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The 125 kW (168 hp) AE 300 engine replaces the earlier Thielert Centurion 1.7 and 2.0 engines and is known for its good fuel efficiency, using 12.1 litres (2.7 imp gal; 3.2 US gal) per hour while loitering at maximum endurance or 30 litres (7 imp gal; 8 US gal) per hour at maximum continuous power (92%).
The Diamond DA62 is a five- to seven-seat, twin-engine light aircraft produced by Diamond Aircraft Industries and first announced in March 2012. [2] [3] [4] The prototype, designated as the DA52, first flew on 3 April 2012 after six months of development. [3] [5] In June 2014 it was announced the production aircraft would be designated the DA62 ...
The Diamond DA50 is a five seat, single-engine, composite aircraft designed and built by Diamond Aircraft Industries. First shown in 2006, it made its maiden flight on 4 April 2007. The project has been proposed to be powered by several different engines, but was certified on 9 September 2020 with the Continental CD-300 diesel.
Diamond Star DA40-TDI diesel powered model Diamond Star DA40 FP Fixed Pitch variant Diamond Star DA40-180 instrument panel showing the Garmin G1000 glass cockpit installation G1000-equipped Diamond DA-40. The Diamond DA40 Diamond Star is an Austrian four-seat, single-engine, light aircraft constructed from composite materials.
Variants powered by the Rotax engine have been approved for use with standard automotive gasoline, automotive-grade oil Mobil is also recommended for use as a lubricant. [ 19 ] [ 5 ] In the event of a loss of coolant , the Rotax engine is capable of 'dry running' for up to 2 hours without any resulting damage if run at or below 56 percent power.
Mechanics nicknamed them Parts Recovery Turbines, since the increased exhaust heat meant a return to the engine destroying exhaust valves. The fuel burn for the PRT-equipped aircraft was nearly the same as the older Pratt and Whitney R-2800, while producing more useful power. [5] Effective 15 October 1957 a DA-3/DA-4 engine cost $88,200. [6]
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Data from Austro Engine and type certificate General characteristics Type: Four-cylinder, four-stroke diesel aircraft engine Bore: 83 mm (3.3 in) Stroke: 92 mm (3.6 in) Displacement: 1,991 cm 3 (121 cu in) Length: 738 mm (29 in) Width: 855 mm (34 in) Height: 574 mm (23 in) Dry weight: 186 kg (410 lb) Mean time between failures: > 100,000 h Time between overhauls: 1,800 h Components Fuel type ...