Federal Aviation Regulations Quiz
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Which of the following is a requirement for safety policy?
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Safety objectives
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Commitment of the certificate holder
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A reporting policy
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All of the above
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Flying has become the best and fastest travel option one can experience. Whether for business or pleasure, a passenger will always look forward for the cozy seats and the warm welcome and hospitality of the flight crew. On the other hand, a lot of negative thoughts have occurred because of air disasters caused by either engine failure or human error. See moreThe safety of passengers can no longer be discerned. With this, a lot of strict regulations have been implemented.
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Under FAA Rules for Personnel and Cargo Accommodation, which of the following is NOT safe for doors and exits?
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Each external door must be operable only from the outside
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Direct visual inspection of the locking mechanisms of doors and exits
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The passenger entrance door must qualify as a floor level emergency exit
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An evacuation demonstration must be conducted
Correct Answer
A. Each external door must be operable only from the outsideExplanation
According to FAA Rules for Personnel and Cargo Accommodation, each external door must be operable from both the inside and the outside for safety reasons. This allows passengers and crew members to enter or exit the aircraft in case of an emergency. Therefore, the statement that says "Each external door must be operable only from the outside" is not safe and does not comply with FAA regulations.Rate this question:
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- 3.
Which of the following is the primary or first standard requirement for turbine engine gyroscopic loads?
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A yaw velocity of 2.5 radius per second
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The conditions prescribed in FARs 23.351 and 23.423
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A pitch velocity of 1.0 radians per second
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A normal load factor of 2.5
Correct Answer
A. The conditions prescribed in FARs 23.351 and 23.423Explanation
The primary or first standard requirement for turbine engine gyroscopic loads is the conditions prescribed in FARs 23.351 and 23.423. These Federal Aviation Regulations outline the specific conditions and standards that must be met for turbine engine gyroscopic loads.Rate this question:
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- 4.
Under FAA operating limitations and information, which of the following is NOT applicable under the Minimum Flight Crew requirements?
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Workload of each crew member
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Flight path control
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Collision avoidance
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Command conference before take off
Correct Answer
A. Command conference before take offExplanation
A command conference before takeoff is not applicable under the Minimum Flight Crew requirements according to FAA operating limitations and information. This means that it is not necessary for the crew members to have a conference or meeting before taking off. The other options, such as workload of each crew member, flight path control, and collision avoidance, are all applicable and important considerations for the minimum flight crew requirements.Rate this question:
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Which of the following should be retracted during a lateral and directional trim?
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Landing gear and wing flaps
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wheels and engine brakes
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Tail and front end flaps
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None of the above
Correct Answer
A. Landing gear and wing flapsExplanation
During a lateral and directional trim, the aircraft's landing gear and wing flaps should be retracted. Retracting the landing gear helps reduce drag and improves the aircraft's aerodynamic efficiency. Similarly, retracting the wing flaps reduces lift and drag, allowing the aircraft to maintain a desired trim level. By retracting these components, the aircraft can achieve better control and stability during lateral and directional maneuvers.Rate this question:
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- 6.
Which of the following is a critical information with the airplane in the landing configuration?
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Flaps are initiated
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Landing gears are ready
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Maximum weight of the airplane
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Brakes are in a stable condition
Correct Answer
A. Maximum weight of the airplaneExplanation
The maximum weight of the airplane is a critical piece of information in the landing configuration because it determines the performance and safety of the aircraft during landing. Exceeding the maximum weight limit can lead to difficulties in controlling the aircraft, longer landing distances, and potential damage to the landing gear or other components. Therefore, knowing the maximum weight of the airplane is essential for ensuring a safe and successful landing.Rate this question:
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- 7.
In case of engine failure during take off, on what speed should the pilot decelerate?
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30 knots
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35 knots
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40 knots
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50 knots
Correct Answer
A. 35 knotsExplanation
During takeoff, if there is an engine failure, the pilot needs to decelerate to a safe speed to ensure a controlled landing. The correct answer of 35 knots suggests that this is the appropriate speed at which the pilot should decelerate in such a situation. This speed allows for a balance between maintaining sufficient airspeed for control and maneuverability, while also reducing speed to ensure a safe landing.Rate this question:
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Which of the following is not a part of safety accountability and authority?
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Hazard identification
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Safety risk management
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Safety risk controls
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Disaster preparedness
Correct Answer
A. Disaster preparednessExplanation
Disaster preparedness is not a part of safety accountability and authority because it focuses on preparing for and responding to large-scale emergencies or natural disasters, rather than the day-to-day safety measures and responsibilities that fall under safety accountability and authority. Hazard identification, safety risk management, and safety risk controls are all essential components of safety accountability and authority, as they involve identifying potential hazards, managing and mitigating safety risks, and implementing controls to prevent accidents or injuries.Rate this question:
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Current Version
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Mar 21, 2023Quiz Edited by
ProProfs Editorial Team -
Feb 13, 2016Quiz Created by
Randellobraga38
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