| Dornier Do-132 1969 | ![]() |
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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
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