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ZENAIR Zenith (CH-2000)

From SKYbrary Wiki

CH2T
Aircraft
Name Zenith (CH-2000)
Manufacturer ZENAIR
Body Narrow
Wing Fixed Wing
WTC Light
APC A
Type code L1P
Engine Piston
Engine count Single
Mass group 1


Manufacturered as:

AMD CH-2000 Alarus
AMD Zenith
AMD CH-2000 Zenith
AMD Alarus
JORDAN AEROSPACE Sama
JORDAN AEROSPACE CH-2000 Sama
ZENAIR Zenith (CH-2000)
ZENAIR CH-2000 Zenith


ZENAIR Zenith (CH-2000)

ZENAIR Zenith (CH-2000)

Description

The CH-2000 is a two-seat, fixed tricycle gear general aviation aircraft, used primarily for flight training.

Technical Data

Wing span 8.79 m28.839 ft
Length 7.01 m22.999 ft
Height 2.08 m6.824 ft
Powerplant 1 x Lycoming O-235-N2C four cylinder, horizontally opposed, four stroke aircraft engine, 116 hp.
Engine model Lycoming O-235

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 100 kts MACH IAS kts IAS kts Vapp (IAS) kts
Distance 472 m ROC ft/min ROC ft/min ROC ft/min ROC ft/min MACH ROD ft/min ROD ft/min MCS kts Distance 520 m
MTOW 700700 kg
0.7 tonnes
kg
Ceiling FL120 ROD ft/min APC A
WTC L Range 850850 nm
1,574,200 m
1,574.2 km
5,164,698.167 ft
NM

Accidents & Serious Incidents involving CH2T

None on SKYbrary