Airbus A330 Operational Limitations and Performance Quiz

The correct minimum dispatch weight is 9000 kg, which is the smallest amount of cargo that can be dispatched.

The minimum diversion is the amount of weight that must be diverted to achieve a desired balance in an aircraft. In this case, the correct answer is 4100 kg as stated in the question.

The correct minimum psi for a fuel truck is 50. This level of pressure is important to ensure safe and efficient fuel transfer operations.

A 330-200 aircraft, like the Airbus A330-200, typically requires 138 feet to make a complete 180-degree turn due to its wingspan and turning radius. The incorrect answers are not the correct distance required for this specific aircraft model.

A 330-300 180 turn refers to a full turn in a specific airplane model. The correct answer is 151 feet as it is the calculated distance required for this maneuver.

Pack Flow Low should be switched when the number of passengers is less than 200, which is 60% of its capacity. This ensures optimal performance and efficiency in the system.

The average fuel burn rate of the APU is 200 kg/hour, making it the correct answer. It is important for aircraft operators to monitor and manage the fuel consumption of APUs efficiently to maintain operational efficiency and cost-effectiveness.

The correct answer specifies that during the day, the minimum altitude for a turn with no SID is 400 feet, while during the night it is 1000 feet.

ETOPS stands for Extended Range Twin Operations and it is critical for twin-engine aircraft like the A330 flying long routes over water. The alternate max x-wind is typically calculated as a percentage of the maximum crosswind landing capability of the aircraft to ensure safe operations during a diversion to an alternate airport in case of emergencies. In the case of the A330, the ETOPS alternate max x-wind is 80% of the max x-wind landing (planning), which equates to 32 knots.

The correct answer specifies the average aircraft fuel burn per hour as 5.5 or 100kg/min, with 25 kg/min dedicated for taxi. The incorrect answers differ in their values for fuel burn and do not align with the correct average fuel burn rate.

The maneuvering load acceleration limit for aircraft is typically expressed as a range from negative g-forces (such as -1g) to positive g-forces (such as +2.5g) that the aircraft structure is designed to withstand during flight maneuvers.

The correct answer of 32 knots accounts for the maximum crosswind component that an aircraft is certified to take off in, including gusts. Options 20 knots, 45 knots, and 50 knots are incorrect as they do not align with the specified certification for crosswind limitations during takeoff.

In aviation, the maximum allowable tailwind component for landing in a 330-300 aircraft is typically 15 knots. Exceeding this limit can greatly affect the aircraft's performance and safety during the landing phase.

The maximum tailwind component allowed for an automatic landing when the aircraft weight is 330-300 is 10 knots. This limitation ensures safe landing conditions and reduces the risk of accidents.

The correct answer is 40 knots. This is the maximum demonstrated crosswind that Max has shown capability of handling. It is important for pilots to be aware of the maximum crosswind limitations for their aircraft to ensure safe operations.

The correct answer is 40 knots for door operation, with a higher limit of 50 knots if the wind is blowing directly into the door. This ensures safe operation and prevents damage to the door mechanism.

The maximum wind speed for cargo operation is typically limited to 40 knots, but can increase to 50 knots if the wind is blowing directly into the cargo operation. This ensures safe handling of cargo and aircraft during loading and unloading procedures.

In aviation, passenger/cargo doors are required to be closed when wind speeds reach or exceed 60 knots to ensure the safety of the aircraft and its occupants.

Vmo is the maximum operating speed for a specific aircraft, typically expressed in knots indicated airspeed or Mach number. The correct Vmo range for the aircraft in question is 330 to FL300. The other options provided are not accurate representations of Vmo.

Mmo in aviation refers to the maximum operating speed of an aircraft, typically given as a Mach number for a specific altitude range.

The maximum allowable tailwind component for a Boeing 737-800 aircraft is 10 knots. This limit is important to ensure safe takeoff and landing operations, as excessive tailwinds can affect the aircraft's performance and handling.

The enhanced max crosswind for the 330-200 aircraft is 45 knots, which indicates the maximum crosswind component that the aircraft can safely operate in.

Flap 1 speed refers to the airspeed at which the aircraft's flaps should be extended to the first position. In this case, the correct Flap 1 speed is 240 knots.

Flap 2a speed refers to the specific speed at which the flaps are set at position 2a with the slats at position 1 to ensure optimal aircraft performance during approach and landing. It is important for pilots to know this speed to maintain safe operations during these critical phases of flight.

Flap 2 speed is the speed at which the flaps and slats are set to position 2, which is crucial for the aircraft's performance during takeoff and landing.

Flap 3 speed refers to the speed at which an aircraft should be flying when the flaps are set at position 3. The correct flap 3 speed is 186 knots to ensure proper aerodynamic performance and safety during takeoff and landing.

The correct maximum altitude for flap slats extension is 20,000 feet. At altitudes above this limit, the aircraft must retract the flap slats to prevent damage and ensure safe operation.

In aviation, VLE commonly refers to 'Velocity Limitation Envelope', indicating the maximum allowable speed for a particular aircraft.