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AIRCRAFT SYSTEM LEARNING

ATA 27 — Flight Controls

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

Flight Controls

Primary and secondary flight-control systems.

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PLAIN-LANGUAGE OVERVIEW

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.

SYSTEM PURPOSE

Why it exists

Allow controlled changes in aircraft attitude, lift and drag while maintaining stability and structural or flight-envelope protections where designed.

MAIN COMPONENTS

What belongs here

  • Ailerons and spoilers
  • Elevators or stabilators
  • Rudder
  • Flaps and slats
  • Control columns, pedals or sidesticks
  • Actuators and power-control units
  • Flight-control computers
  • Position sensors and feedback systems
INDICATIONS & CONTROLS

What users may see

Surface-position indications, configuration displays, trim position, control-law or mode status, disagree messages and computer or actuator faults may be presented.

MAINTENANCE CONCERNS

What technicians commonly evaluate

Rigging, free play, hydraulic or electrical power, sensor agreement, actuator leakage, control-surface condition, software/configuration and exact operational-test prerequisites require careful control.

AIRCRAFT APPLICABILITY

General ATA knowledge

General ATA knowledge is separated from aircraft-family and exact-variant information.

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CONNECTED KNOWLEDGE

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