What this system is
ATA 27 covers primary and secondary flight-control systems. Depending on the aircraft, control may be mechanical, hydraulic, electrically signalled, powered or a combination.
ATA 27 covers primary and secondary flight-control systems. Depending on the aircraft, control may be mechanical, hydraulic, electrically signalled, powered or a combination.
Primary and secondary flight-control systems.
ATA 27 covers primary and secondary flight-control systems. Depending on the aircraft, control may be mechanical, hydraulic, electrically signalled, powered or a combination.
Allow controlled changes in aircraft attitude, lift and drag while maintaining stability and structural or flight-envelope protections where designed.
Surface-position indications, configuration displays, trim position, control-law or mode status, disagree messages and computer or actuator faults may be presented.
Rigging, free play, hydraulic or electrical power, sensor agreement, actuator leakage, control-surface condition, software/configuration and exact operational-test prerequisites require careful control.
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A flight-control architecture in which pilot commands are transmitted and processed electrically rather than solely through direct mechanical linkage.
BEGINNERAngle of attackThe angle between the local airflow and a defined reference line on the aircraft or wing.
INTERMEDIATEStall warning systemA system that warns when the aircraft approaches an aerodynamic stall condition.
ADVANCEDFlight control computerA computer that processes commands and sensor inputs to control or monitor aircraft flight-control functions.
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