CH15
ZENAIR CH-150 Acro-Zenith
ZENAIR CH-150 Acro-Zenith
Aircraft
Name
CH-150 Acro-Zenith
Manufacturer
Body
Narrow
Wing
Fixed Wing
WTC
L
APC
A
Type Code
L1P
Engine
Piston
Engine Count
Single
Manufactured as
ZENAIR CH-150 Acro-Zenith
ZENAIR CH-150 Acro-Z
ZENAIR Acro-Z
ZENAIR Acro-Zenith
Cite This Page
SKYbrary Aviation Safety. (March 8, 2021). CH15.
Retrieved June 4, 2026
from https://skybrary.aero/aircraft/ch15
UID: 17751
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CH15
The Zenith CH 150 Acro Zenith is a Canadian single-engine, low wing, all-aluminum aircraft designed by Chris Heintz and produced by Zenair in kit form for amateur construction.
Technical Data
Wing span (metric)
6.15 m
Length (metric)
6.17 m
Height (metric)
1.52 m
Powerplant
1 x Lycoming 0-320, 110 kW (150 hp).
Engine Model(s)
Lycoming O-320
Indicative Performance Data
Take-Off
V2
n/a
Distance
210 m
MTOW
522 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
126 kts
MACH
n/a
Ceiling
160
Range
260 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
190 m
