FAA · AMP
A&P Powerplant (AMP) practice questions with answers
15 free practice questions for the Aviation Mechanic Powerplant (AMP) Knowledge Test, spread across the exam's topics. Try each one, then open the answer to see why every option is right or wrong.
Question 1 · Reciprocating Engines
When piston rings are installed, their end gaps are usually staggered to:
- AAllow oil to reach the combustion chamber freely
- BMake the rings rotate faster in service
- CRaise the compression ratio of the engine
- DReduce blow-by
Show answer and explanation
Answer: D) Reduce blow-by
- AIncorrect. That would raise consumption.
- BIncorrect. Staggering is about sealing.
- CIncorrect. Rings don't change displacement geometry.
- DCorrect. Aligned gaps would leak more gas.
Question 2 · Reciprocating Engines
Which reciprocating engine type is most common in light aircraft today?
- ASingle-row radial
- BHorizontally opposed
- CInverted inline
- DTwin-row V-type
Show answer and explanation
Answer: B) Horizontally opposed
- AIncorrect. Radials are mostly found on older aircraft.
- BCorrect. Opposed engines are compact, smooth and easy to cowl.
- CIncorrect. These are uncommon today.
- DIncorrect. These are rare in light aircraft.
Question 3 · Turbine Engines
In a gas turbine combustion chamber, what is the main purpose of the primary airflow?
- AMixing with the fuel to support combustion
- BForming a cooling film along the combustion liner walls
- CDiluting the hot gases to lower their temperature before the turbine
- DCooling the turbine blades and nozzle guide vanes
Show answer and explanation
Answer: A) Mixing with the fuel to support combustion
Primary air is the smaller share of combustor airflow and mixes with fuel to support combustion. Secondary air cools the liner and dilutes the gases, and compressor bleed air cools the turbine blades.
- ACorrect. Primary air enters near the fuel nozzles and mixes with the fuel to form a burnable mixture and sustain the flame.
- BIncorrect. Secondary air does this job, cooling the liner and insulating it from the flame.
- CIncorrect. Dilution (quenching) of the combustion gases is done by secondary air, not primary air.
- DIncorrect. Turbine blades and vanes are cooled by air bled from the compressor and routed through them, not by the combustor's primary air.
Question 4 · Engine Inspection
Under 14 CFR 91.421, an owner may use a new maintenance record, without previous operating history, for an aircraft engine that has been:
- ARebuilt by the manufacturer or by an agency approved by the manufacturer
- BMajor overhauled by a certificated repair station to the service limits
- COverhauled by an A&P mechanic holding an IA to the manufacturer's limits
- DTop overhauled by the manufacturer with new cylinder assemblies installed
Show answer and explanation
Answer: A) Rebuilt by the manufacturer or by an agency approved by the manufacturer
14 CFR 91.421 allows a zero-time record only for an engine rebuilt to new-engine standards by the manufacturer or by an agency approved by the manufacturer. Overhauled engines keep their previous operating history.
- ACorrect. 91.421(a) allows a new record without previous operating history for an engine rebuilt by the manufacturer or by an agency approved by the manufacturer. Under 91.421(c), a rebuilt engine meets the same tolerances and limits as a new engine.
- BIncorrect. An engine overhauled to service limits is not rebuilt to new-engine standards. It keeps its total time, and only the time since overhaul is reset.
- CIncorrect. 91.421 does not cover overhauls by individual mechanics, even ones with an inspection authorization. Only the manufacturer or a manufacturer-approved agency can rebuild an engine to zero time.
- DIncorrect. A top overhaul is not a rebuild. 91.421(c) requires complete disassembly, inspection, repair, reassembly, testing and approval to the same standards as a new engine.
Question 5 · Engine Instrument Systems
Why must thermocouple leads not be shortened or lengthened?
- AThey are color coded
- BThey carry fuel
- CResistance is calibrated
- DThey are life-limited
Show answer and explanation
Answer: C) Resistance is calibrated
- AIncorrect. Color is not the reason.
- BIncorrect. They carry a small voltage.
- CCorrect. Lead resistance is part of the calibration; changing length gives errors.
- DIncorrect. This is not the reason.
Question 6 · Engine Fire Protection Systems
A missing yellow disc on a fire extinguisher discharge indicator shows that:
- AThe squib was replaced
- BThe bottle overheated
- CThe bottle is fully charged
- DThe bottle was fired normally
Show answer and explanation
Answer: D) The bottle was fired normally
- AIncorrect. This is not shown by the disc.
