Cockpit Reference Guide
Table Of Contents
- Copyright
- Record of Revisions
- Table of Contents
- List of Figures
- List of Tables
- WARRANTY
- Warnings and Cautions
- Section 1: Introduction
- Section 2: Primary Flight Display
- Section 3: Audio Panel
- Section 4: Multi Function Display
- 4.1 Introduction
- 4.2 MFD Softkeys
- 4.3 Engine Indication System Window
- ENGINE Page
- Manifold Pressure Gauge
- Tachometer
- Fuel Qty Indicator
- Fuel Flow Indicator (Normally Aspirated)
- Fuel Pressure Indicator (Turbocharged Only)
- Oil Pressure Indicator
- Oil Temperature Indicator
- EGT Indicator (Normally Aspirated)
- TIT Indicator (Turbocharged Only)
- CHT Indicator
- Voltmeter
- Ammeter
- Rudder Trim Indicator
- Elevator Trim Indicator
- Flaps Position Indicator
- 4.3 MFD Page Groups
- 4.4 Navigation Map Page
- Navigation Map Page Operations
- Changing the Map Orientation
- Clearing Lightning Data
- Selecting a Map Range
- Using the Auto Zoom Feature
- Identifying Aviation Map Data
- Decluttering the Map
- Map Panning
- Displaying Topographic Data on the Navigation Map Page
- Displaying Terrain Data on the Navigation Map Page
- Displaying Traffic on the Navigation Map Page
- Displaying Lightning Data on the Navigation Map Page
- Lightning Data Display Range
- MFD Navigation Status Window
- Navigation Map Page Menu
- Navigation Map Page Operations
- 4.5 Traffic Map Page
- 4.6 WEATHER MAP Page
- 4.7 Terrain Proximity Page
- 4.8 Direct-To Navigation
- 4.9 Flight Plans
- 4.10 Procedures
- Appendix A
- Index
- Figure 1-1 G1000 Controls
- Figure 1-2 G1000 Power-Up
- Figure 1-3 G1000 Normal Mode
- Figure 1-4 G1000 Reversionary Mode: Failed PFD
- Figure 2-1 Default PFD Information
- Figure 2-2 Additional PFD Information
- Figure 2-3 PFD Setup Menu
- Figure 2-4 PFD Softkeys (1 of 2)
- Figure 2-4 PFD Softkeys (2 of 2)
- Figure 2-5 Airspeed Indicator
- Figure 2-6 Red Pointer at Vne
- Figure 2-7 Attitude Indicator
- Figure 2-8 Attitude Indicator Nose High
- Figure 2-9 Attitude Indicator Nose Low
- Figure 2-10 Altimeter
- Figure 2-11 Colors Associated with the Altitude Alerter
- Figure 2-12 Altimeter within 1,000 ft. of Reference Altitude
- Figure 2-13 Altimeter within 200 ft. of Reference Altitude
- Figure 2-14 Altimeter (Metric)
- Figure 2-16 Marker Beacon and Vertical Deviation
- Figure 2-16 Vertical Speed Indicator
- Figure 2-17 ARC HSI
- Figure 2-18 Horizontal Situation Indicator
- Figure 2-20 Turn Rate Indicator and Trend Vector
- Figure 2-21 Selected Course Box
- Figure 2-22 HSI with Bearing Information
- Figure 2-24 BRG2 Information Window
- Figure 2-25 GPS INTEG, GPS SUSP, NAV1 and NAV2
- Figure 2-26 Communication Frequency Window
- Figure 2-27 Navigation Frequency Window
- Figure 2-28 Navigation Status Bars
- Figure 2-28 Navigation Status Bar Message
- Figure 2-29 Transponder Status Bar
- Figure 3-1 Front Panel Controls
- Figure 3-2 Transceivers
- Figure 3-3 Split COM, PA and Speaker
- Figure 3-4 Marker Beacon
- Figure 3-5 Marker Beacon Signal Indicator Lights on the PFD
- Figure 3-6 Aircraft Radios
- Figure 3-7 ICS Isolation
- Figure 3-8 Reversionary Mode
- Figure 4-2 MFD Softkeys
- Figure 4-3 ENGINE Page (Normally Aspirated)
- Figure 4-4 ENGINE Page (Turbocharged)
- Figure 4-5 Page Group Window
- Figure 4-6 Page Title Window
- Figure 4-6 Menu With Options
- Figure 4-7 Menu With No Options
- Figure 4-8 Navigation Map Page
- Figure 4-9 Navigation Map Range
- Figure 4-10 Navigation Map Panning
- Figure 4-11 TRAFFIC, TOPO and TERRAIN Softkeys
- Figure 4-12 Topography Scale
- Figure 4-13 MFD Navigation Status Window
- Figure 4-14 Navigation Map Page Menu Options
- Figure 4-15 Traffic Map Page
- Figure 4-16 Weather Map Page
- Figure 4-17 Terrain Scale
- Figure 4-18 Direct-to Page
- Figure 4-19 Flight Plan Waypoint Direct-to
- Figure 4-20 Nearest Airport Direct-to
- Figure 4-21 Manual Course Direct-to
- Figure 4-22 New Flight Plan
- Figure 4-23 Remove Waypoint Confirmation
- Figure 4-24 Removing an Approach
- Figure 4-25 Flight Plan Catalog Page
- Figure 4-26 Flight Plan Catalog Page Options
- Figure 4-27 Activate Stored Flight Plan Confirmation
- Figure 4-28 Delete Flight Plan Confirmation
- Figure 4-29 Procedures Page
- Figure 4-30 Selecting an Approach Procedure
- Figure 4-31 Selecting an Approach Transition
- Figure 4-32 Activating an Approach Procedure
- Figure 4-33 Approach with No Procedure Turn
- Figure 4-34 Flying the Missed Approach
- Figure 4-35 Flying the Procedure Turn
- Figure 4-36 Flying the DME Arc and Vectors to the DME Arc
- Figure 4-37 Flying a Holding Pattern
