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(案例分析)某天某机组重庆机场落地02R,落地后左转脱离,在滑行道C上滑行时机组执行着陆后动作着陆后检查单,请问是否正确并简述其原因?(case analysis)The flight Crew landed at 02R Chongqing airport one day, after landing, left turn and vacating, the crew completed after landing actions and after landing checklist, was this right and why?

答案:飞机已脱离跑道(或在跑道内以安全滑行速度滑行)机组已经明确滑行路线及道口位置,并且飞机处于稳定滑行状态时,完成着陆后程序及着陆后检查单

飞机试题CRJ900题库练习
当FCP面板上选择了XFER按钮:With the XFER pushbutton on the FCP panel selected:
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飞行员看到他的飞行天气预报图显示出他将在航线的山区遇到一条锋面,他应该想到
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万一出现擦机尾,给机组的指示是:In case of tail strike, indications for the crew will be:
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判断正误:起动时滑油压力应显示正值,且可能超过峰值182psi(最大显示值)True or False:Oil pressures should show positive value during start and may peak beyond 182 psi (maximum display value).
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起飞时,PF按压TOGA电门,报出:“( )”。For takeoff, the PF presses TOGA switch, calls out:“( )”.
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请简述起飞后检查的动作。Please briefly describe the actions for After Takeoff Check.
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正常起飞,加速高度可以通过DS软件获得,无论单发和双发起飞时,都应遵守这一加速高度。The acceleration altitude can be got via the
calculation of DS software for normal takeoff; this acceleration altitude limitation shall be followed for takeoff with both or single engine(s).
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CANCEL MOD 行键会The CANCEL MOD line key will:
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ADG放出后,AC ESS BUS可重新建立到正常电源通过:After an ADG deployment, AC ESS BUS power can be re-established to its normal power source by:
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显示窗口的一条状态信息和一个绿色指示确认勤务舱门已经关闭A status message and a green indication in the indicator window confirm that the service door is closed.
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飞机试题CRJ900题库练习

(案例分析)某天某机组重庆机场落地02R,落地后左转脱离,在滑行道C上滑行时机组执行着陆后动作着陆后检查单,请问是否正确并简述其原因?(case analysis)The flight Crew landed at 02R Chongqing airport one day, after landing, left turn and vacating, the crew completed after landing actions and after landing checklist, was this right and why?

答案:飞机已脱离跑道(或在跑道内以安全滑行速度滑行)机组已经明确滑行路线及道口位置,并且飞机处于稳定滑行状态时,完成着陆后程序及着陆后检查单

飞机试题CRJ900题库练习
相关题目
当FCP面板上选择了XFER按钮:With the XFER pushbutton on the FCP panel selected:

A. 飞行指引1是现用系统且副驾驶控制两侧飞行指引模式。Flight director 1 is the active system and the co-pilot has control of both flight director modes

B. 飞行指引1不可用且飞行指引2需被任一飞行员选择。Flight director 1 is disabled and flight director 2 needs to be selected by either pilot

C. 自动驾驶接通且两个飞行指引都不是现用的。Autopilot is engaged and both flight directors are inactive

D. 飞行指引2被用于现用飞行指引。Flight director 2 is used as the active flight director

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飞行员看到他的飞行天气预报图显示出他将在航线的山区遇到一条锋面,他应该想到

A. 锋将因地形上升绝热冷却而由暖锋变成冷锋;

B. 锋将受地形阻挡移速减慢天气转好;

C. 地形抬升将补充锋的抬升并使飞行条件更加恶劣

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万一出现擦机尾,给机组的指示是:In case of tail strike, indications for the crew will be:

A. 红色信息'TAIL STRIKE' 和主警告灯。 Red message 'TAIL STRIKE' and Master Warning.

B. 琥珀色信息'TAIL STRIKE'和主警戒灯。 Amber message 'TAIL STRIKE' and Master caution.

C. 主起落架喇叭声响起。Landing gear horn will sound.

D. 驾驶舱内无指示。 No indications in the Flight Compartment.

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判断正误:起动时滑油压力应显示正值,且可能超过峰值182psi(最大显示值)True or False:Oil pressures should show positive value during start and may peak beyond 182 psi (maximum display value).
https://www.shititong.cn/cha-kan/shiti/00007381-7af0-e99d-c073-9874ad40f400.html
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起飞时,PF按压TOGA电门,报出:“( )”。For takeoff, the PF presses TOGA switch, calls out:“( )”.

A. TO/TO 两个,起飞; Two TO/TO, takeoff;

B. TO/TO 两个,形态OK; Two TO/TO, CONFIG OK;

C. 起飞; Takeoff;

D. TO/TO 两个,形态OK,起飞. Two TO/TO, CONFIG OK, takeoff.

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请简述起飞后检查的动作。Please briefly describe the actions for After Takeoff Check.
https://www.shititong.cn/cha-kan/shiti/00007381-7ae8-980b-c073-9874ad40f400.html
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正常起飞,加速高度可以通过DS软件获得,无论单发和双发起飞时,都应遵守这一加速高度。The acceleration altitude can be got via the
calculation of DS software for normal takeoff; this acceleration altitude limitation shall be followed for takeoff with both or single engine(s).
https://www.shititong.cn/cha-kan/shiti/00007381-7ae8-21fd-c073-9874ad40f400.html
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CANCEL MOD 行键会The CANCEL MOD line key will:

A. 取消输入草稿栏的数据Cancel the data entered to the scratch pad.

B. 删除上一次执行键按压后所作的变动Delete a changes made since the last time the exec button was pushed.

C. 仅删除航段页上已飞过的路点Delete only the previous waypoint on the legs page.

D. 仅取消之前输入Only cancels the previous entry

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ADG放出后,AC ESS BUS可重新建立到正常电源通过:After an ADG deployment, AC ESS BUS power can be re-established to its normal power source by:

A. 重新建立电源到AC BUS(es) 1(2),转换会是自动的。Regaining power to AC BUS(es) 1(2). Transfer will then be automatic.

B. 重新建立电源到AC BUS(es) 1(2),然后按压PWR TXFR OVERRIDE 按键Regaining power to AC BUS(es) 1(2). Then press PWR TXFR OVERRIDE button.

C. 先让飞机着陆,让机务重新收起ADG然后重置系统。Land the airplane, have maintenance re-stow the ADG then re-set the system.

D. 循环发电机电门。Cycling any of the GEN switches.

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显示窗口的一条状态信息和一个绿色指示确认勤务舱门已经关闭A status message and a green indication in the indicator window confirm that the service door is closed.

A. 是Yes

B. 否No

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