2a533b Volume 3

1. The master caution light can be extinguished or reset by

Depressing it momentarily

Depressing it several times

Resetting the circuit breaker

Actuating the light reset switch

2. Which indicator helps the pilot maintain a specific rate of climb or dive

Altimeter

Machmeter

True A/S

Vertical velocity

3. What type of error is caused by the location and manner in which a pitot tube is installed

Density error

Instrument error

Installation error

AOA error

4. Mechanical error within the A/S indicator is called

Density error

Instrument error

Installation error

AOA error

5. When activated, which switch causes the No. 1 SCADC to output fixed values of altitude, vertical speed, mach, A/S, and true A/S?

Pilot's SCADC self-test switch

Pilot's SCADC test disconnect

Copilot's SCADC self-test switch

Copilot's SCADC test disconnect

6. Which integrated flight management system subsystem uses multiple satellites to calculate the aircrafts present longitude and latitude

Automatic flight display system

Color weather radar system

Global positioning system

Inertial navigation system

7. At what altitudes is the ground proximity warning system active

0-1,000 feet

50-2,450 feet

100-12,450 feet

1,000-10,000 feet

8. What does an optical data bus use as the controlling protocol for high-speed message transfer

MIL-STD-3910B

MIL-STD-1553B

Optic transceiver

Star coupler

9. Which video symbology display system component receives compass, A/S, roll/pitch, and radio altitude information via the system electronic unit?

Symbol generator unit

Target availability unit

Resolution advisory unit

Navigation data control unit

10. Which integrated flight management system subsystem may be used to detect airborne targets?

Automatic flight display system

Color weather radar system

Global positioning system

Inertial navigation system

11. Which caution//advisory warning lights indicate actuation and normal operation of aircraft equipment

Blue

Black

Green

Yellow

12. The maximum number of avionics units the military standard 1553B data bus is capable of transferring data between is

16

25

32

64

13. When the bus controller detects a transmission error while communicating with a RT on the military standard 1553B data bus, the bus controller

Retransmits the command several times, and then tries the backup data bus

Is disabled and the backup controller resumes transmission

Attempts to retransmit to the RT until contact is made

Establishes communications with a different RT

14. To view data on the alphanumeric display of the CITS computer display panel, the DIS mode switch must be in what position

STIM

KYBD

START

CMPTR

15. The standard datum plane is a theoretical plane where the atmospheric pressure is

30.00'' of mercury (Hg) and the temperature is +15 degrees C

30.00'' Hg and the temperature is +40 degrees C

29.92'' Hg and the temperature is +15 degrees C

29.92'' Hg and the temperature is +40 degrees C

16. Static pressure is

Less at low radar altitudes and greater at higher radar altitudes

Less at low attack angles and greater at higher attack angles

Greater at low A/Ss and less at higher A/Ss

Greater at low altitudes and less at higher altitudes

17. Density error can be corrected by adjusting the

Barometric scale on the front of the indicator

Barometric scale on the back of the indicator

High pressure scale on the front of the indicator

High pressure scale on the back of the indicator

18. Which error(s) must be corrected to make an A/S indicator display true A/S

Altitude

Altitude and impact

Temperature and impact

Altitude and temperature

19. What are the HUD master control switch positions

OFF, NIGHT, TEST, and DAY

OFF, NIGHT, AUTO, and DAY

OFF, ACTIVE, AUTO, and DAY

20. According to the principles applicable to the A/S indicator, as altitude increases, the maximum allowable A/S

Increases

Decreases

Stays the same

Increases, and then decreases

21. During what aircraft maneuver is the static pressure inside the diaphragm of the vertical velocity indicator greater than on the outside

Roll

Dive

Climb

Level flight

22. The primary difference between indicated A/S and true A/S is the

Density error

Instrument error

Installation error

AOA error

23. To locate a CMC autoflow chart in the system integration manual, you use the

Table of contents

CMC integration

CMC-to-Autoflow Cross-Reference LIST

CMC, PAGE, and ENTRY POINT index

24. What is the range of the indicated A/S tape on the Mach-A/S indicator

50-500 knots

50-600 knots

100-500 knots

100-600 knots

25. The data loader system is comprised of a

Data cable and data receptacle

Data card and data receptacle

Data cable and data recorder

Data card and data recorder

26. To represent increasing levels of urgency or threat, symbols generated by the traffic alert and collision avoidance system change

