WT-9 Dynamic Club S FLIGHT MANUAL Section 1 Page 1-2
1.4 Descriptive data
1.4.1 Airplane description
WT-9 Dynamic Club S is low-wing monoplane with fixed landing gear. The airframe
consists of a sandwich shells from advanced composite material. There are two places
in the cockpit, side by side type. This airplane is intended for sporting, recreation and
tourist flying in accordance with VFR.
WT-9 Dynamic Club S has been approved by the DaeC in the Category of
Airworthiness : Normal
As the power plant this airplane uses the 4 cylimder, 4 stroke ROTAX engines, 912
ULS. Propelers: This plane is fitted with 2 blades hydraulic constant speed MTV-21-A
1.4.2 Technical data
Wing span.................................................…. 9,00 m
Wing area…................................................... 10,3 m
2
Wing aspect ratio............................................ 7,82
Length............................................................. 6,4 m
Height.........................................................… 2,0 m
Aerodynamic mean chord ( MAC )............… 1,185 m
Control surfaces
Aileron span………........................................ 1,25 m
Aileron area…................................................. 0,273 m
2
Flap span………............................................. 2,28 m
Flap area…….................................................. 0,75 m
2
Horizontal tail span……………….……......... 2,40 m
Horizontal tail area…………………............... 1,68 m
2
Vertical tail span………………...............….... 1,022 m
Vertical tail area……………….................….. 1,02 m
2
Landing gear
Wheel spacing.……………………............…. 1,49 m
Wheel base..................................................…. 2,27 m
Main wheel diameter……………................… 0,35 m
Nose wheel diameter………………………… 0,32 m
Weights
Empty weight ……………………………….….... 334,1 kg
Maximum take-off weight…….....................……. 472,5 kg
Useful load……….....................................……..... 138,4 kg
Fuel tanks capacity…………................................. 126 litres
The ROTAX 912 ULS (73 kW- 100HP) with a maximum rpm limitation on take off of
5800 1/min. The propeller MTV-21-A diameter is 1,7 m
Date: 1.12.2001
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