B_실전 모의고사 D형

Question 1 of 40

1. Question

1 point(s)

PFD에 Pitch disagree의 의미는?

Captain과 F/O의 Pitch 차이가 3도 이상 날 때
Captain과 F/O의 Pitch 차이가 5도 이상 날 때
Captain과 F/O의 Altimeter 차이가 200ft 이상 날 때
Captain과 F/O의 Pitch 차이가 10도 이상 날 때

Question 2 of 40

2. Question

1 point(s)

Hydraulic Brake Pressure에 대한 설명 중 맞는 것은?

normal pressure – 3000 psi maximum pressure – 3500 psi
normal pressure – 3500 psi maximum pressure – 3000 psi
normal pressure – 1000 psi maximum pressure – 1850 psi
normal pressure – 1850 psi maximum pressure – 2000 psi

Question 3 of 40

3. 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 4 of 40

4. Question

1 point(s)

RVSM 을 위해 sea level 의 공항에서 Max Difference Between Captain & F/O는 얼마인가?

50 ft
75 ft
200 ft
300 ft

Question 5 of 40

5. Question

1 point(s)

Cross-wind 20knot일 때 추천되는 takeoff 방법은?

Rolling take off
Reduced thrust take off
Standing take off
Static take off

Question 6 of 40

6. Question

1 point(s)

Landing gear transfer unit에 관하여 작동 조건이 아닌 것은?

airborne
No. 1 engine RPM drops below a limit value
landing gear lever is positioned UP
both main landing gear is not up and locked

Question 7 of 40

7. Question

1 point(s)

Non-normal 상황발생, QRH에서 APP SPD를 Vref40+30kts를 사용할 경우, Speed calculation 을 어떻게 해야하는가?

Vref40 + 30kts (no wind additive)
Vref40+30kts wind additive(min +5kts)
Vref40+30kts wind additive(min +5kts to max +15kts)
Vref40+30kts wind additive(max +10kts)

Question 8 of 40

8. Question

1 point(s)

Secondary engine indications에 표시되지 않는 계기는?

Fuel flow
oil pressure
EGT
oil temp

Question 9 of 40

9. Question

1 point(s)

During takeoff and landing, new predictive windshear caution alerts are inhibited between 80kts and 400ft RA, new warning alert은?

Between 50ft RA
Between 100ft RA and 50 kts
Between 100kts and 50ft RA
Between 100kts

Question 10 of 40

10. Question

1 point(s)

다음 중 amber DUAL BLEED light가 들어오는 경우가 아닌 것은?

When the APU bleed valve is open and the No.1 engine bleed valve is On.
When the APU bleed valve is open and the No.2 engine bleed switch is ON.
When the APU bleed valve is open, the No.2 engine bleed switch is ON and the isolation valve is open.
When the APU bleed valve is open and the No.1 engine bleed switch is ON and isolation valve is close.

Question 11 of 40

11. 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 12 of 40

12. Question

1 point(s)

TR UNIT light가 illuminate – Amber가 아닌 경우는 ?

TR1 failed in Flight
TR3 failed on Ground
TR2 failed
TR2 and TR3 failed

Question 13 of 40

13. 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 14 of 40

14. Question

1 point(s)

CARGO FIRE DISCHARGE light는 Bottle이 Discharge 얼마 후 On 되는가?

extinguisher bottle has discharged
10 sec after extinguisher bottle has discharged
30 sec after extinguisher bottle has discharged
60 min after extinguisher bottle has discharged

Question 15 of 40

15. Question

1 point(s)

지상에서 Wing Anti-Ice switch on 일 때, Control valve가 자동으로 close되는 조건은?

Either engine thrust is above takeoff warning setting or thermal switch is activated in either distribution duct. Switch remains ON
Either engine thrust is above takeoff warning setting and thermal switch is activated in either distribution duct. Switch remains ON
Thrust on both engines is below takeoff warning setting and temperature inside both distribution ducts is below thermal switch activation temperature
Thrust on both engines is below takeoff warning setting or temperature inside both distribution ducts is below thermal switch activation temperature

Question 16 of 40

16. 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 17 of 40

17. Question

1 point(s)

Max depth of slush for takeoff?

1.0 inches
0.5 inches
0.3 inches
0.7 inches

Question 18 of 40

18. Question

1 point(s)

비행 중, TR UNIT amber light illuminate 경우에 해당하는 것은?

TR1 or TR2 has failed
TR1 and TR2 has failed
TR1, or TR2 and TR3 has failed.
any TR fault

Question 19 of 40

19. 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 20 of 40

20. Question

1 point(s)

Auto brake에 관하여 맞는 것은?

Speed brake나 thrust reverse 사용에 관계없이 select된 auto brake level로 brake pressure 가 일정하게 적용된다.
Auto brake를 select하고 landing 시 main wheel이 touch down하면 바로 auto brake가 작동된다
Auto brake 작동 중 speed brake lever를 down에 위치해도 auto brake는 계속 작동된다.
Dry runway 상에서 maximum auto brake는 full pedal brake 보다는 deceleration rate가 적다.

