Step2Study
AviationAMP100% Free

FAA Aviation Mechanic Powerplant (AMP)

Practice bank
335 Qs
Real exam
100 Qs
Time limit
120 min
Passing
70%

Exam blueprint

Reciprocating Engines
20%
Turbine Engines
20%
Ignition and Starting Systems
15%
Fuel, Induction and Lubrication
20%
Propellers
10%
Engine Inspection
15%

Practice

Untimed · instant feedback · 4 practice tests of 90 questions

Questions per test

Custom practice

Flashcard on every question Mental map when you miss

Exam simulation

4 timed tests · 100 questions each · 120 min · pass 70% · 335 questions in the bank

+50 XP per test · +100 XP for a pass

Random simulation (weighted by domain)

Everything is open to everyone. Create a free account to save scores, XP, badges and get progress emails.

Free study resources

All resources →

Part of a learning path

Study with friends

Challenge a friend to beat your score.

FAA Aviation Mechanic Powerplant (AMP) practice test questions

Sample questions from the 335-question bank, with answers and explanations.

All questions
  1. 1. A direct-cranking electric starter on a reciprocating engine uses a Bendix drive to engage the engine ring gear. What principle allows the drive pinion to move forward and mesh with the ring gear when the starter motor is energized?

    Ignition and Starting Systems

    • A. The pinion is held in mesh by spring pressure until the starter switch is released
    • B. Inertia of the pinion causes it to screw forward along helical splines on the rapidly rotating armature shaft
    • C. An electric solenoid physically shifts the pinion into mesh independent of shaft rotation
    • D. Engine oil pressure forces the pinion outward along the starter shaft
    Show answer

    B. Inertia of the pinion causes it to screw forward along helical splines on the rapidly rotating armature shaft

    In a Bendix (inertia) drive, the pinion is mounted on a helically splined sleeve. When the starter motor spins up quickly, the pinion's inertia causes it to lag momentarily and screw forward along the splines into mesh with the ring gear. Once the engine starts and overspeeds the pinion, it automatically screws back out of mesh.

  2. 2. A technician inspects the combustor liner of a turbine engine and notes rows of small holes and slots along the liner wall. What is the primary purpose of these holes?

    Turbine Engines

    • A. To meter bleed air to the anti-ice system
    • B. To allow fuel to be injected directly into the primary combustion zone
    • C. To admit compressor discharge air that forms a cooling air film along the liner wall
    • D. To allow igniter plugs to be inserted into the combustion chamber
    Show answer

    C. To admit compressor discharge air that forms a cooling air film along the liner wall

    Combustor liners use film/effusion cooling holes that admit compressor discharge air, which flows along the inner wall as a protective film, insulating the liner from the extreme radiant and convective heat of combustion gases.

  3. 3. A mechanic is comparing the oil pressure and scavenge pumps in a turbine engine lubrication system. The scavenge pump has a significantly greater pumping capacity than the pressure pump. What is the primary reason for this design?

    Fuel, Induction and Lubrication

    • A. The scavenge pump also removes fuel that has leaked into the oil system
    • B. The scavenge pump must overcome higher discharge pressure than the pressure pump
    • C. A larger scavenge pump reduces the need for an oil cooler in the system
    • D. Oil returning from the bearings is aerated (mixed with air), increasing its volume and requiring greater capacity to return it to the tank
    Show answer

    D. Oil returning from the bearings is aerated (mixed with air), increasing its volume and requiring greater capacity to return it to the tank

    As oil passes through bearing compartments, it becomes aerated with air, significantly increasing its volume. The scavenge pump must therefore have greater capacity than the pressure pump to ensure all the aerated oil is returned to the tank and bearing sumps do not flood, even though the mass of oil is the same.

  4. 4. A mechanic is servicing a ground-adjustable pitch propeller on a light aircraft. When can the blade angle of this type of propeller be changed?

