AMP · 7% of the exam
Turbine Engines practice questions
10 free Turbine Engines questions for the Aviation Mechanic Powerplant (AMP) Knowledge Test exam, each with the correct answer and an explanation for every option.
What this domain covers
Gas turbine engine theory, components and operation.
- Exam weight
- 7%
- On a real exam
- ≈ 7 questions
- In our bank
- 45 questions
Topics that come up most
- Turbine engine types
- Compressor, combustor and turbine sections
- Thrust and performance factors
- Starting and operation
- Inspection basics
How to study it
Compare engine types side by side; questions ask which type has which characteristic.
Sample Turbine Engines questions
Try each one before opening the answer. Original questions written to the official exam objectives.
Question 1
During a ground start of a turbine engine, light-off is normal and EGT stays within limits. However, rotor speed levels off well below idle and does not accelerate any further. What condition is this?
- AA hung start
- BA hot start
- CA no-light start
- DA wet start
Show answer and explanation
Answer: A) A hung start
A hung start has a normal light-off, but RPM hangs below idle and does not accelerate. Insufficient starter power is a common cause, and the engine should be shut down.
- ACorrect. A hung start is a normal light-off where RPM stays at a low value and does not rise to normal idle. A common cause is too little starter power. The engine should be shut down.
- BIncorrect. In a hot start, the engine turns normally but exhaust temperature goes over the prescribed limit. Here EGT stayed within limits.
- CIncorrect. In a no-light (false) start, the fuel-air mixture does not ignite. The scenario says light-off was normal.
- DIncorrect. A wet start is fuel entering the engine without ignition, which can leave fuel pooled in the combustor or tailpipe. Here the engine lit off normally.
Question 2
What is the main reason for washing a turbine engine compressor in the field?
- ATo lower turbine inlet temperature by cooling the hot section after shutdown
- BTo remove blade deposits that reduce compressor efficiency and raise EGT
- CTo remove carbon buildup from the fuel nozzles and combustion liners
- DTo clean the blades so cracks can be found during a borescope inspection
Show answer and explanation
Answer: B) To remove blade deposits that reduce compressor efficiency and raise EGT
Field washing removes dirt and salt deposits from the compressor blades. This restores compressor efficiency and airflow, which lowers EGT and brings back lost performance.
- AIncorrect. Compressor washing is not a cooling procedure. Lower EGT after a wash comes from better compressor efficiency, not from cooling hot-section parts.
- BCorrect. Dirt and salt deposits on compressor blades reduce airflow and efficiency, so the engine runs hotter to make the same power. Washing removes these deposits and restores performance.
- CIncorrect. Carbon deposits form in the hot section. A compressor wash is aimed at the compressor blades, not the fuel nozzles or combustor.
- DIncorrect. Cracks are found by inspection methods such as borescope inspection. Washing the compressor is done to recover performance, not to find cracks.
Question 3
A turbine engine's speed is controlled mainly by:
- AFuel flow
- BA carburetor throttle plate
- CPropeller blade angle only
- DMagneto timing
Show answer and explanation
Answer: A) Fuel flow
- ACorrect. There's no throttle valve restricting the air.
- BIncorrect. That's a piston engine.
- CIncorrect. Prop pitch affects load, not the gas generator directly.
- DIncorrect. Turbines don't use magnetos for control.
Question 4
What is a turbine engine flameout?
- ALoss of combustion
- BNormal engine shutdown
- CA tailpipe fire on start
- DAn afterburner light-off
Show answer and explanation
Answer: A) Loss of combustion
- ACorrect. Combustion stops while fuel or air supply is disrupted.
- BIncorrect. A flameout is unintended.
- CIncorrect. That is a torching or tailpipe fire.
- DIncorrect. This is different.
Question 5
In turbine maintenance, FOD refers to:
- AFuel oil dilution
- BIngested object damage
- CFan overspeed detection
- DFlight operations data
Show answer and explanation
Answer: B) Ingested object damage
- AIncorrect. This is not FOD.
- BCorrect. Foreign object damage comes from debris drawn into the engine.
- CIncorrect. This is not FOD.
- DIncorrect. This is not FOD.
Question 6
What does trimming a turbine engine involve?
- ABlending nicks out of compressor blades to restore smooth airflow
- BRigging the thrust reverser actuators to their correct deployed travel
- CAdjusting the fuel control unit so the engine meets its dataplate performance
- DRecalibrating the EGT indicating system to match a test thermocouple
Show answer and explanation
Answer: C) Adjusting the fuel control unit so the engine meets its dataplate performance
Trimming adjusts the fuel control unit so the engine produces rated thrust. The technician uses the engine dataplate values (such as EPR at a given RPM) as the target.
