DEKO 8 VLA Club

by Aerotek
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DEKO 8 VLA Club - Photo #1

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.

Specifications

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)

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