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> 108年 - 航空器通信助航裝備1-100#79863
108年 - 航空器通信助航裝備1-100#79863
科目:
航空通訊助航裝備 |
年份:
108年 |
選擇題數:
100 |
申論題數:
0
試卷資訊
所屬科目:
航空通訊助航裝備
選擇題 (100)
1.一般長距離通訊使用: (A)高頻通信系統‧HF. (B)非常高頻通信系統‧VHF. (C)非常高頻導 航通信系統‧VOR. (D)測距儀‧DME.
2.一般飛機進場通信使用: (A)高頻通信系統‧HF. (B)非常高頻通信系統‧VHF. (C)自動方向尋 找通信導航設備‧ADF. (D)測距儀‧DME.
3.飛行通話對講系統:(flight interphone system). (A)飛行員相互通信‧Flight crew intercommunication. (B).無線電通 信‧Radio communication (C)地面人員通話‧Ground communication. (D) 以上皆是‧
4.飛機 selective call system 是用做: (A)地面呼叫飛機‧Ground call aircraft. (B)飛機呼叫飛機‧Aircraft call aircraft. (C)通話系統‧Interphone system. (D)導航系統‧Navigation system.
5.飛機 HF coupler 是用來: (A)調天線‧Antenna tuning. (B)調駐波比‧The VSWR tuning. (C)A 和 B‧ (D)調頻率‧
6.飛機 VHF control panel 做為: (A)調頻率‧Frequency tuning. (B)通話‧Interphone. (C)供應電力‧ Power supply. (D)發報機‧Radio transmitting.
7.等式 C=λf , C 代表: (A)光速‧The speed of light. (B)電容‧Capacity. (C)振幅‧Amplitude. (D)頻碼‧Code of frequency.
8.飛機 VHF-COM 天線是: (A)1/2λ rod antenna.柱狀天線 (B)1/4λ rod antenna. (C)λ dipole antenna.偶極天線 (D)1/2λ dipole antenna.
9.飛機廣播系統的操作優先權是: (A)飛行通話系統‧Flight interphone system. (B)客艙通話系統‧Cabin interphone system. (C)預錄廣播系統‧Pre-annunciation system. (D)空服 員‧Station purser.
10.為何在 VHF-COM 天線調整不是那麼需要? (A)頻率變化小‧The frequency variation is small. (B)寬劍式天線‧The antenna is a wide band sword type. (C)功率小‧ (D)A 和 B 皆對‧
11.透過什麼把麥克風聲音接到無線電通訊系統: (A)聲音選擇面板‧ASP.(audio select panel). (B)無線電控制面板‧RCP. (radio control panel). (C)遙控電子器‧REU. (remote electronic unit). (D) 電子控制器‧EPC.(electronic panel control).
12.在 audio select panel 有什麼? 2 (A)麥克風和聲音線路‧Mike and audio circuits. (B)麥克風線路‧Mike circuit only. (C)聲音線路‧Audio circuit only. (D)繼電器線路‧Relay control circuit.
13.靜音線路 muting circuit 功能: (A)防止聲音回授‧To avoid the acoustic feed back. (B)停止發射‧To stop transmitting. (C)整合音量‧To combine the audio. (D)以上皆非‧
14.通常 VHF-COM 作為: (A)長距離通信‧Long range communication. (B)短距離通信‧Shot range communication. (C)維護通信‧Service intercommunication. (D)導航無 線電通信‧VHF-NAV only.
15.通常 ACARS(ARINC communication addressing & reporting system)使用 何種通訊系統操作: (A)衛星通訊系統‧SATCOM. (B)VHF. (C)HF. (D)以上皆是‧
16.通常 ACARS system 用作: (A)資料傳遞‧DATA link. (B)聲音傳遞‧Voice link. (C)DATA & voice link. (D)以上皆非‧ 題號:00018 題組:0 難易度:1
17.通常民航機裝有幾套 HF 通信系統? (A)2. (B)1. (C)3. (D)4.
18.飛機 SELCAL system 對飛行員而言: (A)導航使用‧Navigation usages. (B)減輕工作‧Relieving the workload of constant monitored ground station. (C)做 VHF-COMM 通信‧ (D)做 HF-COMM 通信‧
19.飛機座艙通話記錄器 CVR (cockpit voice record) 記錄: (A)往來無線電通話‧ (B)駕駛艙聲音‧ (C)A 和 B‧ (D)客艙聲音‧ 3
20.飛機座艙通話記錄器控制面板的消除開關,在何時工作? (A)飛機在地面上‧ (B)煞車掛上‧ (C)任何時候‧ (D)A 和 B‧
21.衛星通信系統使用何種衛星來傳遞信號? (A)同步衛星‧ (B)區域衛星‧ (C)地理衛星‧ (D)位置衛星‧
22.空氣資料電腦 air data computer 收集那些資料: (A)Pitot pressure, TAT (total air temperature). (B)Pitot pressure, TAT , Baro correction. (C)Pitot/static pressures, TAT , Baro correction. (D)Static pressure, TAT , Baro correction.