- Figure A-1 G1000 Alerting System
- Figure A-2 ADVISORY Softkey Annunciation
- Figure A-3 G1000 System Failure Annunciations
- Section 1: Introduction
- Section 2: Primary Flight Display
- Section 3: Audio Panel
- Section 4: Multi Function Display
- 4.1 Introduction
- 4.2 MFD Softkeys
- 4.3 Engine Indication System Window
- ENGINE Page
- Manifold Pressure Gauge
- Tachometer
- Fuel Qty Indicator
- Fuel Flow Indicator (Normally Aspirated)
- Fuel Pressure Indicator (Turbocharged Only)
- Oil Pressure Indicator
- Oil Temperature Indicator
- EGT Indicator (Normally Aspirated)
- TIT Indicator (Turbocharged Only)
- CHT Indicator
- Voltmeter
- Ammeter
- Rudder Trim Indicator
- Elevator Trim Indicator
- Flaps Position Indicator
- 4.3 MFD Page Groups
- 4.4 Navigation Map Page
- Navigation Map Page Operations
- Changing the Map Orientation
- Clearing Lightning Data
- Selecting a Map Range
- Using the Auto Zoom Feature
- Identifying Aviation Map Data
- Decluttering the Map
- Map Panning
- Displaying Topographic Data on the Navigation Map Page
- Displaying Terrain Data on the Navigation Map Page
- Displaying Traffic on the Navigation Map Page
- Displaying Lightning Data on the Navigation Map Page
- Lightning Data Display Range
- MFD Navigation Status Window
- Navigation Map Page Menu
- Navigation Map Page Operations
- 4.5 Traffic Map Page
- 4.6 WEATHER MAP Page
- 4.7 Terrain Proximity Page
- 4.8 Direct-To Navigation
- 4.9 Flight Plans
- 4.10 Procedures
- A.1 Introduction
- A.2 Alert Levels
- A.3 Mooney Specific Aircraft Alerts
- A.4 G1000 System Annunciations
- A.5 G1000 System Message Advisories
Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R
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WARNINGS & CAUTIONS
WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain function.
The G1000 Terrain Proximity feature is NOT intended to be used as a primary reference for terrain avoidance
and does not relieve the pilot from the responsibility of being aware of surroundings during flight. The Terrain
Proximity feature is only to be used as an aid for terrain avoidance and is not certified for use in applications
requiring a certified terrain awareness system. Terrain data is obtained from third party sources. Garmin is
not able to independently verify the accuracy of the terrain data.
WARNING: The displayed minimum safe altitudes (MSAs) are only advisory in nature and should not be relied
upon as the sole source of obstacle and terrain avoidance information. Always refer to current aeronautical
charts for appropriate minimum clearance altitudes.
WARNING: The Garmin G1000, as installed in Mooney M20M/R aircraft, has a very high degree of functional
integrity. However, the pilot must recognize that providing monitoring and/or self-test capability for all
conceivable system failures is not practical. Although unlikely, it may be possible for erroneous operation to
occur without a fault indication shown by the G1000. It is thus the responsibility of the pilot to detect such an
occurrence by means of cross-checking with all redundant or correlated information available in the cockpit.
WARNING: For safety reasons, G1000 operational procedures must be learned on the ground.
WARNING: The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and could
vary significantly from the altitude displayed by pressure altimeters, such as the GDC 74A Air Data Computer,
or other altimeters in aircraft. GPS altitude should never be used for vertical navigation. Always use pressure
altitude displayed by the G1000 PFD or other pressure altimeters in aircraft.
WARNING: The Jeppesen database used in the G1000 system must be updated regularly in order to ensure
that its information remains current. Updates are released every 28 days. A database information packet is
included in the G1000 package. Pilots using an outdated database do so entirely at their own risk.
WARNING: The basemap (land and water data) must not be used for navigation, but rather only for non-navi-
gational situational awareness. Any basemap indication should be compared with other navigation sources.
CAUTION: The United States government operates the Global Positioning System and is solely responsible
for its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy and
performance of all GPS equipment. Portions of the Garmin G1000 utilize GPS as a precision electronic NAVi
-
gation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the G1000 can be misused or
misinterpreted and, therefore, become unsafe.