Cockpit Reference Guide
Table Of Contents
- Flight Instruments
- Selecting the Altimeter Barometric Pressure Setting
- Selecting Standard Barometric Pressure
- Change Altimeter Barometric Pressure Setting Units
- Change Navigation Sources
- Enable/Disable OBS Mode While Navigating with GPS
- Generic Timer
- Configure Vspeed Bugs
- Set Barometric Minimum Descent Altitude
- Displaying Wind Data
- Changing HSI Format
- Engine Indication System
- Nav/Com/Transponder/Audio Panel
- GFC 700 Automatic Flight Control System (Optional)
- GPS Navigation
- Flight Planning
- Trip Planning
- Create a New User Waypoint
- Delete a User Waypoint
- Create a New Flight Plan
- Insert a Waypoint in the Active Flight Plan
- Enter an Airway in a Flight Plan
- 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
- Procedures
- Hazard Avoidance
- Additional Features
- Abnormal Operation
- Annunciations & Alerts
- WARNING Annunciation
- CAUTION Annunciation
- Annunciation Advisory Alerts
- Alert Message
- AFCS Alerts
- Terrain-SVS Alerts
- Voice Alerts
- MFD & PFD Message Advisories
- Database Message Advisories
- GMA 1347 Message Advisories
- GIA 63 Message Advisories
- GIA 63W Message Advisories
- GEA 71 Message Advisories
- GTX 33 Message Advisories
- GRS 77 Message Advisories
- GMU 44 Message Advisories
- GDC 74A Message Advisories
- GDL 69A Message Advisories
- Miscellaneous Message Advisories
- Appendix
- Index
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
51
Abnormal Operation
Flight
Instruments EIS
Nav/Com/
XPDR/Audio AFCS GPS Nav
Flight
Planning Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts Appendix Index
ABNORMAL OPERATION
REVERSIONARY MODE
Should a system detected failure occur in either display, the G1000 automatically
enters reversionary mode. In reversionary mode, critical flight instrumentation is
combined with engine instrumentation on the remaining display.
Reversionary display mode can be manually activated by pressing the DISPLAY
BACKUP Button on the audio panel.
NOTE: The Diamond DA42-L360 Pilot’s Operating Handbook (POH) always
takes precedence over the information found in this section.
ABNORMAL COM OPERATION
When a COM tuning failure is detected by the system, the emergency frequency
(121.500 MHz) is automatically loaded into the active frequency field of the COM
radio for which the tuning failure was detected.
HAZARD DISPLAYS WITH LOSS OF GPS POSITION
If GPS position is lost, or becomes invalid, selected hazards being displayed on the
Navigation Map Page are removed until GPS position is again established.
Loss of Hazard Functions with Loss of GPS
Position