The Riley Executive 400 conversion was available from Riley and McAlpine in six stages, any one of which could be taken on its own if the customer did not want a complete conversion:
1. |
Re-engining with two 400 hp Lycoming IO-720 eight-cylinder horizontally-opposed air-cooled engines, each fitted with two Riley Turbo 300 turbo-superchargers and driving a Hartzell three-blade propeller. New sweptback vertical tail surfaces and a "fatigue-free" steel spar capped wing were included in this stage of the conversion, which contributed 90% of the overall speed increase and 90% of the weight decrease of 800 lb (363 kg) offered by the conversion. |
The pictured aircraft was built as a D.H.104 Dove Mk.2 and registered in France as F-BGOA on May 17, 1952. In the mid-1960s it was converted to a Riley Executive 400, although still registered as a D.H.104. On December 13, 1983 the aircraft was deregistered as "sold abroad", however, it never left France, but was used as an instructional at the Sodetag Training School at Toussus-le-Noble."