G1000 TM cockpit reference guide for the Cessna Nav III
Copyright © 2004, 2005 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software versions 0394.03 or later for Cessna 172R aircraft, 0395.04 or later for Cessna 172S aircraft, 0371.08 or later for normally aspirated Cessna 182 aircraft, 0372.07 or later for turbocharged Cessna 182 aircraft, 0373.04 or later for normally aspirated Cessna 206 aircraft, and 0374.04 or later for turbocharged Cessna 206 aircraft.
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. 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, & 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 Cessna Nav III 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 190-00384-03 (Rev. A) Change Summary Added XM Radio and XM Weather Added ADF capability Added DME capability Added BRG1/BRG2 pointers Added dual audio panel operation Added C172 parameters Changed Airspeed Trend Vector Changed Altitude Trend Vector Added Checklist capability Added Flight ID capability 190-00384-03 (Rev. B) Updated system software numbers 190-00384-04 (Rev.
TABLE OF CONTENTS SECTION 1: SYSTEM OVERVIEW.................................... 1-1 1.1 1.2 1.3 1.4 1.5 1.6 PFD/MFD Controls................................................... 1-2 PFD Softkeys............................................................ 1-4 MFD Softkeys .......................................................... 1-6 MFD Page Groups ................................................... 1-8 Backlighting .............................................................
TABLE OF CONTENTS 7.9 Nearest Intersections ............................................ 7-6 Select the Nearest Intersections Page........................... 7-6 View Information on the Nearest Intersection .............. 7-7 7.10 Nearest NDB ............................................................ 7-7 Select the Nearest NDB Page ....................................... 7-7 Access Information on a Specific NDB .......................... 7-7 7.11 Nearest VOR ................................................
TABLE OF CONTENTS SECTION 11: ABNORMAL OPERATION ..................... 11-1 11.1 Reversionary Mode .............................................. 11-1 11.2 Abnormal COM Operation .................................. 11-2 11.3 Unusual Attitudes ................................................. 11-2 SECTION 12: ANNUNCIATIONS & ALERTS .............. 12-1 12.1 Alert Level Definitions ........................................ 12-2 12.2 NAV III Aircraft Alerts ..........................................
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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.
SECTION 1 SYSTEM OVERVIEW 1.
SECTION 1 SYSTEM OVERVIEW (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. Press to toggle the tuning cursor (light blue box) between the NAV1 and NAV2 fields.
SECTION 1 SYSTEM OVERVIEW 1.2 PFD SOFTKEYS INSET Softkey ON Softkey OFF OFF DCLTR TRAFFIC TOPO (optional) (optional) (optional) TERRAIN STRMSCP NEXRAD XM LTNG BACK ALERTS (optional) INSET PFD OBS CDI DME XPDR IDENT TMR/REF NRST ALERTS Figure 1-2 PFD Top Level Softkeys INSET – Press to display the Inset Map in the lower left corner of the PFD. OFF – Press to remove the Inset Map DCLTR (3) – Press momentarily to select the desired amount of map detail.
SECTION 1 SYSTEM OVERVIEW PFD (optional) METRIC DFLTS DME BRG1 BRG2 STD BARO BACK ALERTS Press the DFLTS softkey to change the PFD metric values to standard Press the STD BARO or BACK softkeys to return to the top level softkeys Figure 1-4 PFD Softkey Flow Chart – 2 BRG2 (bearing) – Press to cycle through the following Nav sources, making the pointer the indicator for the corresponding source and displaying the appropriate information.
SECTION 1 SYSTEM OVERVIEW (optional) CDI OBS XPDR DME TMR/REF IDENT NRST ALERTS GPS VOR1 Press the BACK softkey to return to the top level softkeys VOR2 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 1-5 PFD Softkey Flow Chart – 3 IDENT – Press to provide special aircraft position identification to Air Traffic Control (ATC). BKSP – Press to remove numbers entered one at a time.
