Integrated Flight Deck Cockpit Reference Guide Mooney M20M, M20R, & M20TN
Copyright © 2004 - 2006 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0424.20 or later for the Mooney M20M, M20R, and M20TN. 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.
WARNINGS, CAUTIONS, & NOTES . 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.
WARNINGS, CAUTIONS, & NOTES WARNING: NEXRAD weather data is to be used for long-range planning purposes only. Due to inherent delays in data transmission and the relative age of the data, NEXRAD weather data should not be used for short-range weather avoidance. WARNING: The Garmin G1000, as installed in the Mooney M20M, M20R, and M20TN aircraft, has a very high degree of functional integrity.
WARNINGS, CAUTIONS, & NOTES CAUTION: The Garmin G1000 does not contain any user-serviceable parts. Repairs should only be made by an authorized Garmin service center. Unauthorized repairs or modifications could void both the warranty and the pilot’s authority to operate this device under FAA/FCC regulations. NOTE: When using Stormscope, there are several atmospheric phenomena in addition to nearby thunderstorms that can cause isolated discharge points in the Strike Display Mode.
RECORD OF REVISIONS Part Number 190-00450-01 190-00450-02 Change Summary Reformat of manual Added WX 500 Stormscope Added XM Weather Added ADF/DME Added extended range fuel tanks Changes in EIS softkey labels Added TAWS-B Added Automatic Flight Control System Changed System Software Revision Revision Date of Revision Affected Pages A 12/05 i-Index-2 B 4/06 2-4 11-2 12-1 C 6/06 3-1 – 3-2 5-1 6-1 D 7/06 RR-1 2-4 12-7 Description Initial release Added Altitude Alert and Barometric Minimums info.
RECORD OF REVISIONS Blank Page RR-2 Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN
TABLE OF CONTENTS SECTION 1: SYSTEM OVERVIEW.................................... 1-1 1.1 1.2 1.3 1.4 1.5 PFD/MFD Controls................................................... 1-2 PFD Softkeys............................................................ 1-4 MFD Softkeys .......................................................... 1-7 MFD Page Groups ................................................... 1-8 Backlighting .............................................................
TABLE OF CONTENTS Navigation Mode (GPS, VOR, LOC, or BC)................... 6-12 Navigation Mode Armed....................................... 6-12 Approach Mode (GPS, VAPP or LOC) .......................... 6-13 Go Around (GA) ........................................................ 6-13 6.7 Example Procedures Using AFCS ....................... 6-14 Departure ................................................................. 6-15 Intercepting a VOR Radial ..........................................
TABLE OF CONTENTS 8.6 Invert Active Flight Plan ....................................... 8-3 8.7 Create a New Flight Plan ...................................... 8-4 Create a New Flight Plan Using the MFD ..................... 8-4 Create a New Flight Plan Using the PFD ...................... 8-4 8.8 Load a Departure ................................................... 8-4 8.9 Load an Arrival........................................................ 8-5 8.10 Load an Approach ......................................
TABLE OF CONTENTS 12.2 M20M/M20R/M20TN Aircraft Alerts .................. 12-2 Voice Alerts ............................................................... 12-2 Message Advisory Alerts ............................................ 12-2 12.3 AFCS Alerts............................................................. 12-3 System Status Field ................................................... 12-3 12.4 TAWS ALERTS ......................................................... 12-4 TAWS System Status Annunciations ....
SECTION 1 SYSTEM OVERVIEW SECTION 1: SYSTEM OVERVIEW The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system more easily. It is not intended to be a comprehensive operating guide. Complete operating procedures for the complete system are found in the G1000 Mooney M20M, M20R, and M20TN Pilot’s Guide (190-00647-00).
SECTION 1 SYSTEM OVERVIEW 1.
SECTION 1 SYSTEM OVERVIEW Functionality of the PFD and MFD controls are the same with the exception of the dedicated autopilot keys located only on the MFD bezel. (1) NAV VOL/ID Knob – Controls the NAV audio level. Press to toggle the Morse code identifier ON and OFF. Volume level is shown in the field as a percentage. (2) NAV Frequency Toggle Key – Toggles the standby and active NAV frequencies. (3) Dual NAV Knob – Tunes the MHz (large knob) and kHz (small knob) standby frequencies for the NAV receiver.
SECTION 1 SYSTEM OVERVIEW (16) ENT Key – Accepts a menu selection or data entry. This key is used to approve an operation or complete data entry. It is also used to confirm selections and information entries. (17) Dual ALT Knob – Sets the reference altitude in the box located above the Altimeter. The large knob selects the thousands, while the small knob selects the hundreds.
SECTION 1 SYSTEM OVERVIEW NAV1 – Displays NAV1 waypoint frequency or identifier and DME information in the BRG1 Information Window. GPS – Displays GPS waypoint identifier and GPS distance information in the BRG1 Information Window. ADF – Displays ADF waypoint frequency in the BRG1 Information Window. OFF – Removes the BRG1 Information Window. 360 HSI – Press to display the 360° compass rose. ARC HSI – Press to display the 140° viewable arc.
SECTION 1 SYSTEM OVERVIEW BRG2 (bearing) – Press to cycle through the following Nav sources, making the pointer the indicator for the corresponding source and displaying the the appropriate information. NAV2 – Displays NAV2 waypoint frequency or identifier and DME information in the BRG2 Information Window. GPS – Displays GPS waypoint identifier and GPS distance information in the BRG2 Information Window. ADF – Displays ADF waypoint frequency in the BRG2 Information Window.
SECTION 1 SYSTEM OVERVIEW 1.3 BKSP – Press to remove numbers entered one at a time. BACK – Press to return to the previous level softkeys. IDENT – Press to provide special aircraft position identification to Air Traffic Control (ATC). BACK – Press to return to the previous level softkeys. ALERTS – Press to display the Alerts Window. IDENT – Press to provide special aircraft position identification to Air Traffic Control (ATC). TMR/REF – Press to display the Timer/References Window.
SECTION 1 SYSTEM OVERVIEW 1.5 STRMSCP (optional) – Pressing this softkey displays/removes Stormscope lightning data on the Navigation Map. NEXRAD (optional) – Pressing this softkey displays/removes precipitation data on the Navigation Map. XM LTNG (optional) – Pressing this softkey displays/removes XM Radio lightning data on the Navigation Map. BACK – Pressing this softkey displays the ENGINE and MAP top level softkeys. DCLTR (declutter) – Pressing this softkey removes map information in three levels.
