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AMG · 8% of the exam

Cleaning and Corrosion Control practice questions

10 free Cleaning and Corrosion Control questions for the Aviation Mechanic General (AMG) Knowledge Test exam, each with the correct answer and an explanation for every option.

What this domain covers

Identifying, preventing and treating corrosion and cleaning aircraft.

Exam weight
8%
On a real exam
≈ 5 questions
In our bank
48 questions

Topics that come up most

  • Types of corrosion
  • Causes and conditions
  • Corrosion removal
  • Protective treatments
  • Cleaning materials and methods

How to study it

Learn each corrosion type with how it appears and how it's treated; questions describe what you see.

Sample Cleaning and Corrosion Control questions

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

  1. Question 1

    What does corrosion on magnesium alloy parts usually look like?

    • AWhite, powdery, snow-like deposits
    • BRed-brown rust scale
    • CGreen deposits only
    • DShiny bright metal
    Show answer and explanation

    Answer: A) White, powdery, snow-like deposits

    • ACorrect. Magnesium corrosion products appear as white powdery spots.
    • BIncorrect. Red-brown rust is iron oxide on steel.
    • CIncorrect. Green deposits are typical of copper alloys.
    • DIncorrect. Corrosion dulls the surface.
  2. Question 2

    In galvanic corrosion on an aircraft, what usually serves as the electrolyte?

    • ASealant
    • BDry air trapped in joints
    • CPaint
    • DMoisture, especially salt water
    Show answer and explanation

    Answer: D) Moisture, especially salt water

    • AIncorrect. Sealant keeps electrolyte out.
    • BIncorrect. Dry air is a poor electrolyte.
    • CIncorrect. Intact paint separates metal from moisture.
    • DCorrect. Moisture completes the circuit between the metals.
  3. Question 3

    What does uniform surface corrosion look like on a metal surface?

    • ADeep, isolated pits with white powder inside them
    • BA general roughening or etching of the surface
    • CWorm-like trails under paint
    • DLayers of metal lifting apart
    Show answer and explanation

    Answer: B) A general roughening or etching of the surface

    • AIncorrect. Isolated deep cavities describe pitting corrosion.
    • BCorrect. Uniform attack spreads evenly over the exposed surface.
    • CIncorrect. That describes filiform corrosion.
    • DIncorrect. That describes exfoliation corrosion.
  4. Question 4

    Why should engine exhaust deposits on the aircraft skin be removed promptly?

    • AThey are corrosive and collect in seams, hinges, and fairings downstream of the exhaust
    • BThey are corrosive only while hot, so they must be removed before the skin cools down
    • CThey form a hard carbon film that is harmless to metal but dulls the paint's appearance
    • DThey are corrosive mainly to the cowling surfaces located forward of the exhaust stacks
    Show answer and explanation

    Answer: A) They are corrosive and collect in seams, hinges, and fairings downstream of the exhaust

    Engine exhaust deposits are very corrosive. They build up in the exhaust trail area, especially in gaps, seams, hinges, and fairings downstream of the exhaust, so they should be cleaned off promptly.

    • ACorrect. FAA corrosion guidance identifies exhaust trail areas as corrosion-prone. The deposits are very corrosive and give particular trouble where gaps, seams, hinges, and fairings lie downstream of the exhaust outlets. Trapped deposits can escape normal cleaning.
    • BIncorrect. Exhaust residue stays corrosive after it cools. The concern is ongoing attack on the metal, especially where moisture and residue are trapped.
    • CIncorrect. Removing the deposits is not just cosmetic. They are corrosive to the skin and its finish.
    • DIncorrect. The airflow carries exhaust products aft. The exhaust trail area downstream of the stacks or nozzles is where the deposits collect and cause corrosion.
  5. Question 5

    Electrolyte has leaked from a lead-acid battery onto the battery box and nearby structure. Which solution should be applied to neutralize the deposits before rinsing and inspecting for corrosion?

    • AA dilute boric acid solution
    • BA sodium bicarbonate (baking soda) solution
    • CA dilute acetic acid (vinegar) solution
    • DMethyl ethyl ketone (MEK) solvent
    Show answer and explanation

    Answer: B) A sodium bicarbonate (baking soda) solution

    Lead-acid batteries use sulfuric acid electrolyte, which is neutralized with a mild base: sodium bicarbonate solution. Boric acid (and other weak acids) is for the alkaline electrolyte of nickel-cadmium batteries.

