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Non-Metallic Structures practice questions

10 free Non-Metallic Structures 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

Composite, wood and fabric structures and their repair.

Exam weight
7%
On a real exam
≈ 7 questions
In our bank
40 questions

Topics that come up most

  • Composite materials and layups
  • Bonding and curing
  • Wood structures
  • Fabric covering
  • Windows and transparencies

How to study it

Learn the inspection methods for each material; questions ask how a defect is found.

Sample Non-Metallic Structures questions

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

  1. Question 1

    A composite repair is being cured under vacuum with a heat blanket and a hot bonder. How is the cure temperature of the repair normally monitored and controlled?

    • AWith thermocouples placed in contact with the part at the repair and read by the hot bonder
    • BBy relying on the heat blanket's built-in setpoint, with no sensors placed on the part
    • CBy taking an infrared thermometer reading of the bag surface at the start of the cure
    • DBy watching the vacuum gauge, since bag pressure changes as the resin temperature rises
    Show answer and explanation

    Answer: A) With thermocouples placed in contact with the part at the repair and read by the hot bonder

    Heated composite repairs are monitored with thermocouples in contact with the part. The hot bonder uses them to control the cure temperature profile and avoid under-curing or overheating.

    • ACorrect. Enough thermocouples are placed on the part, at locations chosen from a thermal survey, so the controller can track and control the actual repair temperature throughout the cure.
    • BIncorrect. The blanket setpoint does not show the actual part temperature. Heat sinks such as substructure can leave areas under-cured or overheated.
    • CIncorrect. A single surface reading cannot track temperature through the hours-long cure cycle, and the bagging materials hide the true part temperature.
    • DIncorrect. The vacuum gauge checks bag integrity and consolidation pressure, not temperature. Temperature has to be measured directly.
  2. Question 2

    What are microballoons used for in composite work?

    • AAs a release agent on the tool surface
    • BAs the main load-carrying reinforcement
    • CAs a lightweight filler for fairing
    • DAs a catalyst to speed up curing
    Show answer and explanation

    Answer: C) As a lightweight filler for fairing

    • AIncorrect. Release agents are separate products.
    • BIncorrect. Fibers carry the load, not fillers.
    • CCorrect. Mixed with resin, they make a light, sandable filler.
    • DIncorrect. Hardeners and catalysts are separate.
  3. Question 3

    What is the accepted method for removing fine scratches from an acrylic aircraft window?

    • AWipe the area with acetone or lacquer thinner to soften and level the scratch edges
    • BWet-sand with progressively finer abrasive paper, then buff with a polishing compound
    • CDry-sand with a single coarse-grit paper and firm pressure to remove material quickly
    • DBuff hard with a high-speed wheel until surface heat makes the scratches flow out
    Show answer and explanation

    Answer: B) Wet-sand with progressively finer abrasive paper, then buff with a polishing compound

    Fine scratches in acrylic are removed by wet-sanding with progressively finer abrasive paper and then buffing with compound. Solvents, coarse dry sanding and excess heat can craze or distort the plastic.

    • AIncorrect. Solvents such as acetone and lacquer thinner attack acrylic and can cause crazing. Only cleaners approved for transparent plastics should be used.
    • BCorrect. AC 43.13-1B says to sand with 320- or 400-grit paper on a felt or rubber pad, using soapy water as a lubricant. You then move to finer grits and finish by buffing with compound to remove all sanding marks.
    • CIncorrect. Coarse dry sanding cuts deeper scratches and can overheat the surface. The procedure calls for light pressure, a lubricant and progressively finer grits.
    • DIncorrect. Too much heat from buffing softens and distorts acrylic and can leave residual stress that leads to crazing. Polishing should use light pressure and avoid overheating.
  4. Question 4

    What is the primary purpose of vacuum bagging a wet layup composite repair during its cure?

