Aircraft Systems

Aircraft Systems Overview

• The primary purpose of the aircraft electrical system is to provide power for avionics, lighting, and other essential electrical loads, ensuring operational functionality.

Pitot-Static System

• The pitot-static system measures airspeed, altitude, and vertical speed through pressure differences, utilizing a pitot tube and static ports to gather data for flight instruments.

Carburetor Heat Control

• Carburetor heat control prevents carburetor icing in aircraft with carbureted engines by directing heated air into the carburetor, maintaining optimal fuel-air mixture conditions.

Aircraft Fuel System Functions

• A primary function of the aircraft fuel system includes storing fuel, delivering it to the engine, and managing fuel flow, ensuring efficient power generation.

Hydraulic System Purpose

• The aircraft's hydraulic system provides the necessary force to operate flight control surfaces, landing gear, and brakes by leveraging hydraulic pressure for enhanced maneuverability and safety.

Environmental Control System

• The primary purpose of the aircraft's environmental control system is to regulate cabin temperature, pressure, and air quality, ensuring passenger comfort and operational safety during flight.