Garmin G1000 Pilot’s Guide for the Diamond DA62

WARNING: Do not use outdated database information. Databases used in the G1000 system must be updated regularly in order to ensure that the information remains current. Pilots using any outdated database do so entirely at their own risk. WARNING: Do not use basemap (land and water data) information for primary navigation. Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness. WARNING: Traffic information shown on the G1000 is provided as an aid in visually acquiring traffic. Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic. WARNING: Use of the Lightning Detection System is not intended for hazardous weather penetration (thunderstorm penetration). Lightning Detection System information, as displayed on the G1000, is to be used only for weather avoidance, not penetration. WARNING: XM Weather should not be used for hazardous weather penetration. Weather information provided by the GDL 69A is approved only for weather avoidance, not penetration. 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. Garmin G1000 Pilot’s Guide for the Diamond DA62 190-01895-00 Rev. A ii WARNINGS, CAUTIONS, AND NOTES WARNING: The Garmin G1000, as installed in this aircraft, has a very high degree of functional integrity. However, the pilot must recognize that providing monitoring and/or self-test capability for all conceivable system failures is not practical. Although unlikely, it may be possible for erroneous operation to occur without a fault indication shown by the G1000. It is thus the responsibility of the pilot to detect such an occurrence by means of cross-checking with all redundant or correlated information available in the cockpit. WARNING: For safety reasons, G1000 operational procedures must be learned on the ground. WARNING: The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment. Portions of the Garmin G1000 utilize GPS as a precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the G1000 can be misused or misinterpreted and, therefore, become unsafe. WARNING: To reduce the risk of unsafe operation, carefully review and understand all aspects of the G1000 Pilot’s Guide documentation and the Airplane Flight Manual. 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. For safety purposes, always resolve any discrepancies before continuing navigation. WARNING: The illustrations in this guide are only examples. Never use the G1000 to attempt to penetrate a thunderstorm. Both the FAA Advisory Circular, Subject: Thunderstorms, and the Aeronautical Information Manual (AIM) recommend avoiding “by at least 20 miles any thunderstorm identified as severe or giving an intense radar echo.” WARNING: Lamp(s) inside this product may contain mercury (HG) and must be recycled or disposed of according to local, state, or federal laws. For more information, refer to our website at www.garmin.com/ aboutGarmin/environment/disposal.jsp. WARNING : Because of variation in the earth’s magnetic field, operating the G1000 within the following areas could result in loss of reliable attitude and heading indications. North of 72° North latitude at all longitudes; South of 70° South latitude at all longitudes; North of 65° North latitude between longitude 75° W and 120° W. (Northern Canada); North of 70° North latitude between longitude 70° W and 128° W. (Northern Canada); North of 70° North latitude between longitude 85° E and 114° E. (Northern Russia); South of 55° South latitude between longitude 120° E and 165° E. (Region south of Australia and New Zealand) 190-01895-00 Rev. A Garmin G1000 Pilot’s Guide for the Diamond DA62 iii WARNINGS, CAUTIONS, AND NOTES WARNING: Do not use GPS to navigate to any active waypoint identified as a ‘NON WGS84 WPT’ by a system message. ‘NON WGS84 WPT’ waypoints are derived from an unknown map reference datum that may be incompatible with the map reference datum used by GPS (known as WGS84) and may be positioned in error as displayed. WARNING: Do not use a QFE altimeter setting with this system. System functions will not operate properly with a QFE altimeter setting. Use only a QNH altimeter setting for height above mean sea level, or the standard pressure setting, as applicable. CAUTION: The PFD and MFD displays use a lens coated with a special anti-reflective coating that is very sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI-REFLECTIVE COATING. It is very important to clean the lens using a clean, lint-free cloth and an eyeglass lens cleaner that is specified as safe for anti-reflective coatings. 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 the on-board Lightning Detection System, there are several atmospheric phenomena in addition to nearby thunderstorms that can cause isolated discharge points in the strike display mode. However, clusters of two or more discharge points in the strike display mode do indicate thunderstorm activity if these points reappear after the screen has been cleared. NOTE: All visual depictions contained within this document, including screen images of the G1000 panel and displays, are subject to change and may not reflect the most current G1000 system. Depictions of equipment may differ slightly from the actual equipment. NOTE: This device complies with part 15 of the FCC Rules. Operation is subject to the following two conditions: (1) this device may not cause harmful interference, and (2) this device must accept any interference received, including interference that may cause undesired operation. NOTE: Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of attitude and heading displays while the aircraft is on the ground. Moving the aircraft more than 100 feet away from the source of the interference should alleviate the condition. NOTE: Use of polarized eyewear may cause the flight displays to appear dim or blank. Garmin G1000 Pilot’s Guide for the Diamond DA62 190-01895-00 Rev. A iv WARNINGS, CAUTIONS, AND NOTES NOTE: This product, its packaging, and its components contain chemicals known to the State of California to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with California’s Proposition 65. If you have any questions or would like additional information, please refer to our web site at www.garmin.com/prop65. NOTE : The FAA has asked Garmin to remind pilots who fly with Garmin database-dependent avionics of the following: • It is the pilot’s responsibility to remain familiar with all FAA regulatory and advisory guidance and information related to the use of databases in the National Airspace System. • Garmin equipment will only recognize and use databases that are obtained from Garmin or Jeppesen. Databases obtained from Garmin or Jeppesen are assured compliance with all data quality requirements (DQRs) by virtue of a Type 2 Letter of Authorization (LOA) from the FAA. A copy of the Type 2 LOA is available for each database and can be viewed at http://fly.garmin.com by selecting ‘Type 2 LOA Status.’ • Use of a current Garmin or Jeppesen database in your Garmin equipment is required for compliance with established FAA regulatory guidance, but does not constitute authorization to fly any and all terminal procedures that may be presented by the system. It is the pilot’s responsibility to operate in accordance with established AFM(S) and regulatory guidance or limitations as applicable to the pilot, the aircraft, and installed equipment. NOTE : The pilot/operator must review and be familiar with Garmin’s database exclusion list as discussed in SAIB CE-14-04 to determine what data may be incomplete. The database exclusion list can be viewed at www.flygarmin.com by selecting ‘Database Exclusions List.’ NOTE : The pilot/operator must have access to Garmin and Jeppesen database alerts and consider their impact on the intended aircraft operation. The database alerts can be viewed at www.flygarmin.com by selecting ‘Aviation Database Alerts.’ NOTE : If the pilot/operator wants or needs to adjust the database, contact Garmin Product Support to coordinate the revised DQRs. NOTE: Garmin requests the flight crew report any observed discrepancies related to database information. These discrepancies could come in the form of an incorrect procedure; incorrectly identified terrain, obstacles and fixes; or any other displayed item used for navigation or communication in the air or on the ground. Go to FlyGarmin.com and select ‘Report An Aviation Data Error Report.’ 190-01895-00 Rev. A Garmin G1000 Pilot’s Guide for the Diamond DA62 v REVISION INFORMATION Record of Revision Part Number Revision Date Page Range Description 190-01895-00 A i – I-6 Initial release with GDU SW Version 14.04 Garmin G1000 Pilot’s Guide for the Diamond DA62 190-01895-00 Rev. A vi TABLE OF CONTENTS SECTION 1 SYSTEM OVERVIEW 1.1 Line Replaceable Units ........................................... 2 1.2 Secure Digital (SD) Cards ....................................... 6 1.3 System Power-up ..................................................... 7 1.4 System Operation .................................................... 8 Display Operation ......................................................... 8 G1000 System Annunciations ........................................ 9 System Status............................................................. 10 AHRS Operation ......................................................... 12 GPS Receiver Operation .............................................. 13 1.5 G1000 Controls...................................................... 17 PFD/MFD Controls ...................................................... 17 Softkey Function ......................................................... 19 1.6 Accessing G1000 Functionality............................ 26 Menus ....................................................................... 26 Data Entry.................................................................. 26 Page Groups .............................................................. 28 System Settings .......................................................... 32 Timers ....................................................................... 38 Electronic Checklists ................................................... 41 1.7 Display Backlighting ............................................. 43 SECTION 2 FLIGHT INSTRUMENTS 2.1 Flight Instruments ................................................. 48 Airspeed Indicator ...................................................... 48 Attitude Indicator ....................................................... 50 Altimeter ................................................................... 51 Vertical Speed Indicator (VSI) ....................................... 53 Vertical Deviation ....................................................... 54 Horizontal Situation Indicator (HSI) .............................. 55 Course Deviation Indicator (CDI) .................................. 