Color and size

Size and shape

Shape and color

Shape and position

27. Each type of word used on the Military Standard 1553B data bus is

20 bits long with a 3-bit sync character, 16 information bits, and one parity bit

16 bits long with a 3-bit sync character, 12 information bits, and one parity bit

10 bits long with a 2-bit sync character, seven information bits, and one parity bit

8 bits long with a 2-bit sync character, five information bits, and one parity bit

28. What provides the primary processing and interface functions for the flight management system

Automatic flight display system

Navigation computer

Control display unit

Data loader system

29. The tape capacity of the digital flight data recorder system is

10 minutes

25 minutes

10 hours

25 hours

30. Which digital flight data recorder system unit samples aircraft system data and converts it into digital form

Monitor

Recorder

Air control

Acquisition

31. Which is not an advantage of an active on-board collision system

Works anywhere in the world

Relies on local radar to generate transponder replies

Has an on-board system that queries local transponders for replies

Creates images of the local traffic for display on the multifunction displays

32. Information describing the condition of a RT on a Military Standard 1553B data bus is transmitted as a

Command word in response to a command from the RT

Data word in response to a command from the bus controller

Status word in response to a command from the bus controller

Data word in response to a command from the backup controller

33. The total air temperature is calibrated in

One-degree increments from -70 degrees C to +80 degrees C

One-degree increments from -50 degrees C to +60 degrees C

Two-degree increments from -70 degrees C to +80 degrees C

Two-degree increments from -50 degrees C to +60 degrees C

34. With the stall prevention system control panel test switch in the TEST position, the shaker can be activated by manually moving the

Angle-of-attack (AOA) vane

Autopilot pitch trim knob

AOA indicator bug

Control columns

35. A backup bus controller on the military standard 1553B data bus is

Mandantory and must be active at the sameas the primary bus controller

Mandantory and must not be active at the same time as the primary controller

Optional and may be active at the same time as the primary bus controller

Not required for normal operation, but is required on modern data buses

36. What type of pressure enters the A/S diaphragm of the A/S indicator

Pitot

Static

Engine

Barometric

37. After the receiving RT on a Military Standard 1553B data bus has received and validated the data words from the transmitting RT during an RT-to-RT transfer, it