SECTION 2 FLIGHT INSTRUMENTS SECTION 2: FLIGHT INSTRUMENTS The following discussions pertain to the Primary Flight Display, unless otherwise indicated.
SECTION 2 FLIGHT INSTRUMENTS 10 1 9 2 8 3 7 4 5 6 1 Traffic Annunciation 6 BRG2 Information Window 2 Selected Heading Box 7 Alerts Window 3 Inset Map 8 Selected Course Box 4 BRG1 Information Window 9 Vertical Deviation/Glideslope Indicator 5 DME Information Window 10 Marker Beacon Annunciation Figure 2-2 Additional PFD Information Distance to Next Waypoint Next Waypoint Desired Track to Next Waypoint Current Track Figure 2-3 PFD Navigation Status Window 2-2 Garmin G1000 Cock
SECTION 2 FLIGHT INSTRUMENTS 2.1 AIRSPEED INDICATOR Vspeed References Airspeed Trend Vector Actual Airspeed Vspeed References Speed Ranges True Airspeed Box Figure 2-4 Airspeed Indicator Speed Indication The indicated airspeed is displayed inside the black pointer. The pointer will become red upon reaching Vne. Vspeed References are turned on or off in the Timer/References Window. Press the TMR/REF Softkey to display the widow.
SECTION 2 FLIGHT INSTRUMENTS 2.
SECTION 2 FLIGHT INSTRUMENTS Within 2500 ft Within 100 ft 2.5 MARKER BEACON ANNUNCIATIONS Marker Beacon Annunciation Barometric Minimum Bug Vertical Deviation/Glideslope Indicator Barometric Minimum Box Altitude Reached Figure 2-10 Marker Beacon and Vertical Deviation 2.6 Figure 2-9 Barometric Minimum Descent Altitude Alerting Visual Annunciations 2.
SECTION 2 FLIGHT INSTRUMENTS 2.
SECTION 2 FLIGHT INSTRUMENTS Course Pointer Bearing Pointers and Information Windows The course pointer is a single line arrow (GPS, VOR1, and LOC1) or double line arrow (VOR2 and LOC2) which points in the direction of the set course. Pressing the PFD Softkey provides access to the BRG1 and BRG2 softkeys. The BRG1 pointer is a single line pointer. The BRG2 pointer is a double line pointer.
SECTION 2 FLIGHT INSTRUMENTS DME (optional) To display the DME Information Window, press the PFD Softkey followed by the DME Softkey. Figure 2-19 DME Information Window Navigation Source To change between navigation sources: 1) Press the CDI Softkey to change from GPS to VOR1/LOC1. 2) Press the CDI Softkey again to change from VOR1/LOC1 to VOR2/LOC2. 3) Press the CDI Softkey a third time to return to GPS.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) SECTION 3: ENGINE INDICATION SYSTEM (EIS) 3.1 ENGINE DISPLAY The Mooney M20R Default Engine Page is shown in Figure 3-1. The M20TN display is similar, but shows Turbine Inlet Temperature (TIT) instead of Exhaust Gas Temperature (EGT). The M20M display is also similar to Figure 3-1, but shows TIT and Fuel Pressure (instead of EGT and Fuel Flow). In all cases green indicates normal operation, yellow indicates caution, and red indicates warning.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3.3 ENGINE SYSTEM DISPLAY The Mooney M20R System Engine display is shown in Figure 3-3. The M20TN display is similar, but also shows Turbine Inlet Temperature (TIT). The M20M display is also similar to Figure 3-3, but shows Fuel Pressure instead of Exhaust Gas Temperature (EGT), and also shows TIT. If desired, use the DEC FUEL, INC FUEL, and RST FUEL softkeys to adjust the amount of fuel remaining for totalizer calculations.
SECTION 4 – NAV/COM & TRANSPONDER SECTION 4: NAV/COM AND TRANSPONDER The Nav/Com controls and frequency windows are located on the Primary Flight Display and the MultiFunction Display in the same locations.
SECTION 4 – NAV/COM & TRANSPONDER Standby NAV Frequency Field Tuning Box Selected NAV Frequency Active NAV Frequency Field Navigation Status Window Selected COM Frequency Figure 4-2 Frequency Fields Frequency Toggle Arrow Active COM Frequency Field Tuning Box Figure 4-3 Frequency Toggle Arrow and Tuning Box NAV Controls COM Controls VOL/PUSH ID Knob VOL/PUSH SQ Knob Frequency Toggle Key Dual NAV Knob Dual COM Knob • Turn to tune in desired frequencies.
SECTION 4 – NAV/COM & TRANSPONDER 4.1 RADIO STATUS INDICATIONS 4.4 QUICKLY ACTIVATING 121.500 MHZ • RX – When a COM signal is received, a white ‘RX’ appears by the active COM frequency during signal reception. Pressing and holding the COM Frequency Toggle Key for approximately two (2) seconds automatically tunes the selected COM radio to the emergency frequency. • TX – When a COM radio is keyed, a white TX indication appears to the right of the corresponding COM frequency. 4.
SECTION 4 – NAV/COM & TRANSPONDER 6) 7) Turn the Large FMS Knob to select the volume field if desired. Turn the Small FMS Knob to adjust the ADF volume to the desired level. 4.6 FREQUENCY AUTO-TUNING Auto-tuning on the PFD Press the FMS Knob to exit all the fields. DME Radio (optional) Figure 4-10 Nearest Airports Window (PFD) Figure 4-8 Radio Tuning Window To change the DME tuning source: 1) From the Tuning Window, turn the Large FMS Knob to highlight the DME source field.
SECTION 4 – NAV/COM & TRANSPONDER 4.7 TRANSPONDER Mode Selection The STBY, ON, and ALT softkeys can be accessed by pressing the XPDR Softkey. Ground Mode (Automatic) GND is displayed when the aircraft is on the ground. Figure 4-11 Ground Mode Reply Status When the transponder sends replies to interrogations, an “R” indication appears momentarily in the reply status field. Following is a list of important codes: • 1200 – VFR code in the U.S.
