BLOCK A REVIEW (2018)

Question 1

1. ADI FD flag in view indicates that ________________ is/are unreliable.

Answer 1

Command Bars

Question 2

2. Normally __________ provides heading information to the pilot’s HIS and ________ provides heading information to the co-pilot’s HIS.

Answer 2

INU #1 & INU #2

Question 3

3. The command bars in the ADI cannot display _________ commands.

Answer 3

Constant Airspeed

Question 4

4. If the bearing pointer is set to VOR 1 and subsequently a localizer freq is set into the NAV radios, the bearing pointer will _____________.

Answer 4

Not Display

Question 5

5. The ________ flag in view indicates a heading is invalid.

Answer 5

HDG

Question 6

6. The bearing on either HIS can display ________ information.

Answer 6

TACAN, FMS or ADF, VOR 1 or VOR 2

Question 7

7. The ADF feature of the bearing pointer receives signals from the ______ radio.

Answer 7

COMM #1 UHF

Question 8

8. The radio altimeter decision height for the pilot flying the approach will be sent to the _________ for the approach being flown.

Answer 8

HHT or HHA

Question 9

9. The radio altimeter indicates absolute altitude only, and should not be used as the primary _______.

Answer 9

Decision Height Altitude

Question 10

10. Normalized AOA means ________.

Answer 10

AOA is displayed in % of lift by the pointer on Zero to 1.0 scale

Question 11

11. Pilot and co-pilot AOA indicators operate _____ and indicate ______readings when the airflow around the AOA probe varies, as in a side slip.

Answer 11

Independently and different

Question 12

12. The ______ illuminates anytime a comparator warning monitor light illuminates.

Answer 12

MSTR DISC Light and COMPAR warning light

Question 13

13. Depress the ______ to extinguish the COMPAR WARN light.

Answer 13

MASTR DISC Light or the COMPAR WARN Light

Question 14

14. When the glide slope COMPAR warning light illuminates, ________.

Answer 14

The difference between the pilot’s and co-pilot’s GS subsystem has exceeded the predetermined limit.

Question 15

15. The capture point of a VOR or TACAN radial, when using the NAV/LOC mode of the FD-109 system is approximately _______ degree the _____ dot on the HIS scale.

Answer 15

5 degree, inner

Question 16

16. The pitch command knob is used to manually set the command bars at any desired climb or descent pitch angle within the limit of ________ degrees of climb or ________ degrees of dive.

Answer 16

15, 10

Question 17

17. Momentarily depressing (1/2 sec or less) the remote slew on the yoke causes the heading marker to ________.

Answer 17

Move in 1degree increments

Question 18

18. When taxing the aircraft, do not set the flight director mode selector switch to the ________ position if turning, accelerating or decelerating.

Answer 18

RGA

Question 19

19. Just prior to reaching ________ speed both the pilot and co pilot will actuate their RGA push button switches.

Answer 19

Rotation

Question 20

20. If the rotation is delayed (speed increased), the command bars willcommand a reduced pitch during climb out and provide an increase in climb out speed _____ the increase in rotation speed.

Answer 20

Approximately Equal to

Question 21

21. Aircraft rotation for take off ________ be delayed in order to actuate the RGA push button switch.

Answer 21

Will not

Question 22

22. If the RGA push button switch is not pressed prior to rotation or an incorrect rotation command is displayed on the ADI, rotate to ______ degrees on the ADI pitch tape.

Answer 22

8 to 9

Question 23

23. The RGA System does not ______.

Answer 23

Provide lateral steering commands

Question 24

24. In ACCL mode, the RGA system is programmed to command a _____ pitch change during climb out at a rate of _____ every 6 to 7 seconds.

Answer 24

Nose down, 1 degree

Question 25

25. During climb out with ACCL mode selected, initiate flap retraction at flap retraction speed, provided aircraft altitude is at least ________ ft AGL.

Answer 25

200

Question 26

26. In the ACCL mode, once the flaps are retracted above 16.5 degrees, the command bars command a pitch attitude which ________.

Answer 26

Transitions to a constant airspeed climb

Question 27

27. With 4 engines operating, MAX mode, accelerate to recommended 3 engine climb out speed plus ______ knots and climb out to ________ ft above the runway or obstacle clearance height, whichever is higher.

Answer 27

10, 2000

Question 28

28. Since the constant speed maximum climb command is normally less than the flap retraction speed, the command bars display must be _______ when the appropriate altitude is reached for acceleration to flap retraction speed.

Answer 28

Ignored

Question 29

29. Always set the FD mode selector to _______ before changing the NAV aid frequency or switching NAV receivers.

Answer 29

HDG or GYRO

Question 30

30. During cruise, the AOA indicator can be used to maintain an optimum AOA for _________.

Answer 30

Max Endurance or Range

Question 31

31. The _________ mode provides a command bar for intercepting andtracking a localized beam and GS path.

Answer 31

APPR AUTO

Question 32

32. Setting flight director mode selector to APPR AUTO while a localizer frequency is tuned causes the steering commands of the command bars to operate in the _______ mode until entering the capture range.

Answer 32

HDG