- Development and design
- Variants
- Aircraft on display
- Specifications (150 hp O-320 engine)
- See also
- Notes
- References
name=Tri-Z CH 300 | image=ZenairCH-300TriZenithC-GOVK.jpg | caption=Zenair CH 300 flown by "Red" Morris in the Canada Aviation and Space Museum }}{{Infobox Aircraft Type | type=Homebuilt light aircraft | national origin=Canada | manufacturer=Zenair | designer=Chris Heintz | first flight=9 July 1977 | introduced= | retired= | status= | primary user= | more users= | produced= | number built= | program cost= | unit cost= | developed from= | variants with their own articles=AMD Alarus }} |
The Zenair Tri-Z CH 300 is a three-seat Canadian homebuilt light aircraft. A single-engined low-winged monoplane, the CH 300 first flew in 1977, with several hundred kits sold. Development and designThe CH 300 is an enlarged three-seat derivative of the Zenair Zenith CH 200, designed by Chris Heintz in the mid 1970s as the Tri-Zénith.[1] Like the CH 200, it is a low-winged monoplane of all-metal construction with a fixed nosewheel undercarriage, but is larger and more powerful, and is fitted with a rear bench seat capable of accommodating a third adult or two children, and is fitted with a forward sliding canopy. It is designed to be powered by an engine giving between 125 and 180 hp (93 and 134 kW).[2][2] The first example made its maiden flight on 9 July 1977, with over 400 sets of plans sold by 1982.[2] One CH 300, modified with extra fuel tanks and piloted by Robin "Red" Morris, made a non-stop trans-Canada flight between Vancouver International Airport and Halifax International Airport on 1–2 July 1978, covering the 2,759 mile (4,440 km) in 22 hours, 44 mins, setting three FAI Class C-1c point-to-point speed records.[2][2][3] Plans for the CH 300 remained on sale in 1999.[4] The Zenair CH 300 formed the basis for the factory built Zenair CH-2000, which first flew in 1993.[4][5] Variants- CH 300
Basic model with tricycle landing gear - CH 300 TD
"Taildragger" model with conventional landing gear Aircraft on display- Canada Aviation and Space Museum[6]
Specifications (150 hp O-320 engine){{Aircraft specs |ref=Jane's All The World's Aircraft 1982-83[7] |prime units?=imp |genhide= |crew=1 |capacity=2 passengers |length m=6.85 |length ft= |length in= |length note= |span m=8.10 |span ft= |span in= |span note= |height m=2.08 |height ft= |height in= |height note= |wing area sqm=12.00 |wing area sqft= |wing area note= |aspect ratio=5.48:1 |airfoil= |empty weight kg= |empty weight lb=1100 |empty weight note= |gross weight kg= |gross weight lb= |gross weight note= |max takeoff weight kg= |max takeoff weight lb=1850 |max takeoff weight note= |fuel capacity= |lift kg= |lift lb= |lift note= |more general=
|eng1 number=1 |eng1 name=Lycoming O-320 |eng1 type=air-cooled flat-four |eng1 kw= |eng1 hp=150 |eng1 note= |power original= |prop blade number= |prop name= |prop dia m= |prop dia ft= |prop dia in= |prop note=
|perfhide= |max speed kmh= |max speed mph=160 |max speed kts= |max speed note= |max speed mach= |cruise speed kmh= |cruise speed mph=143 |cruise speed kts= |cruise speed note=(75% power) |stall speed kmh= |stall speed mph=53 |stall speed kts= |stall speed note=(flaps down) |never exceed speed kmh= |never exceed speed mph= |never exceed speed kts= |never exceed speed note= |minimum control speed kmh= |minimum control speed mph= |minimum control speed kts= |minimum control speed note= |range km= |range miles=530 |range nmi= |range note= |combat range km= |combat range miles= |combat range nmi= |combat range note= |ferry range km= |ferry range miles= |ferry range nmi= |ferry range note= |endurance= |ceiling m= |ceiling ft= |ceiling note= |g limits= |roll rate= |glide ratio= |climb rate ms= |climb rate ftmin=1000 |climb rate note= |time to altitude= |sink rate ms= |sink rate ftmin= |sink rate note= |lift to drag= |wing loading kg/m2 |wing loading lb/sqft= |wing loading note= |disk loading kg/m2= |disk loading lb/sqft= |disk loading note= |power/mass= |thrust/weight= |more performance= |avionics= }}
See also{{aircontent |see also= |related=*AMD Alarus |similar aircraft= |lists= }}Notes1. ^Taylor 1976, p.458. 2. ^1 Zenair, Zenair pamphlet, circa 1986. 3. ^"List of records established by the 'Zenair Tri-Z'{{dead link|date=July 2016 |bot=InternetArchiveBot |fix-attempted=yes }}". Fédération Aéronautique Internationale. Retrieved 27 February 2010. 4. ^1 Taylor 1999, p.535. 5. ^Taylor 1999, p.401. 6. ^{{cite web|url = http://www.aviation.technomuses.ca/collections/artifacts/aircraft/ZenairCH-300Tri-Zenith/|title = Zenair CH-300 Tri-Z|accessdate = 9 June 2012|last = Canada Aviation and Space Museum|date = n.d.}} 7. ^1 2 3 Taylor 1982, p.495.
References{{commons category|Zenair CH 300}}{{refbegin}}- Taylor, John W. R. Jane's All The World's Aircraft 1976-77. London:Jane's Yearbooks, 1976. {{ISBN|0-354-00538-3}}.
- Taylor, John W. R. Jane's All The World's Aircraft 1982-83. London:Jane's Yearbooks, 1982. {{ISBN|0-7106-0748-2}}.
- Taylor, Michael J. H. Brassey's World Aircraft & Systems Directory 1999/2000. London:Brassey's, 1999. {{ISBN|1-85753-245-7}}.
{{refend}}{{Zenair}} 6 : Canadian sport aircraft 1970–1979|Homebuilt aircraft|Zenair aircraft|Single-engined tractor aircraft|Low-wing aircraft|Aircraft first flown in 1977 |