    Propellers

    • A. Continuously in flight by moving a cockpit propeller control lever
    • B. Only during full-power engine runup using a hydraulic pitch-change unit
    • C. Automatically in flight through governor oil pressure acting on a piston
    • D. Only with the engine stopped, by loosening the clamping mechanism at the hub and manually resetting each blade
    Show answer

    D. Only with the engine stopped, by loosening the clamping mechanism at the hub and manually resetting each blade

    A ground-adjustable propeller has a fixed pitch during flight; the blade angle can only be reset on the ground with the engine stopped by loosening the hub clamping mechanism, rotating the blades to the desired angle, and re-tightening. There is no in-flight or governor-controlled pitch change capability on this type of propeller.

  5. 5. A turbofan engine's fan case incorporates a heavy Kevlar or steel containment ring surrounding the fan blade path. What is the primary purpose of this structural feature?

    Turbine Engines

    • A. To contain fragments of a fan blade if one fails, preventing them from penetrating the fuselage or wing
    • B. To reduce fan noise during takeoff
    • C. To provide anti-icing heat to the fan blades
    • D. To improve fan aerodynamic efficiency at cruise
    Show answer

    A. To contain fragments of a fan blade if one fails, preventing them from penetrating the fuselage or wing

    The fan containment case is a certification requirement (per 14 CFR Part 33) designed to contain a released fan blade and its fragments within the engine nacelle, preventing damage to the aircraft structure, fuel tanks, or control systems in the event of a blade failure.

  6. 6. A hydromechanical fuel control unit (FCU) on a turbine engine schedules fuel flow to the engine. Which combination of inputs does the FCU primarily use to compute the correct fuel flow?

    Turbine Engines

    • A. Outside air temperature and indicated airspeed only
    • B. Oil pressure and exhaust gas temperature only
    • C. N2 speed and fuel tank quantity
    • D. Compressor inlet air temperature and pressure, engine speed, and throttle (power lever) position
    Show answer

    D. Compressor inlet air temperature and pressure, engine speed, and throttle (power lever) position

    A hydromechanical FCU meters fuel based on compressor inlet pressure (Pt2) and temperature (Tt2), engine rotor speed, and throttle lever position, allowing it to schedule the correct fuel flow for acceleration, deceleration, and steady-state operation while protecting against compressor stalls and overtemperature.

  7. 7. A cylinder on a reciprocating engine shows excessive oil consumption and bluish-gray smoke from the exhaust at idle power, while a differential compression check shows normal readings with no unusual hissing at the intake or exhaust ports. A technician suspects the intake valve guide has excessive stem-to-guide clearance. What is the most likely mechanism causing the oil consumption in this case?

    Reciprocating Engines

    • A. The valve seat is not sealing properly, allowing combustion gases to escape past the intake valve
    • B. The oil control ring end gap has closed completely, trapping oil above the piston
    • C. Piston rings are worn, allowing oil to be pumped up past the rings into the combustion chamber
    • D. Oil is being drawn past the worn intake valve guide into the combustion chamber during the intake stroke
    Show answer

    D. Oil is being drawn past the worn intake valve guide into the combustion chamber during the intake stroke

    A worn or excessively clearanced valve guide can allow oil from the valve spring/rocker area to be drawn down the valve stem into the combustion chamber, particularly during the intake stroke when manifold vacuum pulls oil past the loose guide. This produces bluish-gray exhaust smoke and increased oil consumption without necessarily affecting differential compression readings, since compression seal is governed by valve seating and piston rings, not guide clearance.

  8. 8. In a continuous-flow fuel injection system, what is the primary function of the individual fuel discharge nozzles installed at each cylinder's intake port?

    Reciprocating Engines

    • A. To precisely time fuel injection to coincide with each cylinder's intake valve opening, like a diesel injector
    • B. To continuously spray a metered fuel flow into the intake airstream near the intake valve for vaporization before entering the cylinder
    • C. To atomize fuel directly into the combustion chamber during the power stroke
    • D. To mechanically divide fuel flow equally among cylinders based on engine RPM
    Show answer

    B. To continuously spray a metered fuel flow into the intake airstream near the intake valve for vaporization before entering the cylinder

    Continuous-flow fuel injection nozzles spray fuel continuously (not timed to valve events) into the intake port just upstream of the intake valve, where it mixes with incoming air and vaporizes before entering the cylinder. Fuel division among cylinders is handled by the flow divider, not the nozzles themselves.