SECTION 4 – NAV/COM & TRANSPONDER Blank Page 4-6 Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN
SECTION 5 – AUDIO PANEL SECTION 5: AUDIO PANEL Transceiver Audio (COM 3 is unavailable) Transmitters (COM3 MIC is unavailable) Split COM Telephone (Unavailable) Passenger Address Speaker Marker Beacon/Mute Marker Beacon Signal Sensitivity Aircraft Navigation Radio Audio (ADF & DME optional, AUX unavailable) Manual Squelch Aircraft Navigation Radio Audio Recorded COM Audio Playback ICS Isolation VOL/SQ Volume/Squelch VOL Annunciation SQ Annunciation Reversionary Mode Figure 5-1 Audio Panel Co
SECTION 5 – AUDIO PANEL 5.1 COM RADIO SELECTION Pressing the COM1 MIC or COM2 MIC Key selects the active transmitter (i.e., microphone). The associated receiver audio (COM1 or COM2) also becomes selected when the COM MIC key is pressed. To prevent deselecting the desired received audio when pressing another COM MIC key, press the already selected COM1 or COM2 Key before pressing the other COM MIC key. In this mode, both the pilot and the copilot can transmit simultaneously over separate radios.
SECTION 5 – AUDIO PANEL Marker Beacon Signal Sensitivity The HI SENS Key can be pressed for increased marker beacon signal sensitivity. Figure 5-6 Navigation Radios 5.5 Figure 5-5 Marker Beacon 5.4 NAV RADIO AUDIO SELECTION Pressing DME, ADF, NAV1, or NAV2 selects and deselects the radio source and activates the annunciator. Selected audio can be heard over the headset and the speakers. These four keys can be selected individually or together.
SECTION 5 – AUDIO PANEL 5.6 INTERCOM SQUELCH CONTROL Select manual squelch for intercom audio by pressing the MAN SQ Key to light the annunciator. Pressing the small VOL/SQ Knob now toggles between volume and squelch adjustment by lighting VOL or SQ respectively. Figure 5-8 Volume/Squelch Control 5.7 Figure 5-9 Playback • Pressing PLAY once plays back the latest recorded memory block, then returns to normal operation.
SECTION 6 – AUTOMATIC FLIGHT CONTROL SECTION 6: AUTOMATIC FLIGHT CONTROL NOTE: The information in this section is not applicable to the M20TN aircraft. Refer to the pilot’s guide for the installed autopilot system. one side of the switch is active for more than three seconds without the other side also being active, ‘PTRM’ is displayed in the AFCS System Status field on the PFD. Pressing the MET ARM Switch also acknowledges an autopilot disconnect.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 6.1 MODE ANNUNCIATIONS 6.2 Mode annunciations are displayed on the PFD. Figure 6-3 shows the AFCS Status Bar fields. Modes associated with aircraft movement about the roll axis are displayed on the left side. Modes associated with aircraft movement about the pitch axis are displayed on the right. Armed modes are displayed in white and active modes are displayed in green.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 6.3 AP ENGAGEMENT/DISENGAGEMENT When the key is pressed, the system engages the autopilot. If the flight director is not already active, it is also engaged when the AP Key is pressed. Autopilot engagement is displayed in the Autopilot Status field of the AFCS Status Bar. Autopilot engagement is indicated by a green ‘AP’. Autopilot Engaged Figure 6-5 Autopilot Engaged Annunciation Automatic Disengagement Automatic disengagement typically occurs due to a failure.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 6.4 LOSS OF DATA In general, a flashing yellow mode annunciation indicates either the loss of sensor data (AHRS, ADC, or GIA) or loss of navigation data (VOR, LOC, or GPS) required to compute commands. When such a loss occurs, the system automatically reverts to the default mode for the affected axis (ROL for roll axis, PIT for pitch axis). The flashing annunciation stops when the pilot presses the affected mode button or selects another mode for the axis.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Pitch Hold Mode (PIT) 1) 5) Press the AP or FD Key. ‘PIT’ will be displayed in green in the Active Mode field of the AFCS Status Bar. The system will maintain or give command bar direction for a constant pitch attitude (pitch reference) depending on which key is pressed. If desired, enter an altitude in the Selected Altitude Box by turning the ALT Knob.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Altitude Hold Mode (ALT) 1) Press the ALT Key. The flight director is activated (if not already active) and ‘ALT’ is now displayed in green in the Active Mode field with the current altitude displayed in the Altitude Reference field. 2) Pitch and roll commands will be given to manually maintain the current altitude. Press the AP Key to engage the autopilot for maintaining the current altitude.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Vertical Speed Mode (VS) 1) Press the VS Key. The flight director is now activated (if not already active) and ‘VS’ is displayed in green in the Active Mode field and the Vertical Speed Bug will appear on the Vertical Speed Indicator. Pitch commands are given to manually maintain vertical speed. Press the AP Key to engage the autopilot for maintaining the current vertical speed.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Flight Level Change Mode (FLC) 1) 2) 3) Select the desired altitude by turning the ALT Knob to set the altitude in the Altitude Select box. This altitude must be selected first because Flight Level Change Mode will only fly toward a selected altitude. Press the FLC Key. The flight director is activated (if not already active) and ‘FLC’ is now displayed in green in the Active Mode field and the Airspeed Bug will appear on the Airspeed Indicator.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Go-Around Mode (GA) Glideslope (GS) Pressing the GA Button (not located on the MFD) engages the flight director in a wings level, 7 degree pitch up attitude. Go-Around Mode disengages the autopilot, and arms Altitude Hold Mode automatically. Subsequent autopilot engagement is also allowed. If the pitch attitude is changed manually (e.g with the CWS Button or the NOSE UP/NOSE DN keys), Pitch and Roll Hold modes will automatically be selected.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 6.6 ROLL AXIS MODES Roll Hold Mode (ROL) Mode annunciations for active roll axis modes are shown in green during normal operation.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Heading Select Mode (HDG) 1) 2) 3) Turn the HDG Knob to move the Heading Bug on the HSI to the desired heading. When the knob is turned, the Selected Heading box will appear and remain for three seconds after the knob stops moving. The selected heading will be displayed in the Selected Heading box. With the autopilot and/or flight director engaged, press the HDG Key. ‘HDG’ is now displayed in green in the Active Mode field.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Navigation Mode (GPS, VOR, LOC, or BC) Pressing the NAV Key activates the Navigation Mode. The Navigation Mode acquires and tracks the selected navigation receiver on the HSI (e.g. GPS, VOR or LOC). GPS roll steering commands are followed when the HSI is in GPS Mode, and creates roll steering commands from the Selected Course and deviation when the HSI is in VOR, LOC, or BC (backcourse) modes.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Approach Mode (GPS, VAPP or LOC) The Approach Mode acquires and tracks the selected navigation receiver on the HSI (GPS, VOR or LOC). This mode uses the selected navigation receiver deviation and desired course inputs to fly the approach. The Approach Mode provides greater sensitivity for VOR tracking than Navigation Mode, and allows the autopilot to fly an ILS approach with a glideslope.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 6.7 EXAMPLE PROCEDURES USING AFCS NOTE: The diagrams in the following examples are for instructional purposes only and may not be current. This section provides a scenario-based set of procedures showing various autopilot modes used during a flight. In this scenario, the aircraft departs Reid-Hillview Airport (KRHV) from runway 13L, enroute to Fresno Yosemite International Airport (KFAT).
