Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN

WARNING: The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and could vary significantly from the altitude displayed by pressure altimeters, such as the GDC 74 Air Data Computer, or other altimeters in aircraft. GPS altitude should never be used for vertical navigation. Always use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft. WARNING: Do not use outdated database information.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 Pilots using any outdated database do so entirely at their own risk.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: Do not rely solely upon the display of traffic information for collision avoidance maneuvering. The traffic display does not provide collision avoidance resolution advisories and does not under any circumstances or conditions relieve the pilot’s responsibility to see and avoid other aircraft. WARNING: Do not rely solely upon the display of traffic information to accurately depict all of the traffic within range of the aircraft. Due to lack of equipment, poor signal reception, and/or inaccurate information from aircraft or ground stations, traffic may be present that is not represented on the display. WARNING: Do not rely on information from a lightning detection system display as the sole basis for hazardous weather avoidance. Range limitations and interference may cause the system to display inaccurate or incomplete information. Refer to documentation from the lightning detection system manufacturer for detailed information about the system. WARNING: Do not use data link weather information for maneuvering in, near, or around areas of hazardous weather. Information contained within data link weather products may not accurately depict current weather conditions. WARNING: Do not use the indicated data link weather product age to determine the age of the weather information shown by the data link weather product. Due to time delays inherent in gathering and processing weather data for data link transmission, the weather information shown by the data link weather product may be significantly older than the indicated weather product age. Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 190-00647-03 Rev. A ii WARNINGS, CAUTIONS, AND NOTES WARNING: For safety reasons, G1000 operational procedures must be learned on the ground. WARNING: The Garmin system, 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. 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 G1000 Integrated Avionics System in 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: Do not use the system to attempt to penetrate a thunderstorm. The illustrations in this guide are only examples. Both the FAA Advisory Circular, Subject: Thunderstorms, and the Aeronautical Information Manual (AIM) recommend avoiding any thunderstorm identified as severe of giving intense radar echo by at least 20 miles. 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 system 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) 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. 190-00647-03 Rev. A Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN iii WARNINGS, CAUTIONS, AND NOTES 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 Stormscope, 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: Do not rely solely upon data link services to provide Temporary Flight Restriction (TFR) information. Always confirm TFR information through official sources such as Flight Service Stations or Air Traffic Control. 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 and aviation databases. 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 yards 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. 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. Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 190-00647-03 Rev. A iv WARNINGS, CAUTIONS, AND NOTES 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.’ 190-00647-03 Rev. A Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN v REVISION INFORMATION Record of Revisions Part Number Revision Date Page Range Description 190-00647-00 A 7-19-06 All Initial release 190-00647-01 A B 3-3-08 3-4-08 All All Update to GDU 8.20, added WAAS Revise System Software version number 190-00647-02 A 11-20-08 All Update to GDU 9.03, added SVS 190-00647-03 A 9-5-14 All Update to GDU 14.02 Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 190-00647-03 Rev. A vi TABLE OF CONTENTS SECTION 1 SYSTEM OVERVIEW 1.1 System Description ................................................. 1 1.2 Line Replaceable Units ........................................... 2 1.3 Secure Digital (SD) Cards ....................................... 7 1.4 System Power-Up .................................................... 8 1.5 System Operation .................................................... 9 Normal Display Operation ............................................. 9 Reversionary Display Operation ..................................... 9 G1000 System Annunciations ...................................... 10 AHRS Operation ......................................................... 11 1.6 G1000 Controls...................................................... 13 PFD/MFD Controls ...................................................... 13 Softkey Function ......................................................... 15 1.7 Accessing G1000 Functionality............................ 22 Menus ....................................................................... 22 Data Entry.................................................................. 22 Page Groups .............................................................. 