Zenair CH 180
# Zenair CH 180

The Zenair CH 180 Super Acro-Z is an aerobatic light aircraft, that was designed by Chris Heintz and built by Zenair in the 1980s.

## Specifications

Data from Jane's All the World's Aircraft 1992-93

General characteristics

* Crew: 1
* Length: 20 ft 2 in (6.15 m)
* Wingspan: 20 ft 3 in (6.17 m)
* Height: 5 ft 5 in (1.65 m)
* Wing area: 85 sq ft (7.9 $m^2)$
* Airfoil: NACA 0015
* Empty weight: 800 lb (363 kg)
* Max takeoff weight: 1,150 lb (522 kg)
* Fuel capacity: 27 imp gal (32 US gal; 120 L) in two fuselage tanks
* Powerplant: 1 × Textron Lycoming IO-360 4-cylinder air-cooled horizontally-opposed piston engine, 150 hp (110 kW) with fuel injection
* Propellers: 2-bladed fixed-pitch propeller

Performance

* Cruise speed: 165 kn (190 mph, 306 km/h)
* Stall speed: 42 kn (48 mph, 78 km/h)
* Range: 565 nmi (650 mi, 1,046 km) with max fuel 55% power
* Service ceiling: 16,000 ft (4,900 m)
* g limits: $^+8$ normal (+12 ultimate)
* Roll rate: 270°/s
* Rate of climb: 3,000 ft/min (15 m/s)