  9. 9. A mechanic is checking the float level on a float-type carburetor and finds it set higher than the manufacturer's specification. What is the most likely effect on engine operation?

    Engine Inspection

    • A. The mixture will be too lean at all power settings
    • B. The fuel level in the bowl will be too high, causing an overly rich mixture and possible fuel leakage
    • C. The idle mixture will become too lean while cruise mixture remains normal
    • D. The engine will be prone to fuel starvation during climb
    Show answer

    B. The fuel level in the bowl will be too high, causing an overly rich mixture and possible fuel leakage

    A float level set too high allows the fuel level in the float bowl to rise above the correct point, which increases fuel delivery to the discharge nozzle and produces an excessively rich mixture; it can also cause fuel to leak from the vents or discharge nozzle.

  10. 10. A mechanic is inspecting a reciprocating engine equipped with an oil dilution system used for cold-weather starting. How does this system function?

    Fuel, Induction and Lubrication

    • A. It circulates hot engine coolant through the oil sump to maintain oil temperature
    • B. It injects unleaded gasoline directly into the intake manifold to aid cold starts
    • C. It heats the oil sump electrically to keep oil warm between flights
    • D. It introduces raw fuel into the engine oil supply just before shutdown to thin the oil, which evaporates out after the next start warms the engine
    Show answer

    D. It introduces raw fuel into the engine oil supply just before shutdown to thin the oil, which evaporates out after the next start warms the engine

    An oil dilution system introduces raw gasoline into the engine oil supply just before engine shutdown in cold weather. This thins the oil, making it easier to circulate for the next cold start. As the engine warms up after starting, the gasoline evaporates out of the oil, restoring normal viscosity.

  11. 11. During a ground start, a turbine engine's EGT rapidly rises above the specified start limit while N1 remains very low and slow to accelerate. Which start condition is being experienced?

    Turbine Engines

    • A. Hung start
    • B. Flameout
    • C. Compressor surge
    • D. Hot start
    Show answer

    D. Hot start

    A hot start occurs when excess fuel is introduced relative to the available airflow during start, causing EGT to exceed limits before the engine reaches self-sustaining speed. The technician must abort the start immediately to prevent turbine damage.

  12. 12. A pilot reports that a reciprocating engine runs rough after extended ground operations at low power but smooths out after a brief application of high power. A technician suspects spark plug fouling. What is the most likely cause and appropriate corrective action?

    Ignition and Starting Systems

    • A. Water contamination in the fuel; correct by draining the fuel sumps before the next flight
    • B. Carbon fouling from rich mixture at high power; correct by leaning the mixture during cruise flight
    • C. Oil fouling from worn piston rings; correct by replacing the magneto immediately
    • D. Lead fouling from prolonged low-power ground operation; correct by leaning the mixture during ground operations and periodically clearing the engine with a brief power application
    Show answer

    D. Lead fouling from prolonged low-power ground operation; correct by leaning the mixture during ground operations and periodically clearing the engine with a brief power application

    Extended low-power ground operation with a rich idle mixture allows lead bromide deposits (from the tetraethyl lead in avgas) to build up on spark plug electrodes, causing intermittent misfire; the standard correction is to lean the mixture during ground operations per the AFM and periodically run the engine up briefly to help clear the deposits.

  13. 13. A technician is troubleshooting an oil temperature gauge that reads consistently high during ground runs, while oil pressure remains normal. Inspection reveals the thermostatic bypass valve (Vernatherm) in the oil cooler is stuck in the bypass position. What effect does this have on the lubrication system?

    Reciprocating Engines

    • A. Oil pressure relief valve is disabled, causing excessive pressure
    • B. Oil flows through the cooler continuously, causing overcooling
    • C. Oil is diverted away from the engine bearings, causing lubrication starvation
    • D. Oil bypasses the cooler entirely, preventing it from being cooled
    Show answer

    D. Oil bypasses the cooler entirely, preventing it from being cooled

    The Vernatherm valve normally routes cold oil around (bypasses) the oil cooler until it reaches operating temperature, then redirects oil through the cooler core as it expands. If the valve sticks in the bypass position, oil continues to bypass the cooler even when hot, so it never gets cooled, resulting in the high oil temperature observed with normal oil pressure since flow to the engine is unaffected.

