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C. 在所申請(qǐng)的航空器上擔(dān)任機(jī)長(zhǎng)多于15 小時(shí)
44.在121 公共航空運(yùn)輸中,如果駕駛本機(jī)型上的飛行員經(jīng)歷時(shí)間少于700 小時(shí),并且機(jī)長(zhǎng)不具備
飛行檢查員和飛行教員資格,則在哪種情況下,必須由機(jī)長(zhǎng)操縱飛機(jī)完成起飛和著陸(B)
A. 所用跑道有5 米/秒的側(cè)風(fēng)
B. 在機(jī)場(chǎng)跑道上有風(fēng)切變
C. 機(jī)場(chǎng)空域有雨
45.在121 中,對(duì)于國(guó)際飛行,飛機(jī)在中途機(jī)場(chǎng)著陸時(shí)間為1805Z,則在下列哪一時(shí)刻后,飛機(jī)需
簽派員的重新批準(zhǔn)可在飛(C)
A. 2005Z
B. 1905Z
C. 0005Z
46.3 名飛行員(包括機(jī)長(zhǎng)),有睡眠區(qū),值勤時(shí)間和飛行時(shí)間不超過(B)
A. 18 和12
B. 18 和14
C. 16 和10
47. 某飛行員每年12 月復(fù)訓(xùn),最近一次月份2002 年1 月,則認(rèn)為該次復(fù)訓(xùn)的月份為(A)
A. 2001 年12 月
B. 2002 年2 月
C. 2002 年1 月
48.二類、三類儀表運(yùn)行許可,其實(shí)踐考試由(C)
A. 筆、飛
B. 口、模
C. 口、飛、
49.在參加121 飛行的飛機(jī)上任駕駛員必須滿足條件(A)
A. 三證(駕、體、身份證)
B. 型別、等級(jí)
C. 60 以下
50.121 公共運(yùn)輸飛行中,幾長(zhǎng)不得允許哪一類人員進(jìn)入駕駛艙(B)
A. 經(jīng)由該公司批準(zhǔn)可以進(jìn)入的非機(jī)組人員的公司雇員
B. 機(jī)長(zhǎng)認(rèn)為其進(jìn)入不會(huì)對(duì)飛行安全造成或影響公司雇員,機(jī)長(zhǎng)有最終決定權(quán)
C. 正在執(zhí)行任務(wù)的局方檢查員或局方要任代表,以及由該公司特批準(zhǔn)的人員
51. 121 航線飛行中,擔(dān)任副駕駛必須滿足下列關(guān)于其執(zhí)照和等級(jí)的要求(C)
A. 必須有航線運(yùn)輸駕駛員執(zhí)照
B. 必須有商用駕駛員執(zhí)照和所飛機(jī)型的等級(jí)執(zhí)照
C. 必須有商用駕駛執(zhí)照和多發(fā)等級(jí)和儀表等級(jí)執(zhí)照
52.哪個(gè)對(duì)(C)
A. 只有局方認(rèn)可的在高等學(xué)院擔(dān)任教員的人員,可免除61 部考試
B. 按61 頒發(fā)的飛行員執(zhí)照過地面教員執(zhí)照的人,及擔(dān)任教員的人不需要61 考試
C. 只有已經(jīng)持有按61 頒布飛行教員執(zhí)照和地面教員,方可免除61 考試
53,121 四名飛行員(包括一名第2 機(jī)長(zhǎng)),有睡眠區(qū),派班是安排值勤和飛行時(shí)間(B)
A.20-16
B.20-17
C.18-16
54.121 兩名機(jī)組排班值勤和飛行不超過(B)
A.12-9
B.14-8(不多于兩個(gè)航段飛行延長(zhǎng)至9 小時(shí))
C.12-8(不多于兩個(gè)航段飛行延長(zhǎng)至9 小時(shí))
55.該此除冰防冰時(shí)間如何計(jì)算
保持時(shí)間:開始于最后一次應(yīng)用除冰防冰液的開始時(shí)刻,結(jié)束于應(yīng)用在飛機(jī)上的除冰防冰液失
效的時(shí)刻
56.想當(dāng)副駕駛必須有:
商照和飛機(jī)類別、多發(fā)級(jí)別、儀表等級(jí)
57.如駕駛員執(zhí)照上具有相應(yīng)的類別、級(jí)別和型別等級(jí),如(適用),那么執(zhí)照?qǐng)?zhí)有人僅僅具備了
在相應(yīng)類別、級(jí)別和型別(如適用)航空器上擔(dān)任機(jī)長(zhǎng)的基本條件
1. sinus barotrauma is most likely to occur during 在什么時(shí)候產(chǎn)生
a. level flight in turbulence
b. to from a high altitude aerodrome
c. 下降時(shí)
2. The time of the day when the earth’s surface gives off the greatest amount of terrestrial radiation is
a. a few hours before midnight
b. at sunset
c. mid afternoon
2. the water vapor held in unsaturated air is:
a. invisible always
b. visible only it the temperature is low enough
c. visible always
3. by what factor is the demonstrated all engines take off distance increase to determine a TODR
a. 1.15
b. 1.2
c. 2
4. the effect of clearway on take off performance is
a. increases TODR
b. increases TODA
c. decreases ASDA
5. TODA must exceed TODR in order to
a. allow use of de-rate thrust
b. increase V2
c. reduce Vr
6. the net gradients required in the second segment are
a. 1.6%, 1.8% and 2%
b. 2.4%, 2.7% and 3%
c. 2.1%, 2.2% and 2.3%
7. 題目看不到了,只看到答案
● an area where precipitation drops are not detected
8. thunderstorm in the arctic region will generally more
● northeast to southwest on polar easterlies
9. the purpose of diluting ethylene glycol deicing fluid with water non-precipitation conditions is to
● decrease the freeze point
10.freezing rain encountered during climb is normally evidence that
● a layer of warmer air exists above
11.in a light twin-engine airplane with one engine inoperative, when is it aueptable to allow the all of a
slip-skid indicator to be deflected ant side the reference lin
● when operating at any airspeed greater than Vmc
12.ATIS
● have temperature
13.ATC instructed “hold short of a runway(ILS critical area etc)” the pilot should stop
● so that no part of the aircraft extent beyond the holdline
14.the purpose of dilating ethylene glycol deicing fluid with water in non-precipitation condition is to
a. vaise the entectic point
b. increase the minimum freezing point (outset of on stallzation)
c. decrease the freeze point
15.under what condition may an air carrier pilot continue an instrument approach to the DH, after
receiving a weather report indicating that less than minimum published landing conditions exist at the
airport
● when the weather report is received after the pilot has begun the final approach segment of the
instrument approach
16.what is the recommended technique to counter the loss of airspeed and maintain or increase pitch
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