AMT Study Guide 2026

Everything you need to pass the AMT exam in one place: the exam format, every topic to study, real practice questions with explanations, flashcards, and full-length practice tests. Free, no sign-up needed.

📋 AMT Exam Format at a Glance

100
Questions
180 min
Time Limit
70%
Passing Score

📚 AMT Topics to Study (24)

✍️ Sample AMT Questions & Answers

1. What is the primary reason for using a dual ignition system on a certified aircraft reciprocating engine?
To provide redundancy for safety and improve combustion efficiency for better performance.

A dual ignition system uses two separate magnetos, harnesses, and spark plugs for each cylinder. This provides redundancy, meaning if one entire system fails, the engine can still operate on the other. Additionally, having two spark plugs ignites the fuel-air mixture from two points, leading to a faster, more complete combustion process, which improves engine performance and power output.

2. What is the purpose of safety wiring in aviation maintenance?
To prevent fastener loosening

Safety wiring is a mechanical locking device used to secure fasteners, such as nuts, bolts, and turnbuckles, in critical aircraft applications. It ensures that these components remain tight and do not vibrate loose during operation, thereby preventing potential system failures and maintaining structural integrity. This simple yet effective method is a cornerstone of aviation safety.

3. A propeller is equipped with electrically heated de-ice boots on the leading edges of the blades. How does this system typically operate to remove ice?
The boots are heated in a repeating cycle, melting the layer of ice closest to the blade so it can be thrown off by centrifugal force.

Propeller de-ice systems work by cyclically heating the elements in the boots. This heating is not meant to evaporate all the ice, but rather to melt the thin layer adhering to the blade surface. Once this bond is broken, the centrifugal force of the rotating propeller slings the remaining ice off the blades.

4. According to 14 CFR Part 43.9, which of the following is required to be included in a maintenance record entry after performing a repair?
The signature, certificate number, and kind of certificate held by the person approving the work.

14 CFR 43.9 explicitly requires that a maintenance record entry contain: a description of the work, the date of completion, and if the work was performed satisfactorily, the signature, certificate number, and kind of certificate held by the person approving the work for return to service. Total time-in-service is required for inspection entries under 43.11, not general maintenance entries under 43.9.

5. What is the primary reason for feathering the propeller of a failed engine on a multi-engine aircraft?
To align the blades with the relative wind to minimize aerodynamic drag.

Feathering involves turning the propeller blades to be nearly parallel with the direction of flight. This presents the smallest profile to the oncoming air, which significantly reduces the drag produced by the windmilling propeller of a failed engine, improving the aircraft's single-engine performance.

6. Which of the following describes the primary function of the diffuser section in a gas turbine engine?
To increase the pressure and reduce the velocity of the air leaving the compressor.

The diffuser is a divergent duct located between the compressor section and the combustion section. Its purpose is to slow down the high-velocity air from the compressor and increase its pressure before it enters the combustion chambers, ensuring stable combustion.

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