  14. 14. A pilot operating a fuel-injected engine at high cruise altitude on a hot day is advised to switch on the electric fuel boost pump. What problem is this action primarily intended to prevent?

    Fuel, Induction and Lubrication

    • A. Excessive oil consumption at altitude
    • B. Detonation caused by an over-rich mixture
    • C. Formation of fuel vapor in the lines that could interrupt fuel flow
    • D. Overcharging of the induction manifold
    Show answer

    C. Formation of fuel vapor in the lines that could interrupt fuel flow

    High altitude combined with high temperatures lowers the boiling point margin of fuel, increasing the risk of vapor forming in fuel lines. The boost pump maintains positive fuel line pressure, keeping fuel in liquid form and ensuring uninterrupted flow to the engine-driven pump and injectors.

  15. 15. A technician is calculating the compression ratio of a cylinder that has a swept (displacement) volume of 85 cubic inches and a combustion chamber clearance volume of 10 cubic inches. What is the compression ratio?

    Reciprocating Engines

    • A. 8.5:1
    • B. 8.0:1
    • C. 9.0:1
    • D. 9.5:1
    Show answer

    D. 9.5:1

    Compression ratio = (swept volume + clearance volume) / clearance volume = (85 + 10) / 10 = 95/10 = 9.5:1.

  16. 16. A turbofan engine manufacturer specifies that the engine is 'flat rated' to an outside air temperature of 30°C. What does this rating mean for engine performance?

    Turbine Engines

    • A. The engine's N1 speed is fixed at 30 percent during all cruise operations
    • B. The engine produces its maximum rated thrust only when the OAT is exactly 30°C
    • C. The fuel control automatically limits thrust output so that full rated thrust is available at OATs up to 30°C, after which available thrust decreases as temperature rises further
    • D. The engine maintains a constant EGT regardless of altitude up to 30,000 feet density altitude
    Show answer

    C. The fuel control automatically limits thrust output so that full rated thrust is available at OATs up to 30°C, after which available thrust decreases as temperature rises further

    Flat rating means the fuel control unit limits fuel flow (and thus thrust) so that the engine produces its full rated thrust across a range of ambient temperatures up to the flat-rated temperature. Above that temperature, air density decreases enough that the engine can no longer maintain rated thrust without exceeding internal temperature limits, so available thrust decreases.

  17. 17. A turbine engine ignition system uses a capacitor discharge (CD) exciter unit to fire the igniter plugs. Which statement best describes how this system produces the high-energy spark required for turbine ignition?

    Ignition and Starting Systems

    • A. A rotating magnet continuously induces alternating current directly into the igniter plug without any intermediate storage
    • B. A transformer-rectifier charges a storage capacitor, which is then discharged through a trigger transformer to the igniter plug in a single high-energy pulse
    • C. A set of mechanical breaker points interrupts current flow to produce a continuous stream of low-energy sparks
    • D. An impulse coupling mechanically advances the spark timing at low engine speeds
    Show answer

    B. A transformer-rectifier charges a storage capacitor, which is then discharged through a trigger transformer to the igniter plug in a single high-energy pulse

    In a capacitor discharge ignition (CDI) exciter unit, input power (AC or DC) is stepped up and rectified to charge a storage capacitor to a high voltage; when a triggering circuit fires, the capacitor rapidly discharges through a trigger transformer, delivering a very high-energy, high-voltage pulse to the igniter plug. This design is used on turbine engines because it produces a much higher energy spark than a magneto, necessary to ignite fuel reliably under adverse conditions such as altitude, cold, or wet starts. Magnetos (with rotating magnets and breaker points) and impulse couplings are reciprocating engine ignition components, not part of turbine CD ignition systems.

  18. 18. A technician is diagnosing a lifter noise complaint on an engine equipped with hydraulic valve lifters. During engine operation, the hydraulic lifter is designed to automatically compensate for valve train clearance. What component within the hydraulic lifter allows this automatic clearance adjustment?

