Company | Type | Details / description | Year |
CHERNOV | Che-10 | Single-engined single-seat high-wing ultralight aircraft on skids | 1986 |
AEROSAMARA | Che-15 | Single-engined two-seat ultralight twin-float seaplane | 1997 |
STARATEL | Che-20 Chaika | (Gull) Three-seat open-cockpit flying boat with two 35 hp Vikhr-30M engines | 1989 |
GIDROSAMOLYET | Che-21 | Lightweight seaplane version of Che-23, without landing gear. | |
CHERNOV | Che-22 | Three-seat high-wing multipurpose seaplane prototype with two Rotax 582 engines, enclosed
cockpit, metal wing; developed from Che-20 with Evgeny Yunkerov for possible production | 1993 |
GIDROPLAN | Che-22D (Korvet-912) | Production version with one 80 hp Rotax 912UL engine | |
GIDROPLAN | Che-22R | Production version with one 64 hp Rotax 582 engine | |
GIDROPLAN | Che-22R-2 (Korvet 503) | Production version with two 50 hp Rotax 503 engines | |
GIDROPLAN | Che-22R-2S (Korvet 582) | Production version with two 64 hp Rotax 582 engines | |
GIDROPLAN | Korvet | Basic two-seat amphibian version of Che-22; two 64 hp Rotax 582 engines, metal wing of
new design, fiberglass hull, retractable wheeled landing gear, tail wheel; fully compliant with
AP-23 airworthiness standards | |
GIDROPLAN | Korvet-UT | Dual control version. | |
GIDROPLAN | Korvet-L | Two Rotax 582 UL; static buoyant tips revised to include miniature hydrodynamic float extensions | 2003 |
GIDROPLAN | Korvet-LU | Three-seat version with increased take-off weight, hooded engines, no AR MAK type certificate | |
AVIATEKSIM | Korvet-J | Version with two 85 hp Jabiru 2200 engines | 2003 |
GIDROPLAN | Korvet single | Version with one Jabiru 2200 engine, three blade propeller | 2008 |
GIDROPLAN | Korvet-KIT | Kit version marketed without engines | 2010 |
GIDROPLAN | Korvet Kabriolet | Open cockpit version, under development in 2010; probably one Jabiru 2200 | |
GIDROSAMOLYET | Che-23 | Lightweight two-seat amphibious aircraft with one 64 hp Rotax 582 or 100 hp Rotax 912 engine;
an improved lighter single-engine modification of Che-22 with raised horizontal tail, modified
bow shape, better aerodynamics | 2003 |
GIDROSAMOLYET | Che-23A | Basic production version (one pilot and two passengers), with one 100 hp Rotax 912 power engine | |
GIDROSAMOLYET | Che-23B | Version with increased take-off weight, one pilot and three passengers, increased fuel capacity | |
GIDROSAMOLYET | Che-23V | Version with more powerful 115 hp Rotax 914 engine | |
GIDROSAMOLYET | Che-23M | Modernized version | |
GIDROSAMOLYET | Che-24 | Two/three-seat modernized Che-23 with new more advanced and faster profile wings, retractable
tricycle landing gear; one 100 hp Rotax 912USL engine (in bottom position), but 40- to 80 hp
engines also considered | 2010 |
GIDROSAMOLYET | Che-24M | Simplified seaplane version with 64 hp Rotax 582 engine (100 hp Rotax 912 possible) | 2011 |
GIDROSAMOLYET | Che-24M2 | Planned twin-engine advanced version with two 64 hp Rotax 582 engines | 2011 |
AEROSAMARA | Che-25 | 4/5-seat light multi-purpose amphibious aircraft with two 64 hp Rotax 582 or 100 hp 912ULS | 1996 |
AEROSAMARA | Che-257 | undefined variant | |
AEROSAMARA | Che-259 | undefined variant | |
AEROSAMARA | Che-25K | undefined variant | |
AEROSAMARA | Che-25M | modernized version with two 100 hp Rotax 912 engines; development started in 1999 | 2000 |
GIDROSAMOLYET | Che-26 | Che-24 mod. with two 70 hp Sauer 650 engines, 3-bladed fixed-pitch or variable-pitch propellers | 2012 |
CHERNOV | Che-27 | Multi-purpose five-seat amphibious aircraft prototype | 2003 |
GIDROSAMOLYET | Che-27A | basic version with two 100 hp Rotax 912ULS engines | |
GIDROSAMOLYET | Che-27B | modified version with increased fuel supply | |
GIDROSAMOLYET | Che-27V | version with more powerful 115 hp Rotax 914 or 120 hp Jabiru 3300 engines | |
STATUS-AVIA | Che-27M2 | Strengthened version with increased tail area | 2004 |
STATUS-AVIA | SA-1 Status | Production version with lengthened and expanded fuselage, hull contours changed | 2004 |
GIDROSAMOLYET | Che-28 | Modernized Ch-27 with new more advanced and faster profile wings; only one built | 2011 |
GIDROSAMOLYET | Che-29 | Twin-engine 5/6-seater amphibian; two Rotax 912ULS engines; new wing, longer/wider body | 2011 |
GIDROSAMOLYET | Che-29 Ej25 | Conversions with Subaru Ej25 engines | |
CHERNOV | Che-30 | Twin-engine seaplane prototype similar to Che-20 but with enclosed cockpit | 1991 |
CHERNOV | Che-35 | Twin-engine seaplane project with highly streamlined fuselage | |
AEROVOLGA | Borey | Single-engined amphibious aircraft. | 2016 |
AEROVOLGA | Borey A | Advanced ultra-light aeroplane (AULA) version for the Canadian market | 2019 |
AEROVOLGA | Borey L | Variant that participated in the circumnavigation of the Arctic Circle | 2018 |