AEROSPOOL DYNAMIC WT 9 Ultralight Aeroplane FLIGHT MANUAL

Below you will find brief information for Ultralight Aeroplane DYNAMIC WT 9. This manual contains information for the safe and efficient operation of this ultra light aeroplane. The manual contains supplementary data supplied by the aeroplane manufacturer in accordance with the German Certification Regulations and Airworthiness Requirements for ultra light aircraft of the DaeC ( BFU des DaeC, Ausgabe 10/95 ).

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AEROSPOOL DYNAMIC WT 9 FLIGHT MANUAL | Manualzz

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Key features

  • fixed or retractable tricycle landing gear
  • two places in the cockpit, side by side type
  • ROTAX 912 UL or 912 ULS engine
  • 3 bladed in-flight electricaly adjustable propellers
  • approved for VFR only

Frequently asked questions

It uses a ROTAX 912 UL or 912 ULS engine.

The maximum take-off weight is 450 kg.

The following fuels can be used: EUROSUPER ROZ 95 unleaded accordance DIN 516 07 and O NORM 1100, Unleaded Automobile Gasoline Super 95, Leaded Automobile Gasoline Super 95 accordance DIN 516 00 O NORM 1100, AVGAS 100 LL.

The following manoeuvres are permitted: Steep turns with the angle of bank up to 60°, Lazy eighths, Combat turns. Aerobatic manoeuvres and intentional spins are prohibited!
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