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
4-26
Document No.:
EV97SLNOEN
Date of Issue:
02/2008
Revision:
-
4.11.4 Rudder deflection adjustment
The rudder deflections are set by the aircraft manufacturer. If necessary the rudder deflections can
be adjusted by abjustable stops located on the rudder control cable in the cockpit (see figure on
page 2-29).
4.11.5 Trim tab adjustment
The following may be adjusted:
a) The position of the trim tab control lever may be adjusted against a groove in the quadrant
between the seats.
Loosen the bolts which clamp the ends of the trim tab control cables on the upper/lower tab
surface. Then set the trim tab control lever in the desired position, slightly tighten the cables
and retighten the bolts.
b) Trim tab deflections
Trim tab deflection may be adjusted using the adjustment bolts which clamp the ends of the
control cables. The adjustment bolts are on the upper/lower tab surface
–
see Fig. in par.
2.3.11.10.