G1000 TM cockpit reference guide for Mooney M20M & M20R
Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R
COPYRIGHT Copyright © 2004 Garmin Ltd. or its subsidiaries. All rights reserved. This Cockpit Reference Guide reflects the operation of System Software version 0424.01 for Mooney M20M and M20R aircraft. Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions. Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A. Tel: 913/397.8200 Fax: 913/397.8282 Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.
RECORD OF REVISIONS Revision Date of Revision Affected Pages A 10/19/04 i - xii, 1 - 114 B ii 11/02/24 i - xii, 1 - 114 Description Production Release Update SW number.
TABLE OF CONTENTS Copyright i Record of Revisions ii Table of Contents iii List of Figures vi List of Tables viii WARRANTY ix Warnings and Cautions x Section 1: Introduction 1 1.1 G1000 Controls .......................................................... 2 1.2 Secure Digital Cards ................................................. 4 1.3 System Power-up ...................................................... 4 PFD Power Up 5 MFD Power Up 5 1.4 Initial Operations ..................................
TABLE OF CONTENTS 3.4 Radio Inputs ............................................................. 40 3.5 Intercom System (ICS) Isolation .......................... 41 PILOT Mode 41 COPILOT Mode 41 CREW Mode 41 ALL Mode 41 3.6 Volume/Squelch Control ........................................ 42 Intercom VOL/SQ State 43 Intercom Volume Control 43 Intercom Squelch Threshold Control 43 3.7 Display Backup Mode............................................. 44 Section 4: Multi Function Display 45 4.1 Introduction ..
TABLE OF CONTENTS 4.9 Flight Plans ...............................................................
LIST OF FIGURES LIST OF FIGURES Figure 1-1 G1000 Controls........................................................ 2 Figure 1-2 G1000 Power-Up ..................................................... 5 Figure 1-3 G1000 Normal Mode............................................... 7 Figure 1-4 G1000 Reversionary Mode: Failed PFD .................. 7 Figure 2-1 Default PFD Information ........................................ 10 Figure 2-2 Additional PFD Information ...................................
LIST OF FIGURES Figure 4-34 Flying the Missed Approach ................................ 89 Figure 4-35 Flying the Procedure Turn .................................... 91 Figure 4-36 Flying the DME Arc and Vectors to the DME Arc 93 Figure 4-37 Flying a Holding Pattern ...................................... 95 Figure A-1 G1000 Alerting System .......................................... 97 Figure A-2 ADVISORY Softkey Annunciation ........................... 98 Figure A-3 G1000 System Failure Annunciations ......
LIST OF TABLES LIST OF TABLES Table 3-1 Marker Beacon Signal Characteristics ...................41 Table 3-2 ICS Isolation Mode Transitions ..............................43 Table 3-3 ICS Operation Modes............................................
WARRANTY LIMITED WARRANTY This Garmin product is warranted to be free from defects in materials or workmanship for two years from the date of purchase. Within this period, Garmin will, at its sole option, repair or replace any components that fail in normal use. Such repairs or replacement will be made at no charge to the customer for parts and labor, provided that the customer shall be responsible for any transportation cost.
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.
WARNINGS & CAUTIONS CAUTION: To reduce the risk of unsafe operation, carefully review and understand all aspects of the G1000 Pilot’s Guide documentation and the G1000 Flight Manual Supplement. Thoroughly practice basic operation prior to actual use. During flight operations, carefully compare indications from the G1000 to all available navigation sources, including the information from other NAVAIDs, visual sightings, charts, etc.
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SECTION 1 – INTRODUCTION SECTION 1: INTRODUCTION Garmin® International Inc., a unit of Garmin Ltd. introduces the G1000 Integrated Cockpit System for the Mooney M20M and M20R aircraft.
SECTION 1 – INTRODUCTION 1.
SECTION 1 – INTRODUCTION The G1000 controls and keys have been designed to simplify operations and minimize workload and time to access sophisticated functionality. The following provides an overview of the primary function(s) for each key and control. • (1) NAV VOL / ID Control – Controls the NAV audio level. Press to toggle the ident filter ON and OFF. Volume increase and decrease is shown in the field as a percentage.
SECTION 1 – INTRODUCTION • • • • 4 Press the FMS/CSRS to activate the cursor and turn the large FMS knob to scroll through the list. (14) MENU Key – Displays a context-sensitive list of options. This options list allows the user to access additional features or make settings changes that relate to certain pages. (15) PROC Key – Selects approaches, departures and arrivals from the flight plan.
SECTION 1 – INTRODUCTION PFD Power Up MFD Power Up As the G1000 system begins to initialize, test annunciations are displayed to the pilot on the PFD, as shown in Figure 1-2. All system annunciations should clear within one minute of power up. The PFD also displays the ‘AHRS ALIGN: Keep Wings Level’ message. The AHRS should display valid attitude and heading fields within 1 minute of power up. The AHRS can align itself while the aircraft taxis or during level flight.
SECTION 1 – INTRODUCTION 1.4 INITIAL OPERATIONS 1.6 REVERSIONARY MODE The pilot may wish to change the active pilot profile (see the System Setup Section of the MFD Pilot’s Guide for details). In normal operating mode, the PFD displays graphical flight instrumentation in place of traditional gyro instruments. Attitude, heading, airspeed, altitude, and vertical speed are all shown on one display. The MFD shows a full-color moving map with navigation information.
SECTION 1 – INTRODUCTION Figure 1-3 G1000 Normal Mode Figure 1-4 G1000 Reversionary Mode: Failed PFD Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R 7
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SECTION 2 – PFD SECTION 2: PRIMARY FLIGHT DISPLAY This Cockpit Reference Guide describes the basic features of the Primary Flight Display (PFD) on the G1000 Integrated Cockpit System installed on Mooney aircraft. The system consists of two 10.4 inch color flat panel displays. During normal operation, the left display is configured as a Primary Flight Display. See the PFD Pilot’s Guide for PFD descriptions and operating procedures not covered in this Cockpit Reference Guide.