60 2.2 Supplemental Flight Data .................................... 67 Outside Air Temperature .............................................. 67 Wind Data ................................................................. 69 Vertical Navigation (VNV) Indications ........................... 70 2.3 PFD Annunciations and Alerting Functions ........ 71 System Alerting .......................................................... 71 Marker Beacon Annunciations...................................... 72 Traffic Annunciation .................................................... 72 Altitude Alerting ......................................................... 73 Low Altitude Annunciation .......................................... 73 Minimum Descent Altitude/Decision Height Alerting ...... 74 Radar Altimeter .......................................................... 75 2.4 Abnormal Operations ........................................... 77 Abnormal GPS Conditions ........................................... 77 Unusual Attitudes ....................................................... 78 SECTION 3 ENGINE INDICATION SYSTEM (EIS) 3.1 Engine Display ....................................................... 82 3.2 System Display ...................................................... 84 3.3 Fuel Display............................................................ 86 SECTION 4 AUDIO PANEL AND CNS 4.1 Overview ................................................................ 89 MFD/PFD Controls and Frequency Display ..................... 90 Audio Panel Controls .................................................. 92 4.2 COM Operation ...................................................... 94 COM Transceiver Selection and Activation ..................... 94 COM Transceiver Manual Tuning .................................. 95 Quick-tuning and Activating 121.500 MHz .................... 96 Auto-tuning the COM Frequency .................................. 97 Frequency Spacing .................................................... 101 Automatic Squelch.................................................... 102 Volume .................................................................... 102 4.3 NAV Operation ..................................................... 103 NAV Radio Selection and Activation ........................... 103 NAV Receiver Manual Tuning ..................................... 104 Auto-tuning a NAV Frequency from the MFD ............... 106 Marker Beacon Receiver ............................................ 111 ADF/DME Tuning ...................................................... 112 4.4 GTX 33/GTX 33 ES Mode S Transponder ........... 116 Transponder Controls ................................................ 116 Transponder Mode Selection ...................................... 117 ADS-B TX (Optional).................................................. 120 Entering a Transponder Code ..................................... 120 IDENT Function ........................................................ 122 Flight ID Reporting.................................................... 123 4.5 Additional Audio Panel Functions ..................... 124 Power-up ................................................................. 124 Mono/Stereo Headsets .............................................. 124 Intercom .................................................................. 124 Clearance Recorder and Player................................... 126 Split COM ................................................................ 127 Entertainment Inputs ................................................ 127 4.6 Audio Panel Preflight Procedure ....................... 128 4.7 Abnormal Operation ........................................... 129 190-01895-00 Rev. A Garmin G1000 Pilot’s Guide for the Diamond DA62 vii TABLE OF CONTENTS Stuck Microphone..................................................... 129 COM Tuning Failure................................................... 129 Audio Panel Fail-safe Operation ................................. 129 Reversionary Mode ................................................... 129 SECTION 5 FLIGHT MANAGEMENT 5.1 Introduction ......................................................... 131 Navigation Status Box............................................... 132 5.2 Using Map Displays ............................................. 134 Map Orientation ....................................................... 134 Map Range .............................................................. 136 Map Panning............................................................ 138 Measuring Bearing and Distance ................................ 143 Topography .............................................................. 144 Map Symbols ........................................................... 147 Airways ................................................................... 153 Track Vector ............................................................. 155 Wind Vector ............................................................. 156 Nav Range Ring........................................................ 157 Fuel Range Ring ....................................................... 158 Field of View (SVT) .................................................... 159 Selected Altitude Intercept Arc ................................... 160 5.3 Waypoints............................................................. 161 Airports ................................................................... 162 Intersections ............................................................ 169 NDBs ....................................................................... 171 VORs ....................................................................... 173 User Waypoints ........................................................ 175 5.4 Airspaces .............................................................. 181 5.5 Direct-to-Navigation .......................................... 185 5.6 Flight Planning..................................................... 190 Flight Plan Creation .................................................. 191 Adding Waypoints to an Existing Flight Plan................ 196 Adding Airways to a Flight Plan ................................. 198 Adding Procedures to a Stored Flight Plan .................. 200 Flight Plan Storage ................................................... 207 Flight Plan Editing .................................................... 209 Along Track Offsets ................................................... 212 Parallel Track ............................................................ 214 Activating a Flight Plan Leg ....................................... 217 Inverting a Flight Plan ............................................... 218 Flight Plan Views ...................................................... 219 Closest Point of FPL .................................................. 221 User-Defined Holding Patterns ................................... 221 5.7 Vertical Navigation ............................................. 226 Altitude Constraints .................................................. 228 5.8 Procedures ........................................................... 232 Departures ............................................................... 233 Arrivals ................................................................... 236 Approaches ............................................................. 239 5.9 Trip Planning ........................................................ 247 Trip Planning ............................................................ 247 5.10 RAIM Prediction................................................... 251 5.11 Navigating a Flight Plan ..................................... 254 5.12 Abnormal Operation ........................................... 282 SECTION 6 HAZARD AVOIDANCE 6.1 SiriusXM Weather ................................................ 286 Activating Services.................................................... 286 Using SiriusXM Weather Products .............................. 287 6.2 Garmin Connext Weather ................................... 320 Registering the Iridium Satellite System ...................... 320 Registering Garmin Connext Weather ......................... 321 Accessing Garmin Connext Weather Products.............. 323 Connext Data Requests ............................................. 330 Garmin Connext Weather Products ............................. 334 Abnormal Operations ................................................ 349 6.3 Airborne Color Weather Radar .......................... 351 System Description ................................................... 351 Principles of Pulsed Airborne Weather Radar ............... 351 Safe Operating Distance ............................................ 355 Basic Antenna Tilt Setup ............................................ 356 Weather Mapping and Interpretation ......................... 357 Ground Mapping and Interpretation ........................... 369 Weather Radar Overlay on the Navigation Map Page ... 370 System Status........................................................... 371 6.4 Lightning Detection System............................... 373 Setting Up Lightning Detection Information on the Navigation Map ....................................................... 373 Selecting the Stormscope Page .................................. 377 6.5 Terrain Proximity ................................................. 379 Displaying Terrain Proximity Data ............................... 379 Terrain Proximity Page............................................... 382 Garmin G1000 Pilot’s Guide for the Diamond DA62 190-01895-00 Rev. A viii TABLE OF CONTENTS 6.6 Profile View Terrain ............................................. 384 Profile View Display .................................................. 385 6.7 Terrain-SVS ........................................................... 388 Displaying Terrain-SVS Data ....................................... 389 Terrain-SVS Page ...................................................... 391 Terrain-SVS Alerts ..................................................... 393 System Status........................................................... 396 6.8 Traffic Information Service (TIS) ........................ 397 Displaying Traffic Data .............................................. 398 Traffic Map Page....................................................... 400 TIS Alerts ................................................................. 401 System Status........................................................... 403 6.9 Avidyne TAS600 Traffic........................................ 405 TAS Symbology......................................................... 405 Displaying Traffic Data .............................................. 406 Altitude Display ........................................................ 