avia.wikisort.org - AeroplaneThe Zenair CH 180 Super Acro-Z is an aerobatic light aircraft, that was designed by Chris Heintz and built by Zenair in the 1980s.[1][2][3][4]
Zenair CH 180 |
Role |
Homebuilt light aircraft Type of aircraft |
National origin |
Canada |
Manufacturer |
Zenair |
Designer |
Chris Heintz |
First flight |
1982 |
Developed from |
Zenair CH 150 |
Specifications
Data from Jane's All the World's Aircraft 1992-93[1]
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 m2)
- Airfoil: NACA 0015[5]
- 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)
See also
Related development
References
Текст в блоке "Читать" взят с сайта "Википедия" и доступен по лицензии Creative Commons Attribution-ShareAlike; в отдельных случаях могут действовать дополнительные условия.
Другой контент может иметь иную лицензию. Перед использованием материалов сайта WikiSort.org внимательно изучите правила лицензирования конкретных элементов наполнения сайта.
2019-2025
WikiSort.org - проект по пересортировке и дополнению контента Википедии