SECTION 2 – PFD 1 17 16 15 14 13 2 12 11 3 10 4 9 8 5 7 6 Figure 2-1 Default PFD Information 10 1 NAV Frequency Window 9 Turn Rate Indicator 2 Airspeed Indicator 10 Barometric Setting Box 3 True Airspeed Box 11 Vertical Speed Indicator 4 Heading Box 12 Altimeter 5 Horizontal Situation Indicator 13 Altitude Reference Box 6 Outside Air Temperature Box 14 COM Frequency Window 7 System Time Box 15 Navigation Status Bar 8 Transponder Status Bar 16 Slip/Skid Indica
SECTION 2 – PFD 10 1 9 8 2 7 3 6 5 4 Figure 2-2 Additional PFD Information 1 Traffic Annunciation 6 Alerts Window 2 Selected Heading Box 7 Selected Course Box 3 Inset Map 8 Annunciation Window 4 BRG1 Information Window 9 Vertical Deviation/Glideslope Indicator 5 BRG2 Information Window 10 Marker Beacon Annunciation Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R 11
SECTION 2 – PFD 2.1 BACKLIGHTING The backlighting of the display and the keys can be adjusted for the PFD and MFD. The backlighting intensity ranges from 0.14% to 100.00%. Two modes exist for adjustment: • Auto - The G1000 adjusts the backlighting automatically with reference to the amount of light in the cockpit (default setting). • Manual - Allows the pilot to manually adjust the backlighting. NOTE: Except in reversionary mode, the backlighting can only be adjusted from the PFD.
SECTION 2 – PFD 2.2 SOFTKEY FUNCTION When a softkey is turned on, its color changes to black text on gray background and remains this way until it is turned off, at that time it changes to white text on black background. The CDI, IDENT, TMR/REF, NRST and ALERTS softkeys change momentarily to black text on gray background and automatically switches back to white text on black background.
SECTION 2 – PFD INSET DCLTR OFF DCLTR-1 TRAFFIC TERRAIN TOPO BACK ALERTS Press The BACK or OFF Softkey To Return To The Top Level Softkeys DCLTR-2 DCLTR-3 PFD Press the BACK softkey to return to the top level softkeys METRIC DFLTS 360 HSI ARC HSI STD BARO BACK Press the DFLTS softkey to change the PFD metric values to standard Figure 2-4 PFD Softkeys (1 of 2) 14 Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R ALERTS
SECTION 2 – PFD CDI XPDR OBS TMR/REF IDENT NRST ALERTS CDI (NAV1) Press the BACK softkey to return to the top level softkeys CDI (NAV2) ALT ON STBY VFR CODE IDENT BACK ALERTS Press the BACK softkey to return to the top level softkeys 0 1 2 3 4 5 6 7 IDENT BKSP BACK ALERTS Figure 2-4 PFD Softkeys (2 of 2) Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R 15
SECTION 2 – PFD CDI – Press to change navigation mode on the CDI between GPS NAV1 and NAV2. OBS – Press to select OBS mode on the CDI when navigating by GPS. XPDR – Press to display the transponder mode selection softkeys. STBY – Press to select standby mode. ON – Press to select mode A. ALT – Press to select altitude mode. VFR – Press to automatically squawk 1200 (only in the U.S.A.). CODE – Press to display transponder code selection softkeys 0-7. 0 through 7 – Press numbers to enter code.
SECTION 2 – PFD 2.3 FLIGHT INSTRUMENTS Airspeed Indicator The Airspeed indicator displays airspeed on a rolling number gauge using a moving tape. The following information is also displayed: • • • • Speed Ranges A color coded (white, green, yellow, and red) speed range strip is located on the moving tape. The colors denote flaps operating range, normal operating range, caution range, and never exceed speed (Vne). A red range is also present for low speed awareness.
SECTION 2 – PFD Attitude Indicator Pitch Indication The attitude information displays over a virtual blue sky and brown ground with a white horizon line. The aircraft wing tips are represented by two yellow bars on the horizon line. The yellow inverted “V” represents the aircraft.
SECTION 2 – PFD Roll Indication Major tick marks at 30 and 60 degrees and minor tick marks at 10, 20 and 45 degrees are shown to the left and right on the roll scale. The inverted white triangle indicates 0 on the roll scale. Angle of bank is indicated by the position of the roll pointer on the roll scale. NOTE: Supplemental flight data such as the Inset Map, Alerts and Annunciation Window disappear from the PFD when pitch is more than +30˚ and less than -20˚ or when a 65˚ bank angle is reached.
SECTION 2 – PFD Altimeter Altitude Reference Bug The Altimeter displays barometric altitude values in feet on a rolling number gauge using a moving tape. The Altimeter displays the following information: • • • • • • • The Altitude Reference Bug is displayed at the reference altitude or the edge of the tape (whichever is closer to the current altitude) to provide increased altitude awareness.
SECTION 2 – PFD Altitude Alerting Altitude alerting provides the pilot with a visual and aural alert when approaching the reference altitude. Although flight control systems use the same reference altitude box the altitude alerter does, the altitude alerter is not coupled to a flight control system and can function without one. The visual annunciations appear in the altitude reference box. Anytime the reference altitude is changed, the altitude alerter is reset. There is an altitude band set at +/- 1,000 ft.
SECTION 2 – PFD Metric Display Reference and current altitude can be displayed in meters. The barometric pressure may also be displayed in hectopascals. To display altitude in meters and barometric pressure in hectopascals: 1. 2. Press the PFD softkey to display the second level softkeys. Press the METRIC softkey to display altitude in meters and barometric pressure in hectopascals. Press the BACK softkey to return to the top level softkeys.
SECTION 2 – PFD Vertical Speed Indicator The Vertical Speed Indicator displays the aircraft vertical speed with numeric labels and tick marks at 1,000 ft. and 2,000 ft. in each direction on the non-moving tape. Minor tick marks are at intervals of 500 ft. Vertical Speed Pointer The Vertical Speed Pointer displays the current vertical speed and points to that speed on the non-moving tape.
