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.
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Aircraft Details |
UL (Ultralight) |
LSA (Standard) |
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| 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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