|
|
 |
Boeing MD-10 |
|
 The Automatic Flight System (AFS) is an integral part of the automatic and manual control system of the aircraft. Manual override of the automatic flight controls and autothrottle is always available.
The AFS consists of two Flight Control Computers (FCCs) with integrated autopilots (AP), Flight Directors (FD), autothrottle (AT) and engine trim controls. The AFS features fail-operational Category IIIb autoland through ground roll out and integrated windshear detection/warning with AP FD and ATS guidance escape capability.
The AFS incorporates speed and flight path protective features that automatically override the selected speed and/or flight path commands to prevent overspeed or underspeed.
Advanced Features:
 | | Independent Flight Systems | | | Speed Envelope Limiting | | | Automatic Pitch Trim | | | Yaw Damping/Turn Coordination | | | Elevator Load Feel Control | | | Flap Limiting | | | Automatic Ground Spoiler Control | | | Altitude Alert Warning (visual and aural) | | | Stall Warning with Stick Shaker and AutoSlat Extension | | | Data for EIS Flight Mode Annunciation |
|
|
|
|
|
|
|
|
|
|
|
|
Get quick access to one of
your accounts
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
| Did the content on this page meet your needs? |
|
|
|
|
|
|
|
