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PoliticasYRegulaciones_4

COMENTARIOS ESTADÍSTICAS RÉCORDS
REALIZAR TEST
Título del Test:
PoliticasYRegulaciones_4

Descripción:
Politicas y Regulaciones

Fecha de Creación: 2025/05/22

Categoría: Otros

Número Preguntas: 20

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The tragedy of TWA Flight 800 in 1996 was a significant event that led to the creation of SFAR 88. What caused the accident?. Engine failure. Pilot error. Fuel tank explosion. Weather conditions.

SFAR 88 requires the use of ___________ to minimize the accumulation of flammable vapors in fuel tanks. Non-flammable insulation. Flame-resistant coatings. Spark-resistant tools. Flammability reduction means.

The AC 25.981 provides guidelines to prevent: Bird strikes. Engine failures. Fuel tank ignition sources. Aircraft corrosion.

SFAR 88 is relevant to the safety of which component of the aircraft electrical system?. Avionics. Wiring harnesses. Cockpit instruments. Lighting systems.

What does 14 CFR 25.981 pertain to in aviation?. Aircraft engine maintenance. Fuel tank explosion prevention. Passenger boarding procedures. Air traffic control protocols.

What is the purpose of 14 CFR 25.981?. To regulate passenger seating arrangements. To prevent fuel tank explosions during flight. To set maximum takeoff weight limits for aircraft. To establish flight crew training requirements.

What must be shown in compliance with 14 CFR 25.981 regarding ignition sources?. Demonstrating lightning protection measures. Determining the lowest possible fuel temperature. Proving the presence of emergency exits. Ensuring no ignition source is present where catastrophic failure could occur.

What are Critical Design Configuration Control Limitations (CDCCLs) required by 14 CFR 25.981?. Features that must be strictly avoided during maintenance. Prohibited fuel additives to prevent ignition. Instructions to protect design features that prevent ignition sources. The maximum fuel capacity allowed in an airplane's tank.

CDCCL stands for: Critical Design Control Limitations. Critical Design Configuration Control Limitations. Controlled Design Configuration Limitations. Configured Design Control Limitations.

The main purpose of CDCCL is to: Prevent fuel tank explosions. Improve aircraft fuel efficiency. Enhance aircraft performance. Ensure compliance with noise regulations.

CDCCL is related to the prevention of ignition sources in: Aircraft engines. Avionics systems. Fuel tanks and fuel tank systems. Passenger cabins.

CDCCL requires operators to: Replace all aircraft components regularly. Record detailed information about passenger behavior. Maintain records of modifications and repairs related to fuel tank safety systems. Conduct annual aircraft inspections.

CDCCL ensures that modifications, repairs, and alterations made to the aircraft are in compliance with the________. Original design standards. Safety guidelines from the FAA. Aircraft maintenance manual. Airworthiness directives (ADs).

What is the purpose of CDCCL in the Airbus A320 AMM?. To provide information on passenger seating configurations. To list the required maintenance tasks for routine inspections. To control critical design features and provide maintenance instructions. To outline emergency procedures for various onboard systems.

What are the consequences of not complying with the CDCCL in the Airbus A320 AMM?. Increased fuel efficiency. Improved passenger comfort. Enhanced aircraft performance. Jeopardizing safety and airworthiness.

How often should the CDCCL information be reviewed and updated in the Airbus A320 AMM?. Every 5 years. Only when major modifications are made to the aircraft. As required by the aircraft manufacturer. At each routine maintenance check.

What are Aircraft Limitation Items (ALI) in the context of aircraft maintenance for Airbus A320 family aircraft?. Required training for maintenance personnel. Specific limitations and conditions for safe maintenance procedures. The number of maintenance tasks performed per day. Instructions for passengers during maintenance activities.

Who is responsible for adhering to Aircraft Limitation Items (ALI) during aircraft maintenance?. Air traffic controllers. Ground handling personnel. Aircraft maintenance engineers and technicians. Flight attendants.

Which of the following could be an example of an Aircraft Limitation Item (ALI) in aircraft maintenance for Airbus A320 family aircraft?. The maximum passenger capacity during maintenance activities. The type of in-flight entertainment available. The maximum number of beverage carts allowed in the cabin. The maximum allowable wind speed for open maintenance hangar doors.

How are Aircraft Limitation Items (ALI) communicated to maintenance personnel for Airbus A320 family aircraft?. Through in-person briefings by the maintenance manager. By referring to the aircraft's maintenance manual and task cards. By sending emails to all maintenance personnel. By conducting training sessions for maintenance personnel.

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