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The twin boom Sceptre 1 was developed by Roberts
Sport Aircraft of Yakima, Washington with the intention of marketing it
as a kit for home construction. An alternative engine was the 65hp
(48kW) Rotax. A two seat seat version, the Sceptre 11 made its first
flight in 1985 powered by an 85hp(63kW) Limbach. At least one example of
the Sceptre 1 is maintained in airworthy condition. The type is now
known as the Central Aircraft Sceptre.
N92RA
c/n 00
USA
Single seat light aircraft first flown in 1983
Engine: 52hp(39kW) Rotax 503
Length: 19’5"(5.92m)
Height: 4’11"(1.5m)Wingspan: 26’5"(8.05m)
No.built: 3+ Range: 450miles(724km)
Cruising speed: 100mph(160kmh) Empty weight: 670lb(304kg)
Maximum take-off weight: 1045lb(474kg)
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