    • ATo supply the heat needed to bring the resin to its cure temperature
    • BTo use atmospheric pressure to consolidate the plies and draw out trapped air
    • CTo serve as a permanent moisture barrier sealing the cured repair
    • DTo monitor the repair temperature so the cure cycle can be controlled
    Show answer and explanation

    Answer: B) To use atmospheric pressure to consolidate the plies and draw out trapped air

    Vacuum bagging is a pressure application method. Atmospheric pressure on the evacuated bag consolidates the plies and removes air, volatiles and excess resin, while heat comes from a separate source.

    • AIncorrect. Cure heat comes from heat blankets, heat lamps or ovens. The vacuum bag only holds pressure, although it is often used together with a heat blanket.
    • BCorrect. Evacuating the bag lets atmospheric pressure press evenly on the repair. This compacts the plies, removes trapped air and volatiles, and helps bleed off excess resin, producing a strong, void-free bond.
    • CIncorrect. The bag, breather and release films are removed after cure. Environmental protection comes from the finish system that is applied afterward.
    • DIncorrect. Thermocouples and a hot bonder controller monitor and control temperature. The bag itself does not measure anything.
  5. Question 5

    After a wet-layup composite repair is cured, a technician takes readings with a Barcol impressor. What is this test used to evaluate?

    • AWhether the repair resin has reached an adequate degree of cure
    • BWhether a disbond exists between the repair plies and the parent laminate
    • CWhether the laminate has the specified fiber-to-resin volume ratio
    • DWhether the cured patch meets the required thickness and ply count
    Show answer and explanation

    Answer: A) Whether the repair resin has reached an adequate degree of cure

    A Barcol impressor measures surface indentation hardness, which shows whether the resin has cured properly. Disbonds and thickness need other inspection methods.

    • ACorrect. The Barcol impressor measures surface hardness. Readings below the specified value suggest the resin is undercured.
    • BIncorrect. Disbonds and delaminations are found by tap testing or ultrasonic inspection, not by a surface hardness reading.
    • CIncorrect. Fiber volume is controlled by weighing materials and checked by lab methods such as resin burn-off. A hardness test doesn't measure it.
    • DIncorrect. Thickness and ply count are checked by measurement, layup records or ultrasonic methods, not by indentation hardness.
  6. Question 6

    In composite repair drawings, what does a warp clock show?

    • AThe cure time remaining for each ply
    • BThe reference for ply fiber orientation
    • CThe position of each fastener in the repaired panel
    • DThe resin mix ratio for the repair
    Show answer and explanation

    Answer: B) The reference for ply fiber orientation

    • AIncorrect. Cure is tracked with time and temperature records.
    • BCorrect. Each ply's angle is laid up relative to the warp clock.
    • CIncorrect. Fastener layouts are shown separately.
    • DIncorrect. Mix ratios come from the resin data.
  7. Question 7

    Which design feature is commonly built into composite airframe skins to protect them from lightning strike damage?

    • AExpanded copper or aluminum foil or wire mesh at the outer surface
    • BA fiberglass outer ply that insulates the carbon fiber from the strike
    • CStatic dischargers installed along the trailing edges of the surfaces
    • DA resin-rich outer layer that resists arcing at the attachment point
    Show answer and explanation

    Answer: A) Expanded copper or aluminum foil or wire mesh at the outer surface

    Composite structures are typically protected by a conductive layer, such as expanded metal foil or wire mesh at the outer surface, that carries lightning current. Repairs must restore this protection system.

    • ACorrect. Composites conduct electricity poorly. Metal mesh, foil or wires near the outer surface give the strike current a conductive path, which limits damage to the laminate.
    • BIncorrect. Fiberglass isolation plies are used to prevent galvanic corrosion between carbon fiber and aluminum. An insulating ply does not conduct strike current away, so it does not provide lightning protection.
    • CIncorrect. Static wicks bleed off precipitation static to reduce radio interference. They are not designed to carry lightning strike current.
    • DIncorrect. Extra resin is a non-conductor. It does not provide a current path and would not prevent strike damage.
  8. Question 8

    Why must a technician use exactly the manufacturer's resin-to-hardener mix ratio when laying up a composite repair?

