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.
| DIMENSIONS, EXTERNAL: | |
| 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) |
| DIMENSIONS, INTERNAL: | |
| 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) |
| PERFORMANCE: | |
| 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 |
