These systems are reliant on some power source, meaning they rely upon a powerplant not just to move the airplane, but run the systems
Finally, there are a variety of support systems which for comfort, regulatory, or human physiological reasons, exist to support flight operations, especially those considered high-performance
Understanding the aircraft systems is critical to its safe operation and proper maintenance
Fundamental Aircraft Systems:
Most aircraft have a standardized set of systems which diverge depending on their designed purpose [Figure 1]
Generally speaking, this starts with Pitot-static systems, the manipulation of air pressure which enable avionic and instrument function
The aircraft's induction system is responsible for the vacuum system, which powers typically gyroscopic systems
Individual aircraft systems will vary between vacuum, gyroscopic, or electrically driven(discussed below); however, a combination of the previously mentioned systems are necessary to power many primary flight instruments, including the Airspeed Indicator, Altimeter, and Vertical Speed Indicator
Pilots must physically manipulate an aircraft's state to meet the needs of a given phase of flight
Rudimentary control of the aircraft requires flight control systems
Complex Systems:
Certain aircraft operations demand increasingly complex aircraft, and therefore systems
Pressurization systems allow for high-performance aircraft to operate at high altitudes, taking advantage of atmospheric conditions that enhance aircraft performance
Supplemental oxygen systems become necessary to meet regulatory and human performance requirements associated with operating at higher altitudes
Weather poses a threat to the aircraft, warranting icing mitigation systems to penetrate freezing layers found at higher altitudes and especially during winter months
AOPA A&P Podcasts:
The AOPA publishes A&P Podcasts monthly, answering technical questions provided by the aviation community
Conclusion:
Understanding how systems operate on their own is the first step in understanding how they integrate
For example, landing gear may be electronically operated, but hudraulically actuated