Transmits a command word to indicate receipt of the message

Responds with a status word indicating a successful transfer

Responds with a data word indicating a successful transfer

Transmits a data word to the transmitting RT

38. The HUD show declutter 1, declutter 2, and what three levels of symbol presentation

Enroute (declutter on) levels of symbol presentation

Enroute (declutter off) levels of symbol presentation

Normal (declutter on) levels of symbol presentation

Normal (declutter off) levels of symbol presentation

39. During which standard central air data computer built-in tests can recorded failures be retrieved

0 and 6

1 and 2

3 and 9

5 and 7

40. Which element of the Military standard 1553B data bus is not usually used in avionics bus systems

Remote terminal

Bus controller

Stub coupler

Bus monitor

41. The video symbology display system displays a visual representation of navigation data, A/S, altitude

And axis velocities

And target acquisition

And target availability

Axis velocities, and various cautions

42. Each total air temperature probe contains

Two variable resistance-type sensing elements

Two variable capacitance-type sensing elements

Three variable resistance-type sensing elements

Three variable capacitance-type sensing elements

43. What displays on the Mach-A/S indicator respond to synchro outputs from the standard central air data computer?

Command A/S and minimum A/S speed

IAS and Mach

IAS and minimum safe A/S

Command A/S and mach

44. Which is not a traffic alert and collision avoidance system (TCAS) traffic advisory function

Issue specific aural warning to the aircrew

Provides the inital alert from the TCAS processor

Provides recommendations to the pilot for aircraft maneuvers

Attracts attention to the traffic display on the multifunction display

45. When the DISPLAY switch on the CITS computer display panel is momentarily pressed to DIS RESET,

All of the alphanumeric display is cleared

All lighted matrix switches are turned off and reset

The current line on the alphanumeric display is cleared

All lighted matrix switches are turned on for three seconds, and then off

46. The mission computer provides display mode commands, flight director commands, and

Radio altitude

Radar altitude

Ground faults

Flight failures

47. The HUDs are focused to infinity and permit a wide field of view of

25 degrees horizontal and 18 degrees vertical

25 degrees horizontal and 24 degrees vertical

30 degrees horizontal and 24 degrees vertical

30 degrees horizontal and 30 degrees vertical

48. After the ADTD is first turned on, the heaters/ADTD may take up to

20 minutes to reach 0 degrees C

20 minutes to reach 0 degrees F

30 minutes to reach 20 degrees C

30 minutes to reach 20 degrees F

49. If a fault condition exists, the fault indicators on the front of the flight data acquisition unit are solid

Red

Black

White

Yellow

50. The stall prevention computer produces a shaker signal if the aircraft angle-of-attack (AOA) and the permissible AOA are

Equal

Within two degrees of each other

Within five degrees of each other

Within 10 degrees of each other

51. In a military standard 1553B data bus command word, the field that refers to a function or area within the remote terminal to which command is being directed is the

Address field

Subaddress/mode field

Transmit/receive bit field

Word count/mode code field

52. The sensing elements in the true A/S indicator are surrounded by

Pitot pressure

Static pressure

Engine pressure

Methyl chloride gas

53. Which Mach-A/S indicator displays are manually inserted

Command Mach and command IAS

Command Mach and minimum safe A/S

Mach and minimum safe A/S

Mach and command IAS

54. The aircraft parameter data file is recorded by the

CITS maintenance recorder

Data conversion unit

Data acquisition unit

Digital computer

55. If you have the barometric counter set to 29.92 during a self-test of the ALT-vertical speed indicator, the ALT display should slew to how many feet

20,000

50,000

75,000

80,000

56. Which ground proximity warning system mode is always active when the aircraft is between 50 and 2,450 feet, regardless of aircraft configuration

Mode 1, excessive sink rate

Mode 2, excessive closure rate

Mode 4, proximity to terrain

Mode 5, descent below glideslope

57. Which element of the military standard 1553B data bus gathers and formats information from aircraft sensors for transfer on the data bus

Monitor

Bus controller

Remote terminal

Backup controller

58. Which LRU is the CITS data bus controller

CITS maintenance recorder

Data conversion unit

Data acquisition unit

Digital computer

59. How many different test patterns are used when the CITS computer display panel's DIS TEST switch is used

1

2

3

4

60. In which mode is a CITS maintenance code displayed on the CITS computer display panel

ACFT

GND RDY

FLT FAULT ISLN

GND FAULT ISLN

61. The stall prevention computer produces a pusher signal if the aircraft angle-of-attack (AOA) equals the permissible AOA for

One second

Three seconds

Five seconds

10 seconds

62. The system integration manual does not contain

A description of the CITS system

A description of aircraft power control management

Descriptions of aircraft software configuration

Descriptions of CITS system autoflow

63. The heart of the vertical velocity indicator is a

Barometric scale

Expansion valve

Differential diaphragm

Pressure sensitive diaphragm

64. The absence of which intruder data specifically prohibits the traffic alert and collison avoidance system from issuing resolution advisories

Range

Bearing

Altitude

Closure rate

65. The video symbology display system's symbol generator unit processes analog information, military standard 1553B bus data, and

