FAA required low-altitude VMC demonstrations, and some pilots were practicing single-engine stalls. This is more a reflection of how the aircraft was used than a design failure. It has a maximum payload of 310 kg and a fuel tank capacity of 120 US gal with tip tanks. The Twin Comanche used to have a terrible reputation as a flat spinner in the late 1960s and early 70s. The aircraft has an empty weight of 1,030 kg and a maximum takeoff weight of 1,690 kg. The retractable landing gear has a wheelbase of 2.3 meters. The low-wing cantilever monoplane has a wingspan of 11.21 meters including tip tanks and a wing area of 16.54 square meters. It has an exterior length of 7.67 meters, an exterior height of 1.6 meters, and a fuselage diameter of 1.2 meters. The Piper PA-30 Twin Comanche can accommodate four to six people in flight. My 1966 Twin Comanche PA-30B has two Lycoming IO-320-B1A engines, normally aspirated, producing 160 horsepower per side. It was a twin-engined development of the. The PA-30 was then planned to be replaced by the PA-40 Arapaho from 1973 to 1974, however, the newer Piper aircraft was not able to proceed with further production. The Piper PA-30 Twin Comanche is an American twin-engined cabin monoplane designed and built by Piper Aircraft. The airplane is well supported, thanks to a well-organized owners group and a plentiful supply of parts and modifications. From the 1960s to 1970s, the aircraft suffered several Velocity Minimum Controllable (VMC) loss-of-control accidents. The Twin Comanche is an excellent airplane, and its value in the used market continues to rise. ![]() It was produced at the Piper factory in Lock Haven, Pennsylvania until 1972 when the factory was affected by the flood. On November 7, 1962, the aircraft took to the sky for the first time. ![]() The Piper PA-30 Twin Comanche was a twin-engine development of the PA-24 Comanche.
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