AMT Cheat Sheet 2026

The 30 highest-yield AMT facts, distilled from real exam questions. Print it, save it as a PDF, or study it here — free, no sign-up.

100 questions
180 min time limit
70% to pass
  1. Why is it important to monitor exhaust gas temperature (EGT)? To optimize fuel/air mixture
  2. Fretting corrosion is most likely to be found in which of the following locations on an aircraft? Between two aluminum sheets in a lap joint under a loose rivet.
  3. Which term describes a mandatory correction issued by the FAA for an unsafe condition? Airworthiness Directive
  4. A technician must calculate the center of gravity of an aircraft. What is the correct formula to use? Total Moment / Total Weight
  5. Which aircraft document lists required inspections and maintenance intervals? Maintenance manual
  6. While a gas turbine engine's ultimate purpose is to produce thrust, what is the primary role of the turbine section within the engine? To extract energy from the hot gases to drive the compressor and accessories.
  7. In a reciprocating engine's continuous-flow fuel injection system, what is the primary function of the air bleed incorporated into the fuel discharge nozzle? To assist in atomizing the fuel and improve vaporization at lower power settings.
  8. A modern commercial airliner is typically powered by high-bypass turbofan engines. What is the main benefit of having a high bypass ratio? Improved fuel efficiency and reduced engine noise.
  9. Which material is most commonly used in modern aircraft skin construction? Aluminum alloy
  10. What is the primary thermodynamic cycle upon which all gas turbine engines operate? The Brayton cycle
  11. The production of thrust in a turbine engine is best explained by which physical principle? Newton's Third Law of Motion
  12. In sheet metal layout for riveting, what is the term for the distance measured from the center of a rivet to the nearest edge of the metal? Edge distance
  13. What flight control surface is primarily responsible for pitch control? Elevator
  14. During landing gear retraction, the typical sequence of gear door operation is: Doors open before gear retraction begins, then close after the gear is fully retracted
  15. The purpose of a downlock in a retractable landing gear system is to: Hold the landing gear in the fully extended position during flight
  16. What is the primary effect of loading an aircraft with a center of gravity (CG) at the forward limit? Increased stability and higher stall speed.
  17. During takeoff in an aircraft with a constant-speed propeller, the propeller blade pitch is set to: A low pitch, high RPM position to allow the engine to develop maximum power.
  18. Why are magnetos used in aircraft ignition systems? To provide spark without external power
  19. In a magneto ignition system, what is the specific purpose of an impulse coupling? To produce a hot, retarded spark for engine starting.
  20. What type of engine is most commonly found in small general aviation aircraft? Reciprocating engine
  21. The design principle that ensures a structure can withstand specific loads without permanent deformation is known as its: Elastic limit
  22. What is the primary goal of a Safety Management System (SMS) in aviation? Managing safety risks proactively
  23. What is the purpose of an anti-skid system in aircraft? Prevent wheel lock-up
  24. When servicing an oleo-pneumatic shock strut, the correct extension of the inner cylinder piston is: Specified in the aircraft maintenance manual for a given loading condition
  25. A power-boost brake system uses hydraulic power to: Amplify pilot pedal input forces for more effective braking with less effort
  26. Which of the following tool combinations is used to properly install a solid shank rivet by forming the shop head? A rivet gun and a bucking bar.
  27. In a semi-monocoque fuselage, what is the primary function of longitudinal members such as longerons and stringers? To absorb and transmit bending, tensile, and compressive stresses.
  28. In a dual-spool, axial-flow compressor, how is the low-pressure compressor (N1) typically connected to its corresponding turbine? Via a concentric shaft that passes through the hollow high-pressure (N2) shaft.
  29. Which of the following statements is true regarding Airworthiness Directives (ADs)? Compliance is mandatory for all applicable aircraft.
  30. What is the primary function of an aircraft's hydraulic system? Power flight control systems
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