The Dalotel DM-165 was a French two-seat training monoplane designed by Michel Dalotel. A number of variants were proposed but only the prototype was built.
Design and development.
The DM-165 was a tandem two-seat low-wing monoplane. Powered by a 165 hp (121 kW) Continental IO-346A flat-four piston engine. It had a tailwheel and retractable landing gear which folded inwards. Dalotel was assisted by Société Poulet in the construction of the prototype, registered "F-PPZE", which was first flown in April 1969. The aircraft was successfully tested during 1970 but despite efforts to market the aircraft none were ordered.
Prototype with retractable landing gear and powered by a 165 hp (121 kW) Continental IO-346A piston engine, one built.
Proposed variant with fixed landing gear and powered by a 125 hp (92 kW) engine, not built.
Proposed variant with fixed landing gear and powered by a 160 hp (118 kW) engine, not built.
Proposed variant of the DM-160 with retractable landing gear and constant speed propeller, not built.
Specifications (DM-165).
"Data from" General characteristics* Crew: two* Length: ()* Wingspan: ()* Height: ()* Wing area: ()* Powerplant: 1 × Continental IO-346A flat-four piston engine
Performance* Maximum speed: (, ) 
References.
Notes.
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