Study Materials/Aircraft General Knowledge
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Aircraft General Knowledge

Aircraft systems, structures, engines, and flight instruments.

Overview

Aircraft General Knowledge covers the major systems and components of an aircraft. Pilots must understand how engines work, how electrical and hydraulic systems function, how flight instruments operate, and how to recognize and respond to system failures. This knowledge is critical for safe operation and troubleshooting.

Key Topics

1. Piston Engines

Four-stroke cycle (intake, compression, power, exhaust), carburetor vs. fuel injection, ignition systems (dual magnetos), oil systems, cooling systems, and propeller operation. Understanding engine limitations like CHT and oil temperature/pressure ranges.

2. Flight Instruments

Pitot-static instruments (airspeed indicator, altimeter, vertical speed indicator) and gyroscopic instruments (attitude indicator, heading indicator, turn coordinator). Understanding instrument errors and the vacuum/pressure system.

3. Electrical Systems

Aircraft electrical system components: alternator/generator, battery, bus bar, circuit breakers, and avionics. Understanding load shedding procedures and electrical failure protocols.

4. Fuel Systems

Fuel grades (100LL is blue), fuel system components (tanks, selector, strainer, pump), fuel management procedures, contamination checking (water, debris), and calculating fuel requirements for flight planning.

5. Landing Gear and Brakes

Fixed vs. retractable gear, brake systems (hydraulic disc brakes), tire care and inspection, shimmy dampers, and emergency extension procedures for retractable gear aircraft.

6. Propeller Systems

Fixed-pitch vs. constant-speed propellers, blade angle concepts, propeller governor operation, and the relationship between RPM, manifold pressure, and power output.

Key Terms & Definitions

Manifold Pressure
The pressure of the fuel/air mixture in the engine intake manifold, measured in inches of mercury (inHg)
Pitot-Static System
System providing ram air pressure and static pressure to the airspeed indicator, altimeter, and VSI
Magneto
A self-contained electrical generator providing ignition spark, independent of the aircraft battery
EGT
Exhaust Gas Temperature - used for mixture leaning and engine monitoring
Vacuum System
Engine-driven pump providing suction to power gyroscopic instruments (attitude and heading indicators)

Exam Tips

  • Tip 1:Know which instruments are pitot-static vs. gyroscopic and their power sources
  • Tip 2:Understand the effects of carburetor icing and when to apply carburetor heat
  • Tip 3:Learn the color coding for fuel grades (100LL = blue, Jet A = clear/straw)
  • Tip 4:Know the standard instrument scan pattern and what each instrument indicates
  • Tip 5:Understand how the altimeter works and the effects of temperature/pressure variations on altitude readings

Recommended References

Pilot's Handbook of Aeronautical Knowledge Ch. 7-8

FAA handbook covering aircraft systems and flight instruments

Aircraft Systems for Pilots

Comprehensive guide to understanding aircraft powerplant and systems

EASA Aircraft General Knowledge

European study material for AGK examination

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