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1. This variant had upgraded engines, longer life rotor, and higher take-off weight.
2. Both variants are to have a maximum take-off weight of 242 t.
3. Maximum take-off weight of the RU-38A is 5300 lb ( 2404 kg)
4. These changes increased its empty weight to and its take-off weight to.
5. The prototype featured a wingspan, taildragger landing gear and a gross take-off weight.