    Reciprocating Engines

    • A. A mechanical screw adjuster set at each inspection
    • B. A bimetallic spring that expands with heat to close the gap
    • C. A pneumatic bellows pressurized by intake manifold vacuum
    • D. A plunger and check valve arrangement using engine oil pressure to take up clearance
    Show answer

    D. A plunger and check valve arrangement using engine oil pressure to take up clearance

    A hydraulic lifter uses a spring-loaded plunger inside a cylinder body with a one-way check valve; engine oil under pressure fills the chamber beneath the plunger, which extends to take up all valve train clearance (zero lash) and maintains it automatically as parts wear or thermally expand.

  19. 19. A technician is timing a magneto to the engine (external timing) rather than performing internal E-gap timing. Which of the following describes this procedure?

    Reciprocating Engines

    • A. Rotating the crankshaft to the manufacturer's specified degrees before top dead center on the compression stroke, then adjusting the magneto position until the breaker points just begin to open
    • B. Setting the ignition switch to the BOTH position and verifying no RPM drop occurs
    • C. Setting the breaker points to open exactly at the moment the rotating magnet is at its neutral position
    • D. Adjusting the gap between the magneto rotor and pole shoes to the manufacturer's tolerance
    Show answer

    A. Rotating the crankshaft to the manufacturer's specified degrees before top dead center on the compression stroke, then adjusting the magneto position until the breaker points just begin to open

    External (engine-to-magneto) timing is performed by rotating the crankshaft to the specified number of degrees before top dead center on the compression stroke for the timing cylinder, then rotating the magneto housing on the engine until the breaker points just begin to open (often indicated by a timing light), and securing the magneto in that position.

  20. 20. A mechanic is briefing an owner-pilot on the fuel system of a light twin equipped with individual tanks in each wing. Which statement best describes the primary purpose of the fuel selector valve?

    Fuel, Induction and Lubrication

    • A. It vents fuel tank vapors overboard to prevent excessive internal pressure
    • B. It allows the pilot to choose which tank or combination of tanks supplies fuel to each engine
    • C. It filters solid contaminants from the fuel before it reaches the engine-driven pump
    • D. It regulates fuel pressure delivered to the carburetor or fuel injector
    Show answer

    B. It allows the pilot to choose which tank or combination of tanks supplies fuel to each engine

    The fuel selector valve is a manually (or electrically) operated valve that lets the pilot direct fuel flow from a chosen tank, both tanks, or the off position to the engine(s). Filtering, pressure regulation, and venting are performed by other components.

  21. 21. A technician installs new piston rings in a reciprocating engine cylinder and checks ring end gap by squaring the ring in the bore with an inverted piston, then measuring the gap with a feeler gauge. The measured gap is 0.006 inch, but the overhaul manual specifies a minimum gap of 0.010 inch. What should the technician do?

    Engine Inspection

    • A. Soak the ring in oil to allow it to seat and close the gap over time
    • B. File the ring ends to slightly increase the end gap to meet the minimum specification
    • C. Install the ring as is since the gap is close enough to the minimum
    • D. Install the ring rotated 90 degrees from the original measurement position
    Show answer

    B. File the ring ends to slightly increase the end gap to meet the minimum specification

    Insufficient ring end gap can cause the ring ends to butt together as the ring expands from heat during operation, leading to scuffing, scoring, or a stuck/broken ring. The correct correction is to carefully file the ring ends to open the gap to at least the minimum specified value.

  22. 22. A mechanic discovers that the pressurization valve on a turbine engine's oil tank is stuck in the closed position, preventing bleed air from pressurizing the tank. What is the most likely operational effect of this defect?

    Fuel, Induction and Lubrication

    • A. Oil temperature will decrease significantly, causing thickened oil and reduced flow
    • B. Reduced oil tank pressure may allow the oil pump to cavitate, resulting in inadequate lubrication, especially at altitude or high power
    • C. The oil tank will overpressurize and rupture during high-power operation
    • D. Engine oil consumption will decrease because less oil escapes through the vent system
    Show answer

    B. Reduced oil tank pressure may allow the oil pump to cavitate, resulting in inadequate lubrication, especially at altitude or high power

    Turbine engine oil tanks are often pressurized with bleed air to ensure a positive head of pressure at the oil pump inlet, preventing pump cavitation and foaming, especially during high-altitude or high-power operation. If the pressurization valve fails closed, the tank pressure drops, increasing the risk of pump cavitation and inadequate lubrication.