23.空氣資料電腦 air data computer 提供那些資料: (A)Airspeed, altitude, mach. (B)Attitude, mach, true airspeed. (C)Heading, total air temperature, airspeed. (D)以上皆是‧
24.什麼是國際標準大氣 ISA(International standard atmosphere)條件: (A)壓力: Pressure in MSL(mean sea level) 1013.25 hPd(STD). (B)溫 度: Temperature in MSL 15℃. (C)濕度:Humidity 0%. (D)以上皆是‧
25.什麼是動壓 dynamics pressure Qc? (A)Pt-Ps. 總壓 Pt: total pressure, 靜壓 Ps: ambient static pressure. (B)Pt+Ps. (C)Ps. (D)以上皆非‧
26.高度錶需要什麼資料? (A)Static & Pitot pressure. (B)Pitot pressure. (C)Static pressure. (D)以 上皆非‧
27.空速錶需要什麼資料? (A)Static pressure. (B)Pitot & Static pressures. (C)Pitot pressure. (D)以 上皆非‧
28.什麼是 SSEC(static source error correction)? (A)Corrects static pressure errors caused by the airflow past the aircraft. (B)Corrects static pressure errors caused by the airflow temperature. (C)Corrects static pressure errors caused by the airflow divergent the aircraft. (D)Corrects static pressure errors caused by the airflow stuck the aircraft.
29.什麼是馬赫 Mach number? (A)音速‧The sound speed. (B)真速比‧The ratio of true speed. (C)真 速和當時音速比‧The ratio of true airspeed to the local speed of sound. (D) 真速和音速比‧The ratio of true airspeed to the speed of sound.
30.氣動式空速錶,指示: (A)TAS(true air speed). (B)IAS(indicated air speed). (C)EAS(equivalent air speed). (D)CAS(computed air speed).
31.在高空中 TAS 和 IAS 有何不同? (A)IAS=TAS. (B)IAS>TAS. (C)TAS>IAS. (D)None.
32.什麼地方有高度指示資料? (A)ND(navigation display). (B)SD(system display). (C)PFD(primary flight display). (D)EAD(engine/alert display).
33.什麼地方有垂直速度指示資料? (A)PFD. (B)SD. (C)EAD. (D)ND.
34.EFIS 由那些構成: (A)EICAS. (B)EAD/SD. (C)PFD/ND. (D)EAD/PFD.
35.什麼是 IDS 縮寫? (A)Integrated display system. (B)Integrated drive system. (C)Integrated display shunt. (D)Integrated destroyed system.
36.什麼是 EICAS 縮寫? (A)Engine indicating and crew alerting system. (B)Electricity indicating control assistance system. (C)Electronic information control alert system. (D)EFIS indicating crew alerting system.
37.備用儀錶有那些構成: (A)Airspeed. (B)Altitude. (C)Attitude. (D)以上皆是‧
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.
39.飛機 angle of attack 的定義為 angle between direction of airflow and: (A)The chordline of the wings. (B)The straight line of the flap. (C)The mean chord line of the wings. (D)The pitch line of the wings.
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‧Ultrasonic frequency. (D)調頻波‧Very high frequency.
41.飛機 DFDR 介面設備是: (A)Sensors. (B)CFDIU(central fault display interface unit). (C)DFDAU(digital flight data acquisition unit). (D)CDS(central display system).
42.羅盤卡 compass card 資料來自: (A)DG(directional gyro). (B)DG & flux valve. (C)磁力閥‧Flux valve. (D)以上皆非‧
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.
44.機上 IRS(inertial reference system) & ADIRS(air data inertial system) 用 什麼陀螺儀來感應方位和姿態? (A)機械陀螺儀‧Mechanical gyros. (B)雷射陀螺儀‧Laser gyros. (C) 電子陀螺儀‧Electronic gyros. (D)氣動陀螺儀‧Pneumatic gyros.
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. (B)陀螺 算出‧It calculates by gyros. (C)垂直陀螺算出‧It calculates by vertical gyros. (D)線路算出‧It calculates by magnetic circuits.
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 & Airspeed Indicator. (D) 電羅盤和水平狀態儀‧HSI & RMI.
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‧VOR & ADF. (D)慣性導航系統‧INS.
