大S在这里

      罪行                                 美德

  色欲      Lust                                              贞洁        Chastity

  贪食   Gluttony                                         节制     Temperance

  贪婪     Greed                                           慷慨        Charity

  懒惰      Sloth                                           勤奋      Diligence

  愤怒     Wrath                                           耐心       Patience

  妒忌      Envy                                            宽容        Kindness

  傲慢      Pride                                            谦逊         Humility

在等待航线上，如果有较大侧风，在转弯前注意风速风向。

地速增大（顺风）转弯角度略大于标准转弯

地速减小（逆风）转弯角度略小于标准转弯

正侧风，标准转弯。

所以要根据风向指示器的指示随时调整转弯角度。

另外在近进航线上，一般是向正侧风方向偏角约为侧风强度的一半略小。

Electrical system

补充之前总结

        关于两个alternator可以互相平衡的意思是说如果一个发电机过热，这一个将主动降低负载而让另一个发电机承担更多的载荷，防止过热损坏。

        All alternator failure，the main battery will supply the ECU for 30 mins after that the engine can not work any more.

        Hot Bus: Pilot map/reading light      without battery master ON

        Battery Bus: LH/RH main Bus

                            LH/RH ECU Bus (via diode)

                            LH/RH starter heavy duty power

        LH Main Bus: PFD/ADC/AHRS/COM1/GPS1/NAV1/TXBD/Engine instrument/

                              Pitot heat/Oxygen sys/Gear control/Gear warning/Map light/

                              Flood light/Taxi light/ACL

        RH Main Bus: Avionic Bus/MFD/Horizon/Starter control/Flaps/

                               Avionic CDU cooling fan/Stall warning/AP/

                               Landing light/Navigation light/Instrument light

        Avionic Bus: COM2/GPS2/NAV2/Audio panel/AP/DME/Data link/WX500/ADF/WX radar

        Electrical master ON –> will let the main battery supply the Battery Bus and also the LH/RH Main Bus

        Engine Master –> connect with ECU Bus, excitation battery and also the GLOW and unfeathering accumulator

Auto Pilot

        ALT mode push the ‘UP’ button 1 time make the aircraft climb 20ft.

燃油系统

        通常是同侧油箱供应同侧引擎。燃油是由高压油泵输入共轨系统（common rail）后直接射入气缸，而高压油泵的油来自低压油泵。共轨系统中的油压由ECU根据power setting决定。高压油泵和低压油泵均为引擎机械驱动。未射入气缸的燃油会返回油箱。

共轨系统：为提高柴油机燃烧效率，用电子手段精确控制进入气缸的柴油供给量和供油时刻。如图

Fuel selector valves

        三个模式 On/X-feed/Off

        X-feed表示被另一个油箱feed。哪个油箱真正供油，回油就通向哪个油箱。

油箱

        每个机翼上各有一个油箱，每个油箱分成三个chambers。每侧有1USG unusable fuel，可用的油有50.8加仑

最大可以接受5加仑的unbalance。

        飞机没有低压的booster pumps。

        油箱中有两个Vents，一个包括一个带有check valve的capillary，另一个是一个relief pressure valve。Relief pressure valve是为了在AUX fuel transfer失效的时候保护油箱，防止油压过高。带Check valve的capillary是为了连通油箱和大气，在爬升时保证油箱内外气压平衡而不会把油带出油箱。

Hydraulic

    Brake

        刹车盘 rotor 卡钳 Caliper

        Parking brake set之后要踩几下刹车，给卡钳建立液压压力，才能保证刹车。

   Landing gear

Hydraulically operated

Electrically powered hydraulic pump

Electrically actuated hydraulic valves operated by gear selector switch

Squat switches prevent retraction on the ground

Warning horn with ‘gear up’ and ‘1 power lever in low position ~20%’ or ‘flaps LDG’

Gear down lock=spring loaded

Down lock released by hydraulic pressure for retraction

Green lights=gear down and locked

Red light=gear neither down nor up

Gear held up hydraulically

Emergency operation=free fall (by releasing hydraulic pressure)

If gear problem before landing just on final(for check ride) à Go around à safetyàchecklist

Hydraulic fluidà Red

Nose wheel steered with rudder pedals

Steering angleà30°without use of breaks 52°with one wheel fully breaked