单选题 Drain approximately 2 liters of fuel from the tank.

A、从油箱排出约2升滑油.

B、从油箱排出约2升液压油.

C、从油箱排出约2升燃油.

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相关试题

单选题封面题名应为《飞行员操作手册》或《飞行员操作手册及经联邦航空局批准的飞机飞行手册》。

A、The cover title shall be \"Pilot's Operating Handbook\" or \"Polit's Operating Handbook and FAA Approved Airplane Flight Manual.\"

B、The name of the book might be \"Pilot's Operating Handbook\" or \"FAA Approved Airplane Flight Manual.\"

C、The cover could be named as \"Pilot's Operation Instruction\" or \"Pilot's Operation Instruction and FAA Approved Airplane Flight Instruction.\"

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单选题针对飞机类别适合的机动飞行，应提供以下信息：(a)获准的机动飞行以及合适的进入速度的相关信息；(b)未获授权的机动飞行的相关信息；(c)已获准或未获准或不适合进行螺旋训练的相关信息。

A、The following information on maneuvers appropriate to the Airplane Category shall be given: (a) A Statement of Authorized Maneuvers and Appropriate Entry Speeds (b) A Statement of Unauthorized Maneuvers (c) A Statement that the airplane is Approved for Spins, Unapproved for Spins, or is characteristically incapable of spinning.

B、The following information should be provided to the maneuver flight as appropriate: (a) A Statement of Entry Speed for Authorized Maneuvers (b) A Statement of Unauthorized Maneuvers (c) A Statement that aircraft is Unapproved or not suitable for Spinning.

C、The following appropriate information should be provided to the aircraft maneuvers: (a) A Statement of Appropriate Entry Speed for maneuvers flight (b) A Statement of Unauthorized maneuvers (c) A Statement that aircraft has been unapproved for Spins, or is characteristically incapable of spinning.

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单选题最大操作限制速度是指在正常飞行操作中不得故意超过的速度限制。V用节表示，M用马赫数表示。

A、Maximum Limiting speed Unsticks is the speed restrain which will not be intentionally surpassed in typical flight operations. V is communicated in knots and M in Mach Number.

B、Maximum Restriction Speed is the fastest a plane can fly without breaking the rules in normal flight. The speed is measured in knots and Mach Number.

C、Maximum Operating Limit Speed is the speed limit that may not be deliberately exceeded in normal flight operations. V is expressed in knots and M in Mach Number.

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单选题对于光洁巡航构型和着陆构型，应提供以加速度g表示的机动限制载荷系数。对于获准螺旋或特技飞行的飞机，还应提供襟翼收上时的负限制载荷系数。

A、For clean configuration of landing, the limit load factor in g unit should be provided. For spinning and aerobatic aircraft, the load factor of flaps down should be provided as well.

B、The limit maneuvering load factors, in g units of acceleration, for clean cruise and landing configurations, shall be given. The negative g limit, flaps up, should be given for aircraft approved for spinning or aerobatics.

C、The flight maneuver load factor limit in the unit of g should be given for the smooth configuration of aircraft cruising and landing. For aircraft approved for spin or aerobatics, load limits should also be provided when flaps are opened.

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单选题发动机运行限制包括起飞功率限制、最大连续功率限制以及最大正常运行功率限制。

A、Engine Operating Limits include Limits for Take off Power, Maximum Continuous Power, and Maximum Cruising Power.

B、Engine Operating Limits include limits for Take off Thrust, Maximum Cruise Power, and Maximum Normal Operating Power.

C、Engine Operating Limits include limits for Take off Power, Maximum Continuous Power, and Maximum Normal Operating Power.

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单选题在某些涡轮螺旋桨驱动的飞机上，状态杆是发动机启动和停车的主要控制装置。在其它类型的飞机上，状态杆主要用来控制设置发动机和螺旋桨速度。

A、On some turbopropeller powered airplanes, the condition lever is the primary control for starting and stopping the engine. On others, it is the primary control used to set engine and propeller speed.

B、On some piston powered airplanes, the condition lever is the secondary control for starting and shutting the engine. On others, it is the secondary control used to set engine and piston speed.

C、On some turbopropeller powered airplanes, the status lever is the secondary control for starting and shutting the engine. On others, it is the secondary control used to set engine and propeller speed.

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单选题地面慢车功率指满足飞机以最小推力在地面尽可能慢地运行，但足以保证发动机、发动机附件和飞机正常运行所需的发动机功率。

A、Ground Idle Power refers to the power required to run an engine on the ground, as slowly as possible, yet sufficient to ensure satisfactory engine, engine accessory, and airplane operation with a minimum of thrust.

B、Ground Idle Power refers to the power required to run an engine as slowly as appropriate on the ground while still ensuring satisfactory airplane operation with a maximum of thrust of engine and engine accessory.

C、For Ground Idle Power, it determines the minimum power necessary to initiate and maintain safe airplane operation, engine accessory function, and satisfactory engine performance while limiting the degree of thrust utilized.

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单选题飞机型号数据单内列出的最大连续功率用来表明符合相应的适航标准，同时这个数值也会呈现在《飞行员操作手册》中。

A、The maximum continuous power listed in the Airplane Type Data Sheet is used to show compliance with the applicable airworthiness standards and is the value shown in the Pilot's Operating Handbook.

B、The maximum continuous power listed in the Airplane Type certificate is often used to show compliance with the applicable airworthiness standards and is the value shown in the Pilot's Operating Handbook.

C、The maximum continuous power listed in the Airplane Type Data Sheet is used to show compliance with the applicable airworthiness regulations and is beyond the value shown in the Pilot's Operating Handbook.

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