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Boeing MD- 90 |
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 The MD-90 advanced avionics and integrated cockpit comprise several familiar systems integrated into a flight management concept that provides automatic thrust and guidance control for the full flight regime, including a fail passive Category IIIA autoland system.
The MD-90 concept utilizes two identical, autonomous Digital Flight Guidance Computers (DFGCs). One computer at a time is selected for control of the airplane. A glareshield-mounted Flight Guidance Control Panel (FGCP) allows the flight crew to enter flight mode control inputs to the autopilot, flight director, autothrottle and altitude advisory functions of the selected DFGC.
Advanced Features:
 | | Autopilot | | | Yaw Damper | | | Flight Director | | | Mach Trim Compensation | | | Windshear Coupling | | | Altitude Preselect/Alerting | | | Thrust Mode Selection | | | Autothrottle/Speed Control (AT/SC) | | | ERP and N1 Synchronization | | | Semi-Automatic, manual, and (optional) Automatic Thrust Cutback | | | Flight Mode Annunciation | | | Flight Management System (FMS) Coupling | | | Automatic Pitch Trim | | | CATIIIA Autoland |
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