  23. 23. A technician is comparing a low-tension magneto ignition system to a conventional high-tension system on a reciprocating engine. What is the main operational advantage of the low-tension system?

    Ignition and Starting Systems

    • A. It eliminates the need for spark plugs altogether
    • B. It reduces the risk of high-voltage leakage or flashover through the ignition harness at high altitude
    • C. It produces a higher voltage spark than a high-tension system at all altitudes
    • D. It allows the magneto to operate without an impulse coupling
    Show answer

    B. It reduces the risk of high-voltage leakage or flashover through the ignition harness at high altitude

    In a low-tension system, only low voltage is carried through the distributor and harness to individual step-up coils located near each spark plug, where the voltage is stepped up just before the plug. This reduces the length of high-voltage wiring exposed to reduced air density at altitude, minimizing flashover and insulation breakdown. It still uses spark plugs, still may use an impulse coupling, and does not inherently produce higher voltage overall.

  24. 24. During the start sequence of a turbine engine, the exhaust gas temperature rapidly exceeds the specified start limit while RPM is still low. Which condition most likely caused this hot start?

    Ignition and Starting Systems

    • A. Fuel was introduced too early or in excessive quantity relative to the available airflow through the engine
    • B. Bleed air valves were fully open during the start, increasing airflow
    • C. The starter provided too much rotational energy relative to fuel flow
    • D. The igniters fired continuously throughout the entire start cycle
    Show answer

    A. Fuel was introduced too early or in excessive quantity relative to the available airflow through the engine

    A hot start occurs when the fuel-to-air ratio is too rich during light-off, typically from introducing fuel too soon (before sufficient airflow is established by the starter/compressor) or from excessive fuel flow, causing the flame temperature and EGT to rise rapidly beyond limits before enough airflow can cool the gas path. Excess starter energy or open bleed valves would tend to increase airflow and reduce hot start risk, and continuous igniter operation does not by itself cause overtemperature.

  25. 25. A radial engine's electric starter is connected to the crankshaft through a starter adapter. What two functions does the starter adapter typically provide?

    Reciprocating Engines

    • A. A freewheeling clutch to disengage the starter and a shear section to protect against overtorque
    • B. Propeller feathering and reverse pitch control during start
    • C. Oil pressure boost and fuel pressure boost during cranking
    • D. Ignition timing advance and fuel enrichment during start
    Show answer

    A. A freewheeling clutch to disengage the starter and a shear section to protect against overtorque

    The starter adapter contains a clutch (overrunning or friction type) that allows the starter to disengage automatically once the engine starts and accelerates past the starter's speed, and a shear section (shear pin/section) designed to fail if excessive torque is applied, protecting the starter and gear train from damage.

FAA Aviation Mechanic Powerplant (AMP) flashcards

Tap a card to flip it. 312 flashcards in the full deck.

  • Bendix Drive (Inertia Drive)

    Flip card

    A starter drive mechanism that uses the inertia of a pinion gear on helical splines to automatically engage and disengage the engine ring gear.

    • Pinion lags behind the rapidly accelerating shaft due to inertia, screwing into mesh.
    • Automatically disengages when the engine overspeeds the starter after starting.
    • Simple, self-contained mechanism requiring no separate solenoid to shift the pinion.
    Study this card →
  • Combustor Liner Cooling

    Flip card

    Small holes/slots in the combustor liner admit compressor discharge air to form an insulating film that protects the liner from combustion heat.

    • Uses compressor discharge (P3) air
    • Forms a boundary-layer cooling film
    • Protects liner from radiant/convective heat
    Study this card →
  • Turbine Scavenge Pump Sizing

    Flip card

    Turbine engine oil scavenge pumps are built with greater capacity than the pressure pump to handle the increased volume of aerated oil returning from bearing sumps.

    • Oil becomes aerated (foamy) after lubricating bearings
    • Aeration increases oil volume without increasing mass
    • Scavenge pump capacity must exceed pressure pump capacity to prevent sump flooding
    Study this card →
  • Ground-Adjustable Pitch Propeller

    Flip card

    A propeller whose blade angle can only be changed on the ground with the engine stopped, by loosening a hub clamp, rotating the blades, and re-securing them; it then operates as a fixed-pitch propeller in flight.

