CH25

ZENAIR Zenith (CH-250)

Aircraft
Name
Zenith (CH-250)
Manufacturer
Body
Narrow
Wing
Fixed Wing
WTC
L
APC
A
Type Code
L1P
Engine
Piston
Engine Count
Single
Manufacturered as
ZENAIR Zenith (CH-250)
ZENAIR CH-250 Zenith

CH25

Variants:

  • Zenair CH 250: Improved version of the CH-200 with more fuel, larger baggage area, rear windows and a forward sliding canopy.
  • Zenair CH 250 TD: "Tail Dragger" version with conventional landing gear.
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
700 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
122 kts
MACH
n/a
Ceiling
145
Range
n/a
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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