問題詳情
43．飛機 pitch and roll 姿態資料來自於：
(A)DG(directional gyro).
(B)VG(vertical gyro).
(C)Flux valve.
(D)Magnetic sensors.
(A)DG(directional gyro).
(B)VG(vertical gyro).
(C)Flux valve.
(D)Magnetic sensors.
參考答案
無參考答案
內容推薦
- 41．飛機 DFDR 介面設備是：(A)Sensors. (B)CFDIU(central fault display interface unit).(C)DFDAU(digital flight
- 40．飛機黑盒子 ULB(underwater locator beacon)發送：(A)無線電波‧Radio frequency. (B)聲波‧Acoustic frequency. (C)超音波‧
- 39．飛機 angle of attack 的定義為 angle between direction of airflow and:(A)The chordline of the wings. (B)
- 38．民航機 DFDR(digital flight data recorder) 記錄容量：(A)35 hrs. (B)25 hrs. (C)45 hrs. (D)50 hrs.
- 37．備用儀錶有那些構成：(A)Airspeed. (B)Altitude. (C)Attitude. (D)以上皆是‧
- 36．什麼是 EICAS 縮寫？(A)Engine indicating and crew alerting system. (B)Electricity indicatingcontrol assi
- 33．什麼地方有垂直速度指示資料？(A)PFD. (B)SD. (C)EAD. (D)ND.
- 35．什麼是 IDS 縮寫?(A)Integrated display system. (B)Integrated drive system. (C)Integrateddisplay shunt.
- 32．什麼地方有高度指示資料？(A)ND(navigation display). (B)SD(system display). (C)PFD(primaryflight display). (D)E
- 30．氣動式空速錶，指示：(A)TAS(true air speed). (B)IAS(indicated air speed). (C)EAS(equivalentair speed). (D)CA
內容推薦
- 45．為什麼 IRS/ADIRS 不要裝置磁力閥 flux valve 去感應磁方位？(A)電腦運算算出‧It calculates by an algorithm in the computer.
- 34．EFIS 由那些構成：(A)EICAS. (B)EAD/SD. (C)PFD/ND. (D)EAD/PFD.
- 47．電羅盤 RMI(radio magnetic indicator) 可選那些導航系統？(A)非常高頻無線電導航‧VOR. (B)自動方向尋找‧ADF. (C)非常高頻無線電導航和自動方向尋找‧V
- 46．羅盤卡 compass card 顯示在：(A)姿態儀和水平狀態儀‧HSI & ADI. (B)姿態儀和高度錶‧ADI &ALITIMETER. (C)水平狀態儀和空速錶‧HSI & Airsp
- 49．飛機俯仰翻轉姿態(pitch and roll)顯示在那裡：(A)PFD. (B)ND. (C)RMI. (D)HSI.
- 48．飛機 VOR/LOC 偏航 deviation bar 顯示在什麼儀表：(A)RMI. (B)ADI. (C)HSI. (D)DME.
- 50．飛機 F/D(flight director), A/P(autopilot) system 姿態資料來自於：(A)DG. (B)VG. (C)FCU(fight control unit).
- 51．機上 IRS(inertial reference system)算出：(A)慣性位置‧The inertial position. (B)風速‧Wind speed. (C)地速‧Ground
- 53．機上 ADF 頻率：(A)調幅 (B)高頻 (C)調頻 (D)超高頻
- 56．ADF 檢測指示顯示在 RMI 為：(A)The ADF pointer with lube line at 315 degrees. (B)The ADF pointerwith lube l
- 55．ADF 檢測指示顯示在：(A)HSI. (B)RMI. (C)ADI. (D)以上皆非‧
- 54．ADF 用做長距離導航，稱為：(A)NDB(non directional beacon). (B)Locator. (C)Bearing. (D)Heading.
- 57．什麼是 the quadrant error of ADF？(A)Bearing around the 45 degrees angle to the fuselage are bended.(
- 60．從何處調整 ADF 頻率？(A)飛航管理電腦‧FMC(flight management computer). (B)控制面板‧ADF control panel. (C)多功能指示‧MCDU(
- 59．ADF 聲音從那裡聽到？(A)飛航通話系統‧Flight interphone system. (B)維護通話系統‧Serviceinterphone system. (C)客艙通話系統‧Cab
- 61．VOR 導航原理是比較：(A)參考和變化信號相位‧The reference phase signal and variable phasesignal. (B)參考和固定信號相位‧The re
- 52．機上 IRS 資料顯示在：(A)PFD. (B)ND. (C)PFD & ND. (D)EICAS.
- 63．在 HSI, 為 VOR 偏航指示為：(A)1°/dot. (B)5 °/dot. (C)3°/dot. (D)4°/dot.
- 64．在 VOR 電台提供：(A)方位‧ Heading. (B)真方位‧True heading. (C)電台磁方位‧Stationmagnetic heading. (D)電台真方位‧Statio
- 65．從何處選 VOR course ？(A)自動駕駛面板‧AFCS panel.(auto flight control panel). (B)電羅盤‧RMI. (C)無線電導航接收機‧VOR re
- 66．如何選調 VOR 頻率？(A)FMC(flight management computer). (B)VHF-NAV control panel.(C)MCDU. (D)以上皆是‧
- 67．儀器降落系統 ILS(instrument landing system) 由什麼組成：(A)下滑導引‧G/S(glide slope system). (B)定位導引‧LOC(localize
- 68．儀器降落發射信號含有兩種片辮狀訊號，其頻率為：(A)300 & 150 Hz. (B)150 & 90 Hz. (C)400 & 200 Hz. (D)200 & 100Hz.
- 58．什麼是 BFO(beat frequency oscillation) on ADF 系統?(A)1350 Hz. (B)1030 Hz. (C)1020 Hz. (D)1750 Hz.
- 70．機場 G/S 發射器位於：(A)跑道端‧The departure end of the runway. (B)跑道進場側邊‧Oneside of the front course of the