B_실전 모의고사 A형

Question 1 of 40

1. Question

1 point(s)

Flight Deck Door Lock Panel 에서 LOCK FAIL light 가 illuminate 되는 것은?

Flight deck lock switch auto and lock has failed
Flight deck door lock selector deny
When reject key pad entry is requested
When chime sound

Question 2 of 40

2. Question

1 point(s)

amber AUTO FAIL light가 illuminate되지 않는 조건은?

AC POWER loss
Controller fault
Excessive rate of cabin pressure change
High cabin alititude(above 15,800ft)

Question 3 of 40

3. 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 4 of 40

4. 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 5 of 40

5. Question

1 point(s)

LNAV DISENGAGE 조건 아닌 것?

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

Question 6 of 40

6. Question

1 point(s)

When control pressure released, A/P holds existing attitude.

If aileron pressure released with ( ) or less bank, the A/P rolls wings level and holds existing heading.

3 degrees
6 degrees
10 degrees
15 degrees

Question 7 of 40

7. Question

1 point(s)

Auto pilot가 engage 되어야만 작동되는 system은?

SPEED TRIM
YAW DAMPER
AIDRU
STABILIZER OUT OF TRIM

Question 8 of 40

8. Question

1 point(s)

In the degraded mode, the audio system cannot access the passenger address system through the audio control panel, What are combinations for transmission and reception at the degraded station?

Captain/VHF-1, FO/VHF-2, Observer/VHF-1
Captain/VHF-1, FO/VHF-2, Observer/VHF-2
Captain/VHF-2, FO/VHF-1, Observer/VHF-1
Captain/VHF-1, FO/VHF-1, Observer/VHF-1

Question 9 of 40

9. 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 10 of 40

10. Question

1 point(s)

Generator Drive (DRIVE) Lights가 들어오는 경우가 아닌 것은?

IDG failure
engine shutdown
IDG automatic disconnect due to low oil temperature
IDG disconnected through generator drive DISCONNECT switch

Question 11 of 40

11. Question

1 point(s)

Cross Bus Tie rely가 언제 open되는가?

During VOR / DME Approach and VNAV PATH mode일 때
NDB approach 중 VNAV PATH 일 때
ILS approach 중 G/S를 capture 했을 경우
ILS approach 중 LOC를 capture 했을 경우

Question 12 of 40

12. Question

1 point(s)

Positioning the STBY PWR SW to “BAT” overrides ?

manually switching and places the AC bus, DC bus, and battery bus on battery power
automatic switching and places the AC bus, DC bus, and battery bus on battery power
manually switching and places the AC standby bus, DC standby bus, and battery bus on battery power
automatic switching and places the AC standby bus, DC standby bus, and battery bus on battery power

Question 13 of 40

13. 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 14 of 40

14. Question

1 point(s)

Reverse thrust lever 사용 시 Idle position에 몇 % Deploy 될 때 까지 block되는가?

50 %
55 %
60 %
65 %

Question 15 of 40

15. 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 16 of 40

16. 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 17 of 40

17. Question

1 point(s)

FAULT/INOP Test에 관한 설명으로 맞는 것?

Tests overheat and Fire detection loops on both engines and APU, and wheel well Fire detector
Tests both engine overheat detectors
Tests fault detection circuits for both engines and the APU
Tests bottle discharge circuit continuity for all three extinguisher bottles

Question 18 of 40

18. Question

1 point(s)

APU Fire Switch를 Up하면 어떻게 되는가?

opens fuel shutoff valve, APU bleed air valve, and APU inlet door
activate generator control relay and breaker
disarm APU fire switch to rotate
arms APU extinguisher circuit

Question 19 of 40

19. Question

1 point(s)

Cargo fire 언제 detector fault light 뜨는가?

One or more of the selected detector loop in either cargo compartment has failed
One of the selected detector loop has failed
The selected detector loop in both cargo compartment has failed
Indicate both detector loops for an engine have failed

Question 20 of 40

20. Question

1 point(s)

ENG OVERHEAT 증상이 아닌 것은?

FIRE Warning Bell Sound
The OVHT/DET system annunciator light illuminates
Both MASTER CAUTION lights illuminate
The related ENG OVERHEAT light illuminates.

Question 21 of 40

21. 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 22 of 40

22. Question

1 point(s)

Flap을 extend할 수 있는 maximum 고도는?

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

Question 23 of 40

23. Question

1 point(s)

Auto pilot disengage 되는 경우는?

