What to do if uAvionix Avionics Display will not stabilize?
- RRobert SolisSep 12, 2025
Return to factory for service if uAvionix Avionics Display unit does not align within 3 minutes of power-on.
What to do if uAvionix Avionics Display will not stabilize?
Return to factory for service if uAvionix Avionics Display unit does not align within 3 minutes of power-on.
Brand | uAvionix |
---|---|
Model | AV-30-C |
Category | Avionics Display |
Language | English |
Describes the AV-30-C as a fully digital multi-mode instrument for legacy 3-1/8" panels, field configurable as AI or DG.
Lists primary, supplemental, audio/visual alerting, and miscellaneous functions of the AV-30-C.
Explains how to access the customization menu for Al mode using the MENU button and rotary knob.
Describes the process of editing overlay values in Al mode, accepting current values or using DONE to exit.
Introduces the components displayed in Al mode, including basic elements and customizable overlay fields.
Illustrates locations of inner graphical and outer textual customizable fields in Al mode, with three customizable pages.
Describes the basic attitude and slip display, consisting of a traditional attitude indicator and slip-ball.
Explains the airspeed indicator display, including units, v-Speed band, and color-coded numerals.
Details the flight direction indicator in Al mode, supporting non-slaved DG, magnetometer, or GPS track with heading bug.
Describes the Barometric Corrected Altitude (BCA) display on the right side, locking the barometric setting.
Explains the Derived Angle of Attack (AoA) indication, using stacked bars relative to configured limits.
Illustrates the non-slaved DG heading mode, showing six available textual fields for customization.
Describes displaying GPS navigation data in the traditional HSI format when connected to an external GPS navigator.
Explains AoA determination by comparing aircraft pitch to flight path angle, and how pitch/flight path are measured.
Details pilot-adjustable upper and lower AoA limits, their purpose, and the pilot-lockout feature.
Provides a procedure for setting the upper AoA limit to coincide with the aircraft's stall warning system.
Details the procedure for setting the lower AoA limit to correspond with normal cruise conditions (VA).