23 System Setup and Status ............................................. 27 1.8 Display Backlighting ............................................. 40 SECTION 2 FLIGHT INSTRUMENTS 2.1 Flight Instruments ................................................. 44 Airspeed Indicator ...................................................... 44 Attitude Indicator ....................................................... 46 Altimeter ................................................................... 47 Vertical Speed Indicator (VSI) ....................................... 49 Vertical Deviation ....................................................... 49 Horizontal Situation Indicator (HSI) .............................. 50 Course Deviation Indicator (CDI) .................................. 55 2.2 Supplemental Flight Data .................................... 62 Temperature Displays .................................................. 62 Wind Data ................................................................. 63 Vertical Navigation (VNV) Indications ........................... 64 2.3 PFD Annunciations and Alerting Functions ........ 65 System Alerting .......................................................... 65 Marker Beacon Annunciations...................................... 66 Traffic Annunciation .................................................... 66 Terrain Annunciations ................................................. 67 Altitude Alerting ......................................................... 67 Low Altitude Annunciation .......................................... 68 Minimum Descent Altitude/Decision Height Alerting ...... 68 2.4 Abnormal Operations ........................................... 70 Abnormal GPS Conditions ........................................... 70 Heading Failure Modes................................................ 71 Unusual Attitudes ....................................................... 71 SECTION 3 ENGINE INDICATION SYSTEM 3.1 EIS Display.............................................................. 74 3.2 Engine Page............................................................ 76 Fuel Calculations ........................................................ 79 3.3 Leaning Assist Mode ............................................. 80 3.4 EIS Display in Reversionary Mode....................... 81 Lean Display .............................................................. 83 System 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 Mode S Transponder .............................. 116 Transponder Controls ................................................ 116 Transponder Mode Selection ...................................... 117 Entering a Transponder Code ..................................... 120 IDENT Function ........................................................ 121 ADS-B TX ................................................................. 121 Flight ID Reporting.................................................... 122 4.5 Additional Audio Panel Functions ..................... 123 Power-up ................................................................. 123 Mono/Stereo Headsets .............................................. 123 190-00647-03 Rev. A Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN vii TABLE OF CONTENTS Speaker ................................................................... 123 Intercom .................................................................. 124 Passenger Address (PA) System .................................. 126 Clearance Recorder and Player................................... 126 Split COM ................................................................ 127 Entertainment Inputs ................................................ 128 4.6 Audio Panel Preflight Procedure ....................... 129 4.7 Abnormal Operation ........................................... 130 Stuck Microphone..................................................... 130 COM Tuning Failure................................................... 130 Audio Panel Fail-safe Operation ................................. 130 Reversionary Mode ................................................... 130 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 ................................ 142 Topography .............................................................. 143 Map Symbols ........................................................... 146 Airways ................................................................... 152 Track Vector ............................................................. 154 Wind Vector ............................................................. 155 Nav Range Ring........................................................ 156 Fuel Range Ring ....................................................... 157 Field of View (SVT) .................................................... 158 Selected Altitude Intercept Arc ................................... 159 5.3 Waypoints............................................................. 160 Airports ................................................................... 161 Intersections ............................................................ 168 NDBs ....................................................................... 170 VORs ....................................................................... 172 User Waypoints ........................................................ 174 5.4 Airspaces .............................................................. 180 5.5 Direct-to-Navigation .......................................... 184 5.6 Flight Planning..................................................... 