A
A
I
I
R
R
P
P
L
L
A
A
N
N
E
E
T
T
E
E
C
C
H
H
N
N
I
I
C
C
A
A
L
L
D
D
E
E
S
S
C
C
R
R
I
I
P
P
T
T
I
I
O
O
N
N
,
,
O
O
P
P
E
E
R
R
A
A
T
T
I
I
N
N
G
G
,
,
M
M
A
A
I
I
N
N
T
T
E
E
N
N
A
A
N
N
C
C
E
E
A
A
N
N
D
D
R
R
E
E
P
P
A
A
I
I
R
R
M
M
A
A
N
N
U
U
A
A
L
L
2-37
Document No.:
EV97SLNOEN
Date of Issue:
02/2008
Revision:
-
2.3.12.3 Propeller
2.3.12.3.1 Description
The standard powerplant consists of the four-cylinder, 4 stroke ROTAX 912 (80 hp) engine and V
230 C prop.
The V 230 C is a fixed, wooden, 2-blade propeller with leading edge protection. The prop is
attached to the propeller hub with 6 bolts. A fiberglass spinner is used.
Refer to the manuals supplied with the prop for more information.
Propeller Technical Data
Diameter ............................
63.98
+0.008
-0.01
in
1625
+2
-3
mm
Pitch ................................ 18
°20´
- 18
°55´
Weight ........................................
7.1
±
0.7
lbs
3.2
±
0.3 kg
Propeller blade clearance
measured from ground: .............
12.6
1.2
in
320
30 mm
Manufacturer..........................................................
VZL
Ú Praha
- Let
ò
any, Czech Republic
NOTE
The exact pitch/performance of the prop supplied with each aircraft may differ slightly, therefore
the exact performance of your aircraft may be different.