48.飛機 VOR/LOC 偏航 deviation bar 顯示在什麼儀表: (A)RMI. (B)ADI. (C)HSI. (D)DME.
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.
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). (D)Servo sensors.
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 speed. (D)以上皆是‧
52.機上 IRS 資料顯示在: (A)PFD. (B)ND. (C)PFD & ND. (D)EICAS.
53.機上 ADF 頻率: (A)調幅 (B)高頻 (C)調頻 (D)超高頻
54.ADF 用做長距離導航,稱為: (A)NDB(non directional beacon). (B)Locator. (C)Bearing. (D)Heading.
55.ADF 檢測指示顯示在: (A)HSI. (B)RMI. (C)ADI. (D)以上皆非‧
56.ADF 檢測指示顯示在 RMI 為: (A)The ADF pointer with lube line at 315 degrees. (B)The ADF pointer with lube line at 180 degrees. (C)The ADF pointer with lube line at 90 degrees. (D)The ADF pointer horizontal.
57.什麼是 the quadrant error of ADF? (A)Bearing around the 45 degrees angle to the fuselage are bended. (B)Bearing around the 45 degrees angle to the ADF antennas are bended. (C)Bearing around the 45 degrees angle to the wings are bended. (D)Bearing around the 45 degrees angle to the tail are bended.
58.什麼是 BFO(beat frequency oscillation) on ADF 系統? (A)1350 Hz. (B)1030 Hz. (C)1020 Hz. (D)1750 Hz.
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‧Service interphone system. (C)客艙通話系統‧Cabin interphone system. (D)地面 通話系統‧Ground interphone system.
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(multi-purpose control display unit) on manual mode. (D)以上皆是‧
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 phase signal. (B)參考和固定信號相位‧The reference phase signal and fixed phase signal. (C)參考和控制信號相位‧The reference phase signal and control phase signal. (D)參考和資料信號相位‧The reference phase signal and data phase signal.
62.VOR TO/FROM 指示在: (A)HSI. (B)ADI. (C)RMI. (D)None.
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‧Station magnetic heading. (D)電台真方位‧Station true heading.
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 receiver. (D)自動方向尋找控制面 板‧ADF control panel.
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(localizer system). (C)定位.下滑導引和信標 LOC & G/S & MB. (D)無線電導 航 VOR 系統‧
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 & 100 Hz.
69.如何調 ILS 頻率? (A)G/S only. (B)VOR only. (C)LOC only. (D)ADF only.
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‧One side of the front course of the runway. (C)跑道出場側邊‧The side departure end of the runway. (D)跑道中心線上‧The center end of the runway.
71.下滑 G/S 接收線路自動起動,當在: (A)無線電導航 VOR 頻率選定‧ (B)定位導引 LOC 頻率選定‧ (C) 自動方向尋找 ADF 頻率選定‧ (D)測距儀 DME 頻率選定‧
72.如何作 VOR system 檢測? (A)頻率選定‧The VOR frequency to be selected. (B)航向選定 000‧The course 000?selected. (C)A & B 皆要. (D)航向選定 120‧The course 120?selected.
73.儀器降落系統,其頻率範圍: (A)118 – 137 MHz(even tenths).【小數點後偶數】 (B)108.1 – 111.9 MHz(odd tenths). 【小數點後奇數】 (C)108.1 – 111.9 MHz(even tenths). (D)112 – 137 MHz(odd tenths).
74.儀器降落系統,下滑角 G/S 和定位 LOC 路徑成直線,並和地面成幾 度夾角? (A)5 to 10 degrees. (B)2.5 to 3 degrees. (C)10 to 15 degrees. (D)1.5 to 2 degrees.
75.儀器降落系統,資料顯示在: (A)ADI, DME. (B)RMI, ADI. (C)HSI, ADI. (D)HSI, RMI.
76.儀器降落系統,定位導引天線 LOC antenna 位於: (A)雷達罩‧Radome. (B)直尾翅‧Vertical fin. (C)下機身‧Lower fuselage. (D)上機身‧Upper fuselage.
77.自動方向尋找的天線;由何種天線構成:The ADF antenna includes: (A)Loop & direction antenna. (B)Loop & data antenna. (C)Sense & loop antenna. (D)Rod & loop antenna.
78.非常高頻多向導航系統 VOR 天線位於: (A)雷達罩‧Radome. (B)直尾翅‧Vertical fin. (C)翼尖‧Wing tips. (D) 鼻輪艙‧Nose landing gear bay.
