判断正误True or False: 在五边进近航段，若失去完成进近所需导航精度，则PFD上将显示琥珀色的NO APPR信息。During the final approach segment, if the required navigation accuracy to complete the approach is lost, an amber NO APPR message is displayed on the PFD.

起飞前检查单 ，PLT回答应答机/TCAS 时，应报出（ ） For the Before Takeoff Check，when the PLT respond Transponder/TCAS ON, should also callout （ ） .

滑油压力在 （ ）PSI 以上时，推力手柄不得大于 IDLE 慢车位置。If oil pressure is above （ ） PSI, thrust lever should never excess IDLE .

滑出加油门 N1 不超过 （ ）%。During taxi-out, advance thrust N1 should not above （ ）%.

起动后检查，右座的动作流程是（ ）。For the After Start Check, flow pattern of right seat is （ ）.

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.