Avionics Fly Wire Technology 1 Online Exam Quiz
Avionics Fly Wire Technology 1 GK Quiz. Question and Answers related to Avionics Fly Wire Technology 1. MCQ (Multiple Choice Questions with answers about Avionics Fly Wire Technology 1
In a typical quadruplex actuator system, how is the failure of an actuator identified?
Options
A : By comparing it with the signal of the three good ones
B : By comparing it with a simulation model
C : Using in-lane fault detection
D : Using reflectometry
How is fly by wire system implemented in an aircraft?
Options
A : By using control rods and linkages connecting stick to control surfaces
B : By using high power radio transmitters and receivers
C : By using computers and actuators to control surfaces
D : Artificial intelligence
What type of cable is used in ARINC 629?
Options
A : Coaxial cable
B : Screened twisted pair
C : Unscreened twisted pair
D : Parallel lines
Which one of the following is not true with respect to the FBW system?
Options
A : FBW is not necessary for every aircraft
B : FBW makes an aircraft stealthy
C : FBW provides better control and carefree flying
D : FBW makes aircraft with low stability fly smoothly
Which of the following is not a component of the FBW system?
Options
A : Flight control computer
B : Aircraft motion sensor
C : Actuators
D : Communication receivers
Which one of the following is a military standard data bus?
Options
A : Mil Std 1553
B : ARINC 629
C : ARINC 429
D : COMAC C919
Why are actuators used in FBW systems?
Options
A : Movement of control surfaces
B : Reduce drag
C : Increase lift
D : Safety equipment
The reason for using quadruplex actuation system is _______
Options
A : precise movement
B : to counteract heavy air loads on the control surfaces
C : quick reaction to the control stick movement
D : as a fail safe mechanism
How are FBW signals transmitted?
Options
A : Simplex
B : Duplex
C : Time division multiplexing
D : Code division multiplexing
Why is the BFW system used?
Options
A : To control aerodynamically efficient but unstable body
B : For communications in aircraft
C : Better navigation
D : Reduced chances of enemy detection
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