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Aviation Maintenance Technician, Second Class (AMT2) SWE Practice Exam

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About this Exam

Prepare with the Aviation Maintenance Technician, Second Class (AMT2) SWE Practice Exam practice quiz. This question bank includes 10 questions covering engine, tubed, tire, aviation, and maintenance. Use it to review important concepts, identify knowledge gaps, and build confidence for the related exam, course, or assessment.

Sample Questions

Question 1
A tubed tire at 160 psi requires slippage marks?
No
Yes, because it has a tube
Yes, only if pressure is 150 or less
No, tubes do not matter
Explanation:
Slippage marks are used to detect movement of the inner tube inside a tubed tire. When a tire has a tube, the tube can slip or rotate relative to the tire and rim under pressure, which can lead to improper seating or pinch flats. Marking the tire and tube lets you see any subsequent slip during service. This requirement applies because a tube is present, not because of a specific pressure value. Therefore, a tubed tire at 160 psi should have slippage marks. Tubeless tires don’t have an inner tube, so this check isn’t needed for them.
Question 2
What is the size of the clear heat shrinkable tubing used with the label near engine hoses?
1-1/4 inch
2 inch
3 inch
2-1/2 inch
Explanation:
The size is chosen to give enough coverage for the label while still fitting snugly around the hose after shrinking. When labeling hoses in an engine area, you want a clear tube big enough to fit over the hose and the label and then shrink down to a secure, readable wrap. A 2-1/2 inch final recovered diameter provides that balance for typical engine hoses: large enough to cover the label and a section of hose, yet small enough to shrink tightly and stay in place. Smaller sizes wouldn’t fully cover the label, and a much larger size would not form a tight, secure wrap. The result is a protected, legible label that can withstand heat and fluids in the engine bay.
Question 3
ATF3 lead generator T3 is connected to which connector code?
X5017A6C
X5017A6B
X5020A6B
X5013A7B
Explanation:
Understanding how to read connector codes on the wiring diagram is essential for tracing circuits and verifying installations. For the ATF3 lead generator T3, the diagram shows its lead wires terminating at a specific connector. The code X5017A6B identifies the exact connector and harness variant used for that circuit in this configuration. The X prefix denotes a connector, the numeric portion pinpoints the particular unit, and the suffix A6B indicates the harness variant and position used here. Because the T3 circuit in the diagram routes to X5017A6B, that code is the correct match for this installation. The other codes refer to different connectors or harness variants and would not align with T3’s wiring and pinout in this setup. To verify on the actual schematic, locate the ATF3/T3 symbol, follow the wiring to the connector legend, and confirm that the connection shown is X5017A6B.
Question 4
If the unit requires additional refrigerant, what will you observe in the sight glass?
Steady flow
No change
Bubbles will be present
Vapor lock
Explanation:
When refrigerant is needed, the sight glass will show bubbles. This happens because the pressure drop through the metering device causes some of the liquid refrigerant to flash into vapor as it passes the sight glass. In a properly charged system, the sight glass generally looks clear with a steady flow of liquid and little to no bubbling. Vapor lock isn’t the typical observation here; it would imply a blockage or obstruction due to vapor buildup, not just undercharge.
Question 5
How is cabin pressure controlled at altitude?
The pilot manually controls the cabin altitude via a dial.
Cabin pressure is maintained by ballast only with no automatic control.
Outflow valve is controlled manually.
The pressure controller automatically monitors cabin pressure and controls the outflow valve to maintain the desired cabin altitude.
Explanation:
Maintaining cabin pressure at altitude is done with an automatic feedback loop. The crew selects a desired cabin altitude, and sensors monitor the actual cabin pressure. The pressure controller compares the sensed pressure to the setpoint and automatically commands the outflow valve to open or close. If cabin pressure is too high, the valve opens more to vent air; if too low, the valve closes to retain air. This automatic regulation keeps the cabin at the chosen altitude while also managing the rate of pressurization and protecting against overpressure with relief valves as a safety backup.

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Additional Information

Aviation Maintenance Technician, Second Class (AMT2) SWE Practice Exam

This practice set contains 10 questions from the matching question bank and focuses on engine, tubed, tire, aviation, and maintenance. Work through each question carefully, review the provided solutions, and revisit topics that need more study before your next attempt.

This is an independent study resource intended for practice and review; it is not an official examination or an endorsement by any organization named in the title.

Frequently Asked Questions

This quiz contains a total of 10 practice questions carefully selected to test your knowledge on this subject.
Yes, you will have exactly 0 minutes to complete the exam. A countdown timer will be visible once you start.
Yes, you can retake this practice test as many times as you need. The questions and options may be randomized on subsequent attempts to ensure comprehensive learning.

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