408 Traffic Map Page Display Range ................................. 408 TAS Alerts ................................................................ 410 System Status........................................................... 411 SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM 7.1 AFCS Controls ...................................................... 414 7.2 Flight Director Operation ................................... 416 Activating the Flight Director ..................................... 416 AFCS Status Box ....................................................... 417 Command Bars ......................................................... 418 Flight Director Modes................................................ 418 7.3 Vertical Modes ..................................................... 419 Pitch Hold Mode (PIT) ............................................... 420 Selected Altitude Capture Mode (ALTS) ....................... 421 Altitude Hold Mode (ALT) .......................................... 422 Vertical Speed Mode (VS) .......................................... 423 Flight Level Change Mode (FLC) ................................. 424 Vertical Navigation Modes (VPTH, ALTV) ..................... 425 Glidepath Mode (GP) (SBAS only)............................... 430 Glideslope Mode (GS) ............................................... 432 Takeoff (TO) and Go Around (GA) Modes .................... 433 7.4 Lateral Modes ...................................................... 434 Roll Hold Mode (ROL) ............................................... 435 Heading Select Mode (HDG) ...................................... 436 Navigation Modes (GPS, VOR, LOC, BC) ...................... 437 Approach Modes (GPS, VAPP, LOC) ............................. 439 7.5 Autopilot and Yaw Damper Operation ............. 441 Flight Control ........................................................... 441 Engaging the Autopilot and Yaw Damper .................... 442 Control Wheel Steering ............................................. 442 Disengaging the Autopilot and Yaw Damper................ 443 Underspeed Protection .............................................. 444 7.6 Example Flight Plan ............................................ 446 Departure ................................................................ 446 Intercepting a VOR Radial .......................................... 448 Flying a Flight Plan/GPS Course ................................. 449 Descent ................................................................... 450 Approach ................................................................. 454 Go Around/Missed Approach ..................................... 456 7.7 AFCS Annunciations and Alerts ......................... 458 AFCS Status Alerts .................................................... 458 Overspeed Protection ................................................ 459 SECTION 8 ADDITIONAL FEATURES 8.1 Synthetic Vision Technology (SVT) (Optional) ............................................................. 462 SVT Operation .......................................................... 463 SVT Features ............................................................ 465 Field of View ............................................................ 473 8.2 SafeTaxi ................................................................ 475 8.3 ChartView (Optional) .......................................... 480 ChartView Softkeys ................................................... 481 Terminal Procedures Charts ....................................... 482 Chart Options........................................................... 490 Day/Night View ........................................................ 496 ChartView Cycle Number and Expiration Date ............. 498 8.4 FliteCharts ............................................................ 501 FliteCharts Softkeys .................................................. 502 Terminal Procedures Charts ....................................... 503 Chart Options........................................................... 510 Day/Night View ........................................................ 514 FliteCharts Cycle Number and Expiration Date............. 516 8.5 Airport Directory ................................................. 519 Airport Directory Database Cycle Number and Revision 520 8.6 SiriusXM Satellite Radio Entertainment (Optional) ............................................................. 522 Activating SiriusXM Satellite Radio Services ................ 522 190-01895-00 Rev. A Garmin G1000 Pilot’s Guide for the Diamond DA62 ix TABLE OF CONTENTS Using SiriusXM Radio................................................ 524 8.7 Satellite Telephone Services (Optional)............ 527 Telephone Communication ........................................ 527 Text Messaging (SMS) ............................................... 534 8.8 Electronic Stability and Protection (Garmin ESP™) ...................................................... 545 Roll Engagement ...................................................... 546 Pitch Engagement..................................................... 547 High Airspeed Protection ........................................... 548 8.9 Scheduler.............................................................. 549 8.10 Electronic Checklists ........................................... 551 8.11 Flight Data Logging ............................................ 554 8.12 Auxiliary Video (Optional) .................................. 556 Video Setup ............................................................. 557 Display Selection ...................................................... 557 Zoom/Range ............................................................ 558 8.13 Abnormal Operation ........................................... 559 SVT Troubleshooting ................................................. 559 Reversionary Mode ................................................... 559 Unusual Attitudes ..................................................... 560 GDL 69/69A Data Link Receiver Troubleshooting.......... 561 APPENDICES Annunciations and Alerts ............................................. 563 SVS Terrain Alerts...................................................... 582 SVS Terrain Status Annunciations ............................... 583 Database Management ................................................ 584 Jeppesen Databases.................................................. 584 Garmin Databases .................................................... 586 Glossary.......................................................................... 593 Frequently Asked Questions ........................................ 599 General TIS Information ............................................... 603 Introduction ............................................................. 603 TIS VS. TAS/TCAS ....................................................... 603 TIS Limitations.......................................................... 603 Map Symbols ................................................................. 605 INDEX Index ................................................................................ I-1 Garmin G1000 Pilot’s Guide for the Diamond DA62 190-01895-00 Rev. A x TABLE OF CONTENTS B lank Page 190-01895-00 Rev. A Garmin G1000 Pilot’s Guide for the Diamond DA62 1 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX SECTION 1 SYSTEM OVERVIEW NOTE: Refer to the Automatic Flight Control System (AFCS) Section for details on the Garmin AFCS. The G1000 Integrated Avionics System presents flight instrumentation, position, navigation, communication, and identification information using flat-panel color displays. The system is distributed across the following Line Replaceable Units (LRUs): • GDU 1040 Primary Flight Display (PFD) • GDU 1045 Multi Function Display (MFD) • GMA 1347 Audio Panel with Integrated Marker Beacon Receiver • GIA 63W Integrated Avionics Units (IAU) • GDC 74A Air Data Computer (ADC) • GEA 71 Engine/Airframe Unit • GTX 33 Mode S Transponder • GRS 77 Attitude and Heading Reference System (AHRS) • GMU 44 Magnetometer • GDL 69/69A Data Link Receiver • GSA 80 AFCS Yaw Damper Servo • GSA 81 AFCS Servos (3) • GSM 86 Servo Mounts (4) • GSR 56 Iridium Transceiver (optional) • GWX 70 Weather Radar • GRA 5500 Radar Altimeter (optional) Figure 1-1 shows interactions between the LRUs. Additional/optional equipment are shown in Figure 1-2. The Diamond DA62 may be optionally equipped with a Garmin AFCS Automated Flight Control System, providing flight director (FD), autopilot (AP), and manual electric trim (MET) functions of the G1000 System. Garmin G1000 Pilot’s Guide for the Diamond DA62 190-01895-00 Rev. A 2 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 1.1 LINE REPLACEABLE UNITS • GDU 1040/1045 (2) – A GDU 1040 is configured as the Primary Flight Display (PFD) and a GDU 1045 as the Multi Function Display (MFD). Both displays feature 10.4-inch LCD screens with 1024 x 768 resolution. The displays communicate with each other through a High-speed Data Bus (HSDB) Ethernet connection. Each display is also paired with an Ethernet connection to an IAU. • GMA 1347 – The Audio Panel integrates navigation/communication radio (NAV/COM) digital audio, intercom, and marker beacon controls, and is installed between the displays. This unit also provides manual control of display Reversionary Mode (red DISPLAY BACKUP button; see Section 1.4, System Operation) and communicates with both IAUs using an RS-232 digital interface. • GIA 63W (2) – The Integrated Avionics Units (IAU) function as the main communications hub, linking all LRUs with the PFD. Each GIA 63W contains a GPS SBAS receiver, VHF COM/NAV/GS receivers, a flight director (FD; if Garmin AFCS is installed), and system integration microprocessors. Each GIA 63W is paired with the on-side display via an HSDB connection. The IAUs are not paired together and do not communicate with each other directly. NOTE: Refer to the Airplane Flight Manual (AFM) to determine whether SBAS functionality is approved. • GDC 74A – The Air Data Computer (ADC) processes data from the pitot/static system and outside air temperature (OAT) sensor. The ADC provides pressure altitude, airspeed, vertical speed, and OAT information to the G1000 System, and it communicates with the primary IAU, displays, and AHRS using an ARINC 429 digital interface. • GEA 71 – The Engine Airframe Unit receives and processes signals from the engine and airframe sensors. This unit communicates with both IAUs using an RS-485 digital interface. • GTX 33 or GTX 33 with Extended Squitter – The GTX 33 solid-state Transponder provides Modes A, C, and S capability. The GTX 33 with Extended Squitter will also provide 1090 MHz Extended Squitter (1090ES) transmit capability. The transponder communicates with both IAUs through an RS-232 digital interface. • GRS 77 (2) – The Attitude and Heading Reference System (AHRS) provides aircraft attitude and heading information via ARINC 429 to both the PFD and the primary IAU. The AHRS contains advanced sensors (including accelerometers and rate sensors) and interfaces with the Magnetometer to obtain magnetic field information, with the ADC to obtain air data, and with both IAUs to obtain GPS information. AHRS operation is discussed in Section 1.4, System Operation. • GMU 44 – The Magnetometer measures local magnetic field and sends data to the AHRS for processing to determine aircraft magnetic heading. This unit receives power directly from the AHRS and communicates with it via an RS-485 digital interface. • GDL 69/69A – The Data Link Satellite Radio Receiver provides real-time weather information to MFD maps and the PFD Inset Map. The GDL 69A model is also capable of providing digital audio entertainment. The Data Link Receiver communicates with the MFD via an HSDB connection. A subscription to XM Satellite Radio Service is required to enable Data Link Receiver capability. • GSA 80, GSA 81 and GSM 86 – The GSA servos are used for the automatic control of pitch, pitch trim, roll and yaw. These units interface with each IAU. The GSM 86 servo mounts are responsible for transferring the output torque of the servo actuators to the mechanical flight-control surface linkages (not displayed in Figure 1-1). 