为了达到下一个高度限制，推荐的垂直速度显示为：the recommended vertical speed required to reach the next altitude constraint is displayed as:

双发起动好且起动机脱开后（ ）通知机务拔掉耳机，并提醒机务盖好盖板。After both engines start and the starter is disconnected, （ ） shall advise maintenance to disconnect headset, and remind maintenance to stow the cover well.

地面交输引气起动发动机，工作的发动机推力手柄前推达至最小（ ）psi的引气压力, 最大80%的 N2。For cross bleed engine start on the ground , advance the operating engine thrust lever to achieve a minimum of （ ） psi bleed air pressure, to a maximum of 80% N2.

外接气源起动发动机，则该外接气源需在起动时提供（ ）psi(ISA条件)的总管压力。If an external air source is required, it should be capable of supplying（ ）psi (ISA conditions) manifold pressure at the initiation of start.

左发起动后，执行燃油单向活门测试时，如果2 分钟不显示R FUEL LO PRESS（右侧燃油低压）信息，则右发执行冷转，最长（ ）秒。 After left engine start, when conducting Fuel feed check valve test, if after 2minutes, the R FUEL LO PRESS caution message isstill not displayed, dry motor for （ ） seconds maximum.

发动机起动，当N2≥（ ），起动机脱开。For Engine Start procedure, when N2≥（ ），starter will cut out.

发动机起动，当N2≥（ ）且ITT≤（ ）时，提起左发油门杆至慢车位。For Engine Start procedure, when N2≥（ ）and ITT≤（ ），advance left engine thrust lever to IDLE.

初始检查中，源选择面板应确保4个旋钮都在（ ）位。During originating check, the 4 knobs on source selector panel shall be in ( ) position.

飞行阶段分为下列五个主要类型，顺序为（ ）The flight phases include the following five major categories, they are ( ) in sequence.

发动机起动前，机组应完成起动前流程，确认液压泵4 个电门向前，电门位置：AUTO/ON/AUTO/AUTO。Flight crew shall complete the flows for before-start,verify 4 switches for hydraulic pumps being selected forward，switch position：AUTO/ON/AUTO/AUTO。

在地面，由右座起动发动机。On the ground, the right-seated pilot will start the engine.