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- Subject
- Airport Engineeringcivil-engineering-mcqs › airport-engineering
- Published
- 19 Jan 2019
- Last updated
- 28 May 2026
Explanation
The maximum gross take-off weight of an aircraft is greater than its maximum structural landing weight. This is because the aircraft typically burns fuel during flight, reducing weight before landing, so the landing weight limit is set lower to ensure structural safety upon touchdown.
More Airport Engineering MCQs
Practice related questions from the same subject.
- 1.Assertion (A): The proportion of incoming and outgoing flights affects the airport's capacity. Reason (R): Landing operations are usually prioritized over departures. Choose the correct option:
- 2.Which of the following statements accurately describe ICAO's recommendations for adjusting the basic runway length?
- 3.What is the required length of the clear zone for a non-instrument runway used by small aircraft?
- 4.According to ICAO standards, what is the minimum required runway length for airports classified as type A and type E?
- 5.An aircraft cruises at a speed of 500 km/h. If it encounters a headwind blowing at 50 km/h, what will be its airspeed and ground speed respectively?
- 6.What is the wind speed threshold below which the calm period is measured as a percentage of time?
- 7.Per ICAO guidelines, what color are all the markings on runways required to be?
- 8.What are the width and spacing of the transverse centerline bars along the extended centerline of a runway in an approach lighting system?
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