189 Flight Plan Creation .................................................. 190 Adding Waypoints to an Existing Flight Plan................ 195 Adding Airways to a Flight Plan ................................. 197 Adding Procedures to a Stored Flight Plan .................. 199 Flight Plan Storage ................................................... 206 Flight Plan Editing .................................................... 208 Along Track Offsets ................................................... 211 Parallel Track ............................................................ 213 Activating a Flight Plan Leg ....................................... 216 Inverting a Flight Plan ............................................... 217 Flight Plan Views ...................................................... 218 Closest Point of FPL .................................................. 220 User-Defined Holding Patterns ................................... 220 5.7 Vertical Navigation ............................................. 225 Altitude Constraints .................................................. 227 5.8 Procedures ........................................................... 231 Departures ............................................................... 232 Arrivals ................................................................... 235 Approaches ............................................................. 238 5.9 Trip Planning ........................................................ 246 Trip Planning ............................................................ 246 5.10 RAIM Prediction................................................... 250 5.11 Navigating a Flight Plan ..................................... 253 5.12 Abnormal Operation ........................................... 281 SECTION 6 HAZARD AVOIDANCE 6.1 SiriusXM Weather ................................................ 284 Activating Services.................................................... 284 Accessing SiriusXM Weather Products ........................ 285 SiriusXM Weather Abnormal Operations ..................... 318 6.2 WX-500 Stormscope ........................................... 320 Setting Up Stormscope on the Navigation Map ........... 320 Selecting the Stormscope Page .................................. 324 6.3 Terrain Proximity ................................................. 326 Displaying Terrain Proximity Data ............................... 326 6.4 Profile View Terrain ............................................. 331 Profile View Display .................................................. 332 6.5 Terrain-SVS ........................................................... 335 Displaying Terrain-SVS Data ....................................... 336 Terrain-SVS Page ...................................................... 338 Terrain-SVS Alerts ..................................................... 340 System Status........................................................... 343 6.6 TAWS-B ................................................................. 344 Displaying TAWS-B Data ............................................ 345 TAWS-B Page ........................................................... 348 Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 190-00647-03 Rev. A viii TABLE OF CONTENTS TAWS-B Alerts .......................................................... 350 System Status........................................................... 356 6.7 Traffic Information Service (TIS) ........................ 358 Displaying Traffic Data .............................................. 359 Traffic Map Page....................................................... 361 TIS Alerts ................................................................. 362 System Status........................................................... 363 6.8 SKY497 Traffic ...................................................... 366 TAS Symbology......................................................... 366 Operation ................................................................ 367 Altitude Display ........................................................ 369 Traffic Map Page Display Range ................................. 370 TAS Alerts ................................................................ 371 System Status........................................................... 372 SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM 7.1 AFCS Controls ...................................................... 374 7.2 Flight Director Operation ................................... 376 Activating the Flight Director ..................................... 376 AFCS Status Box ....................................................... 377 Command Bars ......................................................... 378 Flight Director Modes................................................ 378 7.3 Vertical Modes ..................................................... 379 Pitch Hold Mode (PIT) ............................................... 380 Selected Altitude Capture Mode (ALTS) ....................... 381 Altitude Hold Mode (ALT) .......................................... 382 Vertical Speed Mode (VS) .......................................... 383 Flight Level Change Mode (FLC) ................................. 384 Vertical Navigation Modes (VPTH, ALTV) ..................... 386 Glidepath Mode (GP) (WAAS only) ............................. 391 Glideslope Mode (GS) ............................................... 392 Go Around Mode (GA) .............................................. 393 7.4 Lateral Modes ...................................................... 