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5) Align and hold both control wheels (1) in the neutral position with a ruler and clamps.
6) Check the alignment of ailerons (2) in relation to the trailing edge of the wing tips.
7) If necessary, perform the following operations to adjust input rod (3) :
CAUTION : MAKE SURE THE FLAP AREA IS CLEAR.
b) Extend the flaps.
c) Open main switch-breaker.
d) Install the warning sign prohibiting main switch-breaker operation.
WARNING
DO NOT OPERATE
MAINTENANCE WORK IN PROGRESS
AAAA
Validity : S / N 1 - 9999 27 10 00 Page 201
(BA) S EP 04
e) Adjust input rod (3) - refer to 20-00-11.
f) Remove the warning sign prohibiting main switch-breaker operation.
g) Close main switch-breaker.
CAUTION : MAKE SURE THE FLAP AREA IS CLEAR.
I h) Retract the flaps.
8) Position the clinometers on the ailerons and set 0° - refer to 20-00-13.
9) Remove the ruler and the clamps.
10) Rotate and hold control wheel (1) in maximum L.H. position, with torque rod (18) lever (34) to maximum travel.
11) Check the travel angles of L.H. and R.H. ailerons :
NOTE : The roll control system has been designed in such a way (one adjustable rod only) that when the 0° is set, the travel values must be within tolerances.
- L.H. aileron up : 15° ± 1°30'
- R.H. aileron down : 15° ± 1°30'
12) Fully rotate control wheel (1) in the opposite direction to the right and repeat step 11) for ailerons (2) reverse position.
13) If the travel cannot be adjusted to the required values, moderately grind (using a file) or replace faulty adjustable stop (36).
NOTE : Adjustable stops (36) are factory-adjusted, then -riveted to the cabin floor. It is extremely unlikely that they will require reworking.
14) Make sure all the tools and materials are removed and the work area is clean and free from debris.
15) Install the cowling under hull 218.
16) Lower the aircraft to ground and remove the jacks - refer to 07-10-00.
17) If the aircraft is equipped with the roll / yaw interconnection system, check rod adjustment - refer to 27-20-02.
C. Adjustment of ailerons with travel jig(s) (Figures 202A, 204, 205 and 207)
NOTE : The adjustment of the roll control must be preceded by a check of slack values -Paragraph 4. C.
1) Remove the cowling under hull 218.
2) Position travel jigs (4) 8653 TB10 00000 on the wings at the level of the rivets line of rib N10.
3) Align and hold both control wheels (1) in the neutral position with a ruler and clamps.
4) Make sure the ailerons are in neutral position (0°).
5) If necessary, perform the following operations to adjust input rod (3) :
CAUTION : MAKE SURE THE FLAP AREA IS CLEAR.
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