SECTION 2 – PFD Horizontal Situation Indicator The Horizontal Situation Indicator (HSI) displays a rotating compass card with letters at the cardinal points and numeric labels every 30 degrees. Major tick marks are at 10 degree intervals and minor tick marks for every 5 degrees. The HSI is displayed in a heading up orientation. The HSI compass can be displayed as a 360° rose or 140° arc by pressing the PFD softkey, followed by the 360 HSI or the ARC HSI softkey.
SECTION 2 – PFD Heading Indication Course Deviation Indicator A digital reading of the current magnetic heading appears on top of the HSI. A rotatable heading bug on the compass rose and arc marks the desired heading. When the pilot selects a heading, a digital reading will appear for 3 seconds in a box left of the lubber line, next to the HSI.
SECTION 2 – PFD Bearing Pointers and Information Windows There are 2 bearing pointers available, 1 or 2 can be displayed on the HSI. Pressing the PFD softkey provides access to the BRG1 and BRG2 softkeys. BRG1 pointer is a single cyan (light blue) line with an open arrowhead at the end. BRG2 pointer is a double cyan (light blue) line with an open arrowhead at the end. The bearing pointers never override the CDI.
SECTION 2 – PFD Navigation Source The HSI can display two sources of navigation, GPS or NAV (VOR, localizer, and glideslope). In GPS mode the flight plan legs are sequenced automatically. Enabling OBS mode suspends auto sequencing of waypoints, but retains the current “active to” waypoint as your navigation reference even after passing the waypoint. When OBS is disabled the GPS returns to normal operation, with automatic sequencing of waypoints.
SECTION 2 – PFD 2.4 COMMUNICATION, NAVIGATION & SURVEILLANCE Communication Frequency Window The Communication Frequency window provides the control and display of dual VHF Radio Communication Transceivers (COM1 and COM2). The Communication Frequency window displays the following information: • COM1 and COM2 active and standby frequencies • Color coded indication of the active COM transceiver NOTE: Operating procedures for the Communication Frequency window are located in the VHF NAV/COM Pilot’s Guide.
SECTION 2 – PFD Navigation Status Bar The Navigation Status Bar resides at the top of the PFD and displays valuable information while flying a route. The following information is displayed: • • • • • The next waypoint in the active flight plan Distance to the next waypoint (DIS) Desired track to the next waypoint (DTK) Current track angle (TRK) GPS Navigation Annunciations NOTE: The fields in the PFD Navigation Status Bar cannot be changed.
SECTION 2 – PFD Transponder Status Bar The Transponder Status Bar displays the transponder code, reply symbol, and mode of operation. TIS (Traffic Information System) surveillance data up-linked by Air Traffic Control (ATC) radar through the GTX33 Mode S Transponder appears on the Inset Map (PFD), Navigation and Traffic Map Pages on the MFD (refer to the MFD Pilot’s Guide). If the transponder is configured with Automated Airborne Determination, normal operation begins when lift off is sensed.
SECTION 3 – AUDIO PANEL SECTION 3: AUDIO PANEL The GMA 1347 Audio Panel features the following three (3) major groups of keys in descending order, as shown in Figure 3-1: • Communication keys • Navigation keys • Intercom keys Each key is labeled with a white inscription in its center, indicating the name of the associated channel. The triangular key annunciator lights are white when illuminated and point to the corresponding keys.
SECTION 3 – AUDIO PANEL Transceiver Audio Transmitters Telephone Split COM Passenger Address Speaker Marker Beacon Signal Sensitivity Marker Beacon/Mute Aircraft Navigation Radio Audio Aircraft Navigation Radio Audio Manual Squelch Digital Recording Playback ICS Isolation VOL/SQ VOL Annunciation SQ Annunciation Reversionary Mode Figure 3-1 Front Panel Controls 32 Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R
SECTION 3 – AUDIO PANEL Microphones The GMA 1347 features six (6) different microphone channeling modes: • • • • • • COM1 MIC COM2 MIC COM3 MIC COM 1/2 (Split COM) PA COM 1/2 and PA (Split COM and PA) NOTE: A push-to-talk (PTT) switch must be pressed to open the selected output channel. Each audio panel can accept up to six (6) microphone inputs, thus allowing for a two-person crew and up to four (4) passenger intercom stations in the aircraft.
SECTION 3 – AUDIO PANEL 3.2 UNIT OPERATION Power-up Settings Upon power-up, the unit undergoes a self-test during which all panel annunciator lights illuminate for approximately two (2) seconds. Once the self-test is completed, the settings are restored to the settings that were current before the unit was last powered off.
SECTION 3 – AUDIO PANEL Transceiver Keys Pressing a COM Key As illustrated below, the following eight (8) transceiver 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. Pressing COM1, COM2, or COM3 selects the corresponding radio as the active audio source.
SECTION 3 – AUDIO PANEL COM Swap The GMA 1347 allows for the use of a remotely mounted 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.
SECTION 3 – AUDIO PANEL Split COM and PA Speaker Output When in split COM mode (COM 1/2 activated), the copilot can make PA announcements while the pilot continues to use COM1 independently. When the PA key is pressed after the split COM mode is activated, the copilot’s microphone is output over the cabin speaker when keyed. Pressing the PA key again returns the copilot to normal split COM operation. Pressing the SPKR key selects the aircraft radios to be output to the cabin speaker.
SECTION 3 – AUDIO PANEL 3.3 MARKER BEACON RECEIVER Description and Operation The GMA 1347 provides a marker beacon receiver to be used as part of an ILS approach. In addition to the normal marker beacon receiver functions, the GMA 1347 provides an audio muting capability. The marker beacon receiver is always “ON” and receives at 75 MHz.
SECTION 3 – AUDIO PANEL Beacon Outer Marker Audio Frequency 400 Hz Audio Keying ——— Middle Marker 1,300 Hz •—•— Airway/Inner Marker 3,000 Hz •••• Rate 2 dashes per second 95 dot-dash combinations per minute 6 dots per second Lamp Color Blue Amber White Table 3-1 Marker Beacon Signal Characteristics Inner Marker Middle Marker Figure 3-5 Marker Beacon Signal Indicator Lights on the PFD Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R Outer Marker 39
SECTION 3 – AUDIO PANEL 3.4 RADIO INPUTS Pressing DME, ADF, AUX, NAV1, or NAV2 selects the corresponding audio source and activates the annunciator. Pressing the selected audio source key again deselects this audio source. Selected aircraft audio can be heard over the appropriate headset and over the speakers if SPKR is selected. Note that all aircraft radio keys can be selected concurrently.
