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CAX · 13% of the exam

Operation of Systems and High-Altitude Operations practice questions

10 free Operation of Systems and High-Altitude Operations questions for the Commercial Pilot Airplane (CAX) Knowledge Test exam, each with the correct answer and an explanation for every option.

What this domain covers

How complex and high-performance aeroplane systems work, and the physiological and equipment demands of flying at altitude.

Exam weight
13%
On a real exam
≈ 13 questions
In our bank
77 questions

Topics that come up most

  • Constant-speed propellers and manifold pressure
  • Turbocharging and engine management
  • Retractable landing gear systems
  • Pressurisation and cabin altitude
  • Supplemental oxygen requirements and equipment

How to study it

Learn the oxygen rule's three altitude bands (above 12,500, 14,000 and 15,000 feet MSL) and who must use or be offered oxygen in each.

Sample Operation of Systems and High-Altitude Operations questions

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

  1. Question 1

    Why is the mixture usually set full rich for takeoff at low-elevation airports?

    • ABecause leaning is illegal below 3,000 feet
    • BTo save fuel during takeoff
    • CTo raise oil pressure
    • DExtra fuel helps cool the engine
    Show answer and explanation

    Answer: D) Extra fuel helps cool the engine

    • AIncorrect. It's a POH procedure.
    • BIncorrect. Full rich uses more fuel.
    • CIncorrect. The mixture doesn't control oil pressure.
    • DCorrect. Follow the POH for high elevations.
  2. Question 2

    In a pressurized airplane, the pressure differential gauge displays the difference between which two pressures?

    • AAir pressure inside the pressurized hull and ambient air pressure outside the airplane
    • BEngine manifold pressure and the ambient air pressure at the airplane's flight altitude
    • CBleed air pressure entering the cabin and the pressure released through the outflow valve
    • DCabin pressure selected on the controller and the cabin pressure presently maintained
    Show answer and explanation

    Answer: A) Air pressure inside the pressurized hull and ambient air pressure outside the airplane

    Cabin pressure differential is the difference between pressure inside the pressurized hull and outside ambient pressure. Relief valves automatically limit it to a predetermined maximum to protect the structure, and an instrument displays it to the crew.

    • ACorrect. Pressure differential is inside pressure minus outside ambient pressure. The structure is designed for a maximum differential, and pressure relief valves automatically limit the positive differential to a predetermined value.
    • BIncorrect. That comparison relates to engine induction or turbocharger performance. It has nothing to do with the load on the pressurized structure.
    • CIncorrect. The outflow valve controls cabin pressure by regulating how much air is released from the cabin. The differential that relief valves limit and the gauge displays is cabin pressure versus outside atmospheric pressure, not inflow versus outflow.
    • DIncorrect. That difference is the controller's error between selected and actual cabin pressure. It is not the structural pressure differential across the hull.
  3. Question 3

    In an airplane with a constant-speed propeller, what is the normal sequence of control movements when increasing power?

    • AClose the cowl flaps, then advance the throttle
    • BIncrease manifold pressure, then increase RPM
    • CLean the mixture, then increase RPM and manifold pressure
    • DEnrich the mixture, increase RPM, then increase manifold pressure
    Show answer and explanation

    Answer: D) Enrich the mixture, increase RPM, then increase manifold pressure

    With a constant-speed propeller, increase power by enriching the mixture, raising RPM, then raising manifold pressure. Reduce power in the reverse order (manifold pressure first, then RPM), so the engine never runs at high manifold pressure with low RPM.

    • AIncorrect. Cowl flaps don't belong in the power-change sequence. Higher power makes more heat, so cowl flaps are usually opened, not closed, when power goes up for a climb.
    • BIncorrect. Raising manifold pressure while RPM is still low creates high cylinder pressures that can overstress the engine. This order is used when reducing power, not increasing it.
    • CIncorrect. Before increasing power, the mixture is enriched, not leaned. More fuel keeps the engine cool and helps prevent detonation at higher power.
    • DCorrect. To increase power, enrich the mixture as needed, raise RPM with the propeller control, then raise manifold pressure with the throttle. This is the reverse of the reduction sequence (throttle back first, then RPM) and avoids high manifold pressure at low RPM.
  4. Question 4

    A circuit breaker trips in flight. What is common practice?

    • AHold it in so it can't trip again
    • BReset it once after a cooling period, if needed
    • CReset it repeatedly until it stays in
    • DReplace it with a higher-rated breaker in flight
    Show answer and explanation

    Answer: B) Reset it once after a cooling period, if needed

    • AIncorrect. That defeats its protection.
    • BCorrect. Repeated resets can start a fire.
    • CIncorrect. That can cause a fire.
    • DIncorrect. That isn't possible or safe.
  5. Question 5

    During a long climb in a piston airplane, the cylinder head temperature approaches the red line. Which combination of actions will best lower it?

    • ALean the mixture, close the cowl flaps and reduce airspeed
    • BEnrich the mixture, open the cowl flaps and increase airspeed
    • CLean the mixture, open the cowl flaps and steepen the climb
    • DEnrich the mixture, close the cowl flaps and reduce airspeed
    Show answer and explanation

    Answer: B) Enrich the mixture, open the cowl flaps and increase airspeed

    To lower high cylinder head temperatures, enrich the mixture, open the cowl flaps and increase airspeed with a shallower climb; reducing power also helps. Leaning, closing the cowl flaps or slowing down all reduce cooling.

