CH10

ZENAIR CH-100 Mono-Zenith

Aircraft
Name
CH-100 Mono-Zenith
Manufacturer
Body
Narrow
Wing
Fixed Wing
WTC
L
APC
A
Type Code
L1P
Engine
Piston
Engine Count
Single
Manufacturered as
ZENAIR CH-100 Mono-Zenith
ZENAIR CH-100 Mono-Z
ZENAIR Mono-Zenith
ZENAIR Mono-Z

CH10

The Zenair Mono-Z CH 100 is a single-seat, single-engined Canadian light aircraft of the 1970s. It is a smaller version of the Zenair CH 200 with a less powerful engine, which was sold as a homebuilt aircraft by Zenair.

Technical Data
Wing span (metric)
6.71 m
Length (metric)
5.94 m
Height (metric)
1.98 m
Powerplant

1 x Volkswagen, 65 hp.

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
91 kts
MACH
n/a
Ceiling
140
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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