Porsche PFM 3200
Type
|
Air-cooled
six-cylinder, horizontally opposed piston engine
|
Manufacturer
|
Porsche
|
First run
|
c
1981
|
 |
| Porsche PFM 3200 aircraft engine in Technik Museum Speyer |
Design and development
In the 1950s, European light aircraft builders began adapting the air-cooled automobile engines from the Porsche 356 and Volkswagen Beetle into aircraft engines with a series of limited modifications. Porsche cooperated with some of these builders and produced a series of factory-built engines for about six years between 1957 and 1963, the Porsche 678 series. These relatively small engines displaced about 1.6 litres (97 cubic inches) and produced between 55 and 70 horsepower, depending on the version.
Porsche decided to re-enter the aviation market with much larger engines derived from the Porsche 911, starting development in 1981. As the engines ran at higher speed than most aircraft engine designs, the propeller drive used a 0.442:1 reduction gearing so it could drive common propellers. The high operating speed meant the engine ran more smoothly than older designs, and the use of a muffler meant it was quieter as well. With about 3.2 litres (195 cubic inches) displacement, the normally aspirated N-series models produced about 210 hp, while the turbocharged T-series produced about 240 hp. This was roughly twice the horsepower of a conventional lower-rpm design of the same size. With single-lever operation, fully aerobatic fuel and oil supplies, direct fuel injection with automatic altitude compensation and optional turbocharging, the PFM 3200 series were some of the most advanced engines on the market.
After being introduced in late 1985 and starting to generate increasing interest in the general aviation (GA) market, Porsche exited the field during the massive downturn in the market in the late 1980s, closing the lines in 1991. It is suggested that the program cost them US$75 million to develop and produce the small number of engines delivered (about 80). Although marketed for only a short period, the PFM was found on a variety of aircraft as the primary powerplant, or as one-off modifications. These included the Extra 330, Mooney M20L, Socata TB-16, Robin DR400, Ruschmeyer MF-85 and others. Only the M20L went into production, with 40 produced in 1988, and one more in 1989.
In a letter dated September 17, 2007, Porsche informed the FAA that they were surrendering their type certificate for the PFM 3200 engine and that they would no longer support the engine. In March 2009, the FAA issued a special airworthiness information bulletin stating that type certificates for existing aircraft with the PFM 3200 engine were still valid and would remain so as long as the aircraft meet FAR part 43 maintenance requirements and FAR part 91 operation requirements. However, the bulletin also said that Porsche is not exporting new or replacement parts for the engine and there is no guidance as to how compliance would be possible once existing OEM parts are exhausted.
Porsche decided to re-enter the aviation market with much larger engines derived from the Porsche 911, starting development in 1981. As the engines ran at higher speed than most aircraft engine designs, the propeller drive used a 0.442:1 reduction gearing so it could drive common propellers. The high operating speed meant the engine ran more smoothly than older designs, and the use of a muffler meant it was quieter as well. With about 3.2 litres (195 cubic inches) displacement, the normally aspirated N-series models produced about 210 hp, while the turbocharged T-series produced about 240 hp. This was roughly twice the horsepower of a conventional lower-rpm design of the same size. With single-lever operation, fully aerobatic fuel and oil supplies, direct fuel injection with automatic altitude compensation and optional turbocharging, the PFM 3200 series were some of the most advanced engines on the market.
After being introduced in late 1985 and starting to generate increasing interest in the general aviation (GA) market, Porsche exited the field during the massive downturn in the market in the late 1980s, closing the lines in 1991. It is suggested that the program cost them US$75 million to develop and produce the small number of engines delivered (about 80). Although marketed for only a short period, the PFM was found on a variety of aircraft as the primary powerplant, or as one-off modifications. These included the Extra 330, Mooney M20L, Socata TB-16, Robin DR400, Ruschmeyer MF-85 and others. Only the M20L went into production, with 40 produced in 1988, and one more in 1989.
In a letter dated September 17, 2007, Porsche informed the FAA that they were surrendering their type certificate for the PFM 3200 engine and that they would no longer support the engine. In March 2009, the FAA issued a special airworthiness information bulletin stating that type certificates for existing aircraft with the PFM 3200 engine were still valid and would remain so as long as the aircraft meet FAR part 43 maintenance requirements and FAR part 91 operation requirements. However, the bulletin also said that Porsche is not exporting new or replacement parts for the engine and there is no guidance as to how compliance would be possible once existing OEM parts are exhausted.
Versions
- N00: de-rated for automotive fuel
- N01: 212 hp at 5300 rpm
- N03: type-certified N01 for the Mooney M20L, 217 hp at 5300 rpm
- T03: similar to the N03 but with a Garrett turbocharger, 241 hp at 5300 rpm, critical altitude 18,000 ft
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Last updated on 12 June 2013 at 12:54.
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