190-01895-00 Rev. A Garmin G1000 Pilot’s Guide for the Diamond DA62 3 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX • GRA 5500 – The optional Radar Altimeter provides altitude above the ground (AGL) to the MFD, through the GIA 63W, using an RS-422 digital interface. • GWX 70 – Provides airborne weather and ground mapped radar data to the MFD, via HSDB ethernet connection. Garmin G1000 Pilot’s Guide for the Diamond DA62 190-01895-00 Rev. A 4 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Figure 1-1 G1000 System Block Diagram GMU 44 Magnetometer Heading Reversionary Control Reversionary Control GMA 1347 Audio Panel GDU 1040 Primary Flight Display GDU 1045 Multi Function Display GDC 74A Air Data Computer OAT Airspeed Altitude Vertical Speed GRS 77 AHRS Attitude Rate of Turn Slip/Skid GTX 33/33ES Transponder GEA 71 Engine/Airframe Unit GSA 81 Roll Servo Autopilot Calculations (optional) GSA 81 Pitch Servo Autopilot Calculations (optional) GSA 80 Yaw Damper Servo Yaw Damper Calculations (optional) GSA 81 Pitch Trim Servo Autopilot Calculations (optional) No. 1 GIA 63W Integrated Avionics Unit System Inegration Processors I/O Processors VHF COM VHF NAV/LOC GPS/SBAS Glideslope Flight Director (with AFCS option) GPS Output No. 2 GIA 63W Integrated Avionics Unit System Integration Processors I/O Processors VHF COM VHF NAV/LOC GPS/SBAS Glideslope GPS Output 190-01895-00 Rev. A Garmin G1000 Pilot’s Guide for the Diamond DA62 5 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX No. 2 GIA 63W Integrated Avionics Unit System Integration Processors I/O Processors VHF COM VHF NAV/LOC GPS/SBAS Glideslope GDL 69/69A Data Link Receiver Real-time Weather Digital Audio Entertainment (optional subscription- based service) Avidyne TAS600 Series Traffic Advisory System (optional) Honeywell KN 63 DME (optional) Avidyne TWX 670 Lightning Strike and Thunderstorm Detection (optional) Garmin GRA 5500 Radar Altimeter (optional) Becker RA 3502-(1) ADF Receiver (optional) Free Flight Radar Altimeter (optional)) GWX 70 Weather Radar Airborne Weather Radar (optional) Figure 1-2 G1000 With Optional/Additional Interfaces NOTE: For information on additional equipment shown in Figure 1-2, consult the applicable optional interface user’s guide. This document assumes that the reader is already familiar with the operation of this additional equipment. Garmin G1000 Pilot’s Guide for the Diamond DA62 190-01895-00 Rev. A 6 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 1.2 SECURE DIGITAL (SD) CARDS NOTE: Ensure the G1000 System is powered off before inserting an SD card. NOTE: Refer to the Appendix for instructions on updating databases. The PFD and MFD data card slots use Secure Digital (SD) cards and are located on the upper right side of the display bezels. Each display bezel is equipped with two SD card slots. SD cards are used for aviation database and system software updates as well as terrain database storage. Installing an SD card: 1) Insert the SD card in the SD card slot, pushing the card in until the spring latch engages. The front of the card should remain flush with the face of the display bezel. 2) To eject the card, gently press on the SD card to release the spring latch. Figure 1-3 Display Bezel SD Card Slots SD Card Slots 190-01895-00 Rev. A Garmin G1000 Pilot’s Guide for the Diamond DA62 7 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 1.3 SYSTEM POWER-UP NOTE: See the Airplane Flight Manual (AFM) for specific procedures concerning avionics power application and emergency power supply operation. NOTE: Refer to the Appendix for system-specific annunciations and alerts. The G1000 System is integrated with the aircraft electrical system and receives power directly from electrical busses. The PFD, MFD, and supporting sub-systems include both power-on and continuous built-in test features that exercise the processor, RAM, ROM, external inputs, and outputs to provide safe operation. During system initialization, test annunciations are displayed, as shown in Figure 1-4. All system annunciations should disappear typically within the first minute of power-up. Upon power-up, key annunciator lights also become momentarily illuminated on the Audio Panel and the display bezels. On the PFD, the AHRS begins to initialize and displays “AHRS ALIGN: Keep Wings Level”. The AHRS should display valid attitude and heading fields typically within the first minute of power-up. The AHRS can align itself both while taxiing and during level flight. When the MFD powers up, the screen (Figure 1-5) displays the following information: • System version • Copyright • Land database name and version • Obstacle database name and version • Terrain database name and version • Aviation database name, version, and effective dates Current database information includes valid operating dates, cycle number, and database type. When this information has been reviewed for currency (to ensure that no databases have expired), the pilot is prompted to continue. Pressing the ENT Key acknowledges this information, and displays the Navigation Map Page. When the system has acquired a sufficient number of satellites to determine a position, the aircraft’s current position is shown on the Navigation Map Page. Figure 1-4 PFD Initialization Figure 1-5 Example MFD Power-up Garmin G1000 Pilot’s Guide for the Diamond DA62 190-01895-00 Rev. A 8 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 1.4 SYSTEM OPERATION NOTE: Refer to the Appendix for detailed descriptions of all alerts and annunciations. Refer to the Airplane Flight Manual (AFM) for additional information regarding pilot responses to these annunciations. The displays are connected together via a single Ethernet bus for high-speed communication. As shown in Figure 1-1, each IAU is connected to the on-side display. This allows the units to share information, enabling true system integration DISPLAY OPERATION NOTE: In normal operating mode, backlighting can only be adjusted from the PFD. In Reversionary Mode, it can be adjusted from the remaining display. In normal operating mode, the PFD presents graphical flight instrumentation (attitude, heading, airspeed, altitude, vertical speed), replacing the traditional flight instrument cluster (see the Flight Instruments Section for more information). The MFD normally displays a full-color moving map with navigation information (see the Flight Management Section), while the left portion of the MFD is dedicated to the Engine Indication System (EIS; see the EIS Section). Both displays offer control for COM and NAV frequency selection. Figure 1-6 G1000 Normal Operation In the event of a display failure, the G1000 System automatically switches to reversionary (backup) mode. In Reversionary Mode, all important flight information from the PFD is presented on the remaining display in the same format as in normal operating mode, with the addition of the EIS. EIS operation while in Reversionary Mode is discussed in the EIS Section. As when the PFD is operating normally, windows for flight planning, nearest airports, and procedures are available. The Inset Map is moved to the right side of the display. If a display fails, the appropriate IAU-display Ethernet interface is cut off. Thus, the IAU can no longer communicate with the remaining display (refer to Figure 1-1), and the NAV and COM functions provided to the failed display by the IAU are flagged as invalid on the remaining display. The system reverts to backup paths for the AHRS, ADC, Engine/Airframe Unit, and Transponder, as required. The change to backup paths is completely automated for all LRUs and no pilot action is required. 190-01895-00 Rev. A Garmin G1000 Pilot’s Guide for the Diamond DA62 9 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX If the system fails to detect a display problem, Reversionary Mode may be manually activated by pressing the Audio Panel’s red DISPLAY BACKUP Button. Pressing this button again deactivates Reversionary Mode. DISPLAY BACKUP Button Manually Activates/ Deactivates Reversionary Mode on Both Displays Figure 1-7 G1000 Reversionary Mode (Failed PFD) NAV1 and COM1 (provided by the failed PFD) Flagged Invalid G1000 SYSTEM ANNUNCIATIONS When an LRU or an LRU function fails, a large red ‘X’ is typically displayed over the instrument experiencing failed data (Figure 1-8 displays all possible flags and responsible LRUs). The G1000 System alerts the pilot when backup paths are utilized by the LRUs. Upon G1000 power-up, certain instruments remain invalid as equipment begins to initialize. All instruments should be operational within one minute of power-up. If any instrument remains flagged, the G1000 should be serviced by a Garmin-authorized repair facility. Figure 1-8 G1000 System Failure Annunciations GDC 74A GRS 77, GMU 44 or GIA 63W GIA 63W GIA 63W GIA 63W or DME/ADF Source GEA 71, GIA 63W, or ECU GDC 74A GTX 33 or GIA 63W GIA 63W Database Mismatch in PFD and MFD Garmin G1000 Pilot’s Guide for the Diamond DA62 190-01895-00 Rev. A 10 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX SYSTEM STATUS The System Status Page displays the statuses, serial numbers, and software version numbers for all detected system LRUs. Active LRUs are indicated by green check marks; failed, by red ‘X’s. Failed LRUs should be noted and a service center or Garmin-authorized dealer informed. Viewing LRU information: 1) Use the FMS