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ZENAIR CH-300 Tri-Zenith

From SKYbrary Wiki

CH30
Aircraft
Name CH-300 Tri-Zenith
Manufacturer ZENAIR
Body Narrow
Wing Fixed Wing
WTC Light
APC A
Type code L1P
Engine Piston
Engine count Single
Mass group 1


Manufacturered as:

ZENAIR Tri-Z
ZENAIR Tri-Zenith
ZENAIR CH-300 Tri-Zenith
ZENAIR CH-300 Tri-Z


ZENAIR CH-300 Tri-Zenith

ZENAIR CH-300 Tri-Zenith

Description

The Zenair Tri-Z CH 300 is a three-seat Canadian homebuilt light aircraft. A single-engined low-winged monoplane.

Technical Data

Wing span 8.10 m26.575 ft
Length 6.85 m22.474 ft
Height 2.08 m6.824 ft
Powerplant 1 x Lycoming O-320 air-cooled flat-four, 150 hp (110 kW).
Engine model Lycoming O-320

Performance Data

Take-Off Initial Climb
(to 5000 ft)
Initial Climb
(to FL150)
Initial Climb
(to FL240)
MACH Climb Cruise Initial Descent
(to FL240)
Descent
(to FL100)
Descent (FL100
& below)
Approach
V2 (IAS) kts IAS kts IAS kts IAS kts MACH TAS 132 kts MACH IAS kts IAS kts Vapp (IAS) kts
Distance m ROC ft/min ROC ft/min ROC ft/min ROC ft/min MACH ROD ft/min ROD ft/min MCS kts Distance m
MTOW 900900 kg
0.9 tonnes
kg
Ceiling FL100 ROD ft/min APC A
WTC L Range NM

Accidents & Serious Incidents involving CH30

None on SKYbrary