WT-9 Dynamic Club S FLIGHT MANUAL Section 7 Page 7-
SECTION 7
AIRPLANE AND SYSTEM DESCRIPTION
Page
7.1 Introduction 7-1
7.2 Airframe 7-1
7.3 Flight controls 7-2
7.4 Instrument panel 7-3
7.5 Landing gear system 7-4
7.6 Seats and safety harness 7-5
7.7 Baggage compartment 7-5
7.8 Doors, windows and exits 7-5
7.9 Powerplant 7-6
7.10 Fuel system 7-10
7.11 Electrical system 7-11
7.12 Pitot and static pressure system 7-12
7.13 Avionics 7-12
7.14 Miscellaneous equipment 7-12
7.1 Introduction
This section provides a description of the operation of the aeroplane and its systems.
Refer to Section 9, Supplements, for details of optional systems and equipment.
7.2 Airframe
WT-9 Dynamic Club S is a single engine airplane, controlled aerodynamically, made
from advanced composite material, low-wing monoplane with two side-by side seats.
The aeroplane is equipped with a fixed tricycle undercarriage.
Fuselage
The fuselage sandwich shell is divided in the symmetry plane. The shell is of three
layer construction. The external and internal shell layers are made of glass and
carbon fibre fabrics, which are saturated with a resin. Between them there is a filling
of hard foam panels. The fin is made together with the fuselage. The wing central
panel is fixed at the fuselage.
Date: 1.12.2001
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