27) 更換左側(cè)空調(diào)組件管道壓力傳感器 Replace L/H A/C pack duct pressure transmitter
28) 拆下并安裝左空調(diào)空氣混合活門 Remove and install L/H air mix valve
29) 操作測試增壓控制系統(tǒng)進行 Do a operational test of pressurization control system
30) 目視檢查右組件聚水袋 Visually check/inspect right pack water coalesce bag
ATA22 自動駕駛
自動駕駛 autopilot
巡航 cruise
俯仰 pitch
橫滾 roll
上仰/下俯 pitch up / down
傳感器 transducer
偏航阻尼器 yaw damper
馬赫配平作動器 mach trim actuator
自動油門 auto-throttle
自動斷開 disengages automatically
速度限制 SPD LIM
失速管理 stall management
伺服馬達 servo motor
驅(qū)動組件 drive unit
高配平 high trim
速度配平 speed trim
起飛/復(fù)飛電門 takeoff/go around switch
當任一A/P 接通CMD 方式時飛機橫滾不柔和。Airplane roll is not smooth (jerky) with any A/P engaged in CMD
任一A/P 接通CMD 方式時，坡度角小于正常坡度角。 Goes less than the normal bank angle with any A/P engaged in CMD
自動駕駛儀接通時操縱桿(盤)移動。 Control columns(wheels) move when the autopilot engages
當將CMD 電門按壓關(guān)斷時，不能斷開。 Does not disengage when CMD switch is pushed to off
航向選擇方式或VOR 方式時坡度角大于調(diào)定的坡度角限制。Goes more than the set bank angle limit in HDG SEL or VOR
俯仰或橫滾方式接不通或自動脫開,自動駕駛儀進入CWS 方式。Pitch or roll mode does not engage or disengages automatically, autopilot went to CWS mode
行程不在限制范圍內(nèi)，桿力正常。Travel is not within limits, column force is normal
偏航阻尼器自動斷開。Yaw damper disengaged automatically
在MCP 速度（高度層改變）俯仰方式調(diào)定時，飛機不保持調(diào)定的空速。Airplane does not keep the set airspeed with MCP SPD (LVL CHG) pitch mode set
按壓斷開電門時，不能斷開。Does not disengage when disengage switch is pushed
俯仰振動（縱向跳躍） Pitch oscillation (porpoising)
1) 在自動駕駛多通道進近期間。Found during autopilot multi-channel approach
2) 在任何自動駕駛接通CMD 時。Found with any autopilot engaged in CMD
自動駕駛儀 Autopilot
1) 處于雙通道方式時A 和 B 自動脫開。A and B disengage automatically while in dual mode
2) A/P 琥珀色警告信號牌燈閃亮，自動駕駛儀進入 CWS 方式。A/P amber warning annunciator light on flashing, autopilot went to CWS mode
3) A/P 紅色警告信號牌燈恒亮。A/P red warning annunciator light on steady
偏航阻尼 YAW DAMPER
1) 飛機準備時YAW DAMPER電門接不通. The YAW DAMPER switch could not be set on when preparing for taking off.
ATA23 通信
通信 communication
天線 antenna
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