B_실전모의고사 B형

Question 1 of 40

1. Question

1 point(s)

활주로에서의 감속률은 공중에서의 감속률의 몇 배 정도 되는가?

2 배
3 배
4 배
5 배

Question 2 of 40

2. Question

1 point(s)

Landing distance에 영향을 주는 요소라고 보기 힘든 것은?

speedbrakes
surface conditions of the runway.
Bouncing
height and speed over the threshold

Question 3 of 40

3. Question

1 point(s)

CARGO compartment에 single fire extinguisher bottle이 장착되어있는 항공기에 관한 설명으로 틀린 것은?

The cargo fire DISCH light illuminates once the bottle is discharged indicating the fire suppression system has been fully activated. It may take up to 60 seconds for the light to illuminate.
Detection of a fire in either the forward or aft compartment will cause the FWD or AFT cargo fire warning light to illuminate.
The extinguisher is armed by pushing the appropriate cargo fire ARMED switch.
A single fire extinguisher bottle is installed in the air conditioning mix bay on the forward wing spar.

Question 4 of 40

4. Question

1 point(s)

Engine “COWL ANTI-ICE” L’T가 illuminated되었을 경우 조치 방법은?

reduce thrust lever until the COWL ANTI-ICE light extinguishes
Advance thrust lever up to 40%
all bleed air off
Engine shut down

Question 5 of 40

5. Question

1 point(s)

SPOILER 작동 위한 AILERON 사용 각도는?

5°
10°
15°
20°

Question 6 of 40

6. Question

1 point(s)

심한 Headwind T/O일 경우, T/O thrust가 완전히 안 들어가는 경우가 있는데, 이때에는 수동으로 T/O thrust를 setting해야 한다. 몇 knots 이상의 바람에서 이 같은 현상이 생기는가?

15kts or greater
20kts or greater
25kts or greater
30kts or greater

Question 7 of 40

7. Question

1 point(s)

Which of the following will cause activation of the takeoff configuration warning horn?

Leading edge flaps in the extend position and trailing edge flaps at flaps 5.
Leading edge flaps in the full extend position and trailing edge flaps at flaps 15.
Spoilers not down with the speed brake lever in the DOWN position.
speed brake lever is not in the DOWN position

Question 8 of 40

8. Question

1 point(s)

The Ground Proximity Warning System Test에 관한 설명으로 맞는 것은?

in flight에서는 inhibit 된다.
Lift-off부터 1,000 feet RA 사이에서 test 할 수 있다.
지상에서, 그리고 1,000 feet RA 이상에서 test 할 수 있다.
언제든지 test를 수행할 수 있다.

Question 9 of 40

9. Question

1 point(s)

Landing gear manual extension에 관하여 맞는 것은?

Manual landing gear access door open시 landing gear retraction은 불가능하다.
HYD B SYSTEM을 이용하여 landing gear를 down 시킨다.
Manual gear extension handles는 captain 좌석 왼쪽 뒤에 위치한다.
Manual gear extension handle을 당기면 landing gear door lock을 release 시키고 이에 따라 landing gear가 free fall 하게 된다.

Question 10 of 40

10. Question

1 point(s)

AUTO BRAKE DISARM light가 illuminate되는 조건 중 틀린 것은?

SPEED BRAKE lever moved to down detent during RTO or landing
manual brakes applied during RTO or landing
landing made with RTO selected
Selector – OFF

Question 11 of 40

11. Question

1 point(s)

Electric Hydraulic Pump의 ground 작동을 위한 Minimum Fuel은?

660 kg
710 kg
760 kg
810 kg

Question 12 of 40

12. Question

1 point(s)

BLUE ENG V/V CLOSED, SPAR V/V CLOSED light가 DIM의 의미는?

related engine or spar fuel shutoff valve is closed
related engine or spar fuel shutoff valve is open
related engine or spar fuel shutoff valve is in transit,
valve position and engine start lever or engine fire switch disagree.

Question 13 of 40

13. Question

1 point(s)

The DFDR has Continuously records the most recent flight data, saving the most current data for the last ( ) hours of operation.

