Cockpit Reference Guide
Table Of Contents
- Flight Instruments
- Selecting the Altimeter Barometric Pressure Setting
- Selecting Standard Barometric Pressure
- Change Altimeter Barometric Pressure Setting Units
- Synchronizing the Altimeter Barometric Pressure Settings
- Synchronize CDI
- Change Navigation Sources
- Enable/Disable OBS Mode While Navigating with GPS
- Generic Timer
- Configure Vspeed Bugs Individually
- Turn Vspeed Bugs On or Off by Category
- Set Minimum Descent Altitude/Decision Height
- Displaying Wind Data
- Engine & Airframe Systems
- Nav/Com/Transponder/Audio Panel
- Automatic Flight Control System
- GPS Navigation
- Flight Planning
- Weight Planning
- Trip Planning
- Create a User Waypoint Defined by Latitude & Longitude
- Create a User Waypoint Defined by Radials from Other Waypoints
- Create a User Waypoint Defined by a Radial & Distance from Another Waypoint
- Delete a User Waypoint
- Create a Flight Plan
- Import a Flight Plan from an SD Card
- Insert a Waypoint in the Active Flight Plan
- Enter an Airway in a Flight Plan
- Creating a User-Defined Hold at an Active Flight Plan Waypoint
- Creating a User-Defined Hold at the Aircraft Present Position
- Removing a User-Defined Hold (Created at the Aircraft P.POS)
- Removing a User-Defined Hold (Created at an Active Waypoint)
- Invert An Active Flight Plan
- Remove a Departure, Arrival, Approach, or Airway from a Flight Plan
- Store a Flight Plan
- Edit a Stored Flight Plan
- Delete a Waypoint from the Flight Plan
- Invert and Activate a Stored Flight Plan
- Copy a Flight Plan
- Delete a Flight Plan
- Graphical Flight Plan Creation
- Export a Flight Plan to an SD Card
- Procedures
- Load and Activate a Departure Procedure
- Activate A Departure Leg
- Load An Arrival Procedure
- Activate An Arrival Leg
- Load and/or Activate an Approach Procedure
- Activate An Approach in the Active Flight Plan
- Activate a Vector to Final Approach Fix
- Activate A Missed Approach in the Active Flight Plan
- Temperature Compensated Altitude
- Hazard Avoidance
- Customizing the Hazard Displays on the Navigation Map
- SiriusXM Weather (Subscription Optional)
- Connext Weather (Optional)
- Traffic Information Service (TIS)
- Traffic Collision Avoidance System (TCAS II) (Optional)
- Terrain Awareness & Warning System
- Profile View Terrain and Obstacles (Optional)
- Airborne Color Weather Radar
- Additional Features
- Abnormal Operation
- Annunciations & Alerts
- CAS Messages
- Comparator Annunciations
- Reversionary Sensor Annunciations
- TAWS-A Alerts
- TAWS-B Alerts
- TCAS II Alerts and Annunciations
- CPDLC ATC Alert
- Other Prodigy® Aural Alerts
- Flight Plan Import/Export Messages
- Pilot Profile Import/Export Messages
- MFD & PFD Message Advisories
- Database Message Advisories
- GMA 1347D Message Advisories
- GIA 63W Message Advisories
- GSD 41 Message Advisories
- GEA 71 Message Advisories
- GTX 33 Message Advisories
- GRS 77 Message Advisories
- GMU 44 Message Advisories
- GSR 56 Message Advisories
- GDL 59 Message Advisories
- GDL 69A Message Advisories
- GDR 66 Message Advisories
- GWX 68 Alert Messages
- GCU 477 Message Advisories
- GMC 715 Message Advisories
- Miscellaneous Message Advisories
- Other System Annunciations
- Appendix
- Index
Cockpit Reference Guide for the Prodigy
®
Flight Deck 300
190-00761-04 Rev. A
130
Annunciations & Alerts
Flight
InstrumentsEAS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
AlertsAppendixIndex
COMPARATOR ANNUNCIATIONS
Note that operating the system in the vicinity of metal buildings or other metal
structures can cause sensor differences that may result in nuisance miscompare
annunciations during start up, shut down, or while taxiing.
Comparator
Window Text
Condition
ALT MISCOMP
Difference in altitude sensors is > 200 ft.
IAS MISCOMP
If both airspeed sensors detect < 35 knots, this is inhibited.
If either airspeed sensor detects > 35 knots, and the difference in sensors is > 15 kts.
If either airspeed sensor detects > 80 knots, and the difference in sensors is > 10 kts.
HDG MISCOMP
Difference in heading sensors is > 10 degrees.
PIT MISCOMP
Difference in pitch sensors is > 5 degrees.
ROL MISCOMP
Difference in roll sensors is > 6 degrees.
ALT NO COMP
No data from one or both altitude sensors.
IAS NO COMP
No data from one or both airspeed sensors.
HDG NO COMP
No data from one or both heading sensors.
PIT NO COMP
No data from one or both pitch sensors.
ROL NO COMP
No data from one or both roll sensors..
REVERSIONARY SENSOR ANNUNCIATIONS
Reversionary
Sensor Window
Text
Condition
BOTH ON ADC1
Both PFDs are displaying data from the number one Air Data Computer.
BOTH ON ADC2
Both PFDs are displaying data from the number two Air Data Computer.
BOTH ON ADCSTBY
Both PFDs are displaying data from the standby air data input.
BOTH ON AHRS1
Both PFDs are displaying data from the number one Attitude & Heading
Reference System.
BOTH ON AHRS2
Both PFDs are displaying data from the number two Attitude & Heading
Reference System.
BOTH ON ATTSTBY
Both PFDs are displaying data from the standby attitude and heading reference
input.
BOTH ON GPS1
Both PFDs are displaying data from the number one GPS receiver.