Autopilot Instrument Inputs and Failures

Hard4 min readInstrumentation
Moderately Examined
Why this matters

A pilot's understanding of autopilot instrument inputs and failures is vital for maintaining safe flight, especially when system malfunctions occur without clear warnings. Recognizing how failures propagate and when to intervene can prevent loss of control or unsafe aircraft states.

Autopilot instrument inputs and failures describe how autopilot systems rely on accurate data from various aircraft sensors and systems, and how failures or incorrect data can impact autopilot performance. Understanding these relationships is crucial for anticipating how the autopilot will behave during system malfunctions, especially during critical phases like approach and landing.

Quick Check

Which of the following are primary instrument inputs to the autopilot system?

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    Explanation

    Key Autopilot Instrument Inputs

    Autopilot systems depend on several primary inputs:

    • Attitude information from the Inertial Reference System (IRS) provides pitch, roll, and yaw data.
    • Airspeed, altitude, and pressure data from the Air Data Computer (ADC) are essential for speed and altitude hold functions.
    • Flight path and trajectory information, often from navigation systems or the Flight Management System (FMS), enables lateral and vertical guidance.
    • Control surface position feedback ensures the autopilot knows the actual position of ailerons, elevators, and rudder.
    • Aircraft configuration inputs (such as flap or gear position) are used for envelope protection and approach logic.
    • Pilot selections via the Mode Control Panel (MCP) or Flight Control Unit (FCU) set targets and modes.

    Typical Failures and Effects

    Failures can be sensor-based (e.g., IRS or ADC malfunction), system-based (e.g., electrical power loss), or related to the autopilot itself. Key points:

    • Incorrect sensor data (such as faulty attitude or airspeed) may cause the autopilot to command unsafe maneuvers, sometimes without immediate failure warnings.
    • Loss of critical inputs (like ILS signals during approach) may trigger autopilot disengagement or warnings, particularly below alert height.
    • Autopilot channel failures in multi-channel systems are managed by redundancy. In fail-operational (three-channel) systems, one failure allows continued operation; in fail-passive (two-channel), a single failure leads to autopilot disengagement.
    • Series actuator saturation can result in loss of control authority, requiring pilot intervention.

    Automatic Mode Reversion

    If the autopilot loses suitable data for a selected mode (e.g., navigation discontinuity, altitude change during capture, or excessive vertical speed selection), it may automatically revert to a safer mode or disengage to prevent unsafe flight.

    Pilot Action and System Protection

    Modern autopilots include interlocks and synchronization features to prevent engagement when conditions are unsafe or data is invalid. However, pilots must remain vigilant, as some failures may not trigger immediate warnings, making prompt recognition and manual intervention critical.

    The essentials

    Key Points

    Autopilot relies on accurate data from the IRS, ADC, and pilot inputs via the MCP/FCU.
    Sensor failures or incorrect data can cause autopilot disengagement or unsafe commands.
    Fail-operational systems allow continued autoland after a single failure; fail-passive systems disengage autopilot.
    Loss of ILS or radio altimeter signals during approach may trigger warnings or autopilot disconnect.
    Automatic mode reversion occurs if suitable data for the current mode is lost.
    Series actuator saturation can lead to loss of autopilot control authority.
    Prompt pilot intervention is essential when failures or unexpected autopilot behavior occur.
    Watch out

    Exam Traps & Typical Mistakes

    Confusing autopilot inputs (IRS, ADC, MCP) with outputs or unrelated systems (e.g., GPWS, TCAS).
    Assuming a fail-passive system can complete an autoland after a failure—manual landing is required.
    Believing the autopilot always gives a warning for incorrect sensor data—some failures may not trigger alerts.
    Misunderstanding the distinction between fail-operational and fail-passive system responses.
    Thinking the autopilot can compensate for all failures without pilot intervention.
    Test yourself

    Example Exam Questions

    Question 2Medium

    What is the typical autopilot system response if it receives conflicting data from two autopilot channels during a fail-passive autoland below alert height?

    Question 3Medium

    Which failure below alert height will trigger a warning and require pilot intervention during autoland?

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