12
20
25
30

Question 14 of 40

14. Question

1 point(s)

Flaps and Slats의 Alternate Extension에 대한 설명으로 잘못된 것은?

hydraulic system B fail 시 사용된다.
standby hydraulic system의 동력을 이용하여 LE devices를 Fully Extend 한다.
standby hydraulic system의 동력을 이용하여 LE devices를 Retract 한다.
TE Flaps을 Extend 및 Retract한다.

Question 15 of 40

15. Question

1 point(s)

Runaway Stabilizer일때 제일 먼저 해야하는 절차는?

Control stand에 있는 STAB TRIM CUTOUT SWITCHES를 CUTOUT에 위치시킨다.
Control column을 꽉 쥐고 Auto pilot를 disengage 시킨다.
Stabilizer trim override switch를 override에 위치시킨다.
Stabilizer trim wheel을 손으로 꽉 쥔다.

Question 16 of 40

16. Question

1 point(s)

Flap을 extend할 수 있는 maximum 고도는?

10,000 feet
15,000 feet
17,000 feet
20,000 feet

Question 17 of 40

17. Question

1 point(s)

Both FLT CONTROL switch를 STBY RUD에 위치하였을 때 Yaw Damper switch에 대한 설명으로 맞는 것은?

disengages yaw damper
yaw damper S/W on 불가능
engages main yaw damper to main rudder power control unit
engages standby yaw damper to standby rudder power control unit

Question 18 of 40

18. Question

1 point(s)

Fault/Inop test시 light on 되는 것으로 틀린 것은?

Both master fire warning lights
the OVHT/DET system annunciator light illuminates
the FAULT light illuminates
the APU DET INOP light illuminates.

Question 19 of 40

19. Question

1 point(s)

Master FIRE WARN light push 했을 때 아닌 것은?

SYS annunciator light extinguished
silences fire warning bell
extinguishes both master FIRE WARN lights
resets system for additional warnings.

Question 20 of 40

20. Question

1 point(s)

If uncommanded movement of the Reverser is made or storage is not complete following condition will occur :

Electro – Mechanical Lock
Isolation Valve Open
STBY HYD activation
Control Valve (deploy)

Question 21 of 40

21. Question

1 point(s)

Thrust reverser system을 작동시키는 power source는?

해당 engine에서 생산되는 pneumatic power
다른 engine에서 생산되는 pneumatic power
Hydraulic power
해당 engine의 oil pressure

Question 22 of 40

22. Question

1 point(s)

Engine starting 중 EGT가 start limit를 초과할 때 나타나는 현상이 아닌 것은?

The EEC automatically turn off the ignition
The EEC automatically shut off fuel to the engine
The EGT display, both box and dial, turn red
Following engine shut down, the EGT box turns amber to remind the crew of the exceedance

Question 23 of 40

23. Question

1 point(s)

Overhead panel의 ENG CONTROL light on되었다. 틀린 것은?

In flight – on
On Ground below 80 kts prior to takeoff
approximately 30 seconds after touchdown on Ground
engine is operating and airplane on ground and below 80 kts prior to takeoff

Question 24 of 40

24. Question

1 point(s)

Engine starting 중 Start lever를 IDLE에 위치시키면 작동되는 구성품이 아닌 것은?

the fuel valves on the wing spar
the fuel valves on engine
Ignition System
Engine Starter

Question 25 of 40

25. Question

1 point(s)

Oil filter bypass alerts시 blinking is inhibited되는 것 중 틀린 것은?

Oil pressure at or below red line
during takeoff from 80 knots to 400 feet RA
during landing below 200 feet RA until 30 seconds after touchdown
during periods when blinking is inhibited, alerts illuminate steady

Question 26 of 40

26. Question

1 point(s)

정상상태에서 AC standby bus는 어디서 전원을 받는가?

AC transfer bus 1
DC transfer bus 1
hot battery bus
static inverter

Question 27 of 40

27. Question

1 point(s)

STBY Electrical system이 아닌 것은?

DC BUS No. 1
DC standby bus
battery bus
main battery

Question 28 of 40

28. Question

1 point(s)

STANDBY Power Off (PWR OFF) Light가 들어오는 조건으로 잘못된 것은?