    • Blade angle set only on the ground
    • Engine must be stopped for adjustment
    • Acts as fixed pitch once set and locked
    Study this card →
  • Fan Blade Containment

    Flip card

    A structural design requirement where the fan case is built to contain a fan blade failure, preventing debris from exiting the engine and damaging the aircraft.

    • Required by 14 CFR Part 33 certification standards
    • Made of Kevlar wrap or heavy steel/titanium
    • Prevents uncontained failure events
    Study this card →
  • Hydromechanical Fuel Control Unit

    Flip card

    A mechanical/hydraulic device that meters fuel flow to a turbine engine based on compressor inlet conditions, rotor speed, and throttle position.

    • Uses Pt2/Tt2, N speed, and throttle position
    • Prevents overtemperature and compressor stall during transients
    • Being replaced in modern engines by FADEC
    Study this card →
  • Valve Guide Wear (Oil Consumption)

    Flip card

    Excessive clearance between a valve stem and its guide can allow oil to be drawn into the combustion chamber, especially on the intake valve during the intake stroke, causing increased oil consumption and blue exhaust smoke.

    • Common on intake guides due to manifold vacuum pulling oil down the stem
    • Differential compression test may remain normal since it tests seat/ring sealing, not guide wear
    • Symptoms: bluish-gray smoke, high oil consumption without compression loss
    Study this card →
  • Fuel Injector Nozzle (Continuous-Flow)

    Flip card

    A calibrated orifice at each cylinder's intake port that continuously sprays metered fuel into the airstream for vaporization before entering the cylinder.

    • Fuel flow is continuous, not timed to valve events
    • Located at intake port near intake valve, not inside cylinder
    • Flow divider (not nozzles) apportions fuel equally to each cylinder
    Study this card →
  • Carburetor Float Level

    Flip card

    The float level sets the fuel level in the carburetor bowl relative to the discharge nozzle, directly controlling mixture strength.

    • Float too high = fuel level too high = rich mixture/possible leakage
    • Float too low = fuel level too low = lean mixture/possible starvation
    • Level is checked per manufacturer's dimension using a float gauge
    Study this card →
  • Oil Dilution System

    Flip card

    A cold-weather starting aid that mixes raw fuel into engine oil before shutdown to reduce viscosity for easier starting; the fuel evaporates from the oil after the engine warms up.

    • Fuel is introduced into oil supply just before shutdown
    • Thinned oil circulates more easily during cold starts
    • Gasoline evaporates from oil as engine warms after starting
    Study this card →
  • Hot Start

    Flip card

    A turbine engine start condition where EGT exceeds the specified limit due to excess fuel relative to airflow before the engine reaches idle.

    • Caused by too much fuel or insufficient starter airflow
    • Requires immediate abort to prevent turbine damage
    • Different from a hung start, which involves low RPM, not high EGT
    Study this card →
  • Lead Fouling

    Flip card

    Deposits of lead bromide on spark plug electrodes caused by extended low-power/idle operation with leaded avgas, leading to intermittent misfire that often clears with a brief high-power run.

    • Most common during prolonged ground idle or descent at low power
    • Leaning the mixture during ground ops reduces lead deposit formation
    • A brief high-power 'clearing' runup can help burn off deposits
    Study this card →
  • Thermostatic Bypass Valve (Vernatherm)

    Flip card

    A wax-pellet type thermostatic valve in the oil system that routes cold oil around the oil cooler and directs hot oil through the cooler core once operating temperature is reached.

    • Bypasses cooler when oil is cold for faster warm-up
    • Expands with heat to route oil through cooler core
    • Stuck-in-bypass failure causes chronic high oil temperature with normal pressure
    Study this card →
  • Electric Fuel Boost Pump

    Flip card

    An auxiliary pump that pressurizes fuel lines to prevent vapor formation and assist the engine-driven pump during high altitude, hot weather, takeoff, and engine starting.

