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Brand | BOMBARDIER |
---|---|
Model | Primus 2000XP |
Category | Avionics Display |
Language | English |
AFCS functions controlled by the FGC, including flight director modes.
Diagram illustrating AFCS components and their interconnections.
How the autopilot system automatically controls aircraft attitude via servos.
Method for engaging the autopilot using the AP button on the guidance panel.
Limits on autopilot pitch and roll rate during operation.
Specific limits for roll and pitch angles during autopilot engagement.
Various methods for disengaging the autopilot system.
Provides stability augmentation and turn coordination via rudder actuators.
Overview of lateral and vertical flight director modes.
Used to engage and disengage the autopilot.
Descriptions of lateral modes like HDG, NAV, APR, BC, and BANK.
Descriptions of vertical modes like VS, ALT, FLC, and VNAV.
Descriptions of multi-axis modes such as APR and TOGA.
Automatic lateral mode selected when no other lateral mode is active.
Provides intercept, capture, and tracking of a selected VOR radial.
Automatic intercept, capture, and tracking of the front course localizer beam.
Enables fully coupled ILS approach via localizer and glideslope.
Provides pitch and lateral commands during takeoff.
Provides pitch and lateral commands for go-around.
Detects windshear and provides escape guidance.
Conditions that trigger the Automatic Emergency Descent Mode.
PFD indications and system settings during EDM.
How the EDM operates, transitions, and is canceled.
Indicates failure of one or both AFCS functions (yaw damper, autopilot, FD).
Overview of the circuit breaker system display.
Details on circuit breakers related to the AFCS.