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
35
SECTION 3 – AUDIO PANEL
Transceiver Keys
As illustrated below, the following eight (8) transceiv-
er keys appear at the top of the GMA 1347 front panel:
COM1 MIC, COM2 MIC, COM3 MIC, COM 1/2,
COM1, COM2, COM3, and TEL. COM audio can be
selected by either pressing the desired COM key or by
pressing the corresponding COM MIC key.
NOTE: A PTT switch must be pressed to allow
all microphone transmissions.
Figure 3-2 Transceivers
Pressing a COM MIC Key
Pressing COM1 MIC, COM2 MIC, or COM3 MIC
selects the corresponding radio as the active microphone
source (i.e., as the primary COM radio) and highlights
the corresponding COM frequency in green in the active
frequency field of the PFD and MFD.
Only one microphone source can be selected at a time.
Thus, if COM1 MIC is pressed when COM2 MIC is al
-
ready selected, COM2 MIC is automatically deactivated
and the COM2 MIC annunciator light is turned off. The
corresponding audio selection key (in this case, COM1)
becomes automatically selected if it is not already selected
at the time.
Pressing a COM Key
Pressing COM1, COM2, or COM3 selects the corre-
sponding radio as the active audio source. Each audio
source can be selected independently by pressing COM1,
COM2, or COM3. If selected in this manner, the au-
dio source remains selected independently of the active
microphone source selection. The active COM audio is
always heard through the headsets, and any combination
of audio sources can be selected simultaneously.
During COM signal reception, a white RX inscrip
-
tion appears next to the corresponding COM frequency
on both the PFD and the MFD for the duration of the
reception.
Keying a Microphone
When a microphone is keyed, the active transceiver
MIC key annunciator blinks approximately once per sec-
ond to indicate that the transmission is active, and a white
TX inscription appears next to the corresponding COM
frequency on both the PFD and the MFD for the duration
of the transmission.
When no further aircraft radio activity is detected by
the unit, the amount of ambient background noise from
the radios is further reduced by the MASQ
TM
(Master Avi-
onics Squelch) circuit (information on MASQ
TM
is present-
ed later in this manual).
NOTE: Audio level of the selected COM radio(s)
is controlled by the COM radio volume control
located on both the PFD and MFD (see G1000
VHF NAV/COM Pilot’s Guide for more informa-
tion).