SECTION 6 – AUTOMATIC FLIGHT CONTROL Departure 4) With the autopilot engaged in a climb, set Selected Heading to 070 degrees using the HDG Knob, then press the HDG Key. The autopilot turns the aircraft to the desired heading. 5) As the aircraft climbs to the selected altitude, the autopilot changes from Vertical Speed Mode to Altitude Hold Mode. This is annunciated by the green ‘ALT’ flashing for ten seconds.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Intercepting a VOR Radial 3) The system calculates the point at which the autopilot changes from Heading Mode to Navigation Mode. When the aircraft reaches this point, ‘VOR’ flashes green in the active mode field. The autopilot begins turning to intercept the selected course. 4) The autopilot continues the turn until the aircraft is established on the selected course.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Flying a Flight Plan / GPS Course 3) 1) The aircraft is currently tracking inbound on the 116 degree radial of Panoche VORTAC. Enter Panoche VORTAC (PXN) and Clovis VORTAC (CZQ) into the GPS flight plan, in preparation to intercept this leg. 2) With the flight plan activated, press the CDI Softkey to set the CDI to GPS. This cancels VOR Mode, and the autopilot loses the VOR signal.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Flight Level Change (Descent) 3) 1) In preparation for the approach to KFAT, set Selected Altitude to 3,000 feet using the ALT Knob. Press the FLC Key. ‘FLC’ is annunciated with the airspeed reference, which defaults to the current aircraft airspeed. Altitude Hold Mode is armed automatically. The current cruise speed of 142 knots will be used for the descent. 2) To allow the aircraft to descend, power must be reduced.
SECTION 6 – AUTOMATIC FLIGHT CONTROL ILS Approach Turn the HDG Knob to set the Heading Bug to comply with ATC vectors, as requested. 4) When cleared for the approach, press the APR Key. ‘LOC’ and ‘GS’ appear in white in the roll axis and pitch axis modes armed fields, respectively. The autopilot will calculate when to begin the turn to intercept the final approach course. 5) From this point, the autopilot flies the ILS.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Go-Around / Missed Approach 30 CZQ 27 24 4. 12 21 15 18 e 6-20 At the holding pattern, the pilot commences with the hold. To fly the hold using the Autopilot, the pilot sets Selected Heading using the HDG Knob and presses the HDG Key. The HDG Knob is used for the remainder of the hold to guide the aircraft. G 9 4) During the climb, set a desired hold altitude in the Selected Altitude Box by turning the ALT Knob.
SECTION 7 – NAVIGATION SECTION 7: NAVIGATION The following discussions pertain to the Multi Function Display, unless otherwise indicated. 7.1 NAVIGATION MAP PAGE Select the MAP Page Group 1) Turn the Large FMS Knob until ‘MAP’ is highlighted in the Page Group Window in the lower right of the MFD display. 2) Turn the Small FMS Knob to select the first MAP page (indicated by a solid rectangular icon).
SECTION 7 – NAVIGATION 3) Turn the Small FMS Knob to display a list of waypoints or airports. 4) Continue turning the Small FMS Knob to scroll through the list and highlight the desired waypoint or airport. 5) Press the ENT Key to confirm the selection. Press ENT again to activate a Direct-to. To Re-center the CDI to the Destination Waypoint Press the Direct-to ( ) Key, followed by pressing the ENT Key twice. If a missed approach point (MAP) is the current destination, the approach will be canceled.
SECTION 7 – NAVIGATION 7.3 AIRPORT INFORMATION a list is displayed from which to choose the desired location. 6) To remove the flashing cursor, press the FMS Knob. Access Runway Information 1) With the Airport Information Page displayed, press the FMS Knob to activate the cursor. 2) Turn the Large FMS Knob to place the cursor on the ‘RUNWAYS’ identifier field. 3) Turn the Small FMS Knob to display the next runway for the selected airport.
SECTION 7 – NAVIGATION 7.4 INTERSECTION INFORMATION 7.5 NDB INFORMATION Select the Intersection Information Page 1) Turn the Large FMS Knob to select the ‘WPT’ page group. 2) Turn the Small FMS Knob to select the second rectangular page icon. Figure 7-7 NDB Information Page Select the NDB Information Page 1) Turn the Large FMS Knob to select the ‘WPT’ page group.
SECTION 7 – NAVIGATION 7.6 VOR INFORMATION 7.7 USER WAYPOINT INFORMATION PAGE See the Flight Planning section for a discussion on creating and modifying user defined waypoints. 7.8 NEAREST AIRPORTS Figure 7-8 VOR Information Page Select the VOR Information Page 1) Turn the Large FMS Knob to select the ‘WPT’ page group. 2) Turn the Small FMS Knob to select the fourth rectangular page icon.
SECTION 7 – NAVIGATION Access Information on a Specific Airport 1) With the Nearest Airports Page displayed, press the APT Softkey to place the cursor in the ‘NEAREST AIRPORTS’ field. The first airport in the nearest airports list is highlighted. 2) Press the FMS Knob, then turn the Large FMS Knob to highlight the desired airport. 3) Press the FMS Knob to remove the flashing cursor. Access Runway Information for the Selected Airport 1) Bearing TO 2) Turn the Small FMS Knob to select the desired runway.
SECTION 7 – NAVIGATION 7.9 NEAREST INTERSECTIONS 7.10 NEAREST NDB Figure 7-12 Nearest NDB Page Figure 7-11 Nearest Intersections Page Select the Nearest Intersections Page 1) 2) Turn the Large FMS Knob to select the ‘NRST’ page group. Turn the Small FMS Knob to select the second rectangular page icon. View Information on the Nearest Intersection 1) 2) 3) Select the Nearest NDB Page 1) Turn the Large FMS Knob to select the ‘NRST’ page group.