SECTION 3 – AUDIO PANEL 3.5 INTERCOM SYSTEM (ICS) ISOLATION The intercom system (ICS) provides four (4) isolation modes: ALL, PILOT, COPILOT, and CREW. The desired mode can be selected or deselected using the PILOT and COPLT keys. Figure 3-7 ICS Isolation PILOT Mode CREW Mode PILOT mode is selected when only the PILOT key is annunciated. In PILOT mode, the pilot can hear the selected radios, whereas the copilot and passengers can only communicate with each other and hear MUSIC 1.
SECTION 3 – AUDIO PANEL The following table summarizes the ICS operation for the four (4) ICS isolation modes supported by the unit.
SECTION 3 – AUDIO PANEL When transitioning from auto to manual squelch, the unit “recalls” the previous VOL/SQ selection and sets the state of the unit accordingly (see table below). NOTE: The volume and squelch controls for the COM and NAV radios are located on the PFD and MFD bezels (please refer to the G1000 VHF NAV/COM Pilot’s Guide for details). Intercom VOL/SQ State Intercom Volume Control Intercom volume can be controlled via the VOL/SQ knob.
SECTION 3 – AUDIO PANEL To adjust squelch threshold level manually if the MAN SQ key is already annunciated: 1a. If the VOL annunciation is lit, press the VOL/SQ knob to illuminate the SQ annunciation, and turn the VOL/SQ knob. 1b. If the SQ annunciation is already lit, turn the VOL/SQ knob. 3.7 DISPLAY BACKUP MODE Pressing the red DISPLAY BACKUP button located at the bottom of the audio panel selects the reversionary (or backup) mode for all displays.
SECTION 4 – MFD SECTION 4: MULTI FUNCTION DISPLAY 4.1 INTRODUCTION This section of the G1000 Cockpit Reference Guide introduces the pilot to the major features of the Multi Function Display. A complete description of the MFD with detailed operating procedures is contained in the G1000 Multi Function Pilot’s Guide and the G1000 Engine Indication System Pilot’s Guide. LTNG – Press to display lightning data on the Navigation Map Page (within a 200 nm radius of the aircraft).
SECTION 4 – MFD ENGINE MAP DCLTR CHKLIST NOTE: Nav III does not use the checklist functionality which exists in the G1000 Press the BACK softkey on this level to return to the top softkey level ENGINE LEAN SYSTEM DCLTR-1 BACK DCLTR-2 DCLTR-3 Press the BACK softkey on this level to return to the top softkey level ENGINE LEAN SYSTEM CYL SLCT ASSIST Press the BACK softkey on this level to return to the top softkey level BACK TRAFFIC Press the BACK softkey on this level to return to the to
SECTION 4 – MFD 4.3 ENGINE INDICATION SYSTEM WINDOW The G1000 Engine Indication System (EIS) window provides gauges, bar graphs and numeric readouts of engine and airframe systems parameters to the pilot. The EIS window is displayed on the left side of the MFD during normal operations. In reversionary mode, the PFD and MFD both show the EIS window.
SECTION 4 – MFD Manifold Pressure Gauge Tachometer Fuel Quantity Indicator Fuel Flow Indicator Oil Pressure Indicator Oil Temperature Indicator Exhaust Gas Temperature Cylinder Head Temperature Indicator Voltmeter Ammeter Flaps Position Indicator Turbine Inlet Temperature Indicator Elevator Trim Indicator Rudder Trim Indicator Figure 4-3 ENGINE Page (Normally Aspirated) 48 Figure 4-4 ENGINE Page (Turbocharged) Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R
SECTION 4 – MFD Fuel Flow Indicator (Normally Aspirated) CHT Indicator The Fuel Flow indicator displays current fuel flow values, expressed in gallons per hour (GPH). The CHT (Cylinder Head Temperature) indicator displays the temperature of the hottest cylinder in degrees Fahrenheit. The number of the hottest cylinder appears in the triangle pointer.
SECTION 4 – MFD 4.
SECTION 4 – MFD Working With Menus Much of the operation of the G1000 is accomplished using a menu interface. The G1000 has a bezel-mounted dedicated menu key that when pressed, displays a context-sensitive list of options. This options list allows the pilot to access additional features or make settings changes which specifically relate to the currently displayed page. Some menus provide access to additional submenus that are used to view, edit, select, and, review options.
SECTION 4 – MFD 4.4 NAVIGATION MAP PAGE The Navigation Map Page provides an extensive array of GPS/navigation/mapping capability. Key features include: • Map display showing airports, navaids, airspaces, land data (highways, cities, lakes, rivers, borders, etc.
SECTION 4 – MFD Figure 4-8 Navigation Map Page Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R 53
SECTION 4 – MFD Changing the Map Orientation See the Navigation Map Page Menu section for instructions on how to change the map orientation. Clearing Lightning Data See the Navigation Map Page Menu section for instructions on how to clear lightning data from the map display NOTE: A complete list of available map datums are given in Appendix D of the Pilot’s Guide.
SECTION 4 – MFD Decluttering the Map To pan the map: The Navigation Map Page can be quickly decluttered by repeatedly pressing the DCLTR softkey until the desired detail is depicted. The declutter level label appears above the DCLTR softkey. Table 8.2.1 lists the map features that are turned off at each declutter level. 1. Push in the joystick to display the panning arrow. 2.
SECTION 4 – MFD Latitude and longitude position of pointer Distance, bearing and elevation Panning Arrow Figure 4-10 Navigation Map Panning 56 Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R
SECTION 4 – MFD Displaying Topographic Data on the Navigation Map Page The Navigation Map Page displays various shades of topography land colors representing the rise and fall of land elevation similar to aviation sectional charts. The Navigation Map Page can display a topographic scale representing various key points of terrain elevation colors with their associated elevation value labeled. To display topographic data on the Navigation Map Page: 1. Press the MAP softkey. 2. Press the TOPO softkey.
