AME - Aircraft Maintenance Engineer Maintenance Practices and Materials Questions and Answers

Question 1

An AME is performing a visual inspection on a section of aluminum alloy aircraft skin and observes small, white or gray powdery deposits. This is indicative of which type of corrosion?

Accepted Answer

Surface corrosion

Answer

Surface corrosion is the most common type of corrosion on aluminum and magnesium alloys. It is characterized by a uniform attack on the surface, which first appears as a general dulling or etching of the surface, and then progresses to form white or gray powdery deposits.

Question 2

When performing a dye penetrant inspection, what is the primary purpose of the developer?

Accepted Answer

To draw the penetrant out of the discontinuity by capillary action, making it visible.

Answer

In a liquid dye penetrant inspection, the developer acts as a blotter, drawing the penetrant that has seeped into a crack or flaw back to the surface. This action, known as capillary action, makes the indication visible against the contrasting background of the developer.

Question 3

A castellated nut has been torqued to the minimum specified value, but the cotter pin hole does not align with any of the slots. According to standard maintenance practices, what is the correct procedure?

Accepted Answer

Tighten the nut slightly to align with the next available slot, without exceeding the maximum torque value.

Answer

Standard practice dictates that after reaching the minimum torque value, you may tighten the nut further to align the cotter pin hole with the next slot, as long as the maximum specified torque is not exceeded. Loosening the nut would result in it being under-torqued.

Question 4

Which of the following non-destructive testing (NDT) methods is most suitable for detecting subsurface defects in a non-ferrous material like an aluminum wing spar?

Accepted Answer

Ultrasonic Inspection

Answer

Ultrasonic inspection is highly effective for detecting subsurface flaws like cracks and corrosion in both ferrous and non-ferrous materials. Magnetic particle inspection only works on ferromagnetic materials. Dye penetrant is for surface-breaking defects only. Eddy current is primarily for surface and near-surface defects.

Question 5

During a maintenance task, an AME needs to safety wire a series of three bolts on an engine accessory case. What is the correct procedure for installing the safety wire?

Accepted Answer

The wire should be routed in a way that the tension on the wire counteracts the tendency of the bolt to loosen.

Answer

The fundamental principle of safety wiring is to install the wire in such a manner that it creates a tightening force on the fastener if it starts to loosen. This is often referred to as wiring 'righty-tighty'. While a common rule of thumb is to safety no more than three bolts together, the most critical aspect is the direction of pull.

AME - Aircraft Maintenance Engineer Practice Test

AME - Aircraft Maintenance Engineer Practice Test

AME - Aircraft Maintenance Engineer Maintenance Practices and Materials Questions and Answers