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
36
SECTION 3 – AUDIO PANEL
COM Swap
The GMA 1347 allows for the use of a remotely mount-
ed switch to alternately transfer the active microphone
between COM1 MIC and COM2 MIC. The COM swap
switch is typically mounted on the yoke or control stick.
If COM1 MIC is the active microphone (i.e., both COM1
MIC and COM1 keys are annunciated), pressing the COM
swap switch transfers the active microphone from COM1
MIC to COM2 MIC (i.e., both COM1 MIC and COM1
keys become deselected, and COM2 MIC and COM2
keys become annunciated). Pressing the switch has no ef
-
fect if COM3 is the active transceiver or if COM 1/2 (split
COM) is activated.
Please consult a Garmin-authorized service center for
details on the remote COM swap option.
Split COM
Pressing the COM 1/2 key toggles the state of the split
COM function. During split COM operation, the COM1,
COM1 MIC, COM2 and COM2 MIC keys are annunci-
ated and thus active.
When the COM 1/2 key is selected, COM1 becomes
dedicated solely to the pilot for MIC/audio, while
COM2
becomes dedicated to the copilot for MIC/audio. The
COM1 MIC annunciator blinks when the pilot’s micro-
phone is keyed. The COM2 MIC annunciator blinks
when the copilot’s microphone is keyed.
In this mode, both the pilot and the copilot can
simultaneously transmit over separate radios. Note that,
while the pilot can still monitor
COM3, NAV1, NAV2,
DME, ADF, AUX and MKR audio as selected, the copilot is
only able to monitor/hear COM2.
Split COM mode is cancelled by pressing the COM 1/2
key.
NOTE: Split COM performance varies significantly
across installations and is affected by both the
distance between the antennas and the separa-
tion of the tuned frequencies. In small aircraft
particularly, receiver sensitivity is typically
reduced and squelch breaks are affected. Each
installation should be individually examined to
determine the expected performance of split
COM.
PA Function
The passenger address function is provided via the PA
key. Push-to-talk (PTT) must be used to deliver PA an-
nouncements.
NOTE: PA volume is adjustable in Configuration
mode.