Knob to select the AUX - System Status Page. 2) To place the cursor in the ‘LRU Info’ Box, a) Press the LRU Softkey. Or: a) Press the MENU Key. b) With ‘Select LRU Window’ highlighted, press the ENT Key. 3) Use the FMS Knob to scroll through the box to view LRU status information. Figure 1-9 Example System Status Page 190-01895-00 Rev. A Garmin G1000 Pilot’s Guide for the Diamond DA62 11 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Airframe information which includes system software, Cockpit Reference Guide (CRG) part number, system ID, and checklist are also displayed on this page. Viewing airframe information: 1) Use the FMS Knob to select the AUX - System Status Page. 2) To place the cursor in the ‘Airframe’ Box, a) Press the ARFRM Softkey. Or: a) Press the MENU Key. b) Highlight ‘Select Airframe Window’ and press the ENT Key. 3) Use the FMS Knob to scroll through the box to view airframe information. Pertinent information on all system databases is also displayed on this page. Refer to the Appendices and Additional Features sections for more information about databases. Viewing database information: 1) Use the FMS Knob to select the AUX - System Status Page. 2) To place the cursor in the ‘Database’ Box, a) Press the DBASE Softkey. Or: a) Press the MENU Key. b) Highlight ‘Select Dbase Window’ and press the ENT Key. 3) Use the FMS Knob to scroll through the box to view database status information. The G1000 uses aural tones to convey the priority of airframe-specific alerts. The alerting system’s annunciation tone may be tested from the System Status Page. Refer to the Appendices for airframe-specific alerts. Testing the system annunciation tone: 1) Use the FMS Knob to select the AUX - System Status Page. 2) Press the ANN TEST Softkey. Or: a) Press the MENU Key. b) Highlight ‘Enable Annunciator Test Mode’ and press the ENT Key. Garmin G1000 Pilot’s Guide for the Diamond DA62 190-01895-00 Rev. A 12 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX AHRS OPERATION NOTE: Aggressive maneuvering while AHRS is not operating normally may degrade AHRS accuracy. The Attitude and Heading Reference System (AHRS) performs attitude, heading, and vertical acceleration calculations for the G1000 System, utilizing GPS, magnetometer, and air data in addition to information from its internal sensors. Attitude and heading information are updated on the PFD while the AHRS receives appropriate combinations of information from the external sensor inputs. Figure 1-10 AHRS Operation Attitude/Heading Invalid AHRS no-GPS Mode AHRS Normal Operation AHRS no- Mag Mode AHRS no-Mag/ no-Air Mode Heading Invalid available available unavailable unavailable available unavailable unavailable available Air Data Magnetometer Data unavailable available GPS Data Magnetometer Data Air Data Loss of GPS, magnetometer, or air data inputs is communicated to the pilot by message advisory alerts (refer to Appendix A for specific AHRS alert information). Any failure of the internal AHRS inertial sensors results in loss of attitude and heading information (indicated by red ‘X’ flags over the corresponding flight instruments). Two GPS inputs are provided to the AHRS. If GPS information from one of the inputs fails, the AHRS uses the remaining GPS input and an alert message is issued to inform the pilot. If both GPS inputs fail, the AHRS can continue to provide attitude and heading information to the PFD as long as magnetometer and airspeed data are available and valid. If the magnetometer input fails, the AHRS continues to output valid attitude information; however, the heading output on the PFD is flagged as invalid with a red ‘X’. Failure of the air data input has no effect on the AHRS output while AHRS is receiving valid GPS information. Invalid/unavailable airspeed data in addition to GPS failure results in loss of all attitude and heading information. 190-01895-00 Rev. A Garmin G1000 Pilot’s Guide for the Diamond DA62 13 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX GPS RECEIVER OPERATION Each Integrated Avionics Unit (IAU) contains a GPS receiver. Internal system checking is performed to ensure both GPS receivers are providing accurate data to the PFD. When both GPS receivers are providing accurate data, the GPS receiver producing the better solution is used by the system. Information collected by the specified receiver (GPS1 for the #1 IAU or GPS2 for the #2 IAU) may be viewed on the AUX - GPS Status Page. Viewing GPS receiver status information: 1) Use the large FMS Knob on the MFD to select the Auxiliary Page Group (see Section 1.6 for information on navigating MFD page groups). 2) Use the small FMS Knob to select GPS Status Page (third page in the AUX Page Group). 3) To change the selected GPS receiver: Press the desired GPS Softkey. Or: a) Press the MENU Key. b) Use the FMS Knob to highlight the receiver which is not selected and press the ENT Key. Satellite Signal Strength Bars RAIM Availability Prediction GPS Receiver Status Figure 1-11 GPS Status Page Satellite Constellation Diagram Satellite Signal Information Garmin G1000 Pilot’s Guide for the Diamond DA62 190-01895-00 Rev. A 14 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX NOTE: Refer to the Airplane Flight Manual (AFM) to determine whether SBAS functionality is approved. For SBAS-enabled systems, GPS sensor annunciations are most often seen after system power-up when one GPS receiver has acquired satellites before the other or one of the GPS receivers has not yet acquired a SBAS signal. While the aircraft is on the ground, the SBAS signal may be blocked by obstructions causing one GPS receiver to have difficulty acquiring a good signal. Also, while airborne, turning the aircraft may result in one of the GPS receivers temporarily losing the SBAS signal. If no failure message exists, check the GPS Status Page and compare the information for GPS1 and GPS2. Discrepancies may indicate a problem. GPS RECEIVER STATUS The GPS solution type (ACQUIRING, 2D NAV, 2D DIFF NAV, 3D NAV, 3D DIFF NAV) for the active GPS receiver (GPS1 or GPS2) is shown in the upper right of the GPS Status Page. When the receiver is in the process of acquiring enough satellite signals for navigation, the receiver uses satellite orbital data (collected continuously from the satellites) and last known position to determine the satellites that should be in view. ACQUIRING is indicated as the solution until a sufficient number of satellites have been acquired for computing a solution. When the receiver is in the process of acquiring a 3D navigational GPS solution, 3D NAV is indicated as the solution until the 3D differential fix has finished acquisition. Satellite-Based Augmentation System (SBAS) status should be indicated as INACTIVE at this point. When acquisition is complete, the solution status changes to 3D DIFF NAV and SBAS becomes active. In certain situations, such as when the aircraft is outside or on the fringe of the EGNOS, MSAS (used only in Japan), or WAAS coverage area, it may be desirable to disable EGNOS, MSAS, or WAAS (although it is not recommended). When disabled, the SBAS field in the GPS Status box indicates DISABLED. There may be a small delay for the GPS Status box to be updated upon EGNOS, MSAS, or WAAS enabling/disabling. Disabling EGNOS, MSAS, or WAAS 1) Select the GPS Status Page. 2) If necessary, press the SBAS Softkey. 3) Press the FMS Knob, and turn the large FMS Knob to hightlight ‘EGNOS’, ‘MSAS’, or ‘WAAS’. 4) Press the ENT Key to uncheck the box. 5) Press the FMS Knob to remove the cursor. Figure 1-12 Enable/Disable SBAS 190-01895-00 Rev. A Garmin G1000 Pilot’s Guide for the Diamond DA62 15 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX RAIM PREDICTION Receiver Autonomous Integrity Monitoring (RAIM) is a GPS receiver function that performs a consistency check on all tracked satellites. RAIM ensures that the available satellite geometry allows the receiver to calculate a position within a specified RAIM protection limit (2.0 nautical miles for oceanic and enroute, 1.0 nm for terminal, and 0.3 nm for non-precision approaches). During oceanic, enroute, and terminal phases of flight, RAIM is available nearly 100% of the time. The RAIM prediction function also indicates whether RAIM is available at a specified date and time. RAIM computations predict satellite coverage within ±15 min of the specified arrival date and time. In G1000 systems with SBAS enabled, performing RAIM prediction is not necessary in most cases. However, if the selected approach is outside the SBAS coverage area, it may be necessary to perform a RAIM prediction for the intended approach. NOTE: Refer to the Airplane Flight Manual (AFM) to determine whether SBAS functionality is approved. Because of the tighter protection limit on approaches, there may be times when RAIM is not available. The G1000 automatically monitors RAIM and warns with an alert message when it is not available. If RAIM is not predicted to be available for the final approach course, the approach does not become active, as indicated by the message “Approach is not active”. If RAIM is not available when crossing the FAF, the missed approach procedure must be flown. Predicting RAIM availability: 1) Select the GPS Status Page. 2) Press the RAIM Softkey. 3) Press the FMS Knob. The ‘WAYPOINT’ field is highlighted. 4) Turn the small FMS Knob to display the Waypoint Information Window. 5) Enter the desired waypoint and press the ENT Key (refer to Section 1.6 for instructions on data entry). Or: a) To use the present position, press the MENU Key. b) With ‘Set WPT to Present Position’ highlighted, press the ENT Key. c) Press the ENT Key to accept the waypoint entry. 6) Enter an arrival time and press the ENT Key. 7) Enter an arrival date and press the ENT Key. 8) With the cursor highlighting ‘COMPUTE RAIM?’, press the ENT Key. Once RAIM availability is computed, one of the following is displayed: • ‘COMPUTE RAIM?’