Copy and Edit

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

Description

t r e
David Nunez
Quiz by David Nunez, updated more than 1 year ago
David Nunez
Created by David Nunez almost 6 years ago
2
0
0

Resource summary

Question 1

Question
1.-The horizontal mode of AFCS mantain:
Answer
  • 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

Question 2

Question
2.-How simplex AFCS system Works?
Answer
  • 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

Question 3

Question
3.- How yaw dumper Works?
Answer
  • 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

Question 4

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

Question 5

Question
6.-The rate trigger system of a AFCS:
Answer
  • 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

Question 6

Question
7.-The combined pitch/roll system of AFCS:
Answer
  • 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

Question 7

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

Question 8

Question
1.How does a Primary radar work?
Answer
  • 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

Question 9

Question
2. How does a Secondary Surveillance Radar work?
Answer
  • 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.

Question 10

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

Question 11

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

Question 12

Question
5. Which is the main difference between the Mode A and the Mode C Transponder modes?
Answer
  • 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.

Question 13

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

Question 14

Question
7. What is the concept of ADS-B?
Answer
  • 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.

Question 15

Question
8. What is the meaning of Data Link?
Answer
  • 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.

Question 16

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

Question 17

Question
2. What is the EFIS?
Answer
  • 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.

Question 18

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

Question 19

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

Question 20

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

Question 21

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

Question 22

Question
7. What is LNAV?
Answer
  • 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.

Question 23

Question
8. What is VNAV?
Answer
  • 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.
Show full summary Hide full summary

Want to create your own Quizzes for free with GoConqr? Learn more.

Similar

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
Wimax
Ruben Hernandez2739
SEGUNDO PARCIAL 2INFO
Hector Andres S
Desarrollo y subdesarrollo
laurisbuchheim
Browse Library