AMA · 6% of the exam
Aircraft Electrical Systems practice questions
10 free Aircraft Electrical Systems 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
Airframe electrical systems: wiring, distribution and protection.
- Exam weight
- 6%
- On a real exam
- ≈ 6 questions
- In our bank
- 36 questions
Topics that come up most
- Wire types and installation
- Circuit protection
- Bus systems
- Batteries
- Electrical load analysis
How to study it
Practise electrical load analysis calculations; they are reliable marks.
Sample Aircraft Electrical Systems questions
Try each one before opening the answer. Original questions written to the official exam objectives.
Question 1
What is the function of the overvoltage relay or sensor in an aircraft generating system?
- AVaries generator field current to hold output voltage steady
- BDisconnects the generator when the battery discharges back into it
- CTrips the generator off line when output exceeds a preset limit
- DBalances load sharing between paralleled generators on the bus
Show answer and explanation
Answer: C) Trips the generator off line when output exceeds a preset limit
Overvoltage protection is a fault-protection device. It takes the generator off line when output voltage goes above a safe limit, protecting the bus and connected equipment.
- AIncorrect. That is the voltage regulator's job. The overvoltage device is a protective backup that acts when regulation has failed.
- BIncorrect. That is the reverse-current relay (cutout), which opens when generator output drops below battery voltage.
- CCorrect. If voltage rises above a safe limit, for example after a regulator failure, the overvoltage protection de-energizes the generator and disconnects it from the bus. This protects connected equipment from damage.
- DIncorrect. Load sharing between paralleled generators is handled by paralleling or equalizing circuits that adjust each generator's field, not by overvoltage protection.
Question 2
A technician is adding avionics equipment to an aircraft. What is the main purpose of the electrical load analysis done for this alteration?
- ATo confirm the power sources can supply the total connected load, including the new equipment
- BTo select the wire gauge for the new circuit based on its length and allowable voltage drop
- CTo choose a circuit breaker rating that opens before the new circuit's wire overheats
- DTo find out how the new equipment's weight changes the aircraft's center of gravity
Show answer and explanation
Answer: A) To confirm the power sources can supply the total connected load, including the new equipment
An electrical load analysis checks that the aircraft's power sources can supply all of the connected loads in probable combinations, so it must be redone when equipment is added. Wire sizing, breaker selection, and weight and balance are separate tasks.
- ACorrect. A load analysis adds up the electrical loads in probable combinations and for probable durations. This shows whether the generators/alternators and other power sources can still supply every circuit after the new equipment is added.
- BIncorrect. Wire size is chosen from current, run length, and allowable voltage drop for each circuit. That is a separate task from checking the capacity of the whole system.
- CIncorrect. Sizing a circuit protective device protects a single wire run. It does not tell you whether the power sources can carry the total load.
- DIncorrect. That is a weight-and-balance calculation, not an electrical load analysis.
Question 3
A resettable, trip-free circuit breaker protects an aircraft circuit. An overload occurs while someone is holding the breaker's operating handle in the closed (pushed-in) position. How should the breaker respond?
- AIt opens the circuit even though the handle is being held in the closed position
- BIt keeps the circuit closed while the handle is held, then trips once the handle is released
- CIt opens briefly and then recloses by itself as soon as the overload current falls off
- DIt opens the circuit only after the bus voltage drops below the breaker's rated value
Show answer and explanation
Answer: A) It opens the circuit even though the handle is being held in the closed position
A trip-free circuit breaker opens the circuit during an overload or fault even if its handle is held closed. 14 CFR 25.1357(c) requires this of each resettable circuit protective device.
- ACorrect. A trip-free breaker opens the circuit whenever an overload or fault exists, whatever position the operating control is in. 14 CFR 25.1357(c) requires this of each resettable circuit protective device, so holding the handle in cannot override the protection.
- BIncorrect. This describes a breaker that is not trip-free: holding the control in would defeat the protection and let an overloaded circuit overheat. Trip-free design exists to prevent this.
- CIncorrect. This describes an automatic-reset device. 14 CFR 25.1357(g) allows those only as integral equipment protectors (such as thermal cut-outs), and only when separate protection covers the cable. A trip-free breaker stays open until someone resets it.
