DEKO 8 VLA Club

by Aerotek

4.3

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.

Empty weight:: 992 lbs (450 kg)
MTOW:: 1543 lbs (700 kg)
Stall speed:: 43 kts (49 mph) (80 kph)
Cruise speed:: 92 kts (106 mph) (170 kph)
VNE:: 135 kts (155 mph) (250 kph)
Climb:: 787 ft/min (4 m/s)
Glide ratio:: 9
Take-off distance:: 295 ft (90 m)
Landing distance:: 394 ft (120 m)
Engine:: PZL Franklin 4 (135 hp), option: Lycoming 0-235 (125 hp), Rotax 912 (100hp) , Jabiru 3300 (120 hp)
Fuel consumption:: 5 GPH (18.9 LPH)