- AIncorrect. Blending is a repair for blade damage. It does not set the engine's power output.
- BIncorrect. Reverser rigging is an exhaust and reverser system adjustment. It is not engine trimming.
- CCorrect. Trimming adjusts the fuel control unit so the engine produces its rated thrust, such as the dataplate EPR at a specified RPM.
- DIncorrect. Checking the EGT indicating system makes sure the instruments read accurately. It does not adjust fuel scheduling or engine output.
Question 7
A turbine engine produces thrust mainly by:
- APushing against the air behind the aircraft
- BAccelerating a mass of air rearward
- CBurning fuel without moving air
- DSpinning the compressor only
Show answer and explanation
Answer: B) Accelerating a mass of air rearward
- AIncorrect. Thrust comes from momentum change.
- BCorrect. Newton's third law gives the forward reaction.
- CIncorrect. Airflow is essential.
- DIncorrect. The compressor alone doesn't make thrust.
Question 8
Shrouded tips on turbine blades mainly:
- AIncrease blade weight to slow the rotor
- BRaise the turbine inlet temperature
- CReduce vibration and tip leakage
- DCool the combustor
Show answer and explanation
Answer: C) Reduce vibration and tip leakage
- AIncorrect. That isn't the purpose.
- BIncorrect. They don't affect it directly.
- CCorrect. Shrouds form a ring that dampens blades.
- DIncorrect. That isn't the purpose.
Question 9
A turbofan engine is run at the same takeoff power setting on a hot day and on a cold day at the same field elevation. Compared with the cold day, how does the hot day affect available thrust?
- AThrust increases because hotter inlet air expands more in the combustor
- BThrust decreases because less dense air reduces the mass airflow
- CThrust is unchanged because the fuel control holds a constant rpm
- DThrust increases because the compressor needs less work for warm air
Show answer and explanation
Answer: B) Thrust decreases because less dense air reduces the mass airflow
Turbine thrust depends on the mass of air the engine accelerates. Hot air is less dense, so mass airflow and thrust fall as outside air temperature rises.
- AIncorrect. Thrust depends mainly on the mass of air accelerated. Hot inlet air is less dense, so the engine moves less mass, and any extra expansion does not make up for that loss.
- BCorrect. As temperature rises, air density falls, so less air mass enters the engine and thrust drops. Cold, dense air raises mass airflow and thrust.
- CIncorrect. Holding rpm constant does not hold mass airflow constant. At the same rpm, less dense air means less mass flow and therefore less thrust.
- DIncorrect. Compressing warmer air takes more work for a given pressure rise, not less. Warm air also lowers mass flow, so thrust goes down.
Question 10
Compressor blades are commonly attached to the disk with:
- AAdhesive bonding only
- BRivets through the airfoil
- CDovetail roots
- DSpot welds to the casing
Show answer and explanation
Answer: C) Dovetail roots
- AIncorrect. Mechanical roots are used.
- BIncorrect. That would weaken the blade.
- CCorrect. Turbine blades often use fir-tree roots.
- DIncorrect. Blades mount on the disk.
Turbine Engines: FAQs
How much of the AMP exam is Turbine Engines?
Turbine Engines is 7% of the AMP exam by the official exam guide's weighting, which on a 100-question form works out to roughly 7 questions. The real exam's exact split varies by form.
What does the Turbine Engines domain cover?
Gas turbine engine theory, components and operation.
How should I study Turbine Engines for AMP?
Compare engine types side by side; questions ask which type has which characteristic.
Where can I practise more Turbine Engines questions?
This page has 10 free Turbine Engines questions with answers. The ExamWize AMP question bank has 45 questions in this domain. Every practice exam result breaks your score down by domain, and Review Mode re-drills the questions you missed.
Other AMP topics
- Reciprocating Engines12% of the exam
- Engine Inspection7% of the exam
- Engine Instrument Systems7% of the exam
- Engine Fire Protection Systems7% of the exam
- Engine Electrical Systems11% of the exam
- Engine Lubrication Systems7% of the exam
- Ignition and Starting Systems7% of the exam
- Engine Fuel and Fuel Metering Systems7% of the exam
- Reciprocating Engine Induction and Cooling Systems7% of the exam
- Turbine Engine Air Systems7% of the exam
- Engine Exhaust and Reverser Systems7% of the exam
- Propellers7% of the exam
Also: 15 free questions across all topics, the AMP cheat sheet and the study guide.
Get Turbine Engines exam-ready
The full AMP bank has 45 Turbine Engines questions. Timed practice exams match the real exam's length and domain weights, every result shows your score per domain, and Review Mode re-drills the questions you missed.
Not affiliated with FAA; questions are original, written from the official exam outline, and never copied from the real exam.