Both control wheel에 trim switch로만 가능하다
Dual A/P CMD 상태로 내렸을 때 TO/GA engage
Stabilizer trim switch cut off 했을 때
Standby hydraulic fail 시

Question 24 of 40

24. Question

1 point(s)

STS(Speed Trim System) 작동에 대한 설명 중 틀린 것은?

A/P engage
10 seconds after takeoff
5 seconds following release of trim switches
Sensing of trim requirement

Question 25 of 40

25. Question

1 point(s)

Expanded Localizer Scale Reverts to standard scale when out of LOC mode, and groundspeed is ?

less than 30 knots or radio altitude is greater than 200 feet.
less than 40 knots or radio altitude is greater than 200 feet.
less than 30 knots or radio altitude is greater than 300 feet
less than 40 knots or radio altitude is greater than 300 feet.

Question 26 of 40

26. Question

1 point(s)

Dual FMC failure 시 해당사항 아닌 것은?

FMC Alert L/T illuminate
LNAV and VNAV engage
VTK will appear on both navigation display
the menu page will appear on both CDUs

Question 27 of 40

27. 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 28 of 40

28. Question

1 point(s)

Main tank FUEL PUMP LOW PRESSURE Lights illuminated (amber) 됐을 시 맞는 것은?

One LOW PRESSURE light illuminates MASTER CAUTION and FUEL system annunciator lights.
One LOW PRESSURE light causes MASTER CAUTION and FUEL system annunciator lights to illuminate on MASTER CAUTION light recall.
Two LOW PRESSURE lights illuminated in same tank illuminate MASTER CAUTION and FUEL system annunciator lights.
Two LOW PRESSURE lights illuminated in same tank cause MASTER CAUTION and FUEL system annunciator lights to illuminate on MASTER CAUTION light recall

Question 29 of 40

29. Question

1 point(s)

HTD B로 작동되는 시스템은 다음 중 무엇인가?

Autoslats
Normal nose wheel steering
Ground spoiler
PTU

Question 30 of 40

30. Question

1 point(s)

다음 중 LANDING GEAR LIMIT으로 맞는 것은?

OPERATING EXTEND 270-.82M RETRACT 235K EXTENDED 320K-.82M
OPERATING EXTEND 270-.84M RETRACT 240K EXTENDED 320K-.82M
OPERATING EXTEND 270-.82M RETRACT 235K EXTENDED 320K-.84M
OPERATING EXTEND 270-.82M RETRACT 240K EXTENDED 320K-.82M

Question 31 of 40

31. Question

1 point(s)

Brake Symbol – Amber Range는 얼마인가?

above 2.5
above 3.5
above 4.9
above 9.9

Question 32 of 40

32. 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 33 of 40

33. 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 34 of 40

34. Question

1 point(s)

Landing Airport Elevation 7000FT 이상인 공항에서 LAND ALT SET 절차로 올바른 것은?

이륙 전 : LAND ALT 7,000ft
착륙 전 : 20분 전이나 DESCENT 시작 시 DESTINATION airport ALT set
착륙 전 : DESCENT 시작 시 6,000 ft set
첫 강하 전 : 목적지 공항 고도 설정

Question 35 of 40

35. Question

1 point(s)

Window Heat On Lights의 제한속도와 고도는?

250knots below 10,000ft
250knots above 10,000ft
200knots below 10,000ft
200knots above 10,000ft

Question 36 of 40

36. Question

1 point(s)

What do you do If COWL VALVE OPEN lights remain illuminated bright with engine at IDLE on Ground ?

Turn Wing anti-ice switch Off
Turn APU BLEED air switch On
Increase thrust up to a maximum of 40% N1
Position APU BLEED air switch to OFF and increase thrust slightly (up to a maximum of 30% N1)

Question 37 of 40

37. Question

1 point(s)

APU BLEED를 반드시 CLOSE해야 하는 경우는?

ground air connected and isolation valve open
isolation and engine no. 1 bleed valve open
engine no. 2 bleed valves open
engine no. 1 and engine no. 2 bleed valves open

Question 38 of 40

38. Question

1 point(s)

Max Rate of Climb의 속도는?

Vref 40 + 50 and until intercept 0.76M
Vref 40 + 50 and until intercept 0.82M
Vref 40 + 70 and until intercept 0.76M
Vref 40 + 70 and until intercept 0.82M

Question 39 of 40

39. Question

1 point(s)

활주로에서의 감속률은 공중에서의 감속률의 몇 배 정도 되는가?

2 배
3 배
4 배
5 배

Question 40 of 40

40. 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

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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