AC standby bus
DC standby bus
AC & DC standby bus
battery bus

Question 29 of 40

29. Question

1 point(s)

ELEC amber light가 illuminate 되는 조건은?

a fault exist in AC power system, DC or STBY power system.
a fault exist in AC power system or STBY power system.
a fault exist in AC power system only.
a fault exists in DC power system or standby power system.

Question 30 of 40

30. Question

1 point(s)

Minimum under speed symbol (Under Limit Symbol)은 얼마 이상 set 되어야 없어지나?

A speed 10 knots greater than the minimum speed
A speed 15 knots greater than the minimum speed
A speed 20 knots greater than the minimum speed
A speed 25 knots greater than the minimum speed

Question 31 of 40

31. Question

1 point(s)

400 feet 이하에서 TO/GA mode disengage 시키는 방법?

both F/D switches must be turned OFF
another pitch mode select
A/P engage
LNAV select

Question 32 of 40

32. Question

1 point(s)

LNAV DISENGAGE 조건 아닌 것?

selecting HDG SEL
reaching a route discontinuity
reaching end of active route
VNAV disconnect

Question 33 of 40

33. Question

1 point(s)

다음 ANTI-ICE, RAIN SYSTEM에 관한 설명 중 잘못 된 것은?

The rain removal system for the forward windows consists of windshield wipers and a permanent rain repellent coating on the windows.
The wing anti-ice system provides bleed air to all leading edge slats.
The WING ANTI–ICE switch automatically trips OFF at lift–off when the air/ground sensor goes to the air mode.
Each cowl anti–ice valve is electrically controlled and pressure actuated.

Question 34 of 40

34. Question

1 point(s)

Window heat switch on 했으나 on light 안 들어왔을 때 그 이유가 아닌 것은?

switch is OFF
an overheat is detected
a system failure has occurred
system is at incorrect temperature

Question 35 of 40

35. Question

1 point(s)

다음 중 The Recirculation Fans에 관한 설명으로 맞는 것은?

DC motors에 의해 작동된다
cabin differential pressures가 과도하게 높을 때 airflow를 증가시킨다.
packs의 downstream에서 overheat detection 기능을 한다.
air conditioning pack의 load를 감소시킨다.

Question 36 of 40

36. Question

1 point(s)

다음 중 Thrust Mode Display에 대한 내용으로 잘못 된 것은?

R-TO : reduced takeoff
R-CLB : reduced climb
CRZ : cruise
GA : go–around

Question 37 of 40

37. Question

1 point(s)

If all Temperature Selectors are positioned OFF, the pack controls will cause ?

Left pack : 18°C, Right pack : 30°C
Left pack : 24°C, Right pack : 18°C
Left pack : 18°C, Right pack : 24°C
Left pack : 30°C, Right pack : 24°C

Question 38 of 40

38. Question

1 point(s)

Flap minimum maneuver speed 중 잘못된 것은?

Flaps UP : VREF 40 + 70
Flaps 1 : VREF 40 + 50
Flaps 5 : VREF 40 + 30
Flaps 15 : VREF 40 + 10

Question 39 of 40

39. Question

1 point(s)

Engine fire switch pull 시 작동하는 것 중 틀린 것은?

Arms one discharge squib on each engine fire extinguisher
Closes fuel, hydraulic shutoff and engine bleed air valves
Disables thrust reverser
Activates engine driven hydraulic pump LOW PRESSURE light

Question 40 of 40

40. Question

1 point(s)

다음 중 Bank Angle Alert 가 발생하는 각도가 아닌 것은 ?

30 °
35 °
40 °
45 °

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회사명 : 항공지식개발원∥ 대표: 박정미 ∥사업자번호 : 263-08-00970 서울특별시 마포구 성지길 25-11, 459 (합정동) | 통신판매업 : 제2021-서울마포-0586호 ∥ 문의 : ipilot.service@gmail.com

회사명 : 항공지식개발원∥ 대표: 박정미 ∥사업자번호 : 263-08-00970

서울특별시 마포구 성지길 25-11, 459 (합정동) | 통신판매업 : 제2021-서울마포-0586호 ∥ 문의 : ipilot.service@gmail.com