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Scheibe SF-23A Sperling      


Scheibe Flugzeugbau GmbH was founded by Egon Scheibe in 1951 to build gliders. The first powered design was the SF-23, the prototype of which was first flown powered by a 65hp(48kW) Continental. The first production model was the SF-23A which was followed by the SF-23B (4 built) which was powered by a 100hp(75kW) Continental and the SF-23C (6 built) which was powered by a 115hp(85kW) Lycoming and with a maximum take-off weight of 1609lb(730kg). Production of the Sperling ended in 1961 and a few remain airworthy.

Scheibe SF-23A Sperling G-BCHX

G-BCHX                c/n 2013                    Germany

2 seat light aircraft first flown in 1955

Engine: 95hp(70kW) Continental C90-12F                                                                                       Length: 20’4"(6.19m)                                                                                            Height: 7’2"(2.18m)Wingspan: 32’4"(9.85m)                                                                                                  No.built: 17 Range: 435miles(700km)                                                              Cruising speed: 100mph(160kmh) Empty weight: 926lb(420kg)                                                   Maximum take-off weight: 1455lb(660kg)

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