394 Roll Hold Mode (ROL) ............................................... 395 Heading Select Mode (HDG) ...................................... 396 Navigation Modes (GPS, VOR, LOC, BC) ...................... 397 Approach Modes (GPS, VAPP, LOC) ............................. 399 7.5 Autopilot Operation............................................ 401 Engaging the Autopilot ............................................. 401 Control Wheel Steering ............................................. 402 Disengaging the Autopilot ......................................... 402 7.6 Example Flight Plan ............................................ 403 Departure ................................................................ 404 Intercepting a VOR Radial .......................................... 406 Flying a Flight Plan/GPS Course ................................. 407 Descent ................................................................... 408 Approach ................................................................. 412 Go Around/Missed Approach ..................................... 414 7.7 AFCS Annunciations and Alerts ......................... 416 AFCS Status Alerts .................................................... 416 Overspeed Protection ................................................ 417 SECTION 8 ADDITIONAL FEATURES 8.1 Synthetic Vision Technology (SVT)..................... 420 SVT Operation .......................................................... 421 SVT Features ............................................................ 423 Field of View ............................................................ 432 8.2 SafeTaxi ................................................................ 434 SafeTaxi Cycle Number and Revision .......................... 437 8.3 ChartView ............................................................. 440 ChartView Softkeys ................................................... 441 Terminal Procedures Charts ....................................... 442 Chart Options........................................................... 450 Day/Night View ........................................................ 455 ChartView Cycle Number and Expiration Date ............. 458 8.4 FliteCharts ............................................................ 461 FliteCharts Softkeys .................................................. 462 Terminal Procedures Charts ....................................... 463 Chart Options........................................................... 470 Day/Night View ........................................................ 474 FliteCharts Cycle Number and Expiration Date............. 476 8.5 Airport Directory ................................................. 479 Airport Directory Database Cycle Number and Revision 480 8.6 SiriusXM Radio Entertainment (Optional)........ 482 Activating SiriusXM Satellite Radio Services ................ 482 Using SiriusXM Radio................................................ 484 8.7 Scheduler.............................................................. 488 8.8 Abnormal Operation ........................................... 490 SVT Troubleshooting ................................................. 490 Reversionary Mode ................................................... 490 Unusual Attitudes ..................................................... 491 190-00647-03 Rev. A Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN ix TABLE OF CONTENTS APPENDICES Annunciations and Alerts ............................................. 495 G1000 System Annunciations .................................... 496 G1000 System Message Advisories............................. 497 AFCS Alerts .............................................................. 509 Terrain-SVT Alerts ..................................................... 510 Terrain-SVT System Status Annunciations .................... 510 TAWS Alerts ............................................................. 511 TAWS System Status Annunciations ............................ 512 Flight Plan Import/Export Messages ........................... 513 Pilot Profile Import/Export Messages .......................... 514 Database Management ................................................ 515 Jeppesen Databases.................................................. 516 Garmin Databases .................................................... 520 Garmin Aviation Glossary ............................................ 525 Frequently Asked Questions ........................................ 533 Map Symbols ................................................................. 537 INDEX Index ................................................................................ I-1 Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 190-00647-03 Rev. A x TABLE OF CONTENTS Blank Page 190-00647-03 Rev. A Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 1 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX SECTION 1 SYSTEM OVERVIEW 1.1 SYSTEM DESCRIPTION NOTE: Refer to the Automatic Flight Control System (AFCS) Section for details on the Garmin AFCS. The G1000 is an integrated flight deck system that presents flight instrumentation, position, navigation, communication, and identification information to the pilot using flat-panel color displays. The system consists of the following Line Replaceable Units (LRUs): • GDU 1040 Primary Flight Display (PFD) • GDU 1042/1044 Multi Function Display (MFD) • GMA 1347 Audio Panel with Integrated Marker Beacon Receiver • GIA 63(W) 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 69A Data Link Receiver • GSA 81 AFCS Servos • GSM 85 Servo Gearbox Figure 1-1 shows interactions between the LRUs. Additional/optional equipment are shown in Figure 1-2. The Mooney M20M/M20R/M20TN is equipped with a Garmin Automated Flight Control System (AFCS), providing flight director (FD), autopilot (AP), and manual electric trim (MET) functions of the G1000 System. Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 190-00647-03 Rev. A 2 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 1.2 LINE REPLACEABLE UNITS • GDU 1040 – A GDU 1040 is configured as the Primary Flight Display (PFD). The display is a 10.4-inch LCD screen 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. • GDU 1042/1044 – A GDU 1040 or 1042/1044 (for airframes equipped with the Garmin AFCS) is configured as a Multi Function Display (MFD). The display is a 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 1.5, System Operation) and communicates with both IAUs using an RS-232 digital interface. 190-00647-03 Rev. A Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 3 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX • GIA 63(W) (2) – Functions as the main communication hub, linking all LRUs with the on-side PFD. Each GIA 63W contains a GPS WAAS receiver, VHF COM/NAV/GS receivers, a flight director (FD) and system integration microprocessors. Each GIA 63W is paired with the on-side PFD via HSDB connection. The GIA 63Ws are not paired together and do not communicate with each other directly. 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 – The solid-state Transponder provides Modes A, C, and S capability and communicates with both IAUs through an RS-232 digital interface. Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 190-00647-03 Rev. A 4 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX • GRS 77 – 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 1.5, 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 69A – The Data Link Satellite Radio Receiver provides real-time weather information to MFD maps and the PFD Inset Map, as well as 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 81 and GSM 85 – The GSA 81 servos are used for automatic control of pitch, pitch trim, and roll. These units interface with each IAU. The GSM 85 servo gearboxes are responsible for transferring the output torque of the servo actuators to the mechanical flight-control surface linkages. 190-00647-03 Rev. A Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 5 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Figure 1-1 Basic G1000 System Block Diagram GSA 81 Roll Servo Autopilot Calculations (optional) GSA 81 Pitch Servo Autopilot 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 Glideslope Flight Director (with AFCS option) No. 2 GIA 63W Integrated Avionics Unit System Integration Processors I/O Processors VHF COM VHF NAV/LOC GPS Glideslope GTX 33 Transponder High-Speed Data Bus (Ethernet) Reversionary Control GEA 71 Engine/Airframe Unit GDC 74A Air Data Computer OAT Airspeed Altitude Vertical Speed GRS 77 AHRS Attitude Rate of Turn Slip/Skid GMU 44 Magnetometer Heading GPS Output GPS Output Reversionary Control GMA 1347 Audio Panel GDU 1040 (PFD) GDU 1040 or GDU 1042/1044 (MFD) Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 190-00647-03 Rev. A 6 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX High-Speed Data Bus (Ethernet) No. 2 GIA 63W Integrated Avionics Unit System Integration Processors I/O Processors VHF COM VHF NAV/LOC GPS Glideslope GDL 69A Data Link Real-time Weather and Digital Audio Entertainment (subscription-based service) L3 Stormscope WX-500 Honeywell KN 63 DME L3 SKYWATCH TAS Becker 3250 ADF Figure 1-2 G1000 System Block Diagram With Options NOTE: For information on additional equipment shown in Figure 1-2, consult the applicable user’s guide and the appropriate sections of this pilot’s guide. This document assumes that the reader is already familiar with the operation of this additional equipment. 190-00647-03 Rev. A Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 7 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 1.3 SECURE DIGITAL (SD) CARDS NOTE: Ensure the G1000 System is powered off before inserting an SD card. NOTE: Refer to Appendix B for instructions on updating the aviation database. 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 (the front of the card should be 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 Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 190-00647-03 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 POWER-UP NOTE: See the Aircraft Flight Manual (AFM) for specific procedures concerning avionics power application and emergency power supply operation. NOTE: Refer to Appendix A 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 in a straight line and during level flight. When the MFD powers up, the splash screen (Figure 1-5) displays the following information: • System version • Copyright • Land database name and version • Terrain database name and version • Airport Terrain database name and version • Obstacle database name and version • Aviation database name, version, and effective dates • ChartView or FliteCharts database information • Safe Taxi database information 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 (or right-most softkey) acknowledges this information, and the Navigation Map Page is displayed upon pressing the key a second time. 