SOLOY AVIATION SOLUTIONS
CESSNA 206 WITH WING MOUNT CAMERA
MAINTENANCE MANUAL SUPPLEMENT
WINGS 57-60-00
AILERON TRIM TABS – REMOVAL/INSTALLATION
October,
2011
Page 401
AILERON TRIM TABS – REMOVAL/INSTALLATION
1. AILERON TRIM TAB – REMOVAL
(Figure 1)
A. Remove aileron trim tab adjustment screws (4).
B. Remove upper attachment rivets (3).
C. Remove aileron trim tab (1) from rear of aileron.
2. AILERON TRIM TAB – INSTALLATION
A. Slip aileron trim tab hinge plates between wing skin and the intercostal frame
assembly (2). Verify that the slotted hinge plate is down and that the trim tabs are
being installed on the correct side of the aircraft.
B. Align the trailing edge of the aileron trim tab to the aileron at with the trim tab at 0°.
C. Install aileron trim tab adjustment screws and tighten in place.
D. Install clecos along top to hold hinge plate in place and then remove the clecos
one by one while installing the correct rivets.
(1) If aileron trim tab is being installed for the first time, mark outer rivet locations
and remove trim tab from aileron.
(2) Drill outer rivet locations with trim tab on bench and reinstall trim tab with
clecos holding outer two locations.
(3) Install lower 4 trim tab adjustment screws.
(4) Drill other 6 rivet locations with trim tab installed on aileron.
(5) Clean out metal shavings, then install rivets along upper hinge plate.
E.
Verify that the aileron trim tabs can move 9° up on the left wing and 9° down on
the right wing. The aileron trim tabs do not need to move beyond 0° in the
opposite direction.
NOTE
The aileron trim tabs look very similar side to side. Refer to
Chapter 57 of the Cessna 206 Wing Mount Camera
Illustrated Parts Catalog S2061A for the correct aileron trim
tab component locations.
1. Aileron Trim Tab
3. Rivet
2. Intercostal
Frame
4. Adjustment
Screw
Figure 1:
Aileron Trim Tab Installation
1
3
2
4