SECTION 4 – MFD To display traffic on the Navigation Map Page: 1. Press the MAP softkey. 2. Press the TRAFFIC softkey. Press the TRAFFIC softkey again to remove traffic. NOTE: Traffic and terrain data can also be displayed by using the ‘On/Off’ Navigation Map Page option. See the Navigation Map Page setup section for details.
SECTION 4 – MFD In normal operation, the current mode and rate are displayed in the top right corner of the Navigation Map Page. The mode is described by the word ‘STRIKE’ when in strike mode, or ‘CELL’ when in cell mode. • Vertical speed required (VSR) • Cross track error (XTK) • Currently selected MFD page title The strike data display phases are: 1. Lightning Symbol (latest strikes; less than one minute; a black guard band is placed around the strike symbol during the first six seconds of display) 2.
SECTION 4 – MFD Navigation Map Page Menu The Navigation Map Page can be customized using three page menu options: ‘Map Setup’, ‘Measure Bearing/Distance’, and ‘Clear Lightning Data’. To display the page menu, press the MENU key (with the Navigation Map Page displayed). Figure 4-14 Navigation Map Page Menu Options First Option: ‘MAP SETUP’ The first option is ‘MAP SETUP’. There are five “groups” available under the ‘MAP SETUP’ option: Map, Weather, Traffic, Aviation, and Land.
SECTION 4 – MFD 4.5 TRAFFIC MAP PAGE The Traffic Map Page displays the following information: • Current aircraft location, surrounding Traffic Information System (TIS) traffic, and range marking rings. • The current traffic mode (OPERATE, STANDBY). • A traffic alert message (FAILED, DATA FAILED, NO DATA, UNAVAILABLE). • Traffic display banner (AGE 00:, TRFC COAST, TA OFF SCALE, TRFC RMVD, TRFC FAIL, NO TRFC DATA, TRFC UNAVAIL, TRAFFIC). To select the Traffic Map Page: 1. Select the MAP group of pages.
SECTION 4 – MFD Traffic Mode Map Range Traffic Vehicle (ownship) Figure 4-15 Traffic Map Page 62 Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R
SECTION 4 – MFD TIS Symbology Traffic Map Page Operations TIS traffic is displayed on the Traffic Map Page according to TCAS symbology. A Traffic Advisory (TA) symbol is displayed as a solid yellow circle (or half circle on the outer range ring if the traffic is outside the range of the dedicated traffic page). All other traffic is displayed as a hollow white diamond.
SECTION 4 – MFD Operating Mode 3. Once the aircraft is airborne (determined by system configuration at the time of installation) the system switches from standby mode to operating mode. The G1000 displays ‘OPERATE’ in the upper left hand corner of the display and begins to display traffic on the Traffic or Map Page. The TIS Traffic Advisory (TA) should alert the crew to use additional vigilance to identify the intruding aircraft.
SECTION 4 – MFD TIS Traffic Status The MFD indicates the following TIS traffic status to the pilot. Traffic Banner • AGE - if traffic data is not refreshed within 6 seconds, an age indicator (i.e., ‘AGE 00:06’) is displayed in the lower left corner of the display (when displaying traffic). After another 6 seconds, if data is still not received, the traffic is removed from the display. The pilot should be aware that the quality of displayed traffic is reduced in this condition.
SECTION 4 – MFD 4.6 WEATHER MAP PAGE The G1000 provides an optional display interface for the L-3 Stormscope® WX-500 Series II Weather Mapping Sensor. The WX-500 is a passive weather avoidance system that detects electrical discharges associated with thunderstorms within a 200 nm radius of the aircraft. The Stormscope measures relative bearing and distance of thunderstorm related electrical activity and displays the information on the Weather Map Page.
SECTION 4 – MFD NOTE: The WX-500 has to be receiving valid heading information in order for lightning data to be displayed. To change the viewing mode between 360˚ and 120˚: 1. Select the Weather Map Page. 2. Press the VIEW softkey. The 360 and ARC softkeys are displayed. Press the 360 softkey to display a 360˚ viewing are or press the ARC softkey to display a 120˚ viewing area OR: 3. Press the MENU key. The page menu is displayed with ‘View Arc’ or ‘View 360’ highlighted.
SECTION 4 – MFD 4.7 TERRAIN PROXIMITY PAGE Terrain Proximity Page Operations CAUTION: Terrain and obstacle data are provided only as an aid to situational awareness. No aural messages or textual annunciations are displayed to the pilot during flight operations regarding the presence of terrain or obstacles. The Terrain Proximity Page displays the following: • Current aircraft location. • Range marking rings (25 nm, 25/50 nm, 50/100 nm, and 100/200 nm). • Heading Box (North Up, Track Up, DTK Up, HDG Up).
SECTION 4 – MFD Displaying Obstacle Data Navigation Map Display Conditions The Terrain Proximity Page displays obstacle data with heights greater than 200 feet Above Ground Level (AGL) located at their geographical position location throughout the world. Obstacles are displayed in three levels: • SAFE • CAUTION • WARNING Each level is associated with a color. The G1000 will adjust colors on the Terrain Proximity Page automatically as the aircraft altitude changes.
SECTION 4 – MFD 4.8 DIRECT-TO NAVIGATION To select a direct-to destination: The “Direct-to” function provides a quick method of setting a course to a destination waypoint. Once a Direct-to is activated, the G1000 establishes a point-to-point course line from the present position to the selected Direct-to destination. If the course change is greater than 30 degrees, a course extension is offset from the present position to allow a standard rate turn to intercept the Direct-to course line.
SECTION 4 – MFD Direct to Navigation Operations 4. Continue turning the small FMS knob to scroll through any additional database listings for the selected facility name or city. The small FMS knob can be used to scroll backwards if the desired waypoint was passed up. 5. Press the ENT key to confirm the selected waypoint, and ENT again to activate a Direct-to.