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 MFD Power-Up Splash Screen 190-00647-03 Rev. A Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 9 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 1.5 SYSTEM OPERATION 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. Normal and reversionary G1000 display operation, as well as the various AHRS modes and G1000 System Annunciations are discussed here. NORMAL DISPLAY OPERATION 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 GPS Navigation 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 REVERSIONARY DISPLAY OPERATION NOTE: The G1000 System alerts the pilot when backup paths are utilized by the LRUs. Refer to Appendix A for further information regarding system-specific alerts. 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 the event of a display failure, the G1000 System automatically switches to reversionary (backup) mode. In Reversionary Mode, all important flight information is presented on the remaining display in the same format as in normal operating mode. 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. Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 190-00647-03 Rev. A 10 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. Figure 1-7 G1000 Reversionary Mode (Failed PFD) Pressing the DISPLAY BACKUP Button also activates/deactivates Reversionary Mode. NAV1 and COM1 (provided by the failed PFD) are flagged as 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). For a detailed description of all annunciations and alerts, refer to Appendix A. Refer to the Aircraft Flight Manual (AFM) for additional information regarding pilot responses to these annunciations. 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 GEA 71 or GIA 63(W) GTX 33 or GIA 63(W) GDC 74A GIA 63(W) GDC 74A GIA 63(W) GRS 77 or GMU 44 GIA 63(W) GIA 63(W) 190-00647-03 Rev. A Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 11 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. In addition to using internal sensors, the GRS 77 AHRS uses GPS information, magnetic field data and air data to assist in attitude/heading calculations. In normal mode, the AHRS relies upon GPS and magnetic field measurements. If either of these external measurements is unavailable or invalid, the AHRS uses air data information for attitude determination. Four AHRS modes of operation are available (see Figure 1-14) and depend upon the combination of available sensor inputs. Loss of air data, GPS, or magnetometer sensor inputs is communicated to the pilot by message advisory alerts. The AHRS (GRS 77) corrects for shifts and variations in the Earth’s magnetic field by applying the Magnetic Field Variation Database. The Magnetic Field Variation Database is derived from the International Geomagnetic Reference Field (IGRF). The IGRF is a mathematical model that describes the Earth’s main magnetic field and its annual rate of change. The database is updated approximately every 5 years. See the Appendices for information on updating the Magnetic Field Variation Database. The system will prompt you on startup when an update is available. Failure to update this database could lead to erroneous heading information being displayed to the pilot. AHRS no-GPS Mode AHRS coast-on-gyros until invalid AHRS Normal Mode AHRS no-Mag Mode AHRS no-Mag/ no-Air Mode Heading Invalid Heading Invalid Attitude/Heading Invalid YES YES YES NO NO NO Air Data Available and Reliable? Mag Data Available and Reliable? YES NO Mag Data AND Air Data Available and Reliable? GPS Data Available and Reliable? Figure 1-9 AHRS Operation Loss of GPS, magnetometer, or air data inputs is communicated to the pilot by message advisory alerts. 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). Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 190-00647-03 Rev. A 12 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 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(s) as long as magnetometer and airspeed data are available and valid. If the magnetometer input fails, the AHRS continues to output valid attitude information. If GPS-based track information is available while magnetometer input has failed, the HSI displays the ground track instead of heading using HSI Track Mode. In this mode, a magenta ‘TRK’ annunciation and track readout appear on the HSI. In addition, a yellow ‘HDG’ annunciation with a red X appear above the ‘TRK’ annunciation to indicate the HSI is displaying track instead of heading. If both the heading and track are unavailable, the HSI displays a yellow ‘HDG’ annunciation with a red X over the heading readout box. The system also removes directional numbers and letters from the HSI. Figure 1-10 Heading Failure Displays on the HSI HSI Track Mode (Heading Unavailable, Track Available) Heading and Track Unavailable 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. 190-00647-03 Rev. A Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 13 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 1.6 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 1-11 PFD/MFD Controls 17 18 5 6 8 7 2 4 3 1 9 15 14 13 12 16 11 10 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 light blue 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 Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 190-00647-03 Rev. A 14 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 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 light blue 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 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) 190-00647-03 Rev. A Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 15 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 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 1-12 Dual Concentric Knob 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. Softkey Names (Displayed) Figure 1-13 Softkeys (Second-Level PFD Configuration) Bezel- Mounted