Question 21 of 40

21. 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 22 of 40

22. 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 23 of 40

23. Question

1 point(s)

다음 중 HYD SYS B 로부터 받지 않는 시스템은 무엇인가?

Normal brake
Normal nosewheel steering
Yaw damper
ailerons

Question 24 of 40

24. Question

1 point(s)

Degraded Audio System Operation 중 Degraded mode에서 들을 수 없는 alert는?

Altitude Alert, GPWS, Windshear
TCAS, GPWS, Windshear
GPWS, TCAS, Windshear
TCAS, Altitude Alert, GPWS, Windshear

Question 25 of 40

25. 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 26 of 40

26. Question

1 point(s)

The PASS OXY ON light illuminates amber. What does this indicate?

passenger oxygen system pressure is low.
OVERHEAD annunciator light is extinguished on the Master Caution
passenger oxygen quantity is low.
passenger oxygen system is operating and masks have dropped.

Question 27 of 40

27. Question

1 point(s)

Brake system으로 잘못 된 것은?

Normal Brake는 HYD B system이다
Standby Brake는 HYD B의 압력을 이용한다.
Brake Accumulator는 HYD B의 압력을 이용한다.
Antiskid system은 Normal Brake에만 적용된다.

Question 28 of 40

28. 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 29 of 40

29. Question

1 point(s)

G/S Capture 시기는?

3/5 dot below or above
2.5/5 dot below or above
2/5 dot below or above
1/5 dot below or above

Question 30 of 40

30. Question

1 point(s)

EEC가 Power를 받지 않으면 나오지 않는 indication이 아닌 것은?

EGT
N1
N2
Oil Quantity

Question 31 of 40

31. Question

1 point(s)

활주로에서의 감속률은 공중에서의 감속률의 몇 배 정도 되는가?

2 배
3 배
4 배
5 배

Question 32 of 40

32. Question

1 point(s)

Maximum tank fuel temperature는 얼마인가?

40°C
46°C
49°C
54°C

Question 33 of 40

33. Question

1 point(s)

To display the way point in the FMC data base which are not in the flight plan route, selected range is ?

10nm or less
20nm or less
40nm or less
80nm or less

Question 34 of 40

34. Question

1 point(s)

Which is not a condition for applying VREF ICE ?

Engine anti–ice will be used during landing
Engine anti–ice has been used any time during the flight
Wing anti–ice has been used any time during the flight
Icing conditions were encountered during the flight and the landing temperature is below 10°C

Question 35 of 40

35. Question

1 point(s)

Minimum tank fuel temperature prior to takeoff and inflight는 얼마인가?

–45°C, or 3°C above the fuel freezing point temperature, whichever is higher.
–43°C, or 5°C above the fuel freezing point temperature, whichever is higher.
–43°C, or 3°C above the fuel freezing point temperature, whichever is higher.
–45°C, or 5°C above the fuel freezing point temperature, whichever is higher.

Question 36 of 40

36. Question

1 point(s)

V/S mode로 Non precision app시 Missed approach altitude 를 Set하는 시기는 언제인가?

Final app fix 지나고 300ft 아래에서
Final app fix 지나고 500ft 아래에서
MDA + 500ft에서
MDA + 300ft에서

Question 37 of 40

37. Question

1 point(s)

Two independent Mach/ airspeed warning systems provide a distinct aural warning, a clacker, any time the maximum operating airspeed of Vmo/ Mmo is exceeded. 이럴 때 어떻게 해야 조용해지나?

by reducing airspeed below Vmo/Mmo.
by pressing Master Fire Warning (FIRE WARN) Lights
by pressing MASTER CAUTION Lights
Can not reset

Question 38 of 40

38. Question

1 point(s)

Center tank FUEL PUMP switches – ON 상태에서 LOW PRESSURE light가 몇 초 이상 지속되면 MASTER CAUTION and FUEL system annunciator lights가 illuminate되는가?

35
10초
15초
30초

Question 39 of 40

39. Question

1 point(s)

Auto speed brake 작동 시기로 틀린 것은?

Landing gear strut compresses on touchdown
Radio altitude less than 50ft
Both thrust levers retarded to IDLE
Main landing gear wheels spin up

Question 40 of 40

40. Question

1 point(s)

pressurization을 위한 Cabin altitude 조절 시 작동되 는 V/ V는?

outflow v/v, overflow v/v
outflow v/v
overflow v/v
isolation V/V

Average score
Your score

B737 Type Rating

OPERATION PART

전체문제 해설 확인하기

Information

Results

Results

난이도

1. Question

2. Question

3. Question

4. Question

5. Question

6. Question

7. Question

8. Question

9. Question

10. Question

11. Question

12. Question

13. Question

14. Question

15. Question

16. Question

17. Question

18. Question

19. Question

20. Question

21. Question

22. Question

23. Question

24. Question

25. Question

26. Question

27. Question

28. Question

29. Question

30. Question

31. Question

32. Question

33. Question

34. Question

35. Question

36. Question

37. Question

38. Question

39. Question

40. Question

국토부 항공직렬

조종사 자격증

정비사 | 관제사

한정증명

Information

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