Piper PA-20 Pacer1950 |
LIGHTPLANE | Virtual Aircraft Museum / USA / Piper |
Under the designation Piper PA-20 Pacer, the company began production in 1950 of an updated version of the four-seat PA-16 Clipper. It introduced a number of improvements, including a larger area tailplane with balanced elevators, increased fuel capacity, redesigned landing gear and several interior refinements. As at first powered by a 81kW Avco Lycoming O-235-C1 engine, it had the designation PA-20 Pacer 115, but subsequent versions included the Pacer 125 with a 93kW O-290-D engine, and the generally similar Pacer 135 which introduced a variable-pitch propeller. When production ended in 1955 a total of 1,119 had been built, and the PA-20 Pacer 135 could demonstrate a maximum speed of 225km/h and had a range of 933km.
Fatal error: Uncaught mysqli_sql_exception: Connection refused in /data03/virt15346/domeenid/www.aviastar.org/htdocs/air/usa/piper_pa-20.php:118 Stack trace: #0 /data03/virt15346/domeenid/www.aviastar.org/htdocs/air/usa/piper_pa-20.php(118): mysqli_connect('mysql5.zone.ee', 'd14657sa18989', Object(SensitiveParameterValue)) #1 {main} thrown in /data03/virt15346/domeenid/www.aviastar.org/htdocs/air/usa/piper_pa-20.php on line 118 |