Which of the following is the fundamental control of a common autopilot mode?

Engine control

Altitude control

Automated landing

Pitch, roll and yaw control

Correct Answer : Pitch, roll and yaw control

Explanation : The pitch attitude control loop and the heading control loop, with its inner loop commanding the aircraft bank angle, are thus fundamental inner loops in a common autopilot control mode. They are short, fast period loops which continuously control the control surfaces of an aircraft to maintain the pilot command.

Recently Updated in Avionics Questions

What is the interval for updating data in the navigation database?

1 hour

24 hours

28 days

1 month

Correct Answer : Option (C) : 28 days

Explanation : The navigation database is updated every 28 days, according to the ICAO AiRAC cycle, and is held in non-volatile memory. It is clearly essential to maintain the recency and quality of the database and the operator is responsible for the detail contents of the database which is to ARINC 424 format.

Which one of the following is not a factor for calculating speed breaches by the FMS?

CG position

Aircraft weight

Position of the aircraft

Wind and temperature models

Correct Answer : Option (C) : Position of the aircraft

Explanation : The FMS continually monitors the aircraft envelope and ensures that the speed envelope restrictions are not breached. It also computes the optimum speeds for the various phases of the flight profile. This is carried out taking into account factors such as: Aircraft weight – computed from a knowledge of the take-off weight and the fuel consumed (measured by the engine flow meters), CG position – computed from known aircraft loading and fuel consumed, Flight level and flight plan constraints, Wind and temperature models, Company route cost index.

Which one of the following is not a navigation mode used by FMS for computing position of the aircraft?

Inertial (IRS) � GPS

Inertial (IRS) � VOR/DME

Inertial (IRS) � DME/DME

GPS only

Correct Answer : Option (D) : GPS only

Explanation : Each FMS computes the aircraft position and the position accuracy. The FMS computed position is an optimum combination of the inertial position and the GPS or radio position, depending on which equipment provides the most accurate data. This results in four navigation modes: Inertial (IRS) – GPS, Inertial (IRS) – DME/DME, Inertial (IRS) – VOR/DME, Inertial (IRS) only. The only GPS is not used as the position information is within a radius where the aircraft is flying.