The Zenair CH601 is a two-seat all-metal low-wing aircraft with a simple design. However, its performance exceeds all expectations. It is really a robust aircraft with a maximum speed of 240 km / h and multiples of overload + -6.8G, which would not be ashamed of any acrobatic.

Producer: The American company Zenith Aircraft Company, which is famous worldwide for the production of all-metal sports and ultralight aircraft. Its founder is Chris Heintz, who designed his first aircraft in 1969. Since the 1980s, his company has been producing ready-made aircraft as well as kits and plans for the builders themselves.

Basic parameters:

Dimensions

• Number of seats: 2
  
• Wingspan: 8.23 m
• Length: 6,10 m
  
• Height: 1.98 m
• Wing area: 12.50 m2

Performances

• Number of engines: Single-engine
  
• Engine type: Piston
  
• Fuel: MOGAS / Natural 95
  
• Stall speed (with flaps): 38 knots (71 km / h)
  
• Speed V (NE): 139 knots (257 km / h)
  
• Engine type: Rotax 912 UL
  
• Cruising speed: 114 knots (211 km / h)
  
• Climb: 5.1 m / s
  
• Range: 1158 km

• Ceiling: 3700 m
• Empty weight: 250 kg
  
• Maximum take-off weight: 480 kg
• Payload: 230 kg
  

 Cessna 152is an American aircraft used primarily for flight training and personal use. Cessna 152 is already out of production, but there are still a large number of aircraft. With an airplane life span of more than 15,000 hours and more than 60,000 landings, it is still regularly used for flight training.

The first Cessna 152 aircraft left the factory gate in 1977. A total of over 7,500 of these machines were built. It differs from the previous Cessna 150 mainly by a slightly wider cab, a more suitable Lycoming O-235 engine and flaps with maximum deflection reduced to 30 degrees.

Manufacturer: Cessna Aircraft Company

Basic parameters:

Dimensions

• Number of seats: 2
  
• Wingspan: 10,20 m
  
• Length: 7.30 m
  
• Height: 2.60 m
  
• Wing area: 14,90 m2

• Number of engines: Single-engine
  
• Engine type: Piston
• Fuel: AVGAS
• Consumption: 23l / hour
  
• Stall speed (with flaps): 43 knots (79 km / h)
  
• Speed: 148 knots (275 km / h)
  
• Engine type: Lycoming O-235-L2C
  
• Cruising speed: 107 knots (198 km / h)
  
• Climb: 3.6 m / s
  
• Range: 768 km
  
• Ceiling: 448 km

Weights 

• Empty mass: 490 kg
  
• MTOW: 757 kg
• Payload: 267 kg
  

Cessna 172is a light single-engine upper-wing four-seat aircraft, which since 1956 manufactured by Cessna Aircraft Company. It was developed from the Model 170, which first flew in 1947. Its distinguishing features are: a larger fuselage than the earlier model 140 and a more powerful engine.

Manufacturer: Cessna Aircraft Company

Basic parameters:

Dimensions 

• Number of seats: 4
• Wingspan: 11 m
• Lenght: 8,28 m
• Height: 2,72 m
• Wing area: 16,2 m2

Performances 

• Number of engines: Single-engine
• Engine type: Piston
• Fuel: AVGAS
• Stall speed (with flaps) : 47 uzlů
• Speed: 163 uzlů
• Engine type: Lycoming IO-360-L2A
• Cruising speed: : 122 uzlů
• Climb: 3,66 m/s
• Range: 1289 km

Weights 

• Empty mass: 767 kg
• MTOW: 1111 kg
• Payload: 344 kg

An-2 aircraft was created in OKB Oleg Antonov at Novosibirsk Aviation Plant V. P. Ckalova. The first prototypeAntonova flew in Novosibirsk 31st August 1947 with the designation SChA-1 powered seven-cylinder engine Aš-21 600 kW. During the tests, completed in July 1948, was installed power unit AŠ-61IR 734 kW. It was originally developed as an agricultural aircraft, but due to its capabilities it was used in various fields of activity, including military (transport and airborne). Its advantages include a short take-off and the possibility of operating from unpaved surfaces. The aircraft has been mass-produced in Kiev since 1948, in PZL Mielec in Poland since 1959 and in China in Charbin. They were also imported to Czechoslovakia, where they served in both the civilian and military sectors. They are known to us under the nickname "Andula" and we can see them flying in the clubs today.

Basic parameters:

Dimensions 

• Number of seats: 14
• Wingspan: 18,18 m
• Lenght: 12,74 m
• Height: 4 m
• Wing area: 71,6 m2

Performances 

• Number of engines: Jednomotorové
• Engine type: Pístové
• Fuel: AVGAS
• Engine type: Švecov AŠ-62IR
• Travel speed: 100 uzlů (185 km/h)
• Maximum speed (horizon): 139 knots (258 km / h)
• Fuel consumption: 200l / hour
• Climb: 3.5 m / s
• Range: 900 km 
  
• Available: 4400 m

Weights 

• Empty weight: 3450 kg
• MTOW: 5500 kg
• Payload: 2050 kg