- BIncorrect. That is the red disc.
- CIncorrect. A missing disc means discharge.
- DCorrect. The yellow disc blows out when the bottle is discharged by the crew.
Question 7 · Engine Electrical Systems
An engine-driven generator is rated at 28 volts and 60 amperes. What is its approximate rated power output?
- A1,680 watts
- B88 watts
- C840 watts
- D16,800 watts
Show answer and explanation
Answer: A) 1,680 watts
Electrical power in watts is voltage multiplied by current (P = E × I). For a 28 V, 60 A generator, that is 1,680 W.
- ACorrect. Power equals voltage times current: P = E × I = 28 V × 60 A = 1,680 W.
- BIncorrect. This adds the voltage and current (28 + 60). Power is the product of the two, not the sum.
- CIncorrect. This is half the correct value. A DC generator's power is the full product of voltage and current, with no halving.
- DIncorrect. This is ten times too large, a decimal error. 28 × 60 = 1,680.
Question 8 · Engine Electrical Systems
Why does a self-excited DC generator need residual magnetism?
- ATo set the frequency
- BTo stop reverse current
- CTo cool the armature
- DTo build up voltage
Show answer and explanation
Answer: D) To build up voltage
- AIncorrect. DC has no frequency.
- BIncorrect. A reverse current relay does that.
- CIncorrect. This is unrelated.
- DCorrect. Residual field magnetism starts the voltage build-up.
Question 9 · Engine Lubrication Systems
During a 100-hour inspection, a mechanic cuts open the oil filter. It holds a small amount of very fine, filing-like metal particles and no flakes or chips. What is the appropriate course of action?
- ARemove the engine for teardown before further flight to find the source
- BIdentify the material and continue inspecting to determine serviceability
- CRecord the particles as carbon and return the aircraft to service
- DReplace the oil pump, which is the usual source of fine metal filings
Show answer and explanation
Answer: B) Identify the material and continue inspecting to determine serviceability
A small amount of fine, filing-like particles calls for identifying the material and continuing the inspection against manufacturer limits. Heavy or unusual metal residue, such as flakes or chips, calls for removing the engine to find the source.
- AIncorrect. Removal and teardown are called for when an unusual or heavy amount of metal, such as flakes or chips, is found. A small amount of fine filings calls for further evaluation first.
- BCorrect. A small amount of fine particles isn't necessarily abnormal. Identify the material (for example, check whether it's ferrous with a magnet), compare it with the manufacturer's limits, and continue inspecting to decide whether the engine is serviceable.
- CIncorrect. Carbon can look like metal, but the material has to be identified, not assumed. Calling it carbon without checking skips the evaluation.
- DIncorrect. Fine particles can come from many wearing parts. Replacing a component on assumption, before identifying the material and evaluating the amount, is not proper practice.
Question 10 · Ignition and Starting Systems
In a magneto, more poles on the rotating magnet means:
- AMore sparks per revolution
- BFewer sparks per revolution
- CNo sparks at all
- DLower secondary voltage always
Show answer and explanation
Answer: A) More sparks per revolution
- ACorrect. The flux reverses more often.
- BIncorrect. More poles add reversals.
- CIncorrect. It still produces sparks.
- DIncorrect. Pole count sets spark rate.
Question 11 · Engine Fuel and Fuel Metering Systems
On a turbine engine with a hydromechanical fuel control, what is the purpose of the specific gravity adjustment?
- ATo let the control meter the correct fuel mass when a fuel of different density is used
- BTo make the fuel schedule compensate for changes in outside air temperature
- CTo change the acceleration schedule so the compressor does not stall
- DTo set the idle and maximum speed stops during engine trimming
Show answer and explanation
Answer: A) To let the control meter the correct fuel mass when a fuel of different density is used
Hydromechanical fuel controls meter fuel by volume, but the engine needs a set fuel mass. The specific gravity adjustment corrects the metering when a fuel of a different density is used.
- ACorrect. The control meters fuel by volume, but the engine needs a set fuel weight (mass). When a fuel of a different specific gravity is used, this adjustment corrects the metering so the engine still gets the right mass flow.
- BIncorrect. The control compensates for temperature automatically through its compressor inlet temperature sensing. This is not a manual adjustment for fuel density.
- CIncorrect. The acceleration schedule is set inside the control from engine parameters. The specific gravity adjustment does not set it.
- DIncorrect. Idle speed and maximum speed (trim) have their own adjustments. The specific gravity adjustment only corrects for fuel density.
