CNS/ATM Flashcards

0
Q

What is required to control the RINU-Gs from the NAV/COMM CDU?

A

The pilot or copilot CDU must be powered on.

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1
Q

How are the RINU-Gs controlled?

A

Through the CDU-7000

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2
Q

RINU-G will shut down when the aircraft battery falls below_______.

A

17.5 Vdc

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3
Q

What are the three primary functions of the RINU-G

A
  1. Determines attitude and horizontal velocities of the aircraft.
  2. Determines the ground speed and drift angle of the aircraft.
  3. Determines the ground speed and drift angle of the aircraft.
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4
Q

What information does the GEM V module compute?

A

Position
Velocity
Time
Formats

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5
Q

What are two functions of the

GEM V module?

A

Receiver Autonomous Integrity Monitoring(RAIM)

Fault Detection Exclusion(FDE)

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6
Q

The CDU will currently only display data for _____ satellites, even though the receiver may be using up to _______.

A

5, 12

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7
Q

What is Fault Detection Exclusion?

A

Ability of the receiver to detect and exclude a bad satellite from navigation solution.

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8
Q

How many satellites are required for FDE?

A

Requires receiver be tracking minimum of SIX satellites.

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9
Q

What is RAIM?

A

Receiver Autonomous Integrity Monitoring

Ability of receiver to determine if the integrity of NAV solution meets requirements for the phase of flight.

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10
Q

How many satellites are required for RAIM?

A

Requires receiver to be tracking 5 satellites.

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11
Q

What are the APX118/123 circuit breakers?

A

FLC lower

  • IFF Power
  • Zero IFF
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12
Q

What are the IFF modes with

APX-123?

A

1, 2, 3A, C, S, 4, 5, emergency

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13
Q

Mode 1

APX-123

A
  • military

- 4,096 codes

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14
Q

Mode 2

APX-123

A
  • military
  • platform ID/ sortie ID
  • 4,096 codes
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15
Q

Mode 3/A

APX-123

A
  • civilian
  • temporary platform ID code assigned by controlling agencies
  • used primarily for airspace management
  • 4,096 codes
16
Q

Mode C

APX-123

A
  • civilian
  • pressure altitude code
  • 1,280 codes in 100 ft. Increments
17
Q

Mode S

APX-123

A
  • Civilian
  • selective interrogation
  • permanent address for each A/C
  • level 2 elementary surveillance & enhanced surveillance
18
Q

Mode 4

APX-123

A
  • military
  • true IFF
  • crypto is valid for 24 hours
19
Q

Mode 5

APX-123

A
  • military
  • new crypto based ID with improved Information Assurance
  • mode 5 unique data
20
Q

What is mode 5 unique data?

A
  • national origin
  • mission code
  • 14 bit platform ID number
  • position
  • secure transmission of mode 1,2,3/A, C
21
Q

What are the two levels of mode 5?

A

Level 1: challenge and reply

Level 2: position reporting

22
Q

How is altitude data passed from the CDU-7000 to the transponder(APX-123)?

A

1553 data bus

23
Q

WRA GO one flash

A

Receiver/ Transmitter SRA A1

24
Q

WRA GO 2 flashes

A

Single board computer SRA 2

25
Q

WRA GO 3 flashes

A

Mode 4/5 Crypto SRA A3

26
Q

WRA GO four flashes

A

Signal processor SRA A4

27
Q

WRA GO five flashes

A

Power supply SRA PS1

28
Q

WRA GO six flashes

A

Inop crypto

Return to depot for further investigation

29
Q

How soon must the APX-123 battery be replaced after a low battery indication?

A

2 weeks

30
Q

What 3 fuses are the front of the APX-123 transponder?

A

115 Vac
115 Vac RTN
28 Vdc

31
Q

What happens if the J1 connector on the APX-123 is removed?

A

Transponder enters sleep mode. Keys in the mode 4/5 crypto SRA are zeroized and TOD is lost.

32
Q

What are the two levels of mode S operation?

APX-118

A
Elementary Surveillance (ELS)
Enhanced Surveillance (EHS)
33
Q

Elementary Surveillance information

APX-118

A

24-bit mode S address
Mode C altitude
Aircraft ID (call sign )

34
Q

Mode S EHS information

APX-118

A
ELS info
Mag. Heading
Indicated airspeed
Mach number
Vertical rate
Roll angle
Track angle
True track angle
Ground speed
Selected altitude
35
Q

Where is the mode S address stored?

A

CDU-7000 non volatile memory

36
Q

How is the source of altitude information for the transponder determined?

A

Determined by course selection on pilot EFDS display control panel.