Target data

Optic commands

Mode commands

TEST commands

66. When the failure annunciator on the front of the standard central air data computer is reset, it shows

Solid black

Solid white

Three red wedges on a black background

Three white wedges on a black background

67. The command Mach marker on the Mach-A/S indicator tracks the

Command Mach slew switch

Mach tape as Mach changes

Lubber line as Mach changes

Command Mach counter

68. What type of pressure is applied to the inside of the thermos chamber of the rate-of-climb indicator

Diffused pitot

Diffused static

Unrestricted pitot

Unrestricted static

69. Which standard central air data computer BIT allows slewing of altitude and A/S

1

3

6

9

70. Which is not a resolution advisory?

Corrective

Preventive

Change to current advisory

Change to previous advisory

71. For how many aircraft maximum can the traffic alert and collision avoidance system track and generate displays

24

30

40

48

72. The superior type of data bus stub on a military standard 1553B data bus is the

Transformer-coupled stub with external coupling network

Transformer-coupled stub with internal coupling network

Direct-coupled stub with internal coupling network

Direct-coupled stub with external coupling network

73. Which conditions cause an uncorrected A/S indicator to read higher than it should?

Decreased altitude and decreased temperature

Decreased altitude and increased temperature

Increased altitude and decreased temperature

Increased altitude and increased temperature

74. The word count field in a controller-to-RT transfer message on the military standard 1553B data bus must correspond to the number of

Status words the RT transmits to the bus controller

Data words the RT receives from the bus controller

Status words the RT receives from the bus controller

Command words the RT transmits to the bus controller

75. During self-test of the Mach-A/S indicator, the Mach and indicated A/S tapes drive to

0.92 Mach and 225 knots, respectively

0.92 Mach and 250 knots, respectively

0.825 Mach and 225 knots, respectively

0.825 Mach and 250 knots, respectively

76. What is the purpose of the mode-S traffic alert and collision avoidance system (TCAS) function

Track all TCAS-equipped aircraft

Develop TCAS symbology for traffic advisories

Establish/track aircraft identification and characteristics addresses

Establish resolution advisories based on the intruding aircraft's positon

77. Which type of data bus stub is most suitable for stubs less than one foot in length on the Military Standard 1553B data bus

Transformer coupled stub with external coupling network

Transformer-coupled stub with internal coupling network

Direct-coupled stub with external coupling network

78. During mode command transfers on a military standard 1553B data bus, the word count/mode code field identifies the

Particular mode command being implemented by the RT

Particular mode command being implemented by the bus controller

Number of data words to be transferred by the bus controller

Number of data words to be received by the RT

79. Circuit parameter data from the communications and dependent position determining subsystems is received by the

CITS maintenance recorder

Data conversion unit

Data acquisition unit

Digital computer

2a533b Volume 3

1. The master caution light can be extinguished or reset by

2.

What first name or nickname would you like us to use?

2. Which indicator helps the pilot maintain a specific rate of climb or dive

3. What type of error is caused by the location and manner in which a pitot tube is installed

4. Mechanical error within the A/S indicator is called

5. When activated, which switch causes the No. 1 SCADC to output fixed values of altitude, vertical speed, mach, A/S, and true A/S?

6. Which integrated flight management system subsystem uses multiple satellites to calculate the aircrafts present longitude and latitude

7. At what altitudes is the ground proximity warning system active

8. What does an optical data bus use as the controlling protocol for high-speed message transfer

9. Which video symbology display system component receives compass, A/S, roll/pitch, and radio altitude information via the system electronic unit?

10. Which integrated flight management system subsystem may be used to detect airborne targets?

11. Which caution//advisory warning lights indicate actuation and normal operation of aircraft equipment

12. The maximum number of avionics units the military standard 1553B data bus is capable of transferring data between is

13. When the bus controller detects a transmission error while communicating with a RT on the military standard 1553B data bus, the bus controller

14. To view data on the alphanumeric display of the CITS computer display panel, the DIS mode switch must be in what position

15. The standard datum plane is a theoretical plane where the atmospheric pressure is

16. Static pressure is

17. Density error can be corrected by adjusting the

18. Which error(s) must be corrected to make an A/S indicator display true A/S

19. What are the HUD master control switch positions

20. According to the principles applicable to the A/S indicator, as altitude increases, the maximum allowable A/S

21. During what aircraft maneuver is the static pressure inside the diaphragm of the vertical velocity indicator greater than on the outside

22. The primary difference between indicated A/S and true A/S is the

23. To locate a CMC autoflow chart in the system integration manual, you use the

24. What is the range of the indicated A/S tape on the Mach-A/S indicator

25. The data loader system is comprised of a

26. To represent increasing levels of urgency or threat, symbols generated by the traffic alert and collision avoidance system change

