F
F
L
L
I
I
G
G
H
H
T
T
T
T
R
R
A
A
I
I
N
N
I
I
N
N
G
G
S
S
U
U
P
P
P
P
L
L
E
E
M
M
E
E
N
N
T
T
for SPORT
STAR
Light Sport Aircraft
Document No.: S2006FTSUS Revision: -
Date of Issue: 15/01/2006
Page:
8/130
2.2 Sportstar Brief Description
The SPORTSTAR is light sport aircraft built by Evektor-Aerotechnik,
a certified aircraft manufacturer from the Czech Republic, which has more
than 35 years experience in aircraft industry.
The Sportstar is all-metal, low-wing monoplane of semimonocoque
construction with side-by-side seat arrangement and dual controls. The
airplane is fitted with a tricycle landing gear with the steerable nose wheel.
The standard power unit consists of four-cylinder four-stroke engine Rotax
912 (80 or 100hp) and on-ground adjustable propeller, WOODCOMP
KLASSIC 170/3/R. Optionally, other engines and propellers may be
installed. The airplane’s maximum takeoff weight (MTOW) is 1213 lbs. (550
kg).
Refer to the Aircraft Operating Instructions and Aircraft Maintenance and
Inspection Procedures for more details on the Sportstar technical data,
description of systems, limitations, equipment installed in a particular
airplane, and for other required information.