Letov Air ST-4 Aztek

A two-seat microlight (1996 type), in assembled or kit form. The ST-4 was effectively a side by side version of the Sluka.

Engine: Rotax 582, 64 hp
Wing span: 10.40 m
Wing area: 15.3 sq.m
MAUW: 450 kg
Empty weight: 220 kg
Fuel capacity: 45.5 lt
Max speed: 130 kph
Cruise speed: 100 kph
Minimum speed: 49 kph
Climb rate: 4 m/s
Seats: 2
Fuel consumption: 13 lt/hr
Certification: AAA CR ULL-II/96
Price (1998): 32 290 DM
Kit price (1998): 23 530 DM

Letov Air LK-2 Sluka

LK-2M

LK-2 Sluka single-seat microlight (first flown 1991), assembled or kit form.

LK-2M

LK-2M
Engine: Rotax 447, 42 hp
Wing span: 9.2 m
Wing area: 14 sq.m
MAUW: 290 kg
Empty weight: 140 kg
Certification: VZ, PFA
Max speed: 120 kph
Cruise speed: 85 kph
Minimum speed: 45 kph
Climb rate: 4.5 m/s
Seats: 1
Fuel consumption: 1 lt/hr
Kit price (1998): £7850

Letov Air sro

First flew in May 1997 the L-11 side-by-side two-seat basic trainer and glider-towing lightplane, but in 1998 was in financial difficulties and required investor to complete development. Then also offering LK-2 Sluka single-seat microlight (first flown 1991), LK-3 Nova two-seat microlight/ homebuilt (first flown 1993), and ST-4 Aztek two-seat microlight (1996 type), all three in assembled or kit forms.

1998:
Beranovych 65
CZ-19902 Prag 9 Letány
Czech Republic