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Uetz U4M Pelikan     


The company of Walter Uetz began aircraft manufacture in the 1950’s when they built a number of Jodel D.11’s under licence. They developed the Jodel design into the Uetz U2V (3* built) which first flew in 1962 powered by a 100hp (75kW) Continental and which had a maximum take-off weight of 1540lb(699kg). A four seat version, the Uetz U3M Pelikan(2 built) made its first flight in 1963 powered by a 135hp(100kW) Lycoming and from this was developed the more powerful Uetz U4M. The Uetz (Markwalder) Marabu (1 built) was a three seat light aircraft which first flew in 1965 powered by a 150hp Lycoming and with a maximum take-off weight of 2140lb(971kg). The company ended production in 1965 and four U4M’s remain on the Swiss register of which at least one remains airworthy.

Uetz U4M Pelikan

HB-TBV                 c/n 25                  Switzerland

4 seat light aircraft first flown in 1963

Engine: 150hp(112kW) Lycoming O-320-A2B                                                                                  Length: 24’7"(7.49m)                                                                                           Height: 6’8"(2.03m)Wingspan: 31’6"(9.6m)                                                                                                     No.built: 4* Range: 620miles(997km)                                                                Cruising speed: 120mph(193kmh) Empty weight: 1248lb(566kg)                                                Maximum take-off weight: 2205lb(1001kg)

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