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The Acro 1 was designed by Fred Meyer as an advanced aerobatic aircraft
which is stressed to + or - 12g. An alternative powerplant is the
125hp(93kW) Lycoming IO-240 which reduces the empty weight to
690lb(313kg). Plans were available from Aircraft Technologies.
N5123S c/n 001 USA
Single seat aerobatic aircraft first flown in 1994
Engine:
200hp(148kW) Lycoming IO-360
Length: 17’0”(5.17m)
Height: 4’9”(1.44m)
Wingspan: 20’0”(6.09m)
No.built: 1+
Range: 900miles(1448km)
Cruising speed: 220mph(353kmh) Empty weight: 750lb(340kg)
Maximum take-off weight: 1250lb(567kg)
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