SMA SR305-230

The SMA SR305-230 is an air/oil-cooled, horizontally opposed, four-cylinder, four-stroke, diesel piston aircraft engine. The engine is manufactured by SMA Engines, and is currently the only product of this French company. The engine is offered as a conversion package for the Cessna 182. As of 2012 July, Cessna announced it will offer the 182 with this engine. Delivery expected by 2nd quarter of 2013. Cessna also stated the SMA engine will replace the current avgas engine.[1]

SR305-230
Type Four-cylinder four-stroke diesel aero engine
National origin France
Manufacturer SMA Engines
First run 1998 (First flight)
Major applications Cessna 182
Number built >50
Developed into Continental TD-300

The engine first flew in a Socata TB-20 in March 1998 and was officially introduced at the Paris Air Show in June 1999. French DGAC approval was attained in July 2001 with FAA certification following a year later. Between 17 and 25 July 2006 a converted Cessna 182 (registration F-GJET) flew from Le Bourget to Oshkosh, Wisconsin.

Design

The SMA SR 305-230-1 is a four-cylinder, horizontally opposed turbocharged direct fuel injection diesel engine. The engine installation includes an electronic central processing unit (CPU) that continually calculates the proper fuel/air mixture. If this unit fails completely during flight, the mechanical backup position is selected and the pilot can control the fuel/air mixture as required to complete the flight.

Full-throttle operation at sea level is at 90 inches (3 bar) of manifold pressure. Unlike some aircraft engines, which recommend the maximum power setting be used only for five minutes during the initial takeoff stage, the SR 305 can be operated indefinitely at this setting, although normal cruise uses around 70 inches (2.3 bar) and economy cruise uses around 60 inches (2 bar) of manifold pressure.

The STC conversion on the Cessna 182 includes a new cowl, both to accommodate the different engine dimensions and to provide the required cooling airflow. Belly-mounted cowl flaps are still used, but less cooling airflow is directed over the cylinder barrels and more cooling airflow is directed into side-mounted oil coolers. About one-third of the engine cooling is provided by airflow over the cylinders; the remainder is provided by engine oil. The engine's oil distribution system routes a large oil flow to hot zones in the cylinder heads and upper cylinder barrels, carrying the heat away to the oil coolers.[2]

As of early 2008, SMA had provided over 50 conversion packages. (The installation is usually performed by other companies, not SMA.) Most of those conversions were performed in Europe, with less than a dozen having been performed in North America. The package costs around $75,000, and installation costs around $7,000.

The cost of conversion may be justified in areas where aviation gasoline costs significantly more than jet fuel, and by the fact that the diesel fuel flow at cruise is about 10 gallons (38 litres) per hour, compared to about 13.5 gallons (51 litres) per hour with the original engine.

SMA expects 90 engines to be delivered in 2014, and is working on six-cylinder version called the SR460 which will have an output of 330 to 400 hp (246 to 298 kW).[3]

Applications

Specifications
SMA SR305-230

Data from EASA TCDS[5]

General characteristics

  • Type: Four-cylinder, four-stroke diesel aircraft engine
  • Displacement: 4,988 cm3 (304 cu in)
  • Length: 834 mm (33 in)
  • Width: 930 mm (37 in)
  • Height: 750–784 mm (30–31 in)
  • Dry weight: 195–207 kg (430–456 lb)

Components

Performance

  • Power output: 169–194 kW (227–260 hp) at 2,200 rpm, producing 734–842 N⋅m (541–621 lb⋅ft) of torque, a 18.5-21.2 bar mean effective pressure

See also

Related development

Comparable engines

Related lists

References
  1. "Cessna Unveils Jet A Engine For Skylane". Avweb.com. 2012-07-22. Retrieved 2012-10-11.
  2. Cessna Skylane Joins the Jet Set, Flying Magazine, Vol. 135, No. 5, May 2008, p. 74
  3. Thurber, Matt. "AirVenture Report: 2014" AINonline, 1 September 2014. Accessed: 4 September 2014.
  4. "DA50 Series - Preliminary Technical Specifications". Diamond Aircraft.
  5. "Type Certificate Data Sheets No. E.076" (PDF). EASA. 15 February 2019.
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