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发布时间:2024-02-10 07:01:04

[单选题]If the actual takeoff weight is lower than the lowest weight value of a takeoff weight column,
A. use extrapolation
B. Do not takeoff because the speeds cannot be determined.
C. use full thrust for takeoff

更多"[单选题]If the actual takeoff weight i"的相关试题:

[单选题]In some cases when the actual takeoff weight is lower than the maximum permissible one but no flexible takeoff possible, how to determine the speeds?
A. You can retain the speeds that have been calculated for the maximum permissible takeoff weight;
B. You can retain the speeds associated with the actual takeoff weight provided they are all lower than the speeds calculated for the maximum permissible takeoff weight.
C. You can use either of the above methods.
[单选题]If the V1 for the actual takeoff weight on a wet runway is lower than the minimum V1:
A. the associated takeoff performance such as the maximum takeoff weight must be corrected.
B. take the minimum V1. No correction is necessary.
C. It is impossible to happen.
[单选题]TAKEOFF WEIGHT is:
A. zero fuel weight + takeoff fuel
B. OEW + takeoff fuel
C. OEW + takeoff fuel + payload.
[单选题]How many lower deck compartments does the A320 aircraft have and how many compartments can they be subdivided into?
A. 2, 4
B. 2, 5
C. 3, 5
[单选题]LANDING WEIGHT is equal to:
A. takeoff weight minus trip fuel
B. takeoff fuel minus trip fuel and holding fuel
C. zero fuel weight
[单选题]Correct the determined maximum takeoff weight on dry runway to
A. take into account QRH and bleed effects, then apply the corrections for contaminants.
B. apply the corrections for contaminants, then take into account QRH and bleed effects.
C. No need to consider the QRH effect. But the bleed effects should be considered.
[单选题]The higher the OAT, the lower the maximum takeoff thrust. Is it correct?
A. No, it is incorrect. The maximum takeoff thrust remains the same below TREF.
B. No, it is incorrect. The higher the OAT, the higher the maximum takeoff thrust.
C. Yes, it is correct.
[单选题]A green arrow appears in the lower part of E/WD. Which of the following descriptions is correct?
A. There are too many ECAM messages for the amount of space available in the lower part of the E/WD. The green arrow shows that the information has overflowed off the screen.
B. The pilot can scroll down to view additional messages by pushing the CLR pushbutton on the ECAM control panel.
C. Both of the above
[单选题]The maximum takeoff weight and associated speeds may be affected by the following conditions:
A. OAT, wind, QNH
B. OAT, wind, QNH, visibility
C. OAT, wind, QNE
[单选题]ZERO FUEL WEIGHT(ZFW)is:
A. The weight obtained by addition of the total traffic load and the dry operating weight.
B. The weight obtained by addition of the total traffic load and the operational empty weight.
C. The weight obtained by addition of the total traffic load and the manufacturer’s empty weight.
[单选题]Operational empty weight(OEW)is:
A. The weight of the structure, power plant, furnishings, systems and other items of equipment that are considered as integral part of the aircraft. It is essentially a “dry” weight, including only those fluids contained in closed systems (e.g. hydraulic fluid).
B. The manufacturer’s weight empty plus the operator’s items i.e. the flight and cabin crew and their baggage, unusable fuel, engine oil, emergency equipment, toilet chemicals and fluids, galley structure, catering equipment, seats, documents etc.
C. The total weight of an aircraft ready for a specific type of operation excluding all usable fuel and traffic load. Operational Empty Weight plus items specific to the type of flight i.e. catering, newspapers, pantry equipment etc.
[单选题]Dry operating weight (DOW)is:
A. The weight of the structure, power plant, furnishings, systems and other items of equipment that are considered as integral part of the aircraft. It is essentially a “dry” weight, including only those fluids contained in closed systems (e.g. hydraulic fluid).
B. The manufacturer’s weight empty plus the operator’s items i.e. the flight and cabin crew and their baggage, unusable fuel, engine oil, emergency equipment, toilet chemicals and fluids, galley structure, catering equipment, seats, documents etc.
C. The total weight of an aircraft ready for a specific type of operation excluding all usable fuel and traffic load. Operational Empty Weight plus items specific to the type of flight i.e. catering, newspapers, pantry equipment etc.
[单选题]Manufacturer’s empty weight(MEW) is:
A. The weight of the structure, power plant, furnishings, systems and other items of equipment that are considered as integral part of the aircraft. It is essentially a “dry” weight, including only those fluids contained in closed systems (e.g. hydraulic fluid).
B. The manufacturer’s weight empty plus the operator’s items i.e. the flight and cabin crew and their baggage, unusable fuel, engine oil, emergency equipment, toilet chemicals and fluids, galley structure, catering equipment, seats, documents etc.
C. The total weight of an aircraft ready for a specific type of operation excluding all usable fuel and traffic load. Operational Empty Weight plus items specific to the type of flight i.e. catering, newspapers, pantry equipment etc.
[单选题]The Gross Weight (GW) is displayed in green when the first engine is started. If accuracy is degraded, the last two digits are displayed in dashed lines. On ground, if there is no computed data available, the indication will be displayed as ___?
A. no indication
B. blue dashes
C. amber dashes
[单选题]请写出以下英文单词所代表的中文意思:direction sign、lower window、headway( )。
A.指示标、客显屏、间隔时间
B.指示标、低工位、间隔时间
C.消磁、低工位、高峰期
D.消磁、客显屏、高峰期
[单选题]Maximum landing weight of A320 is ____kg.
A.66000
B.64000
C.62500
[单选题]Maximum takeoff weight of A320 is ____kg.
A.75900
B.75500
C.72500
[单选题]The yellow trapezoidal index moves beneath the roll index. It represents the lateral acceleration of the aircraft on ground and the sideslip in flight(as computed by the FAC). What does 1 centimeter of displacement indicate?
A. 0.1g
B. 0.2g
C. 0.3g
[单选题]Some advisories are inhibited depending on the aircraft altitude, which is correct?
A. A. All intruders flying below 380ft AGL when the own aircraft altitude is below 1 700ft AGL
B. B. All RA below 1 100ft in climb and 900ft in descent. In this case, the RAs are converted into TAs
C. C. Both correct

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