Question 12 · Reciprocating Engine Induction and Cooling Systems
Carburetor (throttle) ice is most likely to form when the throttle is:
- AWide open, because maximum airflow gives maximum venturi cooling
- BPartly closed, because the throttle valve restriction adds cooling
- CWide open, because fuel flow and vaporization cooling are greatest
- DSet anywhere, because only outside air temperature affects icing
Show answer and explanation
Answer: B) Partly closed, because the throttle valve restriction adds cooling
Throttle ice is most likely with the throttle partly closed. The added restriction at the throttle valve increases cooling on top of venturi and fuel-vaporization cooling.
- AIncorrect. At wide-open throttle the throttle valve causes little restriction, so its extra cooling is smallest. Throttle ice is less likely there.
- BCorrect. Throttle ice usually forms at or near a partly closed throttle, as at off-idle or cruise power. The restriction at the throttle valve adds to the venturi and fuel-vaporization cooling.
- CIncorrect. Fuel vaporization does cool the air, but the partly closed throttle valve is what makes ice most likely. Full throttle is not the worst case.
- DIncorrect. Temperature and humidity matter, but throttle position also affects icing. A partly closed throttle makes ice more likely.
Question 13 · Turbine Engine Air Systems
What does an active clearance control (ACC) system do on a high-bypass turbofan engine?
- AOpens compressor bleed valves at low rpm to keep the rear stages from stalling
- BChanges the angle of the compressor stator vanes to match airflow to rotor speed
- CSprays cool fan air onto the engine case at high power so the blade tip gap gets smaller
- DLines the case with abradable rub strips so the blades wear in a fixed tip gap
Show answer and explanation
Answer: C) Sprays cool fan air onto the engine case at high power so the blade tip gap gets smaller
Active clearance control uses cool fan air, controlled by the FADEC, to shrink the engine case. This reduces blade tip clearance and improves efficiency when the engine needs it most.
- AIncorrect. This describes the compressor bleed or surge valve system. It manages stall margin, not blade tip clearance.
- BIncorrect. This describes variable stator vanes. They set the angle at which air enters the rotor blades, not the gap between the blade tips and the case.
- CCorrect. When tight clearance is needed, the FADEC sends cool fan discharge air over the case. The case shrinks and the tip clearance goes down. When the air is shut off, the case expands back to its normal size.
- DIncorrect. Abradable shrouds are a passive way to control clearance. ACC is an active system that changes case size with cooling air during operation.
Question 14 · Engine Exhaust and Reverser Systems
On a high-bypass turbofan with a cascade-type reverser, what happens when the reverser is commanded to deploy?
- AThe translating sleeve moves aft, blocker doors close off the fan duct, and the exposed cascade vanes turn fan air forward
- BTwo clamshell doors rotate into the hot exhaust stream behind the core nozzle and deflect the core gases forward
- CThe cascade vanes swirl the hot core exhaust outward to spoil forward thrust without reversing the direction of the flow
- DBucket-type target doors pivot closed behind the exhaust nozzle and deflect the entire exhaust flow forward and outward
Show answer and explanation
Answer: A) The translating sleeve moves aft, blocker doors close off the fan duct, and the exposed cascade vanes turn fan air forward
In a cascade reverser, the translating sleeve moves aft and blocker doors divert fan air through cascade vanes that turn it forward. Clamshell and bucket/target reversers block the exhaust stream mechanically instead.
- ACorrect. In a cascade reverser, blocker doors divert the fan stream outward through the cascade vanes. The vanes turn the flow forward and produce reverse thrust.
- BIncorrect. This describes a mechanical-blockage (clamshell) reverser, which works on the hot exhaust stream. It does not use cascade vanes in the fan duct.
- CIncorrect. The cascade vanes actually turn the fan flow forward to make reverse thrust. They do not just spoil the core exhaust.
- DIncorrect. This describes a target (bucket) reverser, which is a different mechanical-blockage design used mostly on older turbojets and low-bypass engines.
Question 15 · Propellers
The blade face of a propeller is:
- AThe hub bore
- BThe cambered, curved side
- CThe blade tip only
- DThe flat side
Show answer and explanation
Answer: D) The flat side
- AIncorrect. That isn't the face.
- BIncorrect. That's the blade back.
- CIncorrect. The face is a surface.
- DCorrect. The cambered side is the blade back.
Ready for a full AMP practice exam?
These are a sample from the ExamWize question bank. Full practice exams match the real exam's length, time limit and topic weights, with every answer explained.
Original questions written from the official exam outline. Not affiliated with FAA; never copied from the real exam.