SECTION 7 – NAVIGATION 7.11 NEAREST VOR View Information on the Nearest VOR Select the Nearest VOR Page 1) With the Nearest VOR Page displayed, press the VOR Softkey to place the cursor in the ‘NEAREST VOR’ box. 2) Turn either FMS Knob to select a VOR. 3) Press the FMS Knob to remove the flashing cursor. 1) Turn the Large FMS Knob to select the ‘NRST’ page group. 2) Turn the Small FMS Knob to select the fourth rectangular page icon.
SECTION 7 – NAVIGATION 7.12 NEAREST USER WAYPOINT 7.13 NEAREST FREQUENCIES Figure 7-15 Nearest Frequencies Page Figure 7-14 Nearest User Waypoints Page Select the Nearest User Waypoint Page 1) 2) Turn the Large FMS Knob to select the ‘NRST’ page group. Turn the Small FMS Knob to select the fifth rectangular page icon. Select a Nearest User Waypoint 1) 2) 3) With the Nearest User Waypoint Page displayed, press the FMS Knob to activate the cursor.
SECTION 7 – NAVIGATION 7.14 NEAREST AIRSPACES View Additional Details for a Listed Airspace 1) With the Nearest Airspace Page displayed, press the FMS Knob to activate the cursor. 2) Turn the Large FMS Knob to scroll through the list, highlighting the desired airspace. 3) Press the ALERTS Softkey to place the cursor in the ‘AIRSPACE ALERTS’ field. 4) Turn either FMS Knob to select the desired airspace. 5) Press the FMS Knob to remove the flashing cursor.
SECTION 8 – FLIGHT PLANNING SECTION 8: FLIGHT PLANNING 4) Repeat steps 2 and 3 until the desired name is entered. The following discussions pertain to the Multi Function Display, unless otherwise indicated. 5) Press the ENT Key. 6) Press the ENT Key a again to accept the new waypoint identifier. 7) The cursor is now in the ‘REFERENCE WAYPOINTS’ box. If desired, the waypoint can be defined by a reference waypoint.
SECTION 8 – FLIGHT PLANNING Create User Waypoints from the Navigation Map Page 1) With the Navigation Map Page displayed, push the Joystick to activate the panning function. The target pointer is displayed at the present aircraft position. 2) Move the Joystick to place the pointer at the desired position 3) Press the ENT Key. The User Waypoint Information Page is now displayed with the captured position. 4) Turn the FMS Knob to select a waypoint name.
SECTION 8 – FLIGHT PLANNING 8.4 ACTIVATE A FLIGHT PLAN LEG 1) From the Active Flight Plan Page, press the FMS Knob to activate the cursor and turn the Large FMS Knob to highlight the desired destination waypoint. 2) Press the ACT LEG Softkey (using MFD only). 3) Turn the Large FMS Knob to highlight ‘Delete Flight Plan’ and press the ENT Key. With ‘OK’ highlighted, press the ENT Key to deactivate the flight plan. This will not delete the stored flight plan, only the active flight plan.
SECTION 8 – FLIGHT PLANNING 8.7 CREATE A NEW FLIGHT PLAN 8) Create a New Flight Plan Using the MFD 1) Press the FPL Key and turn the Small FMS Knob to display the Flight Plan Catalog Page. 2) Press the NEW Softkey to display a blank flight plan page for the first empty storage location. Figure 8-10 Create FPL on MFD 3) Turn the Small FMS Knob to display the Waypoint Information Window. 4) Turn the Small FMS Knob to enter the first character of the identifier of the departure waypoint.
SECTION 8 – FLIGHT PLANNING 8.9 LOAD AN ARRIVAL See the Procedures section for a discussion on loading and activating arrival procedures. 8.10 LOAD AN APPROACH See the Procedures section for a discussion on loading and activating approach procedures. 8.11 REMOVE A DEPARTURE, ARRIVAL, OR APPROACH FROM A FLIGHT PLAN 1) With the Active or Stored Flight Plan Page displayed, press the FMS Knob to activate the cursor.
SECTION 8 – FLIGHT PLANNING 8.15 INVERT AND ACTIVATE A STORED FLIGHT PLAN 1) From the Flight Plan Catalog Page, press the FMS Knob to activate the cursor. 2) Turn the Large FMS Knob to highlight the desired flight plan. 3) Press the INVERT Softkey. ‘Invert and activate stored flight plan?’ will be displayed. 4) With ‘OK’ highlighted, press the ENT Key. The selected flight plan is now inverted and activated. The original flight plan remains intact in its flight plan catalog storage location.
SECTION 8 – FLIGHT PLANNING Starting WPT (already stored in memory), by number. Turn the Large FMS Knob to highlight the ‘LEG’ field and turn the Small FMS Knob to select the desired leg of the flight plan, or select ‘CUM’ to apply trip planning calculations to the entire flight plan. Selecting ‘FPL 00’ will display an active flight plan. If an active flight plan is selected, ‘REM’ will be an available option to display planning data for the remainder of the flight plan.
SECTION 8 – FLIGHT PLANNING 8.20 VERTICAL NAVIGATION (VNAV) PAGE 5) Press the ENT Key. The cursor is now positioned over the ‘Before’ and ‘After’ field. NOTE: An active flight plan or Direct-to must be entered in order to utilize VNAV. 6) Turn the Small FMS Knob to select whether the previously set distance is ‘Before’ or ‘After’ the endpoint. NOTE: VNAV is advisory only and cannot be coupled to the autopilot. 7) Press the ENT Key. The cursor is now placed over the VNAV profile endpoint field.
SECTION 8 – FLIGHT PLANNING 10) With the ‘TARGET ALTITUDE’ field highlighted, turn the FMS Knob to select the target altitude. If the selected altitude is above the current aircraft altitude, a profiled climb is created. If the selected altitude is below the current aircraft altitude, a profiled descent will be created. Figure 8-17 Approaching VNAV Profile Message (PFD) 11) Press the ENT Key. The cursor is now placed in the ‘TARGET VERTICAL SPEED’ field.
SECTION 8 – FLIGHT PLANNING Blank Page 8-10 Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN
SECTION 9 – PROCEDURES SECTION 9: PROCEDURES 9.1 ARRIVALS AND DEPARTURES Load and Activate a Departure Procedure 1) With the Navigation Map Page displayed, press the FPL Key. 2) Press the LD DP Softkey. If a flight plan is active, the departure airport will be displayed as the default. A list of available departures is also displayed. 3) If no flight plan is active, use the FMS Knob to enter the identifier of the desired airport. Press the ENT Key.
