DEKO 8 VLA Club

Climb ratio: 800 ft/min | 4 m/s
Glide ratio: 9

Takeoff distance over 50ft (15m) obstacle: 300 ft | 90 m
Landing distance over 50ft (15m) obstacle: 390 ft | 120 m

MEW (manufacturers empty weight): 450 kg | 992 lbs
MTOW (maximum takeoff weight): 700 kg | 1543 lbs

Engine: PZL Franklin 4 (135 hp), option: Lycoming 0-235 (125 hp), Rotax 912 (100hp) , Jabiru 3300 (120 hp)
Fuel consumption: 18 liters/h

This aircraft is under design now, by Polish aeronautical engineers: Daniel Debski Ph.D., Marek Debski Ph.D. and Krzysztof Kotlinski. M.Sc.

Structure: Aluminum tube fuselage with composite joints (Polish Patent) and with Ceconite covering.

Power Plant: PZL Franklin F4 (135 hp) with a three-blade MT- Propeller, variable-pitch propeller.

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