—RAIM has not been computed for the current waypoint, time, and date combination • ‘COMPUTING AVAILABILITY’—RAIM calculation in progress • ‘RAIM AVAILABLE’—RAIM is predicted to be available for the specified waypoint, time, and date • ‘RAIM NOT AVAILABLE’—RAIM is predicted to be unavailable for the specified waypoint, time, and date Garmin G1000 Pilot’s Guide for the Diamond DA62 190-01895-00 Rev. A 16 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX SATELLITE INFORMATION Satellites currently in view are shown at their respective positions on a satellite constellation diagram. This sky view is always oriented north-up, with the outer circle representing the horizon, the inner circle representing 45° above the horizon, and the center point showing the position directly overhead. Each satellite is represented by an oval containing the Pseudo-random noise (PRN) number (i.e., satellite identification number). Satellites whose signals are currently being used are represented by solid ovals. The GPS Status Page can be helpful in troubleshooting weak (or missing) signal levels due to poor satellite coverage or installation problems. As the GPS receiver locks onto satellites, a signal strength bar is displayed for each satellite in view, with the appropriate satellite PRN number (01-32 or 120-138 for SBAS) below each bar. The progress of satellite acquisition is indicated by signal bar appearance: • No signal strength bar—Receiver is looking for the indicated satellite. • Hollow signal strength bar—Receiver has found the satellite and is collecting data. Each satellite has a 30- second data transmission that must be collected (signal strength bar is hollow) before the satellite may be used for navigation (signal strength bar becomes solid). • Solid signal strength bar—Receiver has collected the necessary data and the satellite signal can be used. • Checkered signal strength bar—Receiver has excluded the satellite (Fault Detection and Exclusion; FDE). • “D” indication on signal strength bar—Satellite is being used for differential computations. • Green signal strength bar—Satellites that are actually being used in the position calculation. • Blue signal strength bar—Satellite is locked on but not yet being used in the position calculation. Using the current satellite signal information, the system calculates the aircraft’s GPS position, time, altitude, ground speed, and track for the aircraft (displayed below the satellite signal accuracy measurements for reference). The following quantities denote the accuracy of the aircraft’s GPS fix: • Estimated Position Uncertainty (EPU)—A statistical error indication; the radius of a circle centered on an estimated horizontal position in which actual position has 95% probability of lying • Horizontal Dilution of Precision (HDOP)—Measures satellite geometry quality (i.e., number of satellites received and where they are relative to each other) on a range from 0.0 to 9.9, with lower numbers denoting better accuracy • Horizontal and Vertical Figures of Merit (HFOM and VFOM)—Measures of horizontal and vertical position uncertainty; the current 95% confidence horizontal and vertical accuracy values reported by the GPS receiver NOTE: Refer to the Airplane Flight Manual (AFM) to determine whether SBAS functionality is approved. 190-01895-00 Rev. A Garmin G1000 Pilot’s Guide for the Diamond DA62 17 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 1.5 G1000 CONTROLS The G1000 controls have been designed to simplify operation of the system and minimize workload and the time required to access sophisticated functionality. Controls are located on the PFD and MFD bezels and Audio Panel. PFD and MFD controls and softkeys are discussed in this section. See the Audio Panel and CNS Section for more information about Audio Panel and NAV/COM controls. AFCS controls (on the bezel of the MFD) are described in the AFCS section. PFD/MFD CONTROLS Figure 1-13 PFD/MFD Controls 17 18 5 6 8 7 2 4 3 1 9 12 16 11 10 15 14 13 The NAV, CRS/BARO, COM, FMS, and ALT knobs are concentric dual knobs, each having small (inner) and large (outer) control portion. When a portion of the knob is not specified in the text, either may be used. Large (Outer) Knob Small (Inner) Knob Figure 1-14 Dual Concentric Knob Garmin G1000 Pilot’s Guide for the Diamond DA62 190-01895-00 Rev. A 18 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 1 NAV VOL/ID Knob Turn to control NAV audio volume (shown in the NAV Frequency Box as a percentage) Press to toggle Morse code identifier audio on/off 2 NAV Frequency Transfer Key Transfers the standby and active NAV frequencies 3 NAV Knob Turn to tune NAV receiver standby frequencies (large knob for MHz; small for kHz) Press to toggle cyan tuning box between NAV1 and NAV2 4 Heading Knob Turn to manually select a heading Press to display a digital heading momentarily to the left of the Horizontal Situation Indicator (HSI) and synchronize the Selected Heading to the and current heading 5 Joystick Turn to change map range Press to activate Map Pointer and move in desired direction to pan map 6 CRS/BARO Knob Turn large knob for altimeter barometric pressure setting Turn small knob to adjust course (only when HSI is in VOR or OBS Mode) Press to re-center the CDI and return course pointer directly to bearing of active waypoint/station 7 COM Knob Turn to tune COM transceiver standby frequencies (large knob for MHz; small for kHz) Press to toggle cyan tuning box between COM1 and COM2 The selected COM (green) is controlled with the COM MIC Key (Audio Panel). 8 COM Frequency Transfer Key (EMERG) Transfers the standby and active COM frequencies Press and hold two seconds to tune the emergency frequency (121.5 MHz) automatically into the active frequency field 9 COM VOL/SQ Knob Turn to control COM audio volume level (shown as a percentage in the COM Frequency Box) Press to turn the COM automatic squelch on/off 10 Direct-to Key ( ) Activates the direct-to function and allows the user to enter a destination waypoint and establish a direct course to the selected destination (specified by identifier, chosen from the active route) 11 FPL Key Displays flight plan information 12 CLR Key (DFLT MAP) Erases information, cancels entries, or removes menus Press and hold to display the MFD Navigation Map Page (MFD only). 13 MENU Key Displays a context-sensitive list of options for accessing additional features or making setting changes 14 PROC Key Gives access to IFR departure procedures (DPs), arrival procedures (STARs), and approach procedures (IAPs) for a flight plan or selected airport 190-01895-00 Rev. A Garmin G1000 Pilot’s Guide for the Diamond DA62 19 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 15 ENT Key Validates/confirms selection or data entry 16 FMS Knob (Flight Management System Knob) Press to turn the selection cursor on/off Data Entry: With cursor on, turn to enter data in the highlighted field (large knob moves cursor location; small knob selects character for highlighted cursor location) Scrolling: When a list of information is too long for the window/box, a scroll bar appears, indicating more items to view. With cursor on, turn large knob to scroll through the list. Page Selection: Turn knob on MFD to select the page to view (large knob selects a page group; small knob selects a specific page from the group) 17 Softkey Selection Keys Press to select softkey shown above the bezel key on the PFD/MFD display 18 ALT Knob Sets the Selected Altitude, shown above the Altimeter (the large knob selects the thousands, the small knob selects the hundreds) SOFTKEY FUNCTION The softkeys are located along the bottoms of the displays. The softkeys shown depend on the softkey level or page being displayed. The bezel keys below the softkeys can be used to select the appropriate softkey. When a softkey is selected, its color changes to black text on gray background and remains this way until it is turned off, at which time it reverts to white text on black background. When a softkey function is disabled, the softkey label is subdued (dimmed). Softkeys revert to the previous level after 45 seconds of inactivity. Figure 1-15 Softkeys (Second-Level PFD Configuration) Softkey On Bezel-Mounted Softkeys (Press) Softkey Names (Displayed) In the following descriptions, top level softkeys are denoted with bullets. PFD SOFTKEYS The CDI, IDENT, TMR/REF, NRST, and ALERTS softkeys undergo a momentary change to black text on gray background and automatically switch back to white text on black background when selected. The PFD softkeys provide control over flight management functions, including GPS, NAV, terrain, traffic, and lightning (optional). Each softkey sublevel has a BACK Softkey which can be selected to return to the previous level. The ALERTS Softkey is visible at all softkey levels (label changes if messages are issued). Garmin G1000 Pilot’s Guide for the Diamond DA62 190-01895-00 Rev. A 20 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Figure 1-16 Top Level PFD Softkeys INSET XPDR IDENT TMR/REF NRST ALERTS OBS PFD CDI ADF/DME (optional) Press the CDI Softkey to cycle through navigation sources: - GPS - NAV1 (VOR/LOC) - NAV2 (VOR/LOC) BACK Press the OFF or BACK Softkey to return to the top-level softkeys. DCLTR DCLTR-2 DCLTR-3 DCLTR-1 TOPO ALERTS NEXRAD (optional) TERRAIN XM LTNG (optional) OFF TRAFFIC INSET STRMSCP (optional) TRFC-2 TRFC-1 METAR (optional) or PRECIP or DL LTNG WX LGND (optional) • INSET Displays Inset Map in PFD lower left corner OFF Removes Inset Map DCLTR (3) Selects desired amount of map detail; cycles through declutter levels: DCLTR (No Declutter): All map features visible DCLTR-1: Removes land data DCLTR-2: Removes land and SUA data DCLTR-3: Removes everything except active flight plan WX LGND Displays icon and age on the Inset Map for the selected weather products (optional) TRAFFIC (2) Displays/removes traffic information on Inset Map TRFC-1: Displays traffic on Inset Map. TRFC-2: Removes everything except traffic. Inset Map position HDG UP only. TOPO Displays/removes topographical data (e.g., coastlines, terrain, rivers, lakes) on Inset Map TERRAIN Displays/removes terrain information on Inset Map STRMSCP Displays/removes Stormscope weather information on Inset Map (optional) NEXRAD Displays/removes NEXRAD weather and coverage information on Inset Map (optional) XM LTNG Displays/removes XM lightning information on Inset Map (optional) METAR Displays METAR flags on airport symbols shown on the Inset Map (optional) INSET XPDR IDENT TMR/REF NRST ALERTS OBS PFD CDI ADF/DME (optional) Press the CDI Softkey to cycle through navigation sources: - GPS - NAV1 (VOR/LOC) - NAV2 (VOR/LOC) BACK Press the OFF or BACK Softkey to return to the top-level softkeys. DCLTR DCLTR-2 DCLTR-3 DCLTR-1 TOPO ALERTS NEXRAD (optional) TERRAIN XM LTNG (optional) OFF TRAFFIC INSET STRMSCP (optional) TRFC-2 TRFC-1 METAR (optional) or PRECIP or DL LTNG WX LGND (optional) Figure 1-17 INSET Softkeys 190-01895-00 Rev. A Garmin G1000 Pilot’s Guide for the Diamond DA62 21 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX • PFD Displays second-level softkeys for additional PFD configuration SYN VIS Displays the softkeys for enabling or disabling Synthetic Vision features (optional) PATHWAY Displays rectangular boxes representing the horizontal and vertical flight path of the active flight plan SYN TERR Enables synthetic terrain depiction HRZN HDG Displays compass heading along the Zero-Pitch line APTSIGNS Displays position markers for airports within approximately 15 nm of the current aircraft position. Airport identifiers are displayed when the airport is within approximately 9 nm. DFLTS Resets PFD to default settings, including changing units to standard WIND Displays softkeys to select and configure wind data OPTN1 Displays wind data in