Wheels

Auxiliary mechanical energy source on the vehicle that is not intended to propel the vehicle.

Designed to provide takeoff, landing, rolling out and towing of an aircraft on both concrete and unpaved airfields. landing gear includes chassis, flaps and a braking landing parachute system.

On aircrafts, the air system is used to seal cabin lights and actuate various aggregates and their release mechanisms for braking devices.

Altitude system is designed to create normal comfortable conditions for passengers and crew during the flight of an aircraft at all speeds and altitudes of the flight.

Hydraulic system is designed to control mechanisms and systems that deal with flight safety.

Designed to protect crew and passengers from oxygen deficiency, as well as from their exposure to combustion products in case of fire

Designed to maintain air pressure and temperature in the pressurized cabin of an aircraft at a level that provides normal vital activity of the crew and passengers

Oil system is used to store the oil reserve required for operation of the main engines and the APU engine, to supply oil to the engines for lubrication and cooling, and to pump and cool oil.

On-board radio electronic equipment providing steering, navigation and guidance of an aircraft, set on electrical, electromechanical and electronic devices.

Pneumatic systems are designed to provide pneumatic power to various subsystems of takeoff and landing control mechanization, crew life support, creating conditions for the operation of equipment that need independent on-board power supply.

Power package instruments and control systems gauges. tachometers. thermometers. gas-turbine control systems. Independent flight instrumentation: horizon indicators, heading devices. AAAOS. Aerometric instruments and systems, barometric altimeters, airspeed and Mach number indicators, variometers, air pressure receivers, centralized air signal systems

Ice protection system is designed to protect an aircraft from icing

Fire protection equipment is designed to signal and extinguish a fire in the engine compartment. Includes fire alarm system and fire extinguishing system

Designed for two-way communication between the crew of an aircraft and ground radios and other aircrafts, as well as for internal communication between crew members during flights and on the ground.

On-board avionics equipment is a category of on-board equipment of an aircraft that uses the energy of radio waves in its operation.

Automatic flight control system (AFCS) is designed to provide automatic and director control in the pitch and roll channels, as well as automatic engine thrust control.

A set of on-board devices providing control of aircraft systems and units, as well as control of the aircraft as a whole is called an aircraft control system.

An aircraft power unit for placing fuel, producing it in a particular order, delivering fuel to consumers, and performing auxiliary functions.

Technical device installed on pipelines, equipment and vessels and designed to control (close, open, regulate, distribute, mix, separate) working media flows (liquid, gas, gas-liquid, pulp, steam, plasma, powder, suspension, etc.) by changing the passage section.

Aircrafts up to 495 kg

Aircrafts from 495 kg to 5700 kg.