CH20

ZENAIR Zenith (CH-200)

Aircraft
Name
Zenith (CH-200)
Manufacturer
Body
Narrow
Wing
Fixed Wing
WTC
L
APC
A
Type Code
L1P
Engine
Piston
Engine Count
Single
Manufacturered as
ZENAIR Zenith (CH-200)
ZENAIR CH-200 Zenith
HEINTZ Zenith
HEINTZ CH-200 Zenith

CH20

The Zenair Zenith CH 200 and CH 250 are a family of Canadian single-engined homebuilt light aircraft. It is a low-winged single engine monoplane, that was first flown in France in 1970, with kits being made by the Canadian company Zenair from 1974, with hundreds built and flown.

Technical Data
Wing span (metric)
7.00 m
Length (metric)
6.25 m
Height (metric)
2.11 m
Powerplant

1 x Continental O-200 air-cooled flat-four, 100 hp (suitable for engines of between 85 hp and 160 hp.

Engine Model(s)
Continental O-200
Indicative Performance Data
Take-Off
V2
n/a
Distance
n/a
MTOW
1000 kg
Initial Climb (to 5000 ft)
IAS
n/a
ROC
n/a
Initial Climb (to FL150)
IAS
n/a
ROC
n/a
Initial Climb (to FL240)
IAS
n/a
ROC
n/a
MACH Climb
MACH
n/a
ROC
n/a
Cruise
TAS
130150 kts
MACH
n/a
Ceiling
180
Range
220 NM
Initial Descent (to FL240)
MACH
n/a
ROD
n/a
Descent (to FL100)
IAS
n/a
ROD
n/a
Descent (FL100 & below)
IAS
n/a
MCS
n/a
ROD
n/a
Approach
Vapp (IAS)
n/a
Distance
n/a

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