27. Each type of word used on the Military Standard 1553B data bus is

28. What provides the primary processing and interface functions for the flight management system

29. The tape capacity of the digital flight data recorder system is

30. Which digital flight data recorder system unit samples aircraft system data and converts it into digital form

31. Which is not an advantage of an active on-board collision system

32. Information describing the condition of a RT on a Military Standard 1553B data bus is transmitted as a

33. The total air temperature is calibrated in

34. With the stall prevention system control panel test switch in the TEST position, the shaker can be activated by manually moving the

35. A backup bus controller on the military standard 1553B data bus is

36. What type of pressure enters the A/S diaphragm of the A/S indicator

37. After the receiving RT on a Military Standard 1553B data bus has received and validated the data words from the transmitting RT during an RT-to-RT transfer, it

38. The HUD show declutter 1, declutter 2, and what three levels of symbol presentation

39. During which standard central air data computer built-in tests can recorded failures be retrieved

40. Which element of the Military standard 1553B data bus is not usually used in avionics bus systems

41. The video symbology display system displays a visual representation of navigation data, A/S, altitude

42. Each total air temperature probe contains

43. What displays on the Mach-A/S indicator respond to synchro outputs from the standard central air data computer?

44. Which is not a traffic alert and collision avoidance system (TCAS) traffic advisory function

45. When the DISPLAY switch on the CITS computer display panel is momentarily pressed to DIS RESET,

46. The mission computer provides display mode commands, flight director commands, and

47. The HUDs are focused to infinity and permit a wide field of view of

48. After the ADTD is first turned on, the heaters/ADTD may take up to

49. If a fault condition exists, the fault indicators on the front of the flight data acquisition unit are solid

50. The stall prevention computer produces a shaker signal if the aircraft angle-of-attack (AOA) and the permissible AOA are

51. In a military standard 1553B data bus command word, the field that refers to a function or area within the remote terminal to which command is being directed is the

52. The sensing elements in the true A/S indicator are surrounded by

53. Which Mach-A/S indicator displays are manually inserted

54. The aircraft parameter data file is recorded by the

55. If you have the barometric counter set to 29.92 during a self-test of the ALT-vertical speed indicator, the ALT display should slew to how many feet

56. Which ground proximity warning system mode is always active when the aircraft is between 50 and 2,450 feet, regardless of aircraft configuration

57. Which element of the military standard 1553B data bus gathers and formats information from aircraft sensors for transfer on the data bus

58. Which LRU is the CITS data bus controller

59. How many different test patterns are used when the CITS computer display panel's DIS TEST switch is used

60. In which mode is a CITS maintenance code displayed on the CITS computer display panel

61. The stall prevention computer produces a pusher signal if the aircraft angle-of-attack (AOA) equals the permissible AOA for

62. The system integration manual does not contain

63. The heart of the vertical velocity indicator is a

64. The absence of which intruder data specifically prohibits the traffic alert and collison avoidance system from issuing resolution advisories

65. The video symbology display system's symbol generator unit processes analog information, military standard 1553B bus data, and

66. When the failure annunciator on the front of the standard central air data computer is reset, it shows

67. The command Mach marker on the Mach-A/S indicator tracks the

68. What type of pressure is applied to the inside of the thermos chamber of the rate-of-climb indicator

69. Which standard central air data computer BIT allows slewing of altitude and A/S

70. Which is not a resolution advisory?

71. For how many aircraft maximum can the traffic alert and collision avoidance system track and generate displays

72. The superior type of data bus stub on a military standard 1553B data bus is the

73. Which conditions cause an uncorrected A/S indicator to read higher than it should?

74. The word count field in a controller-to-RT transfer message on the military standard 1553B data bus must correspond to the number of

75. During self-test of the Mach-A/S indicator, the Mach and indicated A/S tapes drive to

76. What is the purpose of the mode-S traffic alert and collision avoidance system (TCAS) function

77. Which type of data bus stub is most suitable for stubs less than one foot in length on the Military Standard 1553B data bus