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russian version
In 1984 SU-26 sport jet aircraft, a future champion, that came out of the Sukhoi experimental design bureau, made its first flight. At the world championship in 1986 it won not only various prizes but also the status of one of the best trainer jets in the world. Later, in 1991, Su-29 two seat trainer was created, and in 1994 its modified models - SU 26 and SU 31- appeared.

All of them are equipped with M14P engines (360 hp) and their 400 hp modifications (M14X). In 2003 a new type of engines is to appear M14R (430 H.P.)

The wings are made of composite materials, based on carbon-plastic longerons, and it is a major achievement of the advanced technologies of the former Soviet Union.
YAK 18     

YAK18T is a fourseater, designed for
primary pilot training and route flights.
Technical characteristics:
Length (m)
8,4
Wing span(m)
11,2
Takeoff mass(kg)
1650
Empty (kg)
1247
Fuel
195
Engine
14P
Max power (h.p.)
360
Vmax (km/h)
295
Cruising speed (km/h)
180-200
Max commercial load (kg)
600
Flight range with max. commercial load (km)
600
Overload range
+5 / -2,5

N 2     

AN 2 is used as a passenger and commercial plane.
Technical characteristics:
Length (m)
12 ,74
Wing span(m)
18 ,18
Takeoff mass(kg)
5500
Empty (kg)
3360
Fuel
900
Engine
SH-62IR
Max power (h.p.)
1000
Vmax (km/h)
250
Cruising speed (km/h)
160-180
Max commercial load (kg)
1500
Flight range with max. commercial load(km)
900
Crew
2
Passengers
12

YAK 52     

YAK 52 is a twoseater used for primary and general pilot training. The plane is specially designed for aerobatics.
Technical characteristics:
Length (m)
7,7
Wing span(m)
9,3
Takeoff mass(kg)
1315
Empty (kg)
1025
Fuel
120
Engine
14P
Max power (h.p.)
360
Vmax (km/h)
300
Cruising speed (km/h)
360
Overload range
+7 / -5

SU 29   

SU 29 is a twoseater designed on the base of SU
26 which retaines all the advantages of its predecessor.

The empty weight of SU 29 is only 50 kg more than that of SU 26 because of using composite materials that form about 60% of the airplanes construction.

When piloted by a single pilot its characteristics are identical to SU 26.

The serial production of this airplane was started in 1992. Su 29 has good sales in the USA, Great Britain, Australia, SAR and other countries.

Technical characteristics:
Normal takeoff mass of the sport variant
860
Max. takeoff mass (kg)
1200
Empty (kg)
735
Engine
14P
Max power (h.p.)
360
Vmax horizontal (km/h)
295
Allowed Vmax (km/h)
450
Landing speed (km/h)
120
Climb rate
16
Max rotation speed
6
Overload range
+12 / -10
Flight range (km)
1200

SU 31    

SU 31 is the result of development of SU 26 sport aircraft. The experimental model made its first flight in June 1992 and in July it made a successful debut at the World Aerobatics Championship in France. Y. Kayris won the bronze flying SU 31.

For the first time the aircraft was exhibited at the "Farnborough-92" Aerospace Expo and then at all major airshows. Since 1994 the Russian national aerobatics team has been flying these airplanes at the Europe and World championships and has achieved great success. In 1994 the airplane passed international certification in aerobatics category. In 1995 it passed the Russian certification.

The construction of the plane is similar to that of SU 29 but they differ in size, undercarriage and cockpit. The inclination angle of the back of the pilots seat is 35 that allows to perform aerobatics at +12/-10 g overloads. 70% of the plane is made of composite materials with wide use of honeycomb constructions.

The export variant of SU-31 is SU 31 X. It has fuel tanks built in wings . SU 31 M has an ejection seat, a new cockpit and fuel tanks built in wings .

Modifications:
SU 31 T a standard one
SU 31 M an aircraftt with an ejection seat and tanks built in wings
SU 31 U an aircraft with the retractable undercarriage
Technical characteristics:
Normal weght (kg)
850
Empty (kg)
760
Engine
14
Max power (h.p.)
360
Vmax horizontal (km/h)
330
Landing speed (km/h)
115
Climb rate, m/
24
Max rotation speed
7
Overload range
+12 / -10
Flight range (km)
1200

ENSTROM 480 

The Enstrom 480 was developed to provide a more affordable, but equally competent, light turbine helicopter to a market historically dominated by the Bell 206B Jet Ranger and MD500.

The 480 has now been certified in 13 countries and has already been operated in 15 countries. With over 50 aircraft in the field now, the 480 is proving to be a popular choice for a wide range of applications, including personal transport, flight instruction, law enforcement, power line patrol, executive transport (charter), electronic news gathering, pipeline patrol, aerial photography, sightseeing, and cargo/passenger delivery.

The ability to quickly change seating configurations in the 480's flexible cabin allows an operator to optimize the aircraft for each day's specific mission. The 480's large, high inertia main rotor system provides an unusually stable and comfortable ride. Tail rotor authority is the best in its class. The conventional flight controls are responsive but not overly sensitive. The aircraft is very forgiving, making it an excellent choice for lower time pilots or for demanding missions. A current design, with excellent performance and an open flexible cabin, makes the 480 a very desirable helicopter.

The Enstrom 480 quickly established itself as the best value for money aircraft in the light turbine class.
Technical characteristics:
Power Plant
(1) Allison 250C-20W
Main rotor diameter, m.
9,75
Fuselage length, m.
8,93
Empty weight, kg.
708
Take-off weight, kg.
1225
Max speed, km/h
263
Cruise speed, km/h
213
Flight range, km
611
Occupants
1 pilot + 3 passengers

ROBINSON R44

The Robinson R44 is a fast, high-performance four place helicopter designed to meet the rigorous demands of today's competitive market. The R44 incorporates the same rugged reliability, easy maintenance and low operating costs found in Robinson's two-seat R22, but with higher performance, expanded comfort, and handling characteristics similar to larger helicopters.

The R44's modern design and excellent performance make it an ideal choice for a variety of private, business, and utility applications including personal and business transport, air taxi, sight-seeing, photography, radio and television news reporting, construction site support, and law enforcement.
Technical characteristics:
Power Plant
(1) Lycoming O-540
Main rotor diameter, m.
10,06
Empty weight, kg.
635
Take-off weight, kg.
1088
Max speed, km/h
225
Cruise speed, km/h
210
Flight range, km
610
Occupants
1 pilot + 3 passengers
 
Contact telephones: (095) 104-18-63 , club tel: 8 (910) 446-22-19, (095) 552-98-67 ,
office tel:
737-05-74, e-mail: club@stealth21.ru, site: www.aerobaticclub.net
english version