TYPE: Utility amphibian.
PROGRAMME: Project announced 2003 as development of L-6. Data generally as for L-6, except where stated.
LANDING GEAR: Nosewheel type; retractable. Mainwheels, size 476x168, nosewheel 400x150. Minimum ground turning radius 14.0 m (46 ft).
POWER PLANT: Two LOM V546 piston engines, each 158 kW (212 hp). Optionally two 173 kW (232 hp) LOM M337B or 184 kW (247 hp) M337C six-cylinder piston engines. Fuel capacity 320 litres (84.5 US gallons; 70.4 Imp gallons); provision for two long-range tanks with combined capacity of 300 litres (79.3 US gallons; 66.0 Imp gallons).
ACCOMMODATION: Eight persons, including up to two pilots.
EQUIPMENT: Optional ballistic parachute.
|Wing span||13.06 m (42 ft 10¼ in)|
|Length overall||10.80 m (35 ft 5¼ in)|
|Max wigth of fuselage||2.00 m (6 ft 6¾ in)|
|Height overall||3.40 m (11 ft 1¾ in)|
|Wheel track||1.18 m (3 ft 10½ in)|
|Wheelbase||3.48 m (11 ft 5 in)|
|Cabin: Length||3.45 m (11 ft 3¾ in)|
|Max width||1.64 m (5 ft 4½ in)|
|Max height||1.24 m (4 ft 0¾ in)|
|Volume||3.7 m³ (131 cu ft)|
|WEIGHTS AND LOADINGS:|
|Weight empty||1,400 kg (3,086 lb)|
|Max payload||670 kg (1,477 lb)|
|Max fuel weight||230 kg (507 lb)|
|Max T-O and landing weight||2,300 kg (5,070 lb)|
|Max power loading||7.28 kg/kW (11.96 lb/hp)|
|Max level speed||140 kt (260 km/h; 164 mph)|
|Normal cruising speed||119 kt (220 km/h; 139 mph)|
|Stalling speed, power off, flaps up||65 kt (120 km/h; 76 mph)|
|Max rate of climb at S/L||336 m (1,102 ft)/min|
|T-O run: land||200 m (660 ft)|
|water||250 m (820 ft)|
|Range||647 n miles (1,200 km; 745 miles)|
|Endurance||5 h 40 min|