    • AIncorrect. Boric acid is a weak acid used to neutralize the alkaline potassium hydroxide electrolyte of nickel-cadmium batteries. It does not neutralize sulfuric acid.
    • BCorrect. FAA corrosion guidance specifies a sodium bicarbonate solution to neutralize sulfuric acid deposits from lead-acid batteries.
    • CIncorrect. Acetic acid is an acid. It cannot neutralize sulfuric acid electrolyte; acidic neutralizers are only suitable for alkaline electrolyte.
    • DIncorrect. MEK is a solvent for cleaning and paint removal. It does not chemically neutralize acid.
  6. Question 6

    Red-brown deposits on a steel part indicate what?

    • AIron oxide (rust)
    • BAluminum oxide
    • CCopper corrosion
    • DFresh primer
    Show answer and explanation

    Answer: A) Iron oxide (rust)

    • ACorrect. Red rust is iron oxide on steel.
    • BIncorrect. That is white or gray.
    • CIncorrect. That is greenish.
    • DIncorrect. This is corrosion.
  7. Question 7

    Corrosion that forms under lap joints, washers or debris where moisture is trapped is called what?

    • AExfoliation corrosion
    • BFiliform corrosion
    • CFretting corrosion from vibration
    • DConcentration cell (crevice)
    Show answer and explanation

    Answer: D) Concentration cell (crevice)

    • AIncorrect. Exfoliation lifts metal in layers along the grain.
    • BIncorrect. Filiform corrosion forms worm-like trails under paint.
    • CIncorrect. Fretting results from small relative motion between parts.
    • DCorrect. Differences in oxygen or ion concentration drive this corrosion.
  8. Question 8

    Why should steel wool not be used to remove corrosion from aluminum?

    • AIt is too expensive to use
    • BIt is too gentle on the metal
    • CIt polishes the surface too much
    • DEmbedded steel particles
    Show answer and explanation

    Answer: D) Embedded steel particles

    • AIncorrect. The problem is contamination.
    • BIncorrect. The problem is contamination.
    • CIncorrect. The problem is contamination.
    • DCorrect. Embedded steel particles cause galvanic corrosion; aluminum wool or approved abrasives are used.
  9. Question 9

    Which corrosion lifts metal in layers, often in extruded parts?

    • AUniform surface
    • BFiliform
    • CFretting
    • DExfoliation
    Show answer and explanation

    Answer: D) Exfoliation

    • AIncorrect. That attacks the surface evenly.
    • BIncorrect. Filiform forms under paint.
    • CIncorrect. Fretting needs relative motion.
    • DCorrect. Exfoliation is a severe intergranular form that delaminates the metal in layers.
  10. Question 10

    Why is sealant often applied to faying surfaces when dissimilar metals are joined?

    • ATo keep moisture out of the joint
    • BTo glue the parts together in place of fasteners
    • CTo make the joint conduct electricity better
    • DTo add weight for balance
    Show answer and explanation

    Answer: A) To keep moisture out of the joint

    • ACorrect. Without an electrolyte, galvanic corrosion cannot proceed.
    • BIncorrect. Fasteners still carry the load.
    • CIncorrect. Sealant's role is moisture exclusion.
    • DIncorrect. Sealant is not used for balance.

Cleaning and Corrosion Control: FAQs

How much of the AMG exam is Cleaning and Corrosion Control?

Cleaning and Corrosion Control is 8% of the AMG exam by the official exam guide's weighting, which on a 60-question form works out to roughly 5 questions. The real exam's exact split varies by form.

What does the Cleaning and Corrosion Control domain cover?

Identifying, preventing and treating corrosion and cleaning aircraft.

How should I study Cleaning and Corrosion Control for AMG?

Learn each corrosion type with how it appears and how it's treated; questions describe what you see.

Where can I practise more Cleaning and Corrosion Control questions?

This page has 10 free Cleaning and Corrosion Control questions with answers. The ExamWize AMG question bank has 48 questions in this domain. Every practice exam result breaks your score down by domain, and Review Mode re-drills the questions you missed.

Get Cleaning and Corrosion Control exam-ready

The full AMG bank has 48 Cleaning and Corrosion Control 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.