SECTION 9 – PROCEDURES 6) A second window is displayed listing available transitions for the arrival. Turn either FMS Knob to highlight the desired transition waypoint and press the ENT Key. Figure 9-4 Select Arrival Transition 7) A third window is displayed listing the available runways. Turn either FMS Knob to select the desired runway and press the ENT Key. 9.2 Not all approaches in the database are approved for GPS use.
SECTION 9 – PROCEDURES 7) Turn the Large FMS Knob to highlight ‘Activate?’ and press the ENT Key to activate the approach. Selecting ‘Load?’ will add the procedure to the flight plan without immediately using it for navigation guidance. Activate An Approach in the Active Flight Plan Figure 9-6 Selecting an Approach Procedure 5) Turn the FMS Knob to highlight the desired approach. Press the ENT Key. 6) The cursor will move to the TRANSITIONS field.
SECTION 9 – PROCEDURES Blank Page 9-4 Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN
SECTION 10 – HAZARD AVOIDANCE SECTION 10: HAZARD AVOIDANCE 10.2 STORMSCOPE® (OPTIONAL) WARNING: The Stormscope system is not intended to be used for hazardous thunderstorm penetration. Weather information on the G1000 MFD is approved for weather avoidance only. Refer to the WX-500 Pilot’s Guide for detailed operation. 10.1 CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1) With the Navigation Map Page displayed, press the MENU Key to display the Navigation Map Page Menu.
SECTION 10 – HAZARD AVOIDANCE At a map range of less than 25 nm, Stormscope lightning data is not displayed, but can still be present. The presence of Stormscope lightning data is indicated by the annunciation ‘LTNG < 25 nm’ in the upper right corner. Stormscope Page 1) Turn the Large FMS Knob until the Map Page group is selected. 2) Turn the Small FMS Knob until the Stormscope Page is selected. This is the third rectangular page icon.
SECTION 10 – HAZARD AVOIDANCE To change the viewing mode between 360˚ and 120˚: 1) Select the Stormscope Page. 2) Press the VIEW Softkey. The 360 and ARC softkeys are displayed. Press the 360 Softkey to display a 360˚ viewing area or press the ARC Softkey to display a 120˚ viewing area. 3) Press the CLEAR Softkey to remove all Stormscope lightning data from the display. 10.3 XM WEATHER (OPTIONAL) WARNING: XM Weather is not intended to be used for hazardous weather penetration.
SECTION 10 – HAZARD AVOIDANCE Displaying Weather on the Weather Data Link Page To select the Weather Data Link Page: 1) Turn the Large FMS Knob to select the Map Page Group. 2) Turn the Small FMS Knob to select the fourth rectangular page icon. 3) Press the available softkeys to select the desired XM weather product. 4) Press the LEGEND Softkey to view the legends for the selected products. If necessary, turn the FMS Knob to scroll through the list.
SECTION 10 – HAZARD AVOIDANCE CELL MOV – Pressing the CELL MOV Softkey shows storm cell movement by displaying an arrow. pointing in the direction of predicted movement. The display is updated every 12 minutes. SIG/AIR – Pressing the SIG/AIR Softkey shows SIGMET and AIRMET information. The display is updated every 12 minutes. METAR – Press the METAR Softkey to graphically display METARs. METARS are shown as colored flags at airports providing METAR reports. The display is updated every 12 minutes.
SECTION 10 – HAZARD AVOIDANCE • • • • • Surface Analysis Freezing Levels Winds Aloft County Warnings Cyclone Warnings Echo Top (Cloud Top and Echo Top Mutually Exclusive) Figure 10-10 Weather Product Symbols The XM Information Page in the AUX Page Group will display the weather products available for the current subscription. A green box by the weather product means that it is available.
SECTION 10 – HAZARD AVOIDANCE 10.4 TRAFFIC INFORMATION SERVICE (TIS) Traffic Advisory, aircraft is 400’ above & Traffic out of Traffic Mode descending, moving in the direction of the line range NOTE: If the G1000 is configured to use the optional Skywatch® Traffic Advisory System, TIS will not be available for use. NOTE: Traffic Information Service (TIS) is only available when the aircraft is within the service volume of a TIS capable terminal radar site.
SECTION 10 – HAZARD AVOIDANCE 10.5 SKYWATCH TRAFFIC ADVISORY SYSTEM (TAS)(OPTIONAL) Traffic Advisory, aircraft is 400’ below Traffic Mode Altitude Mode & climbing Traffic, Out of Range Refer to the SkyWatch pilot’s guide for a detailed discussion of the SkyWatch system. Displaying Traffic on the Traffic Map Page 1) Turn the Large FMS Knob to select the Map Page Group. 2) Turn the Small FMS Knob to select the second rectangular page icon. 3) Press the OPERATE Softkey to begin displaying traffic.
SECTION 10 – HAZARD AVOIDANCE 4) Traffic Advisory Non-Bearing Traffic Off Scale Traffic Advisories Banner Rotate the Joystick clockwise to display a larger area or rotate counter-clockwise to display a smaller area. Non-Threat Traffic Figure 10-13 TAS Traffic on Navigation Map 10.6 TERRAIN AND OBSTACLE PROXIMITY NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south.
SECTION 10 – HAZARD AVOIDANCE Unlighted Obstacle (Height is less than 1000’ AGL) Lighted Obstacle (Height is less than 1000’ AGL) Unlighted Obstacle (Height is greater than 1000’ AGL) Lighted Obstacle (Height is greater than 1000’ AGL) Figure 10-15 Obstacle Symbols Maximum elevation of topography presently displayed on-screen Minimum elevation of topography presently displayed on-screen Aircraft altitude Range of topography elevation presently displayed on-screen Ground elevation at present aircraft
SECTION 10 – HAZARD AVOIDANCE 10.7 TERRAIN AWARENESS & WARNING SYSTEM (TAWS) DISPLAY (OPTIONAL) NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south. NOTE: TAWS operation is only available when the G1000 is configured for a TAWS-B installation. Displaying Terrain on the TAWS Page 1) Turn the Large FMS Knob to select the Map Page Group. 2) Turn the Small FMS Knob to select the TAWS Page.
SECTION 10 – HAZARD AVOIDANCE Potential Impact Point Projected Flight Path 100' Threshold Unlighted Obstacle 1000' AGL Color Red Terrain/Obstacle Location Terrain/Obstacle at or within 100’ below current aircraft altitude. Yellow Terrain/Obstacle between 100’ and 1000’ below current aircraft altitude. Black Terrain/Obstacle is more than 1000’ below aircraft altitude. TAWS Inhibit Flying VFR into an area where unique terrain exists could cause the system to annunciate a nuisance alert.
