CH2T
ZENAIR Zenith (CH-2000)
ZENAIR Zenith (CH-2000)
Aircraft
Name
Zenith (CH-2000)
Manufacturer
Body
Narrow
Wing
Fixed Wing
WTC
L
APC
A
Type Code
L1P
Engine
Piston
Engine Count
Single
Manufactured as
ZENAIR Zenith (CH-2000)
ZENAIR CH-2000 Zenith
JORDAN AEROSPACE Sama
JORDAN AEROSPACE CH-2000 Sama
AMD CH-2000 Alarus
AMD Zenith
AMD CH-2000 Zenith
AMD Alarus
CH2T
The CH-2000 is a two-seat, fixed tricycle gear general aviation aircraft, used primarily for flight training.
Technical Data
Wing span (metric)
8.79 m
Length (metric)
7.01 m
Height (metric)
2.08 m
Powerplant
1 x Lycoming O-235-N2C four cylinder, horizontally opposed, four stroke aircraft engine, 116 hp.
Engine Model(s)
Lycoming O-235
Indicative Performance Data
Take-Off
V2
n/a
Distance
472 m
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
100 kts
MACH
n/a
Ceiling
120
Range
850 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
520 m
