P92 Classic Jabiru
M a i n t e n a n c e M a n u a l
INSPECTIONS
AND SERVICING
Page B-4
Date
:
Issue 3: 4
th
July 2011
Section B
5.
CONTROL SETTINGS
Adjustment of control surfaces must not exceed travel limits reported in table below. Zero
reference mark for stabilator is on left side of aircraft (see figure below).
AILERONS
(starting from tip line-up
)
Up 20
o
Down 15
o
2
o
STABILATOR
Up 16
o
Down 3
o
1
o
TRIM
(
Stab. at 0
o
, see fig. below
)
2
o
12
o
1
o
RUDDER
RH 25
o
LH 25
o
2
o
FLAPS
(
maximum travel
)
0
o
35
o
2
o
Cable tension should be as follows:
CONTROL CABLE TENSION: 20 daN
2 for all
F
IGURE
B-3
S
TABILATOR
Z
ERO REFERENCE
6.
TRIM-TAB ADJUSTMENT
Travel adjustment of trim tab on tail plane should be carried out as follows:
Move stabilator to neutral (0 degrees) and lock in position; (this is accomplished by
aligning the stabilator’s leading edge with the reference rivet located on the left side of
tail cone);
Turn Master-Switch ON;
Trim to maximum pitch-up;
Adjust thread of hinged control rod until tab is deflected downwards 12° (use a
protractor or measure downward displacement of trailing edge -
12° relates to roughly
24mm
-);
Tighten adjustment thread lock-nut and fasten connecting pin of control rod to trim-
tab.
REFERENCE RIVET
