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AMA · 6% of the exam

Rotorcraft Fundamentals practice questions

10 free Rotorcraft Fundamentals questions for the Aviation Mechanic Airframe (AMA) Knowledge Test exam, each with the correct answer and an explanation for every option.

What this domain covers

Helicopter fundamentals: aerodynamics, controls and rotor systems.

Exam weight
6%
On a real exam
≈ 6 questions
In our bank
36 questions

Topics that come up most

  • Rotor systems
  • Helicopter controls
  • Vibration types and causes
  • Blade tracking
  • Transmissions

How to study it

Learn vibration types and their likely causes; troubleshooting questions rely on them.

Sample Rotorcraft Fundamentals questions

Try each one before opening the answer. Original questions written to the official exam objectives.

  1. Question 1

    What is mast bumping on a teetering-rotor helicopter?

    • ATail rotor contact with the ground
    • BNormal engine vibration transmitted through the mast
    • CThe hub striking the mast from excessive flapping
    • DA transmission oil leak
    Show answer and explanation

    Answer: C) The hub striking the mast from excessive flapping

    • AIncorrect. That is a tail strike.
    • BIncorrect. It is a dangerous condition.
    • CCorrect. It can cause catastrophic failure.
    • DIncorrect. It is a structural contact.
  2. Question 2

    In a fully articulated rotor, what does the flapping hinge allow each blade to do?

    • AChange pitch
    • BRise and fall independently
    • CMove fore and aft in the rotor plane
    • DFold for storage only
    Show answer and explanation

    Answer: B) Rise and fall independently

    • AIncorrect. The feathering hinge does that.
    • BCorrect. Flapping helps balance lift across the disc.
    • CIncorrect. That is the lead-lag hinge.
    • DIncorrect. Flapping is a flight motion.
  3. Question 3

    What does the helicopter collective control do?

    • AControls the tail rotor
    • BTilts the rotor disc
    • CChanges all blade pitch
    • DSteers the wheels
    Show answer and explanation

    Answer: C) Changes all blade pitch

    • AIncorrect. That is the antitorque pedals.
    • BIncorrect. That is the cyclic.
    • CCorrect. The collective changes main rotor blade pitch collectively, controlling lift.
    • DIncorrect. This is unrelated.
  4. Question 4

    In forward flight, the advancing side of a helicopter's main rotor disk meets a higher relative wind than the retreating side. Which blade motion mainly compensates for the resulting dissymmetry of lift?

    • ABlade lead and lag about the drag hinge
    • BBlade flapping about the flapping hinge
    • CUniform pitch change applied through the collective
    • DVariable thrust change of the tail rotor blades
    Show answer and explanation

    Answer: B) Blade flapping about the flapping hinge

    Dissymmetry of lift is mainly compensated by blade flapping. The advancing blade flaps up (lower angle of attack) and the retreating blade flaps down (higher angle of attack), and cyclic feathering adds further compensation.

    • AIncorrect. Lead-lag motion about the drag (vertical) hinge lets the blades speed up and slow down in their plane of rotation, which relieves stresses from Coriolis effect. It does not change blade angle of attack to equalize lift.
    • BCorrect. The advancing blade flaps up, which lowers its angle of attack and its lift. The retreating blade flaps down, which raises its angle of attack and its lift. This evens out lift across the disk, and cyclic feathering (less pitch on the advancing blade, more on the retreating blade) adds further compensation.
    • CIncorrect. Collective pitch changes the pitch of all blades by the same amount at the same time. It cannot correct a lift difference between the advancing and retreating sides.
    • DIncorrect. Tail rotor thrust counteracts main rotor torque and gives yaw control. It does not balance lift between the two halves of the main rotor disk.
  5. Question 5

    What is dynamic rollover in a helicopter?

    • ASpinning in a hover
    • BRolling over a skid
    • CA normal landing roll
    • DA rotor overspeed
    Show answer and explanation

    Answer: B) Rolling over a skid

    • AIncorrect. That is loss of tail rotor effectiveness.
    • BCorrect. The helicopter rolls about a skid or wheel in contact with the ground.
    • CIncorrect. It is a hazard.
    • DIncorrect. This is different.
  6. Question 6

    Many helicopters use a dual tachometer with two needles on one dial. What do the two needles indicate?

    • AMain rotor rpm on one needle and tail rotor rpm on the other
    • BEngine rpm on one needle and main rotor rpm on the other
    • CPresent engine rpm on one needle and the peak rpm reached in flight on the other
    • DEngine rpm on both needles, fed from two separate senders for redundancy
    Show answer and explanation

    Answer: B) Engine rpm on one needle and main rotor rpm on the other

    A helicopter dual tachometer shows engine rpm and rotor rpm on one dial. The needles are 'married' when the engine drives the rotor and 'split' when the freewheeling unit disengages.

