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  2. List of Lycoming O-360 variants - Wikipedia

    en.wikipedia.org/wiki/List_of_Lycoming_O-360...

    Same as the IO-360-A1A but it is equipped with an inverted oil system kit for aerobatic flight. [4] AEIO-360-A1B 200 hp (149 kW) at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.70:1. Same as the IO-360-A1B but it is equipped with an inverted oil system kit for aerobatic flight. [4] AEIO-360-A1B6

  3. Spectrometric Oil Analysis Program - Wikipedia

    en.wikipedia.org/wiki/Spectrometric_Oil_Analysis...

    Spectrometric Oil Analysis Program (SOAP) is a method used by aircraft operators, including several Air Forces of the World, to test the health of aircraft engines by performing frequent laboratory testing of the engine oil. The tests reveal the chemical composition of any metal particles suspended in the oil samples. By comparing the results ...

  4. Lycoming O-320 - Wikipedia

    en.wikipedia.org/wiki/Lycoming_O-320

    The LIO-320 is a "left-handed" version with the crankshaft rotating in the opposite direction for use on twin-engined aircraft to eliminate the critical engine. [ 2 ] [ 3 ] The first O-320 (with no suffix) was FAA certified on 28 July 1953 to CAR 13 effective 5 March 1952; this same engine was later re-designated, without change, as the O-320 ...

  5. Ranger L-440 - Wikipedia

    en.wikipedia.org/wiki/Ranger_L-440

    The Ranger L-440 (company designation 6-440C) are six-cylinder inline inverted air-cooled aero-engines produced by the Ranger Aircraft Engine Division of the Fairchild Engine and Airplane Corporation of Farmingdale, New York, United States. The engine was mainly produced for Fairchild's family of training aircraft in the mid-1930s.

  6. Kinner R-5 - Wikipedia

    en.wikipedia.org/wiki/Kinner_R-5

    The main change was the increase in cylinder bore from 117 mm (4.625 in) to 127 mm (5 in) and an increase in piston stroke from 133.3 mm (5.25 in) to 139.7 mm (5.5 in). This led to a corresponding increase in displacement from 7.2 liters (441 cu in) to 8.8 liters (540 cu in). The R-5 was a rough running but reliable engine.

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  8. Lycoming IO-390 - Wikipedia

    en.wikipedia.org/wiki/Lycoming_IO-390

    In November 2009 Lycoming announced that it had obtained an FAA Supplemental Type Certificate to replace the originally fitted Lycoming O-360 engines in the Mooney M20E, M20F and M20J with a new or remanufactured IO-390-A3A6 engine. [8] Also on November 12, 2009 Commander Aircraft received an STC for its model 112B using the MTV-12-B/188-59b ...

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