SUPPLEMENT S2
Chapter 53 – Fuselage
CHAPTER 53 – FUSELAGE
CABIN TRUSS
The truss is modified in the lower central part in order to accommodate the support
for pedals and throttle additional control. The assy 22-5-403-000 (in the red box in
the figure) is welded into the truss standard, which then assumes p/n 22-2-100-005
(Figure C-3).
FIGURE 53-1 TRUSS REINFORCEMENT FOR ADDITIONAL CONTROLS
The truss reinforcement is to be intended as permanent factory made
installation and must not be removed when the kit is not installed on the
aircraft.
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