    • AIncorrect. The tail rotor is geared to the main rotor at a fixed ratio, so it does not need its own needle. The two needles compare engine speed with main rotor speed.
    • BCorrect. When the engine is driving the rotor, the needles are superimposed ('married'). When the freewheeling unit disengages, for example in autorotation, the needles split.
    • CIncorrect. The second needle is not a maximum-reading (drag) pointer. It shows rotor rpm in real time, so the pilot can compare it with engine rpm.
    • DIncorrect. The needles are not redundant engine indications. One shows engine rpm and the other shows rotor rpm, so they read differently when the needles split.
  7. Question 7

    What vibration source is usually associated with a high-frequency vibration in a helicopter?

    • AThe landing skids
    • BThe main rotor blades, which turn the fastest
    • CThe tail rotor, engine or drive train
    • DThe fuel tank
    Show answer and explanation

    Answer: C) The tail rotor, engine or drive train

    • AIncorrect. Skids do not rotate.
    • BIncorrect. The main rotor turns slowly and causes low-frequency vibration.
    • CCorrect. These parts rotate much faster than the main rotor.
    • DIncorrect. Fuel tanks do not generate high-frequency vibration.
  8. Question 8

    What does a rotor brake do on a helicopter?

    • ASteers the helicopter on the ground
    • BIncreases rotor rpm during engine start
    • CControls blade pitch
    • DSlows and stops the rotor after shutdown
    Show answer and explanation

    Answer: D) Slows and stops the rotor after shutdown

    • AIncorrect. It is not a steering device.
    • BIncorrect. It slows the rotor.
    • CIncorrect. That is the swashplate.
    • DCorrect. It also keeps the rotor from turning while parked.
  9. Question 9

    On a typical single-main-rotor helicopter, what is the function of the gearbox mounted at the end of the tail boom?

    • AIt reduces engine output speed to main rotor rpm and drives the main rotor mast
    • BIt lets the rotor system keep turning when the engine stops, for autorotation
    • CIt changes the drive direction, often 90°, and may adjust shaft speed to tail rotor rpm
    • DIt damps vibration and whipping of the long tail rotor drive shaft along the boom
    Show answer and explanation

    Answer: C) It changes the drive direction, often 90°, and may adjust shaft speed to tail rotor rpm

    The tail rotor gearbox changes the direction of drive from the tail rotor drive shaft to the tail rotor, usually by 90°. Its gearing may also adjust shaft speed to the best tail rotor rpm.

    • AIncorrect. The main rotor transmission reduces engine speed and drives the mast. The tail gearbox only serves the tail rotor.
    • BIncorrect. This is the job of the freewheeling (overrunning) unit between the engine and the main transmission, not the tail rotor gearbox.
    • CCorrect. The tail rotor gearbox gives a right-angle drive from the tail rotor drive shaft to the tail rotor. It may also use gearing to set the best tail rotor rpm.
    • DIncorrect. The tail rotor drive shaft is supported along the boom by hanger bearings, and on some designs by dampers. The tail gearbox is a power-transmitting component.
  10. Question 10

    During autorotation, what lets the main rotor keep turning after engine failure?

    • AA freewheeling unit
    • BThe tail rotor gearbox
    • CThe hydraulic pump
    • DThe fuel boost pump
    Show answer and explanation

    Answer: A) A freewheeling unit

    • ACorrect. It disconnects the engine so airflow can drive the rotor.
    • BIncorrect. It does not disengage the engine.
    • CIncorrect. This is unrelated.
    • DIncorrect. This is unrelated.

Rotorcraft Fundamentals: FAQs

How much of the AMA exam is Rotorcraft Fundamentals?

Rotorcraft Fundamentals is 6% of the AMA exam by the official exam guide's weighting, which on a 100-question form works out to roughly 6 questions. The real exam's exact split varies by form.

What does the Rotorcraft Fundamentals domain cover?

Helicopter fundamentals: aerodynamics, controls and rotor systems.

How should I study Rotorcraft Fundamentals for AMA?

Learn vibration types and their likely causes; troubleshooting questions rely on them.

Where can I practise more Rotorcraft Fundamentals questions?

This page has 10 free Rotorcraft Fundamentals questions with answers. The ExamWize AMA question bank has 36 questions in this domain. Every practice exam result breaks your score down by domain, and Review Mode re-drills the questions you missed.

Get Rotorcraft Fundamentals exam-ready

The full AMA bank has 36 Rotorcraft Fundamentals 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.