Garmin Software Version 0858.07 User's Guide Page 60
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Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
190-00525-03 Rev. A
44
Hazard Avoidance
Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
AlertsAppendixIndex
System Self Test
1)
With the Traffic Map Page displayed, set the range to 2/6 nm.
2)
Select the STANDBY Softkey.
3)
Select the TEST Softkey.
4)
Self test takes approximately eight seconds to complete. When completed
successfully, traffic symbols are displayed and a voice alert is heard (see
Alerts and Annunciations section). If the self test fails, the system reverts to
Standby Mode and a voice alert is heard.
Displaying Traffic on the Navigation Map
1)
Ensure TAS is operating.
2)
With the Navigation Map displayed, select the MAP Softkey.
3)
Select the TRAFFIC Softkey. Traffic is now displayed on the map.
TERRAIN AWARENESS & WARNING SYSTEM (TAWS) DISPLAY
NOTE: Terrain data is not displayed when the aircraft latitude is greater than
75 degrees north or 60 degrees south.
Manual System Test
1)
While the TAWS-B Page is displayed, press the MENU Key.
2)
Turn the small FMS Knob to select ‘Test TAWS’.
3)
Press the ENT Key. During the test ‘TAWS TEST’ is displayed in the center
of the TAWS-B Page.
When all is in working order, “TAWS System Test, OK” is heard.
Display Terrain on the TAWS-B Page
1)
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the TAWS-B Page.
3)
If desired, press the VIEW Softkey to access the ARC and 360 softkeys.
When the ARC Softkey is pressed, a radar-like 120° view is displayed.
Press the 360 Softkey to return to the 360° default display.
4)
Rotate the Joystick clockwise to display a larger area or rotate counter-
clockwise to display a smaller area.
- Integrated Flight Deck 1
- Blank Page 10
- Record of Revisions 11
- Table of Contents 14
- FLIGHT INSTRUMENTS 17
- Flight Instruments 19
- DISPLAYING WIND DATA 19
- CHANGING HSI FORMAT 19
- ENGINE INDICATION SYSTEM 21
- Engine Indication System 22
- LEAN ENGINE DISPLAY 22
- ENGINE SYSTEM DISPLAY 24
- Nav/Com/XPDR/Audio Panel 25
- ADF TUNING (OPTIONAL) 25
- DME TUNING (OPTIONAL) 25
- ENTER A TRANSPONDER CODE 25
- ACTIVATE ADS-B TRANSMIT 25
- FLIGHT DIRECTOR ACTIVATION 29
- VERTICAL MODES 30
- LATERAL MODES 31
- GPS NAVIGATION 33
- GPS Navigation 34
- ACTIVATE A STORED FLIGHT PLAN 34
- ACTIVATE A FLIGHT PLAN LEG 34
- STOP NAVIGATING A FLIGHT PLAN 35
- VERTICAL NAVIGATION (VNAV) 35
- FLIGHT PLANNING 37
- Flight Planning 38
- WAYPOINTS 39
- ANOTHER WAYPOINT 41
- DELETE A USER WAYPOINT 42
- CREATE A NEW FLIGHT PLAN 43
- INVERT AN ACTIVE FLIGHT PLAN 46
- STORE A FLIGHT PLAN 47
- EDIT A STORED FLIGHT PLAN 47
- COPY A FLIGHT PLAN 48
- DELETE A FLIGHT PLAN 48
- PROCEDURES 51
- Procedures 52
- ACTIVATE AN ARRIVAL LEG 52
- HAZARD AVOIDANCE 55
- Hazard Avoidance 58
- Weather Products and Symbols 58
- TRAFFIC SYSTEMS 58
- Manual System Test 60
- Enable/Disable Aviation Data 61
- TAWS Inhibit 61
- ADDITIONAL FEATURES 63
- , ChartView, or FliteCharts 64
- , it may 64
- Additional Features 65
- ChartView (Optional) 65
- FliteCharts 65
- (Optional) 65
- Change Day/Night View 66
- AOPA AIRPORT DIRECTORY 66
- Entering a Channel Directly 68
- Assigning Channel Presets 68
- Adjusting Volume 68
- ABNORMAL OPERATION 69
- Abnormal Operation 70
- UNUSUAL ATTITUDES 70
- DEAD RECKONING 71
- ANNUNCIATIONS & ALERTS 73
- Annunciations & Alerts 74
- ADVISORY ANNUNCIATION 74
- ALERT MESSAGE 74
- AFCS ALERTS 74
- TAWS-B ALERTS 75
- VOICE ALERTS 78
- DATABASE MESSAGE ADVISORIES 80
- GMA 1347 MESSAGE ADVISORIES 82
- GIA 63W MESSAGE ADVISORIES 83
- GEA 71 MESSAGE ADVISORIES 85
- GTX 33 MESSAGE ADVISORIES 86
- GRS 77 MESSAGE ADVISORIES 86
- GMU 44 MESSAGE ADVISORIES 87
- GDL 69/69A MESSAGE ADVISORIES 87
- GDC 74A MESSAGE ADVISORIES 87
- GTS 820 MESSAGE ADVISORIES 88
- APPENDIX 95
- Appendix 100
- MFD SOFTKEY MAP 100
- DATABASE UPDATES 102
- Garmin Databases 103
- Jeppesen Databases 104
- Loading Updated Databases 104
- 190-00525-03 Rev. A 109
- 190-00525-03 Rev. A 110
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