumption 3000 m, 110 KTAS 16.2 l/h (4.28 gal/hr) 16.2 l/h (4.28 gal/hr)
Flight distance at the height of 3000 m, with standard drums 1660 km (898 NM) 1927 km (1.065 NM)
Flight distance at the height of 3000 m, with long-distance drums 1950 km (1,053 NM) -