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Maintenance Manual XA41/XA42
AMM-XA42-0040-001 C.00
Page
10
Page date:
Chapter 27
25.09.2018
27-10-00 AILERONS
The ailerons are mechanically connected to the control sticks with these components:
No. Quantity
Component
P/N
-
-
Torque tube
See 27-00-02
1
2
Aileron rod inboard
XA42-2710-109
2
2
Aileron bellcrank fuselage
XA42-2710-050
3
2
Aileron rod CFRP
XA42-2710-114
4
2
Aileron bellcrank wing
XA42-2710-060
5
2
Aileron rod outboard
XA42-2710-119
Figure 27-7: Overview - aileron control rods
The bearings in the bell cranks are sealed ball bearings.
Each aileron is attached to five hinge points with one metal rod.
To prevent flutter, each aileron has a balancing mass in its leading edge.
To decrease the pilot’s control forces, the ailerons have spades. The spade arms are
connected to the center hinge ribs of the ailerons.
Travel stops on the fuselage structure near the torque tube keep the aileron travel in the
specified limits. Refer to chapter 27-00-02 for the exchange of the aileron travel stops.
Before you adjust the control system, examine the control rods, bell crank levers and hinges
for wear and damage.
Make sure that the control rods length is correct. Adjust the length, if necessary. Refer to
chapter 27-00-03
Summary of Contents for XA41
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