SECTION 4 – MFD To select a Direct-to destination from the active flight plan: 1. Press the Direct-to key. The Direct-to Waypoint Page is displayed with the waypoint identifier field highlighted. 2. Turn the large FMS knob to highlight the flight plan ‘FPL’ field. 3. Turn the small FMS knob to display a window showing all waypoints in the active flight plan. 4. Continue turning the small FMS knob to scroll through the list and highlight the desired waypoint. 5.
SECTION 4 – MFD Canceling Direct-to Navigation Once a direct-to is activated, the G1000 provides navigation guidance to the selected destination until the direct-to is either replaced with a new direct-to or flight plan, or cancelled, or if the unit is turned off. To cancel a direct-to: 1. Press the Direct-to key to display the Direct-to Page. 2. Press the MENU key to display the direct-to options menu. 3. With Cancel Direct-To NAV highlighted, press the ENT key.
SECTION 4 – MFD Specifying a Course to a Waypoint When Direct-to is activated, the G1000 sets a direct great circle course to the selected destination. The course to the destination, using the course field on the Direct-to Page can be manually defined. To manually define the direct-to course: 74 1. Press the Direct-to key. 2. Turn the small and large FMS knobs to select the destination waypoint. 3.
SECTION 4 – MFD 4.9 FLIGHT PLANS The G1000 can create up to 99 different flight plans with up to 31 waypoints in each flight plan. The flight plan (FPL) page group consists of three pages: • Active Flight Plan • Flight Plan Catalog • Vertical Navigation The Flight Plan Pages are used to create, edit and copy flight plans. The Vertical Navigation Page is used to create a three-dimensional profile which guides the aircraft to a final (target) altitude at a specified location.
SECTION 4 – MFD empty storage location. Turn the small and large FMS knobs to enter the identifier of the departure waypoint and press the ENT key. 5. Repeat step number 4 to enter the identifier for each additional flight plan waypoint. 6. Once all waypoints have been entered, press the FMS knob to return to the Flight Plan Catalog Page.
SECTION 4 – MFD To edit a flight plan: 1. Press the FPL key and turn the small FMS knob to display the Flight Plan Catalog Page. 2. Press the FMS knob to activate the cursor. 3. Turn the large FMS knob to highlight the desired flight plan and press the ENT key. 4. To add a waypoint to the flight plan: Turn the large FMS knob to select the point where the new waypoint is to be added. (If an existing waypoint is highlighted, the new waypoint is placed directly in front of this waypoint.
SECTION 4 – MFD To remove an approach, arrival or departure from the active flight plan: 1. From the Active Flight Plan Page, press the MENU key to display the Active Flight Plan Page options. 2. Select the ‘Remove Approach’, ‘Remove Arrival’ or ‘Remove Departure’ option and press the ENT key. 3. A confirmation window is displayed listing the procedure the pilot is about to remove. With ‘OK’ highlighted, press the ENT key.
SECTION 4 – MFD Flight Plan Catalog Page Operations The following operations can be performed from the Flight Plan Catalog Page: • • • • • • • • • • Activate a Flight Plan Stop Navigating a Flight Plan Invert and Activate a FPL Create a New Flight Plan Copy a Flight Plan Delete a Flight Plan Delete All Flight Plans Sort Flight Plans by Comment Flight Plan Catalog Page Options Edit a Flight Plan desired flight plan and press the MENU key to display the Flight Plan Catalog Page options. 4.
SECTION 4 – MFD To copy a flight plan to another flight plan catalog location: 1. From the Flight Plan Catalog press the FMS knob to activate the cursor, turn the large FMS knob to highlight the flight plan the pilot wishes to copy, then press the MENU key to display the Flight Plan Catalog Options. 2. Turn the large FMS knob to highlight ‘Copy Flight Plan’ and press the ENT key. 3. A ‘Copy to flight plan?’ confirmation window is displayed. With ‘OK’ highlighted, press the ENT key to copy the flight plan.
SECTION 4 – MFD To delete a flight plan from the Flight Plan Catalog Page: 1. From the Flight Plan Catalog Page, press the FMS knob to activate the cursor, turn the large FMS knob to highlight the flight plan to delete. 2. Press the MENU key to display the Flight Plan Catalog options. 3. Turn the large FMS knob to highlight ‘Delete Flight Plan’ and press the ENT key. 4. A ‘Delete flight plan?’ confirmation window is displayed. With ‘OK’ highlighted, press the ENT key to delete the flight plan.
SECTION 4 – MFD 4.10 PROCEDURES To select a departure: Arrivals and Departures Based upon the active flight plan or Direct-to destination, the Procedures Page provides direct access to approaches, departures and arrivals. The Procedures Page is displayed by pressing the PROC key. 1. 2. 3. Press the PROC key. Turn the large FMS knob to highlight ‘Select Departure’ and press the ENT key. The departure procedure window appears. Turn the FMS knob to select the desired departure and press the ENT key.
SECTION 4 – MFD Approaches The G1000 allows you to fly non-precision and precision approaches to airports with published instrument approach procedures. All available approaches are part of the Jeppesen database stored internally in each PFD and MFD. The G1000 provides both lateral and vertical guidance for ILS precision approaches on the PFD, and lateral guidance for non-precision Localizer, GPS, and VOR and ADF overlay approaches.
SECTION 4 – MFD Selecting Approaches In order to select an approach, there must be an active flight plan or direct-to which terminates at an airport with a published approach. To select an approach: 1. Press the PROC key to display the Procedures Page. Turn the large FMS knob to highlight ‘Select Approach’ and press the ENT key. The approach procedure window appears. 2. Turn the FMS knob to select the desired approach and press the ENT key. The transition window appears.
SECTION 4 – MFD Not all approaches in the database are approved for GPS use. As you select an approach, a ‘GPS’ designation to the right of the procedure name indicates the procedure can be flown using the GPS receiver. Some procedures will not have this designation, meaning the GPS receiver can be used for supplemental navigation guidance only. If the GPS receiver cannot be used for primary guidance, you must use the appropriate receiver for the selected approach (e.g., VOR or ILS).