    • Maintains positive fuel pressure to prevent vaporization
    • Used during takeoff, landing, high altitude cruise, and priming
    • Backs up the engine-driven fuel pump if it fails
    Study this card →
  • Compression Ratio

    Flip card

    The ratio of total cylinder volume (piston at BDC) to clearance volume (piston at TDC), indicating how much the fuel-air charge is compressed.

    • CR = (swept volume + clearance volume) / clearance volume
    • Higher CR increases thermal efficiency but risk of detonation
    • Typical aircraft reciprocating engines run 7:1 to 10:1
    Study this card →
  • Flat Rating

    Flip card

    A design/control feature where the fuel control limits engine thrust so rated thrust is maintained across ambient temperatures up to a specified 'flat rate' temperature, beyond which available thrust decreases.

    • Protects the engine from overtemperature on cold/moderate days by limiting fuel flow
    • Rated thrust is constant below the flat-rate temperature
    • Above flat-rate temp, thrust falls off to protect turbine limits
    Study this card →
  • Capacitor Discharge (CD) Ignition Exciter

    Flip card

    A turbine engine ignition unit that charges a storage capacitor to high voltage and rapidly discharges it through a trigger transformer to produce a high-energy spark at the igniter plug.

    • Produces much higher spark energy than reciprocating magnetos
    • Used because turbine fuel ignition needs a strong, reliable spark
    • Capacitor charges continuously and discharges intermittently at set intervals
    Study this card →
  • Hydraulic Valve Lifter

    Flip card

    A valve lifter that uses a spring-loaded plunger and one-way check valve, filled with pressurized engine oil, to automatically maintain zero valve clearance during engine operation.

    • Uses engine oil pressure to extend the internal plunger
    • Check valve traps oil to maintain zero-lash clearance
    • Automatically compensates for thermal expansion and wear
    Study this card →
  • Magneto-to-Engine (External) Timing

    Flip card

    The procedure of positioning the crankshaft at the specified degrees BTDC on the compression stroke, then rotating the magneto on its mounting until the breaker points just open, to synchronize spark timing with piston position.

    • Uses crankshaft timing marks/degree wheel and a timing light or buzzer box
    • Performed after internal E-gap timing is already set within the magneto
    • Ensures spark occurs at the correct crank angle for combustion
    Study this card →
  • Fuel Selector Valve

    Flip card

    A valve, usually pilot-operated, that directs fuel from a selected tank (or tanks) to the engine and provides an OFF position for shutdown or emergencies.

    • Common positions: LEFT, RIGHT, BOTH, OFF
    • Located between tanks and fuel pump/strainer
    • Allows tank balancing and isolation of a leaking tank
    Study this card →
  • Piston Ring End Gap

    Flip card

    The clearance between the ends of a piston ring when installed squarely in the cylinder bore, required to allow for thermal expansion during engine operation.

    • Measured with a feeler gauge while ring is squared using an inverted piston
    • Insufficient gap causes ring butting, scuffing, or seizure when hot
    • Excessive gap causes blow-by and loss of compression
    Study this card →
  • Turbine Oil Tank Pressurization

    Flip card

    A system using engine bleed air to pressurize the oil tank, ensuring positive oil pump inlet pressure and preventing cavitation at altitude.

    • Uses bleed air through a pressurization valve
    • Prevents pump cavitation and foaming
    • Tank relief valve limits maximum pressure
    Study this card →
  • Low-Tension Ignition System

    Flip card

    An ignition system where low voltage is distributed to individual transformer coils near each spark plug, which then step up the voltage just before the plug fires.

    • Reduces high-voltage wire length exposed to low air pressure
    • Minimizes flashover/leakage at altitude
    • Step-up coils located near spark plugs, not at the magneto
    Study this card →
  • Turbine Engine Hot Start

    Flip card

    A start condition where EGT exceeds the specified limit due to an excessively rich fuel-to-air ratio, usually from fuel introduced too early or in excess relative to airflow.

    • Caused by too much fuel flow for available airflow during light-off
    • Can result from low starter cranking speed limiting airflow
    • Requires immediate abort per checklist to protect turbine section
    Study this card →

Questions are original practice items written to match the published exam objectives. Step2Study is not affiliated with or endorsed by any certification body.