    • AIncorrect. All three actions make overheating worse: a leaner mixture runs hotter, closed cowl flaps cut airflow over the cylinders, and lower airspeed reduces cooling.
    • BCorrect. Extra fuel helps cool the cylinders, open cowl flaps let more air through the engine compartment, and higher airspeed (a shallower climb) increases cooling airflow.
    • CIncorrect. Opening the cowl flaps helps, but leaning raises temperatures, and a steeper climb at lower airspeed cuts cooling airflow while the engine works at high power.
    • DIncorrect. Enriching helps, but closing the cowl flaps and slowing down both reduce the airflow the engine needs for cooling.
  6. Question 6

    In a typical pressurized airplane, the cabin pressure controller maintains the selected cabin altitude during normal operation mainly by adjusting the:

    • AOutflow valve, which meters how much air leaves the cabin
    • BSafety valve, which relieves pressure at maximum differential
    • CDump valve, which vents cabin air when the pilot selects it
    • DCompressor output, which varies the air pumped into the cabin
    Show answer and explanation

    Answer: A) Outflow valve, which meters how much air leaves the cabin

    The pressurization source supplies a fairly steady flow of air into the cabin. The cabin pressure controller sets cabin altitude by modulating the outflow valve. The safety and dump valves are protective or emergency devices, not the normal control.

    • ACorrect. Air comes into the cabin from the pressurization source at a fairly steady rate. The controller modulates the outflow valve to release more or less of that air, and this sets the cabin pressure and therefore the cabin altitude.
    • BIncorrect. The safety (positive-pressure relief) valve is a backup. It opens only to stop the cabin from going over the maximum pressure differential. It does not control cabin altitude in normal operation.
    • CIncorrect. The dump valve releases cabin pressure to the atmosphere when the pilot selects it, for example in an emergency or on the ground. It does not continuously regulate cabin altitude.
    • DIncorrect. The pressurization source (turbocharger compressor, engine bleed air or pneumatic pump) supplies air at a fairly constant rate. Cabin altitude is controlled by regulating the air going out, not the air coming in.
  7. Question 7

    A vacuum system failure typically affects the:

    • AAltimeter
    • BAirspeed indicator
    • CGyro instruments
    • DMagnetic compass
    Show answer and explanation

    Answer: C) Gyro instruments

    • AIncorrect. That's static.
    • BIncorrect. That's pitot-static.
    • CCorrect. The attitude and heading indicators in many light airplanes.
    • DIncorrect. That's self-contained.
  8. Question 8

    In a normally aspirated engine, manifold pressure during a climb at full throttle:

    • AIncreases
    • BDecreases
    • CStays constant
    • DDoubles
    Show answer and explanation

    Answer: B) Decreases

    • AIncorrect. It decreases.
    • BCorrect. Air pressure drops with altitude.
    • CIncorrect. Only turbocharging can hold it.
    • DIncorrect. It decreases.
  9. Question 9

    What is overboost in a turbocharged engine?

    • AOil pressure above normal
    • BRPM below normal cruise
    • CFuel flow below the minimum for the selected power setting
    • DManifold pressure above the engine's limit
    Show answer and explanation

    Answer: D) Manifold pressure above the engine's limit

    • AIncorrect. That's not overboost.
    • BIncorrect. That's not overboost.
    • CIncorrect. That's not overboost.
    • DCorrect. It can damage the engine.
  10. Question 10

    How does a loadmeter differ from a center-zero ammeter?

    • AA loadmeter shows battery voltage
    • BThey are exactly the same
    • CA loadmeter shows load, not discharge
    • DA loadmeter shows fuel flow
    Show answer and explanation

    Answer: C) A loadmeter shows load, not discharge

    • AIncorrect. That's a voltmeter.
    • BIncorrect. They show different things.
    • CCorrect. A center-zero ammeter shows charge or discharge.
    • DIncorrect. That's a fuel flow gauge.

Operation of Systems and High-Altitude Operations: FAQs

How much of the CAX exam is Operation of Systems and High-Altitude Operations?

Operation of Systems and High-Altitude Operations is 13% of the CAX exam by the official exam guide's weighting, which on a 100-question form works out to roughly 13 questions. The real exam's exact split varies by form.

What does the Operation of Systems and High-Altitude Operations domain cover?

How complex and high-performance aeroplane systems work, and the physiological and equipment demands of flying at altitude.

How should I study Operation of Systems and High-Altitude Operations for CAX?

Learn the oxygen rule's three altitude bands (above 12,500, 14,000 and 15,000 feet MSL) and who must use or be offered oxygen in each.

Where can I practise more Operation of Systems and High-Altitude Operations questions?

This page has 10 free Operation of Systems and High-Altitude Operations questions with answers. The ExamWize CAX question bank has 77 questions in this domain. Every practice exam result breaks your score down by domain, and Review Mode re-drills the questions you missed.

Get Operation of Systems and High-Altitude Operations exam-ready

The full CAX bank has 77 Operation of Systems and High-Altitude Operations 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.