SECTION 4 – MFD GPS Approach Examples No Procedure Turn An approach where there is no procedure turn required to get established on the inbound course to the FAF is our example. GPS RWY 12 is used to show how the G1000 sequences through an approach and what type of annunciation and range factor changes can be expected (the G1000 automatically sequences through all legs of an approach without pilot input other than to activate the approach and to sequence past the missed approach point).
Reproduced with permission of Jeppesen Sanderson, Inc. Not to be used for navigation.
SECTION 4 – MFD Flying the Missed Approach As you pass the MAP, and the runway is not in view, a missed approach must be performed. The G1000 continues to give guidance along an extension of the final course segment (FAF to MAP) until you manually initiate the missed approach procedure. 88 1. Upon crossing the MAP, a waypoint message ‘ARRIVING AT WAYPOINT’ appears in the navigation status bar on the PFD.
Reproduced with permission of Jeppesen Sanderson, Inc. Not to be used for navigation.
SECTION 4 – MFD Flying the Procedure Turn The procedure turn portion of the approach is stored as one of the legs of the approach. For this reason the G1000 requires no special operations from the pilot (other than flying the procedure turn itself) beyond what is required for any other type of approach. This example is based upon a flight from KILG (Wilmington, DE New Castle County) to KMIV (Millville, NJ Municipal). The approach into KMIV will be NDB or GPS RWY 14 with the RNB transition. 1.
SECTION 4 – MFD 14. As the pilot approaches the MAP, a waypoint message ‘ARRIVING AT WAYPOINT’ appears. Reproduced with permission of Jeppesen Sanderson, Inc. Not to be used for navigation. 15. Upon crossing the MAP, ‘SUSP’ appears on the HSI and directly above the SUSP softkey, indicating that automatic sequencing of approach waypoints is suspended. A ‘FROM’ indication is displayed in the CDI, but course guidance along the final approach course continues.
SECTION 4 – MFD Flying the DME ARC The GPS overlay for a DME arc approach uses additional Jeppesen provided waypoints to define the arc. When cleared for a DME arc approach, you may do either of the following to intercept the arc: 6. Follow the arc, keeping the CDI needle centered. 7. The next point in the approach is an intermediate fix “WILDE”. As you approach “WILDE” a waypoint message ‘NEXT DTK 072°’ appears.
Reproduced with permission of Jeppesen Sanderson, Inc. Not to be used for navigation.
SECTION 4 – MFD Flying a Holding Pattern This example is based upon a missed approach from KSOP (Moore County, NC). Now you’ve decided to divert to KIGX (Chapel Hill, NC) instead. You select the RNAV (GPS) RWY 9 approach into KIGX. The RNAV (GPS) RWY 9 approach begins with a holding pattern at the IAF, FIKKA. 1. 94 From the Active Flight Plan Page highlight KIGX and press the Direct-to key, then press the ENT key twice. 2. Press the PROC key and select the RNAV (GPS) RWY 9 approach. 3.
SECTION 4 – MFD NOTE: Remember do not press the OBS softkey until you are ready to make the turn. Reproduced with permission of Jeppesen Sanderson, Inc. Not to be used for navigation. 14. Upon crossing the MAP, ‘SUSP’ appears on the HSI and directly above the SUSP softkey, indicating that automatic sequencing of approach waypoints is suspended at the MAP. A ‘FROM’ indication is displayed on the CDI, however course guidance along the final approach course continues.
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APPENDIX A A.1 INTRODUCTION IMPORTANT NOTE: The Aircraft Flight Manual takes precedence over any conflicting information found in Appendix A. • Audio Alerting System: The G1000 system issues audio alert sounds and aural voice messages when specific system conditions are met. See Section A.3 for more information. The G1000 Alerting System conveys alerts to the pilot using a combination of the following items: • Annunciation Window: The Annunciation Window is not used for Mooney aircraft.
APPENDIX A A.2 ALERT LEVELS The G1000 Alerting System uses a single alert level for Mooney aircraft: • MESSAGE ADVISORY: A Message Advidory alert is designed to provide general information to the pilot. This alert is accompanied by a flashing ADVISORY softkey, as shown in Figure A-2. Pressing the ADVISORY softkey acknowledges the presence of the alert and displays the alert text message in the Alerts window. All G1000 system alerts listed in Section A.5 are categorized as Message Advisories.
APPENDIX A A.3 MOONEY SPECIFIC AIRCRAFT ALERTS The following information is configured specifically for the Mooney aircraft. See the Aircraft Flight Manual and/or Flight Manual Supplement for recommended pilot actions. Audio Alerts Audio Alert Altitude Alert Chime Alert Trigger When aircraft altitude reaches the reference altitude threshold (+/- 1,000 ft of reference altitude). When aircraft altitude reaches or goes beyond the reference altitude deviation limit (+/-200 ft of reference altitude).
APPENDIX A A.4 G1000 SYSTEM ANNUNCIATIONS When an LRU or an LRU function fails, a large red ‘X’ is typically displayed on windows associated with the failed data. The following Section describes various system annunciations. Refer to the Aircraft Flight Manual Supplement and/or Flight Manual Supplement for additional information regarding pilot responses to these annunciations.
APPENDIX A System Annunciation Comment Display is not receiving vertical speed input from the air data computer. Display is not receiving valid heading input from AHRS. GPS information is either not present or is invalid for navigation use. Note that AHRS utilizes GPS inputs during normal operation. AHRS operation may be degraded if GPS signals are not present (see AFMS). Display is not receiving valid transponder information.
APPENDIX A A red ‘X’ may be the result of an LRU or an LRU function failure. The figure presented below illustrates all possible flags and the responsible LRUs.
APPENDIX A A.5 G1000 SYSTEM MESSAGE ADVISORIES This section describes various G1000 system message advisories. Certain messages are issued due to an LRU or LRU function failure. Such messages are normally accompanied by a corresponding red ‘X’ annunciation as shown in Section A.4. MFD & PFD Message Advisories IMPORTANT NOTE: This Section provides information regarding G1000 messages that may be displayed.