- DIncorrect. A circuit breaker responds to overcurrent (an overload or fault), not to low bus voltage. Undervoltage is not what trips it.
Question 4
In a split-bus aircraft electrical system, which bus is arranged so that it can be powered from backup sources such as the battery, keeping equipment needed for continued safe flight working after a generator failure?
- AThe essential bus
- BThe nonessential bus
- CThe tie bus
- DThe ground service bus
Show answer and explanation
Answer: A) The essential bus
The essential bus groups the loads needed for safe flight and can be powered from backup sources after a generator failure. Nonessential loads are shed to protect the remaining capacity.
- ACorrect. The essential bus carries the loads needed for safe flight and is arranged so that it can be powered from alternate sources, such as the battery or a remaining generator, after a power-source failure.
- BIncorrect. The nonessential bus carries loads that can be shed, and it is usually among the first to be disconnected when generating capacity is lost.
- CIncorrect. A tie bus connects or parallels other buses and power sources. Its job is not to hold the critical flight loads.
- DIncorrect. A ground service bus powers servicing loads, such as cabin and cargo lighting, from external or battery power on the ground. It is not intended for critical in-flight equipment.
Question 5
What is the primary purpose of the identification markings printed or stamped at intervals along aircraft electrical wires?
- ATo show where the wire bundle must be supported by clamps
- BTo show the rating of the circuit breaker protecting the wire
- CTo record the date of the wire's last insulation test
- DTo identify the wire and the circuit or function it is part of
Show answer and explanation
Answer: D) To identify the wire and the circuit or function it is part of
Wire identification markings identify each wire and the circuit or function it belongs to, so the wiring can be traced against diagrams during maintenance. They do not show clamp locations, breaker ratings or test dates.
- AIncorrect. Clamp spacing and locations come from the installation drawings and standard practices. Wire identification codes do not mark support points.
- BIncorrect. Circuit protection ratings come from the wiring diagrams and electrical load data. They are not what the wire identification code is for.
- CIncorrect. Inspection and test results go in the maintenance records. Wire markings have to stay the same and stay legible for the wire's whole service life.
- DCorrect. Wire identification codes identify each wire and the circuit or function it serves, so technicians can trace the wiring against the wiring diagrams. 14 CFR 25.1711(a) requires wiring components to be identified by a consistent method that shows the component and its function, and 25.1711(c) requires the markings to stay legible for the component's service life.
Question 6
Under AC 43.13-1B, what is the maximum number of terminals generally installed on one terminal-strip stud?
- AEight
- BTwo
- CFour
- DNo limit
Show answer and explanation
Answer: C) Four
- AIncorrect. That exceeds the general limit.
- BIncorrect. Up to four are generally allowed.
- CCorrect. More than four terminals on one stud is not recommended.
- DIncorrect. The guidance sets a maximum of four.
Question 7
When selecting the wire size for an aircraft electrical circuit, which two factors are primarily used?
- AThe type of terminal lug used and the system's nominal voltage
- BThe current to be carried and the allowable voltage drop
- CThe generator output rating and the number of splices in the run
- DThe insulation color code and the spacing of the bundle clamps
Show answer and explanation
Answer: B) The current to be carried and the allowable voltage drop
Aircraft wire is sized so it can carry the circuit current without overheating and so the voltage drop over the run stays within allowable limits.
- AIncorrect. The terminal lug is chosen to fit the wire after the wire size is set. Nominal voltage alone does not set conductor size. What matters is the voltage drop allowed for that system.
- BCorrect. The wire must carry the circuit's current without overheating. It must also keep the voltage drop over the length of the run within allowable limits. AC 43.13-1B Chapter 11 sizes wire using these two factors.
- CIncorrect. Each circuit's wire is sized for that circuit's own load, not for the total generator output. Splices are kept to a minimum, but they do not set the wire gauge.
- DIncorrect. Insulation color is for identification, and clamp spacing is about supporting the bundle. Neither one decides the conductor size.
Question 8
In a DC generator system, which device keeps the battery from discharging back through the generator when the engine is at low RPM and generator output voltage drops below battery voltage?