longitudinal and lateral components OPTN2 Displays wind data total direction and speed OPTN3 Displays wind data total direction with head and cross-wind speed components OFF Removes wind information from display DME Displays/removes DME Information Window (optional) BRG1 Cycles the Bearing 1 Information Window through: NAV1: Waypoint frequency/identifier and DME information GPS: Waypoint identifier and GPS distance information ADF: Waypoint frequency Off: Removes window HSI FMT Displays softkeys to select the HSI format 360 HSI Displays HSI as a 360° compass rose ARC HSI Displays HSI as a 140° viewable arc (Bearing Information windows unavailable) BRG2 Cycles the Bearing 2 Information Window through: NAV2: Waypoint frequency/identifier and DME information GPS: Waypoint identifier and GPS distance information ADF: Waypoint frequency Off: Removes window ALT UNIT Displays softkeys for changing the Altimeter barometric setting and altitude displays to metric units METERS Displays the current and Selected altitudes in meters in addition to feet, when selected IN Displays the Altimeter barometric setting in inches of mercury (in Hg) HPA Displays the Altimeter barometric setting in hectopascals (hPa) STD BARO Sets barometric pressure to 29.92 in Hg (1013 hPa if metric display is selected) • OBS Selects OBS Mode on the CDI when navigating by GPS (only available with active leg) • CDI Cycles CDI through GPS, NAV1 (VOR/LOC), and NAV2 (VOR/LOC) navigation sources • ADF/DME Displays/removes ADF/DME Radio Tuning Window (optional; may appear as ADF, DME, or ADF/DME depending on installation) Garmin G1000 Pilot’s Guide for the Diamond DA62 190-01895-00 Rev. A 22 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX STD BARO BACK ALERTS WIND HSI FMT PFD Press the STD BARO or BACK Softkey to return to the top-level softkeys. ALT UNIT HPA BACK ALERTS METERS IN DFLTS Press the BRG1/BRG2 softkeys to display/remove the Bearing Information windows and cycle through bearing sources: - NAV1/NAV2 - GPS - ADF BACK ALERTS OPTN1 OPTN2 OPTN3 DME (optional) BACK ALERTS 360 HSI ARC HSI BRG1 BRG2 OFF SYN VIS BACK ALERTS PATHWAY SYN TERR HRZN HDG APTSIGNS (optional) Figure 1-18 PFD Configuration Softkeys • XPDR Displays transponder mode selection softkeys: STBY Selects standby mode (Transponder does not reply to any interrogations) ON Selects Mode A (Transponder replies to interrogations) ALT Selects Mode C – altitude reporting mode (Transponder replies to identification and altitude interrogations) GND Manually selects Ground Mode (Transponder does not allow Mode A and Mode C replies, but does permit acquisition squitter and replies to discretely addressed Mode S interrogations) VFR Automatically enters the VFR code (1200 in U.S.A. only) CODE Displays transponder code selection softkeys 0-7 0 — 7 Use numbers to enter code IDENT Activates the Special Position Identification (SPI) pulse for 18 seconds, identifying the transponder return on the ATC screen BKSP Removes numbers entered, one at a time ADS-B TX Enables/disables automatic transmission of ADS-B position and speed. (optional) • IDENT Activates the Special Position Identification (SPI) pulse for 18 seconds, identifying the transponder return on the ATC screen • TMR/REF Displays/removes Timer/References Window 190-01895-00 Rev. A Garmin G1000 Pilot’s Guide for the Diamond DA62 23 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX • NRST Displays/removes Nearest Airports Window • ALERTS Displays/removes Alerts Window HPA BACK ALERTS METERS IN Press the BACK Softkey to return to the top-level softkeys. Press the IDENT or BACK Softkey to return to the top- level softkeys. XPDR STBY ON ALT VFR IDENT BACK ALERTS CODE IDENT BACK ALERTS 0 1 2 3 4 5 6 7 BKSP GND ADS-B TX (optional) Figure 1-19 XPDR Softkeys Garmin G1000 Pilot’s Guide for the Diamond DA62 190-01895-00 Rev. A 24 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX MFD SOFTKEYS MFD softkeys vary depending on the page selected. EIS and Navigation Map Page (default MFD page) softkeys are described here. CHKLIST DCLTR ENGINE DCLTR-2 DCLTR-3 DCLTR-1 MAP The DONE Softkey label changes to UNDO when the checklist item is already checked. EXIT DONE ENGINE EMERGCY SHW CHRT Press the BACK Softkey to return to the top-level softkeys. FUEL PROFILE TOPO (optional) NEXRAD TRAFFIC TERRAIN (optional) XM LTNG Press the BACK softkey to return to the top-level softkeys. AIRWY LO AIRWY HI AIRWY ON AIRWAYS (optional) STRMSCP METAR LEGEND ENGINE SYSTEM INC FUEL RST FUEL DEC FUEL BACK FUEL ENGINE SYSTEM BACK (optional) WX RADAR BACK (optional) Figure 1-20 EIS and MFD Softkeys • ENGINE Displays the Engine Page and top-level engine softkeys (see the EIS Section for more information) SYSTEM Displays the System Page FUEL Displays the Fuel Page DEC FUEL Decreases displayed fuel remaining in 1-gal increments INC FUEL Increases displayed fuel remaining in 1-gal increments RST FUEL Resets displayed fuel remaining to maximum fuel capacity for aircraft and fuel used to zero 190-01895-00 Rev. A Garmin G1000 Pilot’s Guide for the Diamond DA62 25 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX • MAP Enables second-level Navigation Map Page softkeys TRAFFIC Displays/removes traffic information on Navigation Map Page PROFILE Displays/removes profile view on Navigation Map Page TOPO Displays/removes topographical data (e.g., coastlines, terrain, rivers, lakes) on Navigation Map Page TERRAIN Displays/removes terrain information on Navigation Map Page AIRWAYS Selects the desired display of Airways; cycles through: AIRWY ON: All Airways displayed AIRWY LO: Low Altitude (Victor) Airways displayed AIRWY HI: High Altitude Airways (Jet Routes) displayed AIRWAYS: Airways are not displayed STRMSCP Displays/removes Stormscope weather information on Inset Map (optional) NEXRAD Displays/removes NEXRAD weather/coverage on Navigation Map Page (optional) XM LTNG Displays/removes XM lightning information on Navigation Map Page (optional) METAR Displays METAR flags on airport symbols shown on Navigation Map Page (optional) LEGEND Displays the legend for the selected weather products. Available only when NEXRAD, XM LTNG, and/or METAR softkeys are selected. WX RADAR Displays/removes airborne weather radar information on Navigation Map Page. BACK Returns to top-level softkeys • DCLTR (3) Selects desired amount of map detail; cycles through declutter levels: DCLTR (No Declutter): All map features visible DCLTR-1: Removes land data DCLTR-2: Removes land and SUA data DCLTR-3: Removes everything except the active flight plan • SHW CHRT Displays optional Flite Charts or Chart View charts (optional) • CHKLIST Displays the Checklist Page DONE Selects the highlighted checklist item EXIT Returns to the top-level softkeys EMERGCY Immediately accesses the emergency procedures Garmin G1000 Pilot’s Guide for the Diamond DA62 190-01895-00 Rev. A 26 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 1.6 ACCESSING G1000 FUNCTIONALITY MENUS The G1000 has a dedicated MENU Key that when pressed displays a context-sensitive list of options. This options list allows the user to access additional features or make setting changes which specifically relate to the currently displayed window/page. There is no all-encompassing menu. Some menus provide access to additional submenus that are used to view, edit, select, and review options. Menus display ‘No Options’ when there are no additional features or settings for the window/page selected. Navigating a menu: 1) Press the MENU Key to display the menu. 2) Turn the FMS Knob to scroll through a list of available options (a scroll bar always appears to the right of the window/box when the option list is longer than the window/box). 3) Press the ENT Key to select the desired option. 4) Press the CLR Key or FMS Knob to remove the menu and cancel the operation. Figure 1-21 Page Menu Examples No Options for NRST Window Options for FPL Window DATA ENTRY The FMS Knob can be used for directly entering alphanumeric data (e.g., Flight ID, waypoint identifiers, barometric minimum descent altitude) into the G1000 In some instances, such as when entering an identifier, the G1000 tries to predict the desired identifier based on the characters being entered. In this case, if the desired identifier appears, use the ENT Key to confirm the entry without entering the rest of the identifier manually. This can save the pilot from having to enter all the characters of the identifier. Besides character-by-character data entry, the system also provides a shortcut for entering waypoint identifiers. When the cursor is on a field awaiting entry of a waypoint identifier, turning the small FMS Knob counter- clockwise accesses three different lists of waypoint identifiers for quick selection: flight plan (FPL), nearest (NRST), and recently-entered (RECENT). The G1000 automatically fills in the identifier, facility, and city fields with the information for the selected waypoint. 190-01895-00 Rev. A Garmin G1000 Pilot’s Guide for the Diamond DA62 27 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Using the FMS Knob to enter data: 1) If needed, press the FMS Knob to activate the cursor. 2) Use the large FMS Knob to highlight the desired field. 3) Begin entering data. a) To quickly enter a waypoint identifier, turn the small FMS Knob counter-clockwise to display a list of waypoints in the active flight plan (list is titled FPL). If desired, turn the small FMS Knob clockwise to scroll through lists of nearest waypoints (NRST) and recently-entered waypoints (RECENT). b) Turn the large FMS Knob to highlight the desired waypoint from the list and press the ENT Key. Or: a) Turn the small FMS Knob to select a character for the first placeholder. Turning the knob clockwise scrolls through the alphabet (where appropriate) toward the letter Z, starting at K, and the digits zero through nine. Afterwards, turning the knob counter-clockwise scrolls in the opposite direction. b) Use the large FMS Knob to move the cursor to the next placeholder in the field. c) Repeat, using the small FMS Knob to select a character and the large FMS Knob to move the cursor, until the field is complete. d) Press the ENT Key to confirm entry. 4) Press the FMS Knob or CLR Key to cancel data entry (the field reverts back to its previous information). Garmin G1000 Pilot’s Guide for the Diamond DA62 190-01895-00 Rev. A 28 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX PAGE GROUPS NOTE: Refer to other supporting sections in this Pilot’s Guide for details on specific pages. Information on the MFD is presented on pages which are grouped according to function. The page group and active page title are displayed in the upper center of the screen, below the Navigation Status Box. In the bottom right corner of the screen, the current page group, number of pages available in the group, and placement of the current page within the group are indicated by icons. For some of these pages (Airport/Procedures/Weather Information, XM, Procedure Loading), the title of the page changes while the page icon remains the same. Figure 1-22 Page Title and Page Group Icons MFD Page Group Active Page Title Page Groups Selected Page Pages in Current Group There are four main page groups, navigated using the FMS Knob; specific pages within each group can vary depending on the configuration of optional equipment. Selecting a page using the FMS Knob: 1) Turn the large FMS Knob until the desired page group is selected. 