    • AAn off-ratio mix cures improperly, reducing strength and heat and chemical resistance
    • BAdding extra hardener is the approved way to shorten the cure time
    • CThe ratio affects only pot life, so the cured strength is unchanged
    • DExtra resin is harmless because vacuum bagging bleeds the excess out
    Show answer and explanation

    Answer: A) An off-ratio mix cures improperly, reducing strength and heat and chemical resistance

    The resin-to-hardener ratio controls how completely the resin cures. Changing it, even to speed up the cure, reduces the strength, thermal resistance and chemical resistance of the repair.

    • ACorrect. The ratio sets how completely the resin cross-links. Too much or too little hardener leaves the matrix under-cured or brittle, which lowers its strength, thermal resistance and chemical resistance.
    • BIncorrect. FAA guidance specifically says not to change the ratio to alter cure time. Cure time is controlled by temperature and the cure schedule.
    • CIncorrect. An off-ratio mix changes the cured properties, not just the working time. Leftover unreacted resin or hardener weakens the matrix.
    • DIncorrect. Bleeding removes excess volume of the mixed resin. It does not fix a chemically off-ratio mix, which will still cure improperly.
  9. Question 9

    A wet layup composite repair has been bagged and pulled down with a pump. Before heat is applied to cure it, what check is normally made?

    • ATap-test the uncured plies with a coin to find voids and disbonds
    • BShut off the pump and watch the gauge for any drop in vacuum over a set time
    • CLook at the breather and bleeder for full resin saturation to confirm proper resin content
    • DCheck a witness cup of mixed resin to confirm it has fully gelled and hardened
    Show answer and explanation

    Answer: B) Shut off the pump and watch the gauge for any drop in vacuum over a set time

    Before cure, the bagged repair is leak-checked. The pump is isolated and the gauge is watched for vacuum drop to confirm the bag will hold compaction pressure through the cure cycle.

    • AIncorrect. Tap testing is a nondestructive inspection done after cure. Uncured plies can't give a meaningful result.
    • BCorrect. FAA guidance calls for checking the bagged repair for leaks before cure. In a drop test, the pump is isolated and the gauge is watched for a specified time. A leak would reduce compaction pressure and could let air into the laminate.
    • CIncorrect. The bleeder absorbs excess resin during cure, so saturation can't be judged before heat is applied. A saturated breather also blocks vacuum.
    • DIncorrect. A witness sample is used to confirm cure after the cycle. Gelled resin before the bag is checked would mean the working time has already run out.
  10. Question 10

    How should acrylic windshields generally be cleaned?

    • AGasoline
    • BMild soap and water
    • CDry paper towels
    • DAbrasive cleaner
    Show answer and explanation

    Answer: B) Mild soap and water

    • AIncorrect. Solvents can craze acrylic.
    • BCorrect. Use mild soap, water and a soft cloth; many solvents craze acrylic.
    • CIncorrect. These scratch the surface.
    • DIncorrect. This scratches the surface.

Non-Metallic Structures: FAQs

How much of the AMA exam is Non-Metallic Structures?

Non-Metallic Structures is 7% of the AMA exam by the official exam guide's weighting, which on a 100-question form works out to roughly 7 questions. The real exam's exact split varies by form.

What does the Non-Metallic Structures domain cover?

Composite, wood and fabric structures and their repair.

How should I study Non-Metallic Structures for AMA?

Learn the inspection methods for each material; questions ask how a defect is found.

Where can I practise more Non-Metallic Structures questions?

This page has 10 free Non-Metallic Structures questions with answers. The ExamWize AMA question bank has 40 questions in this domain. Every practice exam result breaks your score down by domain, and Review Mode re-drills the questions you missed.

Get Non-Metallic Structures exam-ready

The full AMA bank has 40 Non-Metallic Structures 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.