DYNAMIC

The "Dynamic", completely built from composite materials.

On the left as VLA (standard category) with retractable gear, right as microlight.

The spacy panel takes all of your options.

 

 

DYNAMIC WT-9

 

GENERAL

The Dynamic WT-9 is two-seat light airplane. Thanks to progressive construction design, and using advanced materials such as sandwich shells and carbon composites, it has low weight. The Dynamic is the first light sport airplane, that passed complete aeroelastic investigation. It is one of only a few types in the light sport plane category that the customers can choose from two versions, fixed (ultralight) or hydraulic retractable landing gear (VLA). And even for the base price customers get a ready-to-fly aircraft equipped with Rotax 912UL with 80HP. The long list of additional equipment enables the customer to meet his individual needs.

PANEL 

The basic instrument set consists of air speed indicator, altimeter, magnetic compass, RPM indicator, oil pressure indicator, oil temperature indicator, and cylinder head temperature indicator, radio.

ENGINE

The basic power plant is Rotax 912 UL with 80 HP with a ground adjustable propeller. The VLA power plant is Roax 912 S with 10 HP and an electric variable pitch propeller. Both versions are equipped with two carburetors, electrical starter, double ignition, stainless steal exhaust, and muffler.

FUEL SYSTEM

Two wing tanks taking max. 125 l Mogas. Via a boosted header tank 125 ltr. allowing a range of about 2.000 km! A "low fuel" warning lamp is standard.

LANDING GEAR

Main landing gear consists of 2 laminated spring gears and steering nose gear attached to the firewall by bungee cord shock absorber mechanism. A hydraulic retractable gear (RG-version) is available as option. In both versions the main gear wheels are equipped with hydraulic disc brakes. They are actuated by lever on center console, which also serves as a parking brake.

 

Aircraft Details

 

UL (Ultralight)

LSA (Standard)

     
Empty Weight 270 kg 280 kg
MTOW 472,5kg 560 kg
Wing Span 9,00 m 9,00 m
Length 6,40 m 6,40 m
Height 2,00 m 2,00 m
Wing Area 9,50 qm 9,50 qm
Engine, 4 cylinder, 4 stroke   Rotax 912 UL Rotax 912 ULS
Power   80 Hp 100 Hp
Fuel capacity   75 ltr. 125 ltr.
Fuel consumption   13 l/h 14 l/h
Range   1.200 km 2.000 km
Endurance   5,5 hrs. 9 hrs.
Stall Speed (Vmin) 60 km 62 km
Optimum Speed  (Vopt) 220 km 250 km
Max. Speed (Vmax) 270 km 270 km
Crosswind component   20 ktm 20 km
Take-off distance   200 m 170 m
Landing distance   170 m 180 m
Ceiling   15.000 ft. 15.000 ft.

 

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First posted: December  1993     Last Revision: December  2005

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