2) Turn the small FMS Knob until the desired page is selected. There are also several pages (Airport/Procedures/Weather Information and XM pages) which are selected first from within a main page group with the FMS Knob, then with the appropriate softkey at the bottom of the page (or from the page menu). In this case, the page remains set to the selected page until a different page softkey is selected, even if a different page group is selected. 190-01895-00 Rev. A Garmin G1000 Pilot’s Guide for the Diamond DA62 29 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX • Map Page Group (MAP) Navigation Map Traffic Map Weather Radar (optional) Stormscope (optional) XM Weather Data Link (service optional) Terrain-SVS or Terrain Proximity Figure 1-23 Map Pages • Waypoint Page Group (WPT) Airport/Procedures/Weather Information Pages: - Airport Information (INFO-1, INFO-2 Softkeys) - Departure Information (DP Softkey) - Arrival Information (STAR Softkey) - Approach Information (APR Softkey) - Weather Information (optional) (WX Softkey) Intersection Information NDB Information VOR Information User Waypoint Information Figure 1-24 Waypoint Pages Airport, Procedures and Weather Information Pages Garmin G1000 Pilot’s Guide for the Diamond DA62 190-01895-00 Rev. A 30 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX • Auxiliary Page Group (AUX) Trip Planning Utility GPS Status System Setup Pages: - System Setup 1 (SETUP 1 Softkey) - System Setup 2 (SETUP 2 Softkey) XM Satellite Pages (optional): - XM Radio (RADIO Softkey) - XM Information (INFO Softkey) Satellite Phone - Telephone (TEL Softkey) - SMS (SMS Softkey) System Status Video (optional) Figure 1-25 Auxiliary Pages XM Pages Satellite Phone Pages System Setup Pages • Nearest Page Group (NRST) Nearest Airports Nearest Intersections Nearest NDB Nearest VOR Nearest User Waypoints Nearest Frequencies Nearest Airspaces Figure 1-26 Nearest Pages 190-01895-00 Rev. A Garmin G1000 Pilot’s Guide for the Diamond DA62 31 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX In addition to the main page groups accessed exclusively using the FMS Knob, there are pages for flight planning (FPL) and loading procedures (PROC) which are accessed by key. In some instances, softkeys may be used to access the Procedure Loading pages. The Flight Plan pages are accessed using the FPL Key on the MFD. Main pages within this group are selected by turning the small FMS Knob. Figure 1-27 Flight Plan Pages • Flight Plan Page Group (FPL) Active Flight Plan Flight Plan Catalog - Stored Flight Plan (NEW Softkey) The Procedure Loading pages may be accessed at any time on the MFD by pressing the PROC Key. A menu is initialized, and when a departure, approach, or arrival is selected, the appropriate Procedure Loading page is opened. These pages can also be accessed from the Active and Stored Flight Plan pages using the LD softkeys. Turning the FMS Knob does not scroll through the Procedure Loading pages (note the single page icon in the lower right corner). Figure 1-28 Procedure Loading Pages • Procedure Loading Page Group (PROC) Departure Loading Arrival Loading Approach Loading Information on optional electronic checklist pages is offered later in this section. Checklist pages may be accessed from any page on the MFD using the CHKLIST Softkey. Garmin G1000 Pilot’s Guide for the Diamond DA62 190-01895-00 Rev. A 32 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX SYSTEM SETTINGS G1000 system settings are managed from the System Setup Page. The following settings can be changed: • Date/time • Display Units (see Flight Instruments Section) • Baro Transition Alert (see Flight Instruments Section) • Airspace alerts (see Flight Management Section) • Arrival alerts (see Flight Management Section) • Audio Alerts • MFD Data Bar Fields (see Flight Management Section) • CDI scaling for GPS navigation source (see Flight Instruments Section) • COM channel spacing (see Audio Panel and CNS Section) • Criteria for displaying nearest airports (see Flight Management Section) Restoring system setup defaults: 1) Use the FMS Knob to select the AUX - System Setup Page. 2) Press the DFLTS Softkey. Or: a) Press the MENU Key. b) Highlight ‘Restore Defaults’ and press the ENT Key. Figure 1-29 AUX - System Setup Page 190-01895-00 Rev. A Garmin G1000 Pilot’s Guide for the Diamond DA62 33 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX DATE/TIME The G1000 obtains the current Universal Coordinated Time (UTC) date and time directly from the GPS satellite signals (shown on the AUX - GPS Status Page, Figure 1-11). System time (displayed in the lower right corner of the PFD) can be displayed in three formats: local 12-hr, local 24-hr, or UTC. Local time is set by adding/subtracting an offset (hours:minutes) to/from UTC. Figure 1-30 System Time (Local 24-hr Format) PFD Configuring the system time: 1) Select the AUX - System Setup Page using the FMS Knob. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the ‘Time Format’ field. 4) Turn the small FMS Knob to select the desired format and press the ENT Key to confirm selection. The ‘Time Offset’ field is highlighted. 5) Use the FMS Knob to enter the desired time offset (±HH:MM) and press the ENT Key to confirm selection. Figure 1-31 Date/Time Settings (AUX - System Setup Page) Garmin G1000 Pilot’s Guide for the Diamond DA62 190-01895-00 Rev. A 34 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX DISPLAY UNITS Units in which various quantities are displayed on the G1000 screens are listed on the System Setup Page. The Navigation Angle reference can be set from here (refer to the Flight Instruments Section). Figure 1-32 Display Unit Settings (AUX - System Setup Page) Category Settings Affected Quantities Exceptions Navigation Angle Magnetic (North) True (North) Heading Course Bearing Track Desired Track Wind direction (Trip Planning Page) Distance and Speed Metric Nautical Crosstrack error (HSI) Bearing distances (information windows) DME distance (information window) Flight plan distances Map ranges DIS, GS, TAS, XTK fields (Navigation Status Box) All distances on MFD Altitude buffer distance (System Setup) Arrival Alert trigger distance (System Setup) All speeds on MFD Airspeed Indicator True Airspeed (PFD) Wind speed vector Map range (Traffic Page, Terrain Proximity/TAWS Page) CDI scaling (System Setup) Fuel range calculation (EIS) Altitude and Vertical Speed Feet Meters All altitudes on MFD All elevations on MFD Altimeter Vertical Speed Indicator VNV altitudes (Active Flight Plan) Temperature Celsius Fahrenheit All temperatures on PFD Total Air Temperature (Trip Planning Page) Engine Indication System (EIS) 190-01895-00 Rev. A Garmin G1000 Pilot’s Guide for the Diamond DA62 35 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Category Settings Affected Quantities Exceptions Fuel and Fuel Flow Gallons Imp Gallons Kilograms Liters Pounds Fuel parameters (Trip Planning Page) Engine Indication System (EIS) Weight Pounds Kilograms N/A N/A Position HDDD°MM.MM’ HDDD°MM’SS.S” MGRS UTM/UPS All positions N/A Table 1-1 Display Units Settings (AUX - System Setup Page) Garmin G1000 Pilot’s Guide for the Diamond DA62 190-01895-00 Rev. A 36 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX PILOT PROFILES System settings may be saved under a pilot profile. When the system is powered on, the last selected pilot profile is shown on the MFD Power-up Screen (Figure 1-5). The G1000 can store up to 25 profiles; the currently active profile, the amount of memory used, and the amount of memory available are shown at the top of the System Setup Page in the box labeled ‘Pilot Profile’. From here, pilot profiles may be created, selected, renamed, or deleted. Figure 1-33 Pilot Profile Settings (AUX - System Setup Page) Creating a profile: 1) Use the FMS Knob to select the AUX - System Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight ‘CREATE’ in the Pilot Profile Box. 4) Press the ENT Key. A ‘Create Profile’ window is displayed. 5) Use the FMS Knob to enter a profile name up to 16 characters long and press the ENT Key. Pilot profile names cannot begin with a blank as the first letter. 6) In the next field, use the small FMS Knob to select the desired settings upon which to base the new profile. Profiles can be created based on Garmin factory defaults, default profile settings (initially based on Garmin factory defaults unless edited by the pilot), or current system settings. 7) Press the ENT Key. 190-01895-00 Rev. A Garmin G1000 Pilot’s Guide for the Diamond DA62 37 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 8) With ‘CREATE’ highlighted, press the ENT Key to create the profile Or: Use the large FMS Knob to select ‘CREATE and ACTIVATE’ and press the ENT Key to activate the new profile. 9) To cancel the process, select ‘CANCEL’ with the large FMS Knob and press the ENT Key. Selecting an active profile: 1) Use the FMS Knob to select the AUX - System Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight the active profile field in the Pilot Profile Box. 4) Turn the small FMS Knob to display the pilot profile list and highlight the desired profile. 5) Press the ENT Key. The G1000 loads and displays the system settings for the selected profile. Renaming a profile: 1) Use the FMS Knob to select the AUX - System Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight ‘RENAME’ in the Pilot Profile Box. 4) Press the ENT Key. 5) In the ‘Rename Profile’ window, turn the FMS Knob to select the profile to rename. 6) Press the ENT Key. 7) Use the FMS Knob to enter a new profile name up to 16 characters long and press the ENT Key. 8) With ‘RENAME’ highlighted, press the ENT Key. 9) To cancel the process, use the large FMS Knob to select ‘CANCEL’ and press the ENT Key. Deleting a profile: 1) Use the FMS Knob to select the AUX - System Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight ‘DELETE’ in the Pilot Profile Box. 4) Press the ENT Key. 5) In the ‘Delete Profile’ window, turn the FMS Knob to select the profile to delete. 6) Press the ENT Key. 7) With ‘DELETE’ highlighted, press the ENT Key. 8) To cancel the process, use the large FMS Knob to select ‘CANCEL’ and press the ENT Key. Garmin G1000 Pilot’s Guide for the Diamond DA62 190-01895-00 Rev. A 38 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEAT