Zenith Zodiac CH 601
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The Zenith Zodiac CH 601 is a light, two place aircraft designed by Canadian aeronautical engineer Chris Heintz through his Midland, Ontario based company, Zenair. The CH 601 was introduced in 1984.
Although the CH 601 is currently manufactured as a complete aircraft by Aircraft Manufacturing and Development Co., the majority have been built as amateur-built experimental aircraft. An aircraft kit is produced and distributed in the USA by the Zenith Aircraft Company.
Designed as an easy to build, affordable aircraft the CH 601 has many features, including an all flying rudder, hingeless ailerons, bubble canopy, and assembly using blind rivets.
In Canada the CH 601 can be built and flown as an advanced ultralight or amateur-built. The CH 601 can also be flown under ultralight rules in several other countries. Pilots in the United States may fly the CH 601 under FAA light-sport aircraft rules or as an experimental amateur-built.
[edit] Variants
Several variants of the Zodiac CH601 are available
- Zodiac CH601 HD: an updated model of the original Zodiac CH 600
- Zodiac CH601 HDS: a version of the HD with tapered and shortened wings for higher cruise speed
- Zodiac CH601 (UL): a lightened version, with a gross weight of 1058 lbs (481 kg), suitable for registration as an advanced ultralight
- Zodiac CH601 XL or simply the "Zodiac XL": the newest version, featuring a new wing design, landing gear and fuselage.
The tail sections are the only components common among all Zodiac CH601 models.
[edit] Specifications (XL)
General characteristics
- Crew: 1
- Capacity: 1 passenger
- Length: 20 ft 0 in (6.1 m)
- Wingspan: 27 ft 0 in (8.23 m)
- Height: 6 ft 6 in (1.98 m)
- Wing area: 132 ft² (12.3 m²)
- Empty weight: 695 lb (318 kg)
- Useful load: 625 lb (282 kg)
- Max takeoff weight: 1,320 lb (595 kg)
- Powerplant: 1× Jabiru 3300 flat-6 engine, 110 hp (82 kW) at 3,000 rpm
- Zero-lift drag coefficient:
- Drag area:
- Aspect ratio:
- Lift-to-drag ratio:
Performance
- Never exceed speed: 180 mph (159 knots, 290 km/h)
- Maximum speed: 138 mph (122 knots, 222 km/h)
- Range: 662 mi (5830nm, 1,065 km)
- Rate of climb: 1200 ft/min (6.1 m/s)
- Max wing loading: 9.85 lb/ft² (48.0 kg/m²)
- Minimum power/mass: 0.085 hp/lb (139 W/kg)