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FAA Aviation Mechanic Powerplant (AMP)

First published: September 2, 2026Last verified: September 2, 2026Reviewed by the CertQuestUSA team
TL;DR

FAA Aviation Mechanic Powerplant (AMP): a 300-question practice bank for the real FAA Aviation Certification standard, 4 full papers of 100 questions each with no repeats, every question citing the real regulation it comes from.

Where these questions come from

Every question in this bank cites a real source -- primarily FAA-AMT-POWERPLANT-V2 -- Chapter (73%) and FAA-AMT-POWERPLANT-V1 -- Chapter (25%) of this exam's citations.

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4
full papers, no repeats
100
questions per paper
300
questions in the bank
What this exam covers
5 real sample questions
An EPR system senses 15.0 psia at the inlet and 27.0 psia at turbine discharge. What EPR should it display before correction factors?
A. 0.56
B. 1.80
C. 12.0
D. 42.0
Source: FAA-AMT-POWERPLANT-V2 -- Chapter 10, Engine Pressure Ratio Indicating Systems
What is the purpose of generator overcurrent protection?
A. Limit or disconnect a source when current exceeds safe values
B. Increase wire temperature to improve conductivity
C. Keep a fault energized until it becomes visible
D. Replace voltage regulation under all conditions
Source: FAA-AMT-POWERPLANT-V2 -- Chapter 11, Generator Control and Protective Devices
A 28-volt DC motor draws 14 amperes. Approximately how much electrical power does it consume?
A. 2 W
B. 392 W
C. 42 W
D. 1,960 W
Source: FAA-AMT-POWERPLANT-V2 -- Chapter 11, DC Electrical Power and Load Analysis
Which statement best describes brake mean effective pressure?
A. It is actual pressure measured continuously at the spark plug
B. It equals atmospheric pressure minus manifold pressure
C. It is the maximum instantaneous combustion pressure
D. Average pressure equivalent to the measured brake work
Source: FAA-AMT-POWERPLANT-V1 -- Chapter 1, Engine Performance—Mean Effective Pressure
Why is excessive turbine blade-tip clearance undesirable?
A. It guarantees compressor surge at every power setting
B. Prevent turbine components from expanding into their designed hot-running clearances
C. It increases blade length automatically
D. More gas bypasses the blade tips and does no work
Source: FAA-AMT-POWERPLANT-V1 -- Chapter 2, Turbine Construction—Blade Tip Clearance
Real-world data for this exam
Aircraft Mechanics and Service Technicians: real median wageMay 2025$79,870/yr
Related reading
AMG vs. AMP vs. AMA: What's the Difference Between the FAA Mechanic Knowledge Tests?How Many Questions Are on the FAA Aviation Mechanic General (AMG) Test?

Frequently asked questions

How many questions are on the CertQuestUSA FAA Aviation Mechanic Powerplant (AMP) practice test?
300 questions total, split into 4 full papers of 100 each with no repeats across papers.
What topics does the FAA Aviation Mechanic Powerplant (AMP) test cover?
13 domains, with the heaviest weight on Engine Electrical Systems (12%), Reciprocating Engines (12%), and Engine Fuel and Fuel Metering Systems (8%).
Where do CertQuestUSA's FAA Aviation Mechanic Powerplant (AMP) questions come from?
Primarily FAA-AMT-POWERPLANT-V2 -- Chapter (73%) and FAA-AMT-POWERPLANT-V1 -- Chapter (25%) of this bank's citations -- computed directly from this exam's own question sources, not a generic description.
Is there a free diagnostic for FAA Aviation Mechanic Powerplant (AMP)?
Yes -- 10 real questions across the exam's domains, no sign-up required, with a domain-by-domain breakdown at the end.
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