1969 Five-seater (D-HEIS) with a fully enclosed fuselage, but it is not known if this was flown. Technical data for Do-132 Engine: UACL PT6 A-20 turbo-compressor, main rotor diameter: 10.70m, length: 7.50m, height: 2.80m, take-off weight: 1430kg, empty weight: 675kg, cruising speed: 220km/h, range: 450km |