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AC Mobil 34 Chrysalin

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The AC Mobil 34 Chrysalin is a two-seat light aircraft produced in France in kitplane form. The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules.

Contents

Design and development

Constructed of composite materials, it is a conventional high-wing braced monoplane with fixed tricycle undercarriage. The pilot and passenger sit in side-by-side configuration.

Construction is of fibreglass and vinylester sandwich, which results in a low empty weight of 283 kg (624 lb). The aircraft features folding wings. Standard engine is the 60 kW (80 hp) Rotax 912 air and liquid-cooled, four stroke, four cylinder piston aircraft engine.

Specifications (Chrysalin)

Data from Tacke

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Wingspan: 9.6 m (31 ft 6 in)
  • Wing area: 13.5 m2 (145 sq ft)
  • Empty weight: 283 kg (624 lb)
  • Max takeoff weight: 472.5 kg (1,042 lb)
  • Powerplant: 1 × Rotax 912 air-cooled, four stroke, four cylinder piston engine, 60 kW (80 hp)

    • Performance

  • Maximum speed: 190 km/h (118 mph; 103 kn)
  • Cruise speed: 150 km/h (93 mph; 81 kn)
  • Stall speed: 62 km/h (39 mph; 33 kn)
  • Rate of climb: 5.25 m/s (1,033 ft/min)

    • Related content

    Comparable aircraft:

  • 3Xtrim 3X55 Trener

    • References

    AC Mobil 34 Chrysalin Wikipedia
    (Text) CC BY-SA


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