SECTION 10 – HAZARD AVOIDANCE Manual System Test A system test is automatically performed at power-up. After sucessful completion of the test, “TAWS System Test, OK” will be heard. The system test may also be initiated manually, but only when the aircraft is on the ground. To manually verify proper operation of the aural and visual annunciations of the system, perform the following steps. 1) While the TAWS Page is displayed, press the MENU Key. 2) Turn the Small FMS Knob to select ‘Test TAWS’.
SECTION 10 – HAZARD AVOIDANCE Premature Descent Alert (PDA) Excessive Descent Rate Alert (EDR) A Premature Descent Alert is issued when the system detects that the aircraft is significantly below the normal approach path to a runway. The PDA alert mode functions only during descent to land. The purpose of the Excessive Descent Rate alert is to provide suitable alerts when the aircraft is determined to be closing (descending) upon terrain at an excessive speed.
SECTION 10 – HAZARD AVOIDANCE Unlighted Obstacle (Height is less than 1000’ AGL) Lighted Obstacle (Height is less than 1000’ AGL) Unlighted Obstacle (Height is greater than 1000’ AGL) Lighted Obstacle (Height is greater than 1000’ AGL) Potential Impact Points Figure 10-22 TAWS Symbols “Five-Hundred” Aural Alert Pop-up Alerts The purpose of the aural alert message “Five-hundred” is to provide an advisory alert to the aircrew that the aircraft is five-hundred feet above terrain.
SECTION 10 – HAZARD AVOIDANCE TAWS Alerts Summary The following table shows the possible TAWS alert types with corresponding annunciations and aural messages.
SECTION 10 – HAZARD AVOIDANCE The following system status annunciations may also be issued. PFD/MFD TAWS Page Annunciation MFD Pop-Up Alert Aural Message TAWS System Test Fail None “TAWS System Failure” TAWS Alerting is disabled None None No GPS position or excessively degraded GPS signal None “TAWS Not Available” “TAWS Available” will be heard when sufficient GPS signal is re-established.
SECTION 10 – HAZARD AVOIDANCE Blank Page 10-18 Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN
SECTION 11 – ABNORMAL OPERATION SECTION 11: ABNORMAL OPERATION 11.1 REVERSIONARY MODE Should a system detected failure occur in either display, the G1000 automatically enters Reversionary Mode. In Reversionary Mode, critical flight instrumentation is combined with engine instrumentation on the remaining display. Minimal navigation capability is available on the Reversionary Mode display.
SECTION 11 – ABNORMAL OPERATION 11.2 ABNORMAL COM OPERATION When a COM tuning failure is detected by the system, the emergency frequency (121.500 MHz) is automatically loaded into the active frequency field of the COM radio for which the tuning failure was detected. In the event of a dual display failure, the emergency frequency (121.500 MHz) automatically becomes the active frequency to the pilot through the pilot headset. 11.
SECTION 12 – ANNUNCIATIONS & ALERTS SECTION 12: ANNUNCIATIONS & ALERTS NOTE: The Airplane Flight Manual Supplement supersedes information found in this document. • System Annunciations: Typically, a large red ‘X’ appears in a window when a related LRU fails or detects invalid data. • Audio Alerting System: The G1000 system issues audio alert tones when specific system conditions are met. See the Alert Levels Definitions section for more information.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.1 ALERT LEVEL DEFINITIONS The G1000 Alerting System, as installed in Mooney M20M, M20R, and M20TN aircraft, uses one alert level. • MESSAGE ADVISORY: This level of alert provides general information to the pilot. A message advisory alert does not issue annunciations in the Annunciation Window. Instead, message advisory alerts only issue a flashing ADVISORY Softkey Annunciation, as shown in Figure 12-2.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.3 AFCS ALERTS System Status Field System Status Field The following alert annunciations appear in the AFCS System Status field on the PFD. Figure 12-3 AFCS System Status Field Condition Pitch Failure Annunciation Description Pitch axis control failure. AP is inoperative. Roll Failure Roll axis control failure. AP is inoperative.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.4 TAWS ALERTS Annunciations appear on the PFD and MFD. Pop-up alerts appear only on the MFD.
SECTION 12 – ANNUNCIATIONS & ALERTS TAWS System Status Annunciations PFD/MFD TAWS Page Annunciation MFD Pop-Up Alert Aural Message TAWS System Test Fail None “TAWS System Failure” TAWS Alerting is disabled None None No GPS position or excessively degraded GPS signal None “TAWS Not Available” “TAWS Available” will be heard when sufficient GPS signal is re-established. System Test in progress None None None “TAWS System Test OK” Alert Type None System Test pass 12.
SECTION 12 – ANNUNCIATIONS & ALERTS System Annunciation Comment Display system is not receiving airspeed input from air data computer. Display is not receiving altitude input from the air data computer. 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.
SECTION 12 – ANNUNCIATIONS & ALERTS Traffic Voice Alerts Voice Alert “Traffic” “Traffic Not Available” “Traffic, Traffic” “Traffic Advisory System Test Passed” “Traffic Advisory System Test Failed” Alert Trigger Played when a Traffic Advisory (TA) is issued (TIS system). Played when the traffic system fails or cannot communicate (TIS system). Played when a Traffic Advisory (TA) is issued (Skywatch TAS system). Played when the TAS system passes a pilot-initiated self test.
SECTION 12 – ANNUNCIATIONS & ALERTS A red ‘X’ may be the result of an LRU or an LRU function failure. The Figure 12-3 illustrates all possible flags and the responsible LRUs. GIA 63 Integrated Avionics Units GIA 63 Integrated Avionics Units GDC 74A Air Data Computer GRS 77 AHRS OR GMU 44 Magnetometer GEA 71 Engine Airframe Unit OR GIA 63 Integrated Avionics Unit GIA 63 Integrated Avionics Units GDC 74A Air Data Computer Figure 12-4 G1000 System Failure Annunciations 12.
SECTION 12 – ANNUNCIATIONS & ALERTS MFD & PFD Message Advisories Message DATA LOST – Pilot stored data was lost. Recheck settings. XTALK ERROR – A flight display crosstalk error has occurred. PFD1 SERVICE – PFD1 needs service. Return unit for repair. MFD1 SERVICE – MFD1 needs service. Return unit for repair. PFD1 CONFIG – PFD1 configuration error. Config service req’d. MFD1 CONFIG – MFD1 configuration error. Config service req’d. SW MISMATCH – GDU software mismatch. Xtalk is off.
SECTION 12 – ANNUNCIATIONS & ALERTS 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, the G1000 system should be 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.
SECTION 12 – ANNUNCIATIONS & ALERTS GMA 1347 Message Advisories Alerts Window Message GMA1 FAIL – GMA1 is inoperative. Comments The audio panel self-test has detected a failure. The audio panel is unavailable. The G1000 system should be serviced. GMA1 CONFIG – GMA1 configuration The audio panel configuration settings do not match backup configuration memory. error. Config service req’d. The G1000 system should be serviced. MANIFEST – GMA1 software The audio panel has incorrect software installed.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63 Message Advisories (Cont.) Alerts Window Message Comments MANIFEST – GIA1 software mismatch. Communication halted. The GIA1 and/or GIA 2 has incorrect software installed. The G1000 system should MANIFEST – GIA2 software mismatch. be serviced. Communication halted. COM1 TEMP – COM1 over temp. The system has detected an over temperature condition in COM1 and/or COM2. The Reducing transmitter power. transmitter will operate at reduced power.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63 Message Advisories (Cont.) Alerts Window Message Comments GPS1 SERVICE – GPS1 needs service. Return unit for repair. A failure has been detected in the GPS1 and/or GPS2 receiver. The receiver may still GPS2 SERVICE – GPS2 needs service. be available. The G1000 system should be serviced. Return unit for repair. NAV1 SERVICE – NAV1 needs service. Return unit for repair. A failure has been detected in the NAV1 and/or NAV2 receiver.
SECTION 12 – ANNUNCIATIONS & ALERTS GTX 33 Message Advisories Alerts Window Message XPDR1 CONFIG – XPDR1 config error. Config service req’d. MANIFEST – GTX1 software mismatch. Communication halted. BACKUP PATH – XPDR1 using backup data path. Comments The transponder configuration settings do not match those of backup configuration memory. The G1000 system should be serviced. The transponder has incorrect software installed. The G1000 system should be serviced.
SECTION 12 – ANNUNCIATIONS & ALERTS GMU 44 Message Advisories Alerts Window Message HDG FAULT – AHRS1 magnetometer fault has occurred. MANIFEST – GMU1 software mismatch. Communication halted. Comments A fault has occurred in the GMU 44. Heading is flagged as invalid. The AHRS uses GPS for backup mode operation. The G1000 system should be serviced. The GMU 44 has incorrect software installed. The G1000 system should be serviced.
SECTION 12 – ANNUNCIATIONS & ALERTS Miscellaneous Message Advisories Alerts Window Message Comments FPL WPT LOCK – Flight plan waypoint Upon power-up, the G1000 system detects that a stored flight plan waypoint is is locked. locked. This occurs when an aviation database update eliminates an obsolete waypoint. The flight plan cannot find the specified waypoint and flags this message. This can also occur with user waypoints in a flight plan that is deleted.
SECTION 12 – ANNUNCIATIONS & ALERTS Miscellaneous Message Advisories (Cont.) Alerts Window Message Comments ARSPC NEAR – Airspace near – less Special use airspace is within 2 nm of the aircraft position. than 2 nm. LEG UNSMOOTH – Flight plan leg will The approaching flight plan waypoints are too close to allow for smooth turns. not be smooth. Prepare for steep turns ahead and expect noticeable course deviations.
SECTION 12 – ANNUNCIATIONS & ALERTS Blank Page 12-18 Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN
INDEX A Abnormal COM operation 11-2 Activate a flight plan 8-3 Active flight plan 8-2 ADF 1-5, 1-6, 4-3 ADVISORY 12-1 Advisory alerts 12-2 AFCS 6-1, 6-3, 6-5, 6-7, 6-8, 6-10, 6-12, 6-13, 6-14, 12-3 Age 10-6 AHRS 12-14 Aircraft alerts 12-2 AIRMET 10-5 Airport frequency 7-6 Airport information 7-3 Airspace alerts 7-10 Airspeed indicator 2-3 Airspeed trend vector 2-3 Alerting System 12-1 Alerts 12-1 Alert levels 12-2 Alert Pop-Up 10-15 Altimeter 2-4 Altitude Alerting 2-4 Altitude hold 1-4, 6-4 – 6-9, 6-11, 6-15,
INDEX H M P Hazard Displays 11-2 HDG key 6-11, 6-15, 6-19 Heading hold 6-10 Heading indication 2-7 Heading Select 1-3, 1-4, 6-10, 6-11 Heading Select Mode 6-11 Headset(s) 5-3 Hijack code 4-5 Horizontal situation indicator 2-6 HSI 2-6 Hurricanes 10-5 Manual Electric Trim 6-1 MAP 7-1 Map panning 10-5 Marker beacon 2-5 Messages 12-1 Message advisories 12-2, 12-9 – 12-17 MET 6-1, 6-3, 12-3 METAR 10-3, 10-5 MFD 1-1, 4-4 Military interceptor operations code 4-5 Missed Approach 6-20 Mistrim 12-3 MKR/MUTE 5-2 M
INDEX System message advisories 12-8 T TA 10-7, 12-7 TAF 10-3 TAS 10-8, 10-9, 12-7, 12-14 TAWS 10-11, 10-12, 10-13, 10-15, 10-16, 10-17, 12-4, 12-5 TAWS-B 10-11 TAWS system test 10-13 Terrain 10-9, 10-11, 10-17, 11-2, 12-10, 10-15 TIS 10-7, 12-7 Tornado 10-5 Traffic advisory 10-7, 10-8, 10-9, 10-17, 12-7 Traffic map page 10-7, 10-8, 10-9, 10-15 Transponder 4-5 Transponder Status bar 4-5 Trim 3-2 Tropical storms 10-5 TX 4-3 Weather product symbol 10-5 Weather product symbols 10-6 Weather warnings 10-5 Wind d
INDEX Blank Page Index-4 Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN
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: 44/0870.8501241 f: 44/0870.8501251 Garmin Corporation No. 68, Jangshu 2nd Road Shijr, Taipei County, Taiwan p: 886/2.2642.9199 f: 886/2.2642.9099 www.garmin.com 190-00450-02 Rev. D © 2004, 2006 Garmin Ltd.