79.在水平姿態儀 HSI,方位旗子出現,表示: (A)供電‧ Power on. (B)方位失效‧DG failure. (C)無線電導航失效‧ VOR/LOC failure. (D)以上皆非‧
80.在飛機姿態儀 ADI,旗子出現,表示: (A)電源失效‧ (B)儀錶失效‧ (C)沒有 VG 資料‧ (D)以上皆對‧
81.飛航導航信標系統 marker beacon system 通常和什麼系統一起操作使 用? (A)儀器降落系統‧ILS system. (B)非常高頻無線電導航系統‧VOR system. (C)測距儀‧DME system. (D)自動方向尋找‧ADF system.
82.飛航導航信標系統 marker beacon system 其中 middle marker 由何表示? (A)MM, amber visual warning. (B)1300 Hz sound, audio warning. (C)Dots and dashes Morse codes. (D)以上皆是‧
83.儀器降落系統接收機,內含: (A)LOC receiver circuit. (B)G/S receiver circuit. (C)VOR receiver circuit. (D)LOC & G/S receiver circuits.
84.飛航導航信標系統 marker beacon system 天線位於: (A)上機身 (B)下機身 (C)翼尖 (D)直尾翅
85.飛航導航信標系統(marker beacon system )發射頻率為: (A)1300 MHz. (B)400 MHz. (C)75 MHz. (D)3000 MHz.
86.無線電高度表,量測高度為: (A)高於 2500 呎‧ (B)低於 2500 呎‧ (C)任何高度‧ (D)海平面 以上‧
87.量測地面絕對高度為何? (A)氣壓高度‧Altitude baro. (B)無線電高度‧Terrain radio altitude. (C) 垂直率‧Vertical rate. (D)平均高度‧Mean sea level altitude.
88.無線電高度表,其天線由何構成: (A)接收天線‧Receiving antenna only. (B)發射天線‧Transmitting antenna only. (C)發射和接收天線合為一個天線‧Receiving & transmitting in one antenna. (D)接收及發射各別分開天線‧Receiving antenna and transmitting antenna.
89.無線電高度表,其天線到接收機的同軸饋線 coaxial cable: (A)可調整長度‧The cable length is non-critical you can adjust and cut. (B)不可調整‧The cable length is critical you cannot cut and adjust. (C) 無關‧There are nothing to do the system. (D)以上皆非‧None above.
90.測距儀 DME 和航管系統 ATC;其間相互關係: (A)地線防止干擾‧By ground wires to prevent interference. (B)抑制線路 (suppersion line)防止干擾‧By suppression cables to prevent interference. (C)開路防止干擾‧By open circuit to prevent interference. (D)電容線路 防止干擾‧By capacity circuits to prevent interference.
91.飛機測距儀 DME 量測距離為: (A)斜線距離‧Slant distance. (B)直線距離‧Direct distance. (C)垂直距 離‧Vertical distance. (D)地距離‧Ground distance.
92.飛機姿態儀 ADI 內,跑道信號 rising runway symbol 起動: (A)無線電高度正常‧R/A valid. (B)儀降系統正常‧ILS valid. (C)A.B 兩者皆正常‧R/A and ILS valid. (D)以上皆非‧
93.如何調測距儀 DME 的接收? (A)自動方向尋找控制板‧ADF control panel. (B)非常高頻導航控制 板‧VHF-NAV control panel. (C)測距儀‧DME itself. (D)以上皆非‧
94.測距儀 DME 天線位於: (A)直尾翅‧Vertical fin. (B)翼尖‧Wing tips. (C)下機身‧Lower fuselage. (D)上機身‧Upper fuselage.
95.航管系統 ATC 和測距儀 DME 天線可以互換。 (A)對‧True. (B)錯‧False. (C)未知‧Unknown. (D)依狀況‧On condition.
96.測距儀 DME 摩斯碼 Morse code 頻率為: (A)1020 Hz. (B)1350 Hz. (C)1750 Hz. (D)1450 Hz.
97.測距儀 DME ,接收機叫: (A)發射接收器‧Transceiver. (B)答詢機‧Interrogator. (C)接收機‧ Receiver. (D)發射機‧Transponder.
98.從何處做測距儀 DME 檢測工作? (A)非常高頻無線電導航控制面板‧VHF-NAV control panel. (B)測距儀 面板‧DME front panel. (C)測距儀‧DME indicator. (D)供電‧On power.
99.航管系統碼 ATC code 是: (A)十進位‧Decimal. (B)八進位‧Octal. (C)十六進位‧Hexadecimal. (D)二進位‧Binary coded decimal.
100.航管系統 ATC 咨詢頻率 interrogation frequency 為: (A)1090 Mhz. (B)1030 MHz. (C)1350 MHz. (D)2030 MHz.
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