APPENDIX A Database Message Advisories Alerts Window Message Comments MFD1 DB ERR – MFD1 aviation database error exists. The MFD and/or PFD detected a failure in the aviation database. Attempt to reload the aviation database. If problem persists, have the G1000 system serviced. PFD1 DB ERR – PFD1 aviation database error exists. MFD1 DB ERR – MFD1 basemap database error exists. The MFD and/or PFD detected a failure in the basemap database. PFD1 DB ERR – PFD1 basemap database error exists.
APPENDIX A GIA 63 Message Advisories Alerts Window Message Comments GIA1 CONFIG – GIA1 configuration error. Config service req’d. GIA1 and/or GIA2 configuration settings do not match backup configuration memory. Have the G1000 system serviced. GIA2 CONFIG – GIA2 configuration error. Config service req’d. GIA1 COOLING – GIA1 temperature too low. GIA1 and/or GIA2 temperature is too low to operate correctly. Allow units to warm up to operating temperature. GIA2 COOLING – GIA2 temperature too low.
APPENDIX A GIA 63 Message Advisories (Cont.) Alerts Window Message Comments RAIM UNAVAIL – RAIM is not availGPS satellite coverage is insufficient to perform Receiver Autonomous Integrity able from FAF to MAP waypoints. Monitoring (RAIM) from the FAF to the MAP waypoints. RAIM UNAVAIL – RAIM is not availGPS satellite coverage is insufficient to perform Receiver Autonomous Integrity able. Monitoring (RAIM) for the current phase of flight.
APPENDIX A GIA 63 Message Advisories (Cont.) Alerts Window Message G/S1 FAIL – G/S1 is inoperative. G/S2 FAIL – G/S2 is inoperative. G/S1 SERVICE – G/S1 needs service. Return unit for repair. G/S2 SERVICE – G/S2 needs service. Return unit for repair. Comments A failure has been detected in glideslope receiver 1 and/or receiver 2. Have the G1000 system serviced. A failure has been detected in glideslope receiver 1 and/or receiver 2. The receiver may still be available.
APPENDIX A GRS 77 Message Advisories Alerts Window Message AHRS TAS – AHRS not receiving airspeed. AHRS GPS – AHRS using backup GPS source. AHRS GPS – AHRS not receiving GPS information. MANIFEST – GRS1 software mismatch. Communication halted. BACKUP PATH – AHRS using backup data path. AHRS SERVICE – AHRS Magnetic-field model needs update. GEO LIMITS – Too far North/South, no magnetic compass. Comments The AHRS is not receiving true airspeed from the air data computer.
APPENDIX A GDC 74A Message Advisories Alerts Window Message Comments GDC1 CONFIG – GDC1 configuration GDC 74A configuration settings do not match those of backup configuration error. Config service req’d. memory. Have the G1000 system serviced. MANIFEST – GDC1 software misThe GDC 74A has incorrect software installed. Have the G1000 system serviced. match. Communication halted. BACKUP PATH – Airdata using backup The GDC 74A is using a backup communications data path. Have the G1000 system data path.
APPENDIX A Miscellaneous Message Advisories (Cont.) Alerts Window Message Comments APPR TRG ALT – Approaching target Aircraft is approaching target altitude. Prepare to level aircraft. altitude. LOCKED FPL – Cannot navigate locked This occurs when the pilot attempts to activate a stored flight plan that contains flight plan. locked waypoint. Remove locked waypoint from flight plan. Update flight plan with current waypoint.
INDEX A Accomplishing a Holding Pattern 94 Activate a Flight Plan 79 Active Flight Plan 71 Active Flight Plan Page 75 Active Flight Plan Page Options 75 AIRCRAFT ALERTS 99 Airspeed Indicator 17 Airspeed Trend Vector 17 Air Data Computer 1 Alerting System 97 Alerts 97 Altimeter 20 Altitude Reference Bug 20 Altitude Trend Vector 20 ALT mode 29 Annunciator lights 34 Approaches 83 Approach markers 38 Inner 38, 43 Lamp color 39 Middle 38 Outer 38, 43 Signal Augmentation 38 ARC HSI 24 ARINC leg types 83 Arrivals
INDEX K Key 3, 4 L LED 34 Lightning 66 LTNG 58 lying the Missed Approach 88 M Magnetometer 1 Manual squelch (MAN SQ) 34, 42, 43, 44 Override 43 MAP 58 Map Group Options 60 Map Orientation 54 Map Panning 55 Map Scale 54 Marker beacon 38 Marker Beacon Annunciations 22 MASQ 40 Menus 51 Message Advisories 103, 104, 106, 107, 108, 109, 110 MFD 1, 45 MFD softkeys 45 MKR/MUTE 38 Mode A 29 Mode C 29 Mode S Transponder 29 MUSIC #1 33, 41 MUSIC #2 33, 41 N NAV1 34, 36, 37, 40 NAV2 34, 36, 37, 40 NAVAID x NAVAIDS x
INDEX True Airspeed box 17 Turn Rate Indicator 25 TX 35 V Vectors to the DME ARC 94 Vertical Deviation/Glideslope Indicator 22 Vertical Speed Indicator 23 Vertical Speed Pointer 23 VFR 29 VLOC receiver 85 Volume 35, 36, 43 Volume/squelch 42 Vspeed References 17 W WARN 26 Warning 33 Warnings x, xi Warranty ix Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R 113
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Garmin G1000 Cockpit Reference Guide for Mooney M20M & M20R
Garmin International, Inc. 1200 East 151st Street Olathe, KS 66062, U.S.A. p: 913.397.8200 f: 913.397.8282 Garmin AT, Inc. 2345 Turner Road SE Salem, OR 97302, U.S.A. p: 503.391.3411 f: 503.364.2138 Garmin (Europe) Ltd. Unit 5, The Quadrangle Abbey Park Industrial Estate Romsey, SO51 9DL, U.K. p: 44/1794.519944 f: 44/1794.519222 Garmin Corporation No. 68, Jangshu 2nd Road Shijr, Taipei County, Taiwan p: 886/2.2642.9199 f: 886/2.2642.9099 www.garmin.com © 2004 Garmin Ltd.
