3___UD5___ACGA_L19-20-24-25-23_2017.pdf

Beschreibung

t r e
David Nunez
Quiz von David Nunez, aktualisiert more than 1 year ago
David Nunez
Erstellt von David Nunez vor mehr als 6 Jahre
9
0

Zusammenfassung der Ressource

Frage 1

Frage
1.-The horizontal mode of AFCS mantain:
Antworten
  • Heading, VOR radial/ILS locator and LNAV route and roll angle
  • Heading, altitude and vertical speed
  • Vertical speed, IAS/Mach
  • Turbulence penetration, vertical speed and IAS/Mach

Frage 2

Frage
2.-How simplex AFCS system Works?
Antworten
  • Some components could be redundant, but a single failure renders the system inoperative
  • A single failure does not render the system inoperative
  • It has multiplex simplex systems to avoid failure
  • AFCS does not have simplex system, i aviation are always multiplex, triplex and quadruplex

Frage 3

Frage
3.- How yaw dumper Works?
Antworten
  • It is a system which moves the ailerons to avoid the dutch roll
  • It prevents the dutch roll by using the rudder
  • It prevents the tuck under by using the rudder
  • It only moves the ailerons to prevent the tuck under and it is only used in small aircraft

Frage 4

Frage
4.-The mach trim system:
Antworten
  • Is a system attached to the pitch cannel
  • It does not depend of the AFCS
  • Prevents the tuck under
  • All of above

Frage 5

Frage
6.-The rate trigger system of a AFCS:
Antworten
  • automatically disconnects the autopilot if the rate exceeds a set threshold
  • It is more used for stability tan for control
  • Compare the different outputs from sensors
  • None of above

Frage 6

Frage
7.-The combined pitch/roll system of AFCS:
Antworten
  • Holds altitude, vertical speed, IAS/Mach and Attitude
  • Heading, VOR radial/ILS locator and LNAV route
  • Control TOGA, Control Wheel steering, touch Wheel steering and turbulence penetration
  • None of above

Frage 7

Frage
8.-The speed of response in duplex system of AFCS:
Antworten
  • Can be improved by using comparator
  • Depends only on the singular response of any sensors
  • Both are correct
  • Both are false

Frage 8

Frage
1.How does a Primary radar work?
Antworten
  • It transmits a specific low energy signal (the interrogation) to a known target
  • High energy is directed via an antenna to illuminate a ‘target’
  • Using medium energy beams to detect the ‘target’
  • It works with infrared waves to send the signals

Frage 9

Frage
2. How does a Secondary Surveillance Radar work?
Antworten
  • It transmits a specific low energy signal (the interrogation) to a known target.
  • High energy is directed via an antenna to illuminate a ‘target’.
  • Using medium energy beams to detect the ‘target’.
  • It works with infrared waves to send the signals.

Frage 10

Frage
3. Which is a problem of Primary Radars?
Antworten
  • It only provides range measurement.
  • It only provides azimuth measurement
  • Small ratio reflected/emitted energy.
  • It can not detect objects in movement.

Frage 11

Frage
4. Interrogator and reply signals are concept of:
Antworten
  • Primary Radar.
  • Secondary Surveillance Radar
  • Both of them.
  • None of them.

Frage 12

Frage
5. Which is the main difference between the Mode A and the Mode C Transponder modes?
Antworten
  • A) Mode A only shows the 4 digit code whereas the Mode C shows also the altitude.
  • B) Mode A only shows the 4 digit code whereas the Mode C shows also the velocity.
  • C) A) and B) are true.
  • D) Mode A is like Mode S.

Frage 13

Frage
6. Which is the main difference of Mode S against Mode A and C.
Antworten
  • It is cheaper than the others.
  • It is completely automatic.
  • It allows a specific aircraft to be interrogated.
  • Is only for military use.

Frage 14

Frage
7. What is the concept of ADS-B?
Antworten
  • The aircraft gets it position from the GNSS constellation and then it broadcasts it to other aircrafts/ground stations.
  • It stands for Advisory Data Source-Binary and it controls the defective data and advises the air-crew.
  • It is a non-reactive radar used mainly in civil aviation.
  • None of them.

Frage 15

Frage
8. What is the meaning of Data Link?
Antworten
  • A) The action to link data with cables through the plane.
  • B) To create links between devices that share the same data.
  • C) D) and A).
  • D) Connection between locations to transmit and receive digital info.

Frage 16

Frage
1. What is the Flight Management System?
Antworten
  • Is an integrated automatic system.
  • Provides optimum economy of flight.
  • Reduces flight deck workload.
  • All the above are correct.

Frage 17

Frage
2. What is the EFIS?
Antworten
  • Is the FMS in electronic version.
  • Is the CADC in electronic version.
  • Is the ADI and HSI in electronic version.
  • Is the ADI, HSI and ASI in electronic version.

Frage 18

Frage
3. How many displays are typically in a FMS – Crew Interface?
Antworten
  • 1
  • 2
  • 3
  • 4

Frage 19

Frage
4. What are characteristics of the CDU?
Antworten
  • Small screen with numeric information
  • Big screen with alpha-numeric information.
  • Small screen with alpha-numeric information.
  • Big screen with numeric information.

Frage 20

Frage
5. Which of the following is not a FMS function?
Antworten
  • Air Data.
  • Fuel State.
  • Navigation Database.
  • Stall Speed.

Frage 21

Frage
6. In the aircraft performance model, what are the dimensions computed?
Antworten
  • X,y,z.
  • X, y, z, time.
  • X, x’, y, y’, z, z’.
  • X, y, z, speed.

Frage 22

Frage
7. What is LNAV?
Antworten
  • The ability to navigate laterally in two dimensions plus the ability to navigate in the vertical plane.
  • The ability to navigate laterally in two dimension.
  • The ability to navigate in three-dimensions plus the addition of time constraints for the satisfaction of time of arrival at a waypoint.
  • The capability of four-dimensional navigation together with the addition of an aircraft specific performance model.

Frage 23

Frage
8. What is VNAV?
Antworten
  • The ability to navigate laterally in two dimensions plus the ability to navigate in the vertical plane.
  • The ability to navigate laterally in two dimension.
  • The ability to navigate in three-dimensions plus the addition of time constraints for the satisfaction of time of arrival at a waypoint
  • The capability of four-dimensional navigation together with the addition of an aircraft specific performance model.
Zusammenfassung anzeigen Zusammenfassung ausblenden

ähnlicher Inhalt

PUERTAS GRIEGAS
Nicolas Flores Aguirre
nico floresd
Nicolas Flores Aguirre
NIUCO FLORES
Nicolas Flores Aguirre
Parámetros Eléctricos
Braulio Alejo
Van de Hiele
lizette García
Isomería en el carbono
laurisbuchheim
SOFTWARE
Ian Galindo Qand
NUTRICIÓN EN LAS PLANTAS
Carla Montañana Roig
SEGUNDO PARCIAL 2INFO
Hector Andres S
Desarrollo y subdesarrollo
laurisbuchheim