Questions and Answers
What is the purpose of the autopilot disengage switch mounted on each control yoke?
What components are referred to as actuators in the context of the autopilot system?
Which types of motors are associated with servo actuators?
What does the flight mode annunciator indicate to the pilot?
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How does the flight director display contribute to autopilot function?
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What is NOT a type of servomotor mentioned in the autopilot system?
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What does the flight controller allow the pilot to do while the autopilot is engaged?
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Which mode allows pilots to control the aircraft while actively commanding both autopilots?
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What function is incorporated into the mode-select panel (MSP) in relation to the autopilot?
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What prevents the autopilot from engaging when using the turn knob on the flight controller?
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Which of the following navigation modes is NOT selectable through the MSP?
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What is the primary difference for aircraft fitted with Control Wheel Steering (CWS)?
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What is the primary function of trim tabs in an aircraft?
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How do pilots initiate movement of the control surfaces in an aircraft?
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What distinguishes power-assisted control systems from power-operated systems in an aircraft?
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What initiates the movement of the control surface in a power-assisted control system?
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What is the function of the control valve pistons in a power-assisted system?
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Which scenario is NOT described in the operations of control surfaces in powered flight?
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What type of actuator does NOT rely on direct pilot input in its operation?
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During a climb, what happens to the control lever when the pilot pulls back on the control stick?
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What is the primary function of the inner loop in an autopilot system?
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How does an outer loop in an autopilot system operate?
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What does a closed-loop system indicate about autopilot operation?
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What unusual behavior might occur if aerodynamic feedback is missing in an autopilot system?
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What is the role of the follow-up system in an autopilot?
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From what signal does the autopilot system initially derive its input during flight?
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What happens to the input signal when a control surface is moved?
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What system often operates using the inner loop principle alongside autopilots?
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What does it mean for control surfaces to ‘drift continuously’ during autopilot operation?
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Why are maintenance manual test procedures critical for autopilot systems?
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Study Notes
Autopilot System Overview
- Autopilot disengage switches are located on each control yoke for quick manual override.
- The flight director mode utilizes shared computing circuits with the autopilot, displaying navigational data on the attitude director indicator.
Flight Mode Annunciator
- Positioned near the attitude director indicator, it provides visual cues regarding the active modes for autopilot, flight director, and autothrottle functionalities.
Autopilot Actuators
- Components (actuators, servomotors) manipulate control surfaces via electrical signals converted into mechanical movement.
- Types of servomotors include electro-pneumatic, electro-mechanical, and electro-hydraulic.
- Flight control by the pilot is achieved through a physical connection of the control column to control surfaces, aided by trim tabs for ease of flight.
Powered Flight Controls
- Larger aircraft require powered control surfaces due to physical limitations. Assistance is provided through actuators.
- Two primary actuator types: power-assisted (providing help to pilots) and power-operated (where flight controls are moved solely by the actuator).
Autopilot Functionality
- The autopilot system operates on dual servo loops: an inner loop for attitude correction and an outer loop for external system feedback.
- Aerodynamic feedback is essential for maintaining stable autopilot operations, reflected by closed-loop systems.
Autopilot Engagement Sequence
- Gyro stabilization signals initiate control surface adjustments to correct aircraft drift during autopilot engagement.
- Control surfaces respond, allowing the aircraft to return to desired attitudes as the follow-up system provides continued feedback.
Mode Select Panel (MSP)
- The MSP controls autopilot systems, enabling mode selections such as altitude hold, VOR/ILS approaches, and more.
- Integration with Flight Management Systems (FMS) varies, though modern systems often incorporate both.
Flight Controller Features
- Pilots can alter aircraft attitudes manually with autopilot engaged via a flight controller featuring turn and pitch controls.
- Control Wheel Steering (CWS) is available on some aircraft, streamlining manual flight input without a separate controller.
Servomotor Types and Functionality
- Continuous DC motors allow rapid engagement/disengagement while reducing inertial effects on control surfaces.
- AC servomotors utilize variable AC signals to manage clutch assembly, enabling control over flight mechanisms as required.
Electro-Hydraulic Actuators
- These actuators combine hydraulic forces with electric control signals, enhancing the operation of flight control systems.
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Description
Explore the fundamentals of turbine aeroplane aerodynamics and the functionality of autopilot systems. This quiz covers crucial elements like the autopilot disengage switches, providing insights into flight control mechanisms. Perfect for students in aviation studies.