- AThe voltage regulator
- BThe current limiter
- CThe reverse current relay
- DThe overvoltage relay
Show answer and explanation
Answer: C) The reverse current relay
A reverse current relay (cutout) disconnects the generator from the battery when generator voltage drops below battery voltage, so the battery can't discharge back through the generator. Voltage regulators, current limiters and overvoltage relays protect against other conditions.
- AIncorrect. The voltage regulator adjusts generator field current to hold output voltage at a set value. It does not open the line between the generator and the battery when current reverses.
- BIncorrect. The current limiter keeps the generator from putting out more than its rated current. It protects against overload, not against reverse current from the battery.
- CCorrect. The reverse current relay (cutout) opens the generator-to-bus circuit when generator voltage falls below battery voltage and current starts to flow back into the generator. This disconnects the generator from the battery, as 14 CFR 27.1351(c) requires.
- DIncorrect. The overvoltage relay (overvoltage control) acts when generator voltage goes too high, which is the opposite of the low-RPM condition in the question.
Question 9
A circuit breaker installed in an individual aircraft circuit is primarily sized to protect which of the following?
- AThe wiring in that circuit from overheating caused by overcurrent
- BThe connected equipment from failure of its internal components
- CThe generator or alternator from being overloaded by total bus demand
- DThe battery from over-discharge during extended ground operation
Show answer and explanation
Answer: A) The wiring in that circuit from overheating caused by overcurrent
A circuit breaker is rated to protect the wiring in its circuit. It opens on overcurrent before the conductor overheats. Protection for the equipment itself is a separate function.
- ACorrect. The breaker rating is matched to the wire so the circuit opens before the conductor overheats and its insulation is damaged or catches fire. 14 CFR 25.1357(g) describes circuit protection as protecting the cable to the equipment.
- BIncorrect. Protection inside a unit, such as a thermal cut-out, protects the equipment itself. 25.1357(g) allows such protectors only if there is also circuit protection for the cable, which is the circuit breaker's job.
- CIncorrect. A branch breaker is sized for the current of its own circuit. Overload protection for the generator is handled separately in the power generation and control system.
- DIncorrect. A circuit breaker responds to excess current in its circuit. It does not sense battery state of charge or prevent a battery from being run down.
Question 10
Under AC 43.13-1B, how often are wire identification markings generally placed along a wire?
- AWires are not marked
- BOnly once, at one end of each wire
- CEvery 10 feet
- DAt intervals of not more than about 15 inches
Show answer and explanation
Answer: D) At intervals of not more than about 15 inches
- AIncorrect. Wire identification is required.
- BIncorrect. Markings are spaced along the wire.
- CIncorrect. That is too far apart.
- DCorrect. Markings also appear near each end.
Aircraft Electrical Systems: FAQs
How much of the AMA exam is Aircraft Electrical Systems?
Aircraft Electrical Systems 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 Aircraft Electrical Systems domain cover?
Airframe electrical systems: wiring, distribution and protection.
How should I study Aircraft Electrical Systems for AMA?
Practise electrical load analysis calculations; they are reliable marks.
Where can I practise more Aircraft Electrical Systems questions?
This page has 10 free Aircraft Electrical Systems 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.
Other AMA topics
- Metallic Structures10% of the exam
- Non-Metallic Structures7% of the exam
- Flight Controls6% of the exam
- Airframe Inspection10% of the exam
- Landing Gear Systems6% of the exam
- Hydraulic and Pneumatic Systems7% of the exam
- Environmental Systems6% of the exam
- Aircraft Instrument Systems6% of the exam
- Communication, Light Signals, and Runway Lighting Systems6% of the exam
- Aircraft Fuel Systems6% of the exam
- Ice and Rain Control Systems6% of the exam
- Airframe Fire Protection Systems6% of the exam
- Rotorcraft Fundamentals6% of the exam
- Water and Waste Systems6% of the exam
Also: 15 free questions across all topics, the AMA cheat sheet and the study guide.
Get Aircraft Electrical Systems exam-ready
The full AMA bank has 36 Aircraft Electrical Systems 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.