Federal Aviation Regulations Quiz

The correct answer is "all of the above" because all three options mentioned - safety objectives, commitment of the certificate holder, and a reporting policy - are essential requirements for a safety policy. Safety objectives help define the goals and targets for maintaining a safe environment. The commitment of the certificate holder ensures that the organization is dedicated to implementing and enforcing safety measures. A reporting policy establishes a system for reporting and addressing safety concerns, incidents, and near misses. All three components work together to create an effective safety policy.

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.

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.

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.

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.

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.

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.

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.