Softkeys (Press) Softkey On 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). Figure 1-14 Top-level PFD Softkeys BACK DCLTR TOPO ALERTS NEXRAD (optional) TERRAIN OFF INSET XM LTNG METAR WX LGND (optional) (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) STRMSCP (optional) (optional) Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 190-00647-03 Rev. A 16 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 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: Declutters land data DCLTR-2: Declutters land and SUA data DCLTR-3: Removes everything except for the active flight plan WX LGND Displays icon and age on the Inset Map for the selected weather products (optional) TRAFFIC Displays traffic information on Inset Map TRAFFIC: No Traffic displayed on Inset Map TRFC-1: Traffic displayed on Inset Map TRFC-2: Traffic Only display shown TOPO Displays topographical data (e.g., coastlines, terrain, rivers, lakes) and elevation scale on Inset Map TERRAIN Displays terrain information on Inset Map STRMSCP Displays Stormscope information on Inset Map (optional) NEXRAD Displays NEXRAD weather and coverage on Inset Map (optional) XM LTNG Displays XM lightning information on Inset Map (optional) METAR Displays METAR information on Inset Map (optional) 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 OFF INSET XM LTNG METAR WX LGND (optional) (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) Press the BACK Softkey to return to the top-level softkeys. XPDR STBY ON ALT VFR BACK ALERTS IDENT ADSB-TX CODE IDENT BACK ALERTS 0 1 2 3 4 5 6 7 BKSP TRFC-1 TRFC-2 STRMSCP (optional) (optional) GND (optional) Figure 1-15 INSET Softkeys 190-00647-03 Rev. A Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 17 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 configurations SYN VIS Displays the softkeys for enabling or disabling Synthetic Vision features 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 wind data parameters OPTN 1 Longitudinal and lateral components OPTN 2 Total direction and speed OPTN 3 Total direction with head and crosswind speed components OFF Information not displayed DME Displays/removes the DME Information Window (optional) BRG1 Cycles the Bearing 1 Information Window through NAV1, GPS/ waypoint identifier and GPS- derived distance information, and ADF/frequency. HSI FRMT Displays the softkeys for selecting the two HSI formats 360 HSI Displays HSI as a 360° compass rose ARC HSI Displays HSI as a 140° viewable arc BRG2 Cycles the Bearing 2 Information Window through NAV2 or GPS waypoint identifier and GPS-derived distance information, and ADF/frequency. ALT UNIT Displays softkeys for setting the altimeter and BARO settings to metric units METERS When enabled, displays altimeter in meters IN Press to display the BARO setting as inches of mercury HPA Press to display the BARO setting as hectopacals STD BARO Sets barometric pressure to 29.92 in Hg (1013 hPa if metric units are selected) OBS Selects OBS mode on the CDI when navigating by GPS (only available with active leg) CDI Cycles through GPS, VOR1, and VOR2 navigation modes on the CDI ADF/DME Displays/removes ADF/DME Radio Tuning Window (optional; may appear as blank, ADF, DME, or ADF/DME depending on installation) Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 190-00647-03 Rev. A 18 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Select the STD BARO or BACK Softkey to return to the top-level softkeys ALT UNIT ADF/DME HSI FMT SYN VIS BACK 360 HSI ARC HSI METERS IN HPA SYN TERR HRZN HDG PATHWAY APTSIGNS (optional) ALERTS ALERTS ALERTS ALERTS ALERTS ALERTS Figure 1-16 PFD Configuration Softkeys 190-00647-03 Rev. A Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 19 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 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, the transponder does not allow Mode A and Mode C replies, but it 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 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 NRST Displays/removes Nearest Airports Window ALERTS Displays/removes Alerts Window Figure 1-17 XPDR Softkeys 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 OFF INSET XM LTNG METAR WX LGND (optional) (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) 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 BACK ALERTS IDENT ADSB-TX CODE IDENT BACK ALERTS 0 1 2 3 4 5 6 7 BKSP TRFC-1 TRFC-2 STRMSCP (optional) (optional) GND (optional) Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 190-00647-03 Rev. A 20 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. Press the ENGINE Softkey to return to the top-level softkeys. ENGINE ENGINE BACK (optional) (optional) NEXRAD TERRAIN AIRWAYS (optional) (optional) (optional) XM LTNG METAR LEGEND TOPO MAP TRAFFIC PROFILE MAP ENGINE CHKLIST CHKLIST The DONE Softkey label changes to UNDO when the checklist item is already checked. EXIT DONE ENGINE CHKLIST EMERGCY CHKLIST DCLTR SHW CHRT DCLTR-2 DCLTR-3 DCLTR-1 Press the BACK Softkey to return to the top-level softkeys. LEAN INC FUEL RST FUEL DEC FUEL STRMSCP Figure 1-18 Navigation Map Page Softkeys ENGINE Displays second-level engine softkeys (see the EIS Section for more information) LEAN Displays the EIS Lean Display (softkeys for engine leaning assist are shown when selected) DEC FUEL Decreases calculated fuel remaining by 1 lb for each softkey press INC FUEL Increases calculated fuel remaining by 1 lb for each softkey press RST FUEL Resets calculated fuel remaining to maximum capacity and resets fuel used to zero 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 (Default label is dependent on map setup option