SECTION 1 SYSTEM OVERVIEW ENGINE DCLTR MAP CHKLIST (optional) DCLTR-1 ENGINE LEAN SYSTEM BACK DCLTR-2 DCLTR-3 Press the BACK softkey on this level to return to the top softkey level ENGINE LEAN SYSTEM RST USED BACK TERRAIN TOPO TRAFFIC BACK Press the ENGINE or BACK softkey on any level to return to the default page level ENGINE LEAN SYSTEM CYL SLCT ASSIST BACK The DONE softkey changes to UNDO when the checklist item is already checked ENGINE DONE EXIT EMERGCY CLR ENGINE MAP
SECTION 1 SYSTEM OVERVIEW 1.4 MFD PAGE GROUPS 1. Turn the large FMS knob until the desired page group is selected. 2. Turn the small FMS knob to select pages within the group. See Figure 1-7. Nearest Group Auxiliary Page Group Number of Pages in Current Group Waypoint Page Group Map Page Group Figure 1-7 Page Group Icon 1.5 Selected Page BACKLIGHTING To manually adjust the backlight for the PFD and MFD: 1-8 1. Press the MENU key on the PFD to display the PFD Setup Menu window. 2.
SECTION 2 FLIGHT INSTRUMENTS SECTION 2: FLIGHT INSTRUMENTS 1 16 15 14 13 2 12 11 3 10 4 9 8 5 7 6 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 Indicato
SECTION 2 FLIGHT INSTRUMENTS 11 1 10 9 2 8 3 7 4 5 6 1 Traffic Annunciation 7 Alerts Window 2 Selected Heading Box 8 Selected Course Box 3 Inset Map 9 Annunciation Window 4 BRG1 Information Window 10 Vertical Deviation/Glideslope Indicator 5 DME Information Window 11 Marker Beacon Annunciation 6 BRG2 Information Window 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 Wi
SECTION 2 FLIGHT INSTRUMENTS 2.1 AIRSPEED INDICATOR Actual Airspeed Vspeed References Vspeed References Vspeeds are set using the TMR/REF softkey. Glide, Vr, Vx and Vy are shown on the References window. When active (ON), the Vspeeds are displayed at their respective locations to the right of the airspeed scale. 2.
SECTION 2 FLIGHT INSTRUMENTS 2.3 ALTIMETER 2.4 Altitude Reference Box The Vertical Deviation/Glideslope Indicator appears when an ILS is tuned in the active NAV field. 2.5 Altitude Trend Vector VERTICAL DEVIATION/GLIDESLOPE INDICATOR MARKER BEACON ANNUNCIATIONS Current Altitude Marker Beacon Annunciation Altitude Reference Bug Barometric Setting Box Figure 2-7 Altimeter Vertical Deviation/Glideslope Indicator Altitude Reference Bug The Altitude Reference Bug can be set to any desired altitude.
SECTION 2 FLIGHT INSTRUMENTS 2.6 VERTICAL SPEED INDICATOR 14 13 1 Vertical Speed Pointer 12 2 11 3 10 4 9 8 5 7 6 Figure 2-9 Vertical Speed Indicator 2.7 HORIZONTAL SITUATION INDICATOR (HSI) 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 FLIGHT INSTRUMENTS Turn Rate Indicator and Heading Trend Vector Each tick mark is at 9 (half standard rate tick mark) and 18 (standard rate tick mark) degrees to the left and right of the lubber line. A wide magenta line displays the current turn rate, up to 24 degrees. A magenta arrowhead appears at 25 degrees. This trend vector provides the pilot with a prediction of what the heading will be in 6 seconds at the present turn rate. and BRG2 softkeys. The BRG1 pointer is a single line pointer.
SECTION 2 FLIGHT INSTRUMENTS DME Radio (optional) To display the DME Information Window, press the PFD softkey followed by the DME softkey. Figure 2-17 DME Information Window Navigation Source To change between CDI 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.
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SECTION 3 – ENGINE INDICATION SYSTEM (EIS) SECTION 3: ENGINE INDICATION SYSTEM (EIS) 3.1 3.2 LEAN ENGINE DISPLAY Manifold Pressure Gauge ENGINE DISPLAY In all cases green indicates normal operation, yellow indicates caution, and red indicates warning. Pressing the ENGINE softkey makes available the LEAN and SYSTEM softkeys which in turn provide access to the Lean Page and the System Page, respectively.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3.3 ENGINE SYSTEM DISPLAY If desired, press the RST USED (Reset Used) softkey to reset the amount of fuel used to zero. NOTE: Fuel calculations do not use the aircraft fuel quantity indicators, and are calculated from the last time the fuel was reset.
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 Multi-Function Display in the same locations.
SECTION 4 – NAV/COM & TRANSPONDER Standby NAV Frequency Field Tuning Box Selected NAV Frequency Navigation Status Window Selected COM Frequency Figure 4-2 Frequency Fields Active NAV Frequency Field 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 • TX – When a COM radio is keyed, a white TX indication appears to the right of the corresponding COM frequency. • ID – When the Morse code identifier is ON for a NAV radio, a white ID indication appears to the left of the corresponding active NAV frequency. The Morse code identifier can be heard if the corresponding NAV radio is selected on the audio panel. 4.5 DME Radio (optional) The Tuning window is displayed by pressing the DME softkey.
SECTION 4 – NAV/COM & TRANSPONDER 4.6 FREQUENCY AUTO-TUNING Auto-tuning on the PFD 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 4-9 Nearest Airports Window (PFD) 1. Press the NRST softkey to display the Nearest Airports Window. 2. Turn either FMS knob to highlight the desired frequency. 3.
SECTION 4 – NAV/COM & TRANSPONDER Following is a list of important codes: • 1200 – VFR code in the U.S. (please refer to the ICAO standards for VFR codes in other countries). • 7000 – VFR code commonly used in Europe (please refer to the ICAO standards). • 7500 – Hijack code. • 7600 – Loss of communication code. • 7700 – Emergency code. • 7777 – Military interceptor operations code (NEVER ENTER THIS CODE). • 0000 – Code for military use (in the U.S.).
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SECTION 5 – AUDIO PANEL SECTION 5: AUDIO PANEL Transmitters Transceiver Audio Disabled Passenger Address Speaker Marker Beacon/Mute Marker Beacon Signal Sensitivity Aircraft Navigation Radio Audio (Optional, disabled if ADF and/or DME are not installed) Aircraft Navigation Radio Audio Disabled Manual Squelch Digital Recording Playback ICS Isolation VOL/SQ VOL Annunciation SQ Annunciation Reversionary Mode Figure 5-1 Front Panel Controls Garmin G1000 Cockpit Reference Guide for the Cessna Nav
SECTION 5 – AUDIO PANEL 5.1 COM RADIO SELECTION Marker Beacon Signal Sensitivity 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. Figure 5-4 Marker Beacon 5.
SECTION 5 – AUDIO PANEL 5.5 INTERCOM SQUELCH CONTROL Select manual squelch for intercom audio by pressing the MAN SQ key to light the annunciator. Figure 5-5 Navigation Radios 5.4 INTERCOM SYSTEM (ICS) ISOLATION Pressing the small VOL/SQ knob now toggles between volume and squelch adjustment by lighting VOL or SQ respectively. Press the PILOT and/or COPLT key to select the desired mode as shown in Table 5-1.
SECTION 5 – AUDIO PANEL 5.6 DIGITAL CLEARANCE RECORDER WITH PLAYBACK CAPABILITY Each reception of primary active COM audio is automatically recorded in a memory block. When the next transmission is received, it is recorded in the next memory block, and so on. Once the 2.5 minutes of recording time has been reached, the recorder begins recording over the stored memory blocks, starting from the oldest block. Powering off the unit automatically clears all recorded blocks.
SECTION 6 – AUTOMATIC FLIGHT CONTROL SECTION 6: AUTOMATIC FLIGHT CONTROL Refer to the pilot’s guide for the installed autopilot system.
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SECTION 7 – NAVIGATION SECTION 7: NAVIGATION 7.2 DIRECT-TO NAVIGATION Direct-to Navigation from the MFD 7.1 NAVIGATION MAP PAGE Select the MAP Page Group 1. 2. 3. Turn the large FMS knob until MAP is highlighted in the page group window in the lower right of the MFD display. Identifier Facility Name City Nearest Airport Flight Plan Field Map Orientation Map of the Selected Waypoint Turn the small FMS knob to select the first MAP page (indicated by a solid rectangular icon).
SECTION 7 – NAVIGATION 4. 5. Continue turning the small FMS knob to scroll through the list and highlight the desired waypoint or airport. Press the ENT key to confirm the selection. Press ENT again to activate a Direct-to. To re-center the CDI (HSI) needle to the same destination waypoint: 1. ) key, followed by Press the Direct-to ( pressing the ENT key twice. NOTE: If a missed approach point (MAP) is the current destination, the approach will be canceled.
SECTION 7 – NAVIGATION 7.3 AIRPORT INFORMATION 7. To remove the flashing cursor, press the FMS knob. Access Runway Information 1. Press the FMS knob to activate the cursor. 2. Turn the large FMS knob to place the cursor on the Runways field. 3. Turn the small FMS knob to display the next runway for the selected airport. 4. Continue turning the small FMS knob to select the desired runway. 5. To remove the flashing cursor, press the FMS knob.
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 Figure 7-6 Intersection Information Page Access Information on an Intersection 1. 2. 3. With the Intersection Information Page displayed, press the FMS knob to activate the cursor.
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 Runway Information for the Selected Airport 2. Press the ENT key to display airport information. Press the ENT key again (cursor is on ‘BACK’) to return to the list. 1. Press the RNWY softkey located at the bottom of the display. 3. 2. Turn the small FMS knob to select the desired runway. Load an Airport COM Frequency into the Active COM 1. Turn the large FMS knob to place the cursor on the desired airport frequency shown in the window.
SECTION 7 – NAVIGATION 2. Turn the small FMS knob to select the second rectangular page icon. NOTE: The ADF cannot be auto-tuned from this page. View Information on the Nearest Intersection 1. 2. Press the FMS knob to activate the cursor. Turn either FMS knob to select the desired intersection. Press the ENT key. 7.10 NEAREST NDB 7.11 NEAREST VOR Select the Nearest VOR Page 1. Turn the large FMS knob to select the NRST page group. 2.
SECTION 7 – NAVIGATION Select and Load a VOR Frequency 1. With the Nearest VOR Page selected, press the FREQ softkey to highlight the VOR frequency for the selected VOR. 2. Press the ENT key. The selected VOR frequency is placed in the NAV standby frequency field. OR Press the MENU key. Select the Select Frequency Window option and press the ENT key. Press the ENT key again when the frequency field is highlighted to place the selected VOR frequency in the NAV standby field.
SECTION 7 – NAVIGATION Select and Load the Nearest ARTCC, FSS, or Weather Frequency 1. With the Nearest Frequencies Page selected, press the ARTCC, FSS, or Wx softkey. 2. Turn the large FMS knob to select the frequency. 3. Press the ENT key to load the frequency into the ‘COM’ frequency standby field. 7.14 NEAREST AIRSPACES • If the aircraft is within two nautical miles of an airspace and the current course takes the aircraft inside, ‘Ahead < 2 nm’ is displayed.
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SECTION 8 – FLIGHT PLANNING SECTION 8: FLIGHT PLANNING 8.1 3. Turn the large FMS knob to highlight the latitude/longitude field or the Reference Waypoints field, depending on how the waypoint is to be defined. 4. Turn the FMS knobs to enter the position coordinates or the radial and distance from the reference waypoint. 5. Press the ENT key to accept the new waypoint. 6. Press the FMS knob to remove the flashing cursor. USER DEFINED WAYPOINTS Create User Waypoints from the Navigation Map Page 1.
SECTION 8 – FLIGHT PLANNING Modify a User Waypoint 1. With the User Waypoint Information Page displayed, press the FMS knob to activate the cursor. 2. Turn the large FMS knob to move the cursor to the desired field and turn the small FMS knob to make changes. 3. Press the ENT key to accept the changes. 4. Press the FMS knob to remove the flashing cursor. Figure 8-3 Active Flight Plan Window on the PFD 8.3 1.
SECTION 8 – FLIGHT PLANNING 2. Press the ACT LEG softkey (using MFD only). OR 3. 4. Press the MENU key, select the ‘Activate Leg’ option from the page menu and press the ENT key. This step must be used when activating a leg from the PFD. With ‘Activate’ highlighted, press the ENT key. 8.6 INVERT ACTIVE FLIGHT PLAN 1. From the Active Flight Plan Page, press the MENU key to display the Page Menu. 2. Turn the large FMS knob to highlight ‘Invert Flight Plan’ and press the ENT key.
SECTION 8 – FLIGHT PLANNING Figure 8-10 Create FPL on MFD 3. Turn the small FMS knob to display the Waypoint Information Page. Turn the small FMS knob to enter the first character of the identifier of the departure waypoint. Turn the large FMS knob to move the cursor to the next character field. Repeat using the FMS knobs until the desired identifier has been entered. 1. Press the FPL key and press the small FMS knob to activate the cursor. 2.
SECTION 8 – FLIGHT PLANNING 8.11 REMOVE A DEPARTURE, ARRIVAL, OR APPROACH FROM A FLIGHT PLAN 1. 2. 3. With the Active or Stored Flight Plan Page displayed, press the small FMS knob to activate the cursor. Turn the large FMS knob to highlight the title for the approach, departure or arrival to be deleted. Titles appear in white directly above the procedure’s waypoints. Press the CLR key to display a confirmation window. With ‘OK’ highlighted, press the ENT key to remove the selected procedure. 8.
SECTION 8 – FLIGHT PLANNING 3. 4. Turn the large FMS knob to highlight ‘Invert Flight Plan’ and press the ENT key. The original flight plan remains intact in its flight plan catalog storage location. 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. With ‘OK’ highlighted, press the ENT key to invert the flight plan. 4. A ‘Delete flight plan?’ confirmation window is displayed.
SECTION 8 – FLIGHT PLANNING 3. The current page mode is displayed at the top of the page: ‘AUTOMATIC’ or ‘MANUAL’. To change the page mode, press the AUTO or MANUAL softkey. Figure 8-16 Trip Planning Page 4. 5. For Direct-to planning, press the WPTS softkey and verify that the ‘from’ waypoint field indicates P.POS (present position). If necessary, press the MENU key and select ‘Set WPT to Present Position’ to display P.POS. Press the ENT key and the flashing cursor moves to the ‘to’ waypoint field.
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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 knobs to enter the identifier of the desired airport. Press the ENT key. 4.
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. 9.2 Load and/or Activate an Approach Procedure 1. With the Navigation Map Page displayed, press the FPL key. 2. Press the LD APR softkey. If a flight plan is active, the destination airport will be displayed as the default. A list of available approaches is also displayed. 3.
SECTION 9 – PROCEDURES Figure 9-7 Selecting an Approach Transition 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 1. With the Navigation Map Page displayed, press the PROC key. 2. Turn the large FMS knob to highlight ‘ACTIVATE APPROACH’. 3. Press the ENT key.
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SECTION 10 – HAZARD AVOIDANCE SECTION 10: HAZARD AVOIDANCE 10.2 STORMSCOPE® (OPTIONAL) WARNING: Use of the Stormscope system for hazardous thunderstorm penetration is prohibited. Weather information on the G1000 MFD is approved for weather avoidance only. Refer to the WX-500 Pilot’s Guide for a more detailed discussion on 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. 2. Turn the small FMS knob until the Stormscope Page is selected. This is the third rectangular page icon. Figure 10-5 Lightning Display Range Annunciation To select ‘cell’ or ‘strike’ as the Stormscope lightning mode: 1.
SECTION 10 – HAZARD AVOIDANCE 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. Press the CLEAR softkey to remove all Stormscope lightning data from the display. 10.3 XM WEATHER (SERVICE OPTIONAL) WARNING: Use of XM weather for hazardous weather penetration is prohibited. Weather information provided by XM Radio Service is approved only for weather avoidance, not penetration. 1.
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 either 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. From within the AUX - XM INFORMATION page, the pilot may switch to the AUX - XM RADIO by pressing the RADIO softkey.
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: Traffic Information Service (TIS) is only available when the aircraft is within the service volume of a TIS capable terminal radar site. NOTE: If the G1000 is configured to use a Traffic Advisory System (TAS), TIS will not be available for use. Displaying Traffic on the Traffic Map Page 1.
SECTION 10 – HAZARD AVOIDANCE 10.5 TRAFFIC ADVISORY SYSTEM (TAS) (OPTIONAL) Refer to the Honeywell KTA 870 pilot’s guide for a detailed discussion of the KTA 870 system. System Self Test 1. Set the range to 2/6 nm. 2. Press the STANDBY softkey. 3. Press the TEST softkey. 4. Self test will take approximately eight seconds to complete. When completed sucessfully, traffic symbols will be displayed as shown in Figure 10-12 and a voice alert “TAS System Test OK” will be heard.
SECTION 10 – HAZARD AVOIDANCE Displaying Traffic on the Navigation Map 1. Ensure the KTA 870 system is operating. With the Navigation Map displayed, press the MAP softkey. 2. Press the TRAFFIC softkey. Traffic will now be displayed on the map. Traffic Advisory Non-Bearing Traffic Off Scale Traffic Advisories Banner 2. Turn the small FMS knob to select the last rectangular page icon. 3. If desired, press the VIEW softkey to access the ARC and 360 softkeys.
SECTION 10 – HAZARD AVOIDANCE Displaying Terrain and Obstacles on the Navigation Map 1. With the Navigation Map displayed, press the MAP softkey. 2. Press the TERRAIN softkey. Terrain and obstacle proximity will now be displayed on the map.
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 Cessna aircraft Pilot’s Operating Handbook (POH) supersedes information found in this document. The G1000 Alerting System conveys alerts to the pilot using a combination of the following items: • Annunciation Window: The Annunciation window displays abbreviated annunciation text. Text color is based on alert levels described later in the Alert Levels Definitions section.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.1 ALERT LEVEL DEFINITIONS The G1000 Alerting System, as installed in Cessna Nav III aircraft, uses three alert levels. • WARNING: This level of alert requires immediate pilot attention. A warning alert is accompanied by an annunciation in the Annunciation window. Warning text appearing in the Annunciation window is RED. A warning alert is also accompanied by a flashing WARNING softkey annunciation, as shown in Figure 12-2.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.2 NAV III AIRCRAFT ALERTS The following alerts are configured specifically for the Cessna Nav III aircraft. See the Cessna Pilot’s Operating Handbook (POH) for information regarding pilot responses. Voice Alerts The following voice alerts can be configured for ‘Male’ or ‘Female’ gender by using the Aux System Setup Page on the MFD. Voice Alert “Traffic” “Traffic Not Available” Alert Trigger Played when a Traffic Advisory (TA) is issued.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.3 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 POH for additional information regarding pilot responses to these annunciations. System Annunciation Comment Attitude and Heading Reference System is aligning. Display system is not receiving attitude information from the AHRS.
SECTION 12 – ANNUNCIATIONS & ALERTS System Annunciation Comment 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. AHRS operation may be degraded if GPS signals are not present (see AFMS).
SECTION 12 – ANNUNCIATIONS & ALERTS A red ‘X’ may be the result of an LRU or an LRU function failure. The Figure 12-5 illustrates all possible flags and the responsible LRUs. 12.4 G1000 SYSTEM MESSAGE ADVISORIES This section describes various G1000 system message advisories. Certain messages are issued due to an LRU or an LRU function failure. Such messages are normally accompanied by a corresponding red ‘X’ annunciation as shown previously in the G1000 System Annunciation section.
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 required. MFD1 CONFIG – MFD1 configuration error. Config service required. 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 required. 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 – Transponder 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 – A 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 and Special use airspace is near and ahead of the aircraft position. ahead. 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.
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INDEX A Abnormal COM operation 11-2 Activate a flight plan 8-2 Active flight plan 8-2 ADF 1-4, 1-5, 5-2 Age 10-6 AHRS 12-12 Aircraft alerts 12-3 AIRMET 10-5 Airport frequency 7-6 Airport information 7-3 Airspace alerts 7-9 Airspeed indicator 2-3 Airspeed trend vector 2-3 Alerting system 12-1 Alerts 12-1 Alert levels 12-2 Altitude mode 10-8 Altitude reference bug 2-4 Altitude trend vector 2-4 Altitude volume 10-8 ALT knob 1-3 Approaches 9-2 Approach activation 4-4 Approach markers Signal augmentation 5-2 Arriv
INDEX O HDG 1-2 NAV 1-2 NAV VOL/ID 1-2 Lightning 1-4, 1-7, 10-2, 10-3, 10-4 Load approach 8-4 Load a VOR frequency 7-8 Load departure 8-4 Load the frequency for a controlling agency 7-9 Load the nearest ARTCC frequency 7-9 Loss of communication code 4-5 Page group icon 1-8 PFD 1-1, 4-1, 4-4 PLAY key 5-4 PROC key 1-3 Terrain 10-9, 10-10, 12-8 Terrain proximity 10-9 TIS 1-4, 10-7, 12-15 Tornado 10-5 Traffic advisory 10-7, 10-8, 10-9, 12-3 Traffic map page 10-7, 10-8, 10-9, 10-10 Transponder 4-4 Transponder
Garmin G1000 Cockpit Reference Guide for the Cessna Nav III
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 © 2004, 2005 Garmin Ltd.
