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
6
SECTION 1 – INTRODUCTION
1.4 INITIAL OPERATIONS
The pilot may wish to change the active pilot profile
(see the System Setup Section of the MFD Pilot’s Guide
for details).
When the Power-Up Page list has been reviewed for
currency (to ensure that no databases have expired), the
pilot is prompted to continue. The current database in
-
formation (which is loaded in the system) is displayed
(valid operating dates, cycle number and database type
indicated).
Press the
ENT key (or the right most softkey) to
acknowledge the list information and proceed to the Navi
-
gation Map Page. When the system has acquired a suf-
ficient number of satellites to determine a position, the
aircraft symbol appears showing your present position.
1.5 BACKLIGHTING
The G1000 PFD and MFD displays use photocell tech-
nology to automatically adjust for ambient lighting con-
ditions. Photocell calibration curves are pre-configured
to optimize display appearance through a broad range of
cockpit lighting conditions. PFD, MFD, and GMA 1347
bezel/key lighting is normally controlled directly by the
existing instrument panel dimmer bus.
If desired, the PFD and MFD display backlights
may be adjusted manually. PFD, MFD, and GMA 1347
bezel/key brightness can also be adjusted manually as
well. GMA 1347 bezel/key brightness is directly tied to
the MFD bezel/key adjustment. Section 2 provides in-
structions on how to manually adjust the backlighting.
1.6 REVERSIONARY MODE
In normal operating mode, the PFD displays graphical
flight instrumentation in place of traditional gyro instru-
ments. Attitude, heading, airspeed, altitude, and vertical
speed are all shown on one display. The MFD shows a
full-color moving map with navigation information. Both
displays offer control over COM and NAV frequency selec-
tors, as well as heading, course/baro and altitude reference
functions. On the left of the MFD display, an Engine Indi-
cation System (EIS) cluster shows graphical depictions of
engine and airframe instrumentation. Figure 1-3 gives an
example of the G1000 system in normal mode.
Should a failure occur in either display, the G1000 au
-
tomatically enters reversionary mode. Figure 1-4 shows
an example where the PFD fails. In reversionary mode,
critical flight instrumentation is combined with engine in-
strumentation on the remaining display. Minimal naviga-
tion capability is also available on the reversionary mode
display.
Reversionary display mode can also be manually
activated by the pilot, if the system fails to detect a
display problem. The reversionary mode is activated
manually by pressing the large red button on the bottom
of the GMA 1347. Pressing the red reversionary mode
button again deactivates reversionary mode.
NOTE: The system alerts the pilot when backup
paths are utilized by LRUs. Refer to the Annun-
ciations & Alerts Pilot’s Guide for further informa-
tion regarding these and other system alerts.