CNS/ATM Flashcards
What is required to control the RINU-Gs from the NAV/COMM CDU?
The pilot or copilot CDU must be powered on.
How are the RINU-Gs controlled?
Through the CDU-7000
RINU-G will shut down when the aircraft battery falls below_______.
17.5 Vdc
What are the three primary functions of the RINU-G
- Determines attitude and horizontal velocities of the aircraft.
- Determines the ground speed and drift angle of the aircraft.
- Determines the ground speed and drift angle of the aircraft.
What information does the GEM V module compute?
Position
Velocity
Time
Formats
What are two functions of the
GEM V module?
Receiver Autonomous Integrity Monitoring(RAIM)
Fault Detection Exclusion(FDE)
The CDU will currently only display data for _____ satellites, even though the receiver may be using up to _______.
5, 12
What is Fault Detection Exclusion?
Ability of the receiver to detect and exclude a bad satellite from navigation solution.
How many satellites are required for FDE?
Requires receiver be tracking minimum of SIX satellites.
What is RAIM?
Receiver Autonomous Integrity Monitoring
Ability of receiver to determine if the integrity of NAV solution meets requirements for the phase of flight.
How many satellites are required for RAIM?
Requires receiver to be tracking 5 satellites.
What are the APX118/123 circuit breakers?
FLC lower
- IFF Power
- Zero IFF
What are the IFF modes with
APX-123?
1, 2, 3A, C, S, 4, 5, emergency
Mode 1
APX-123
- military
- 4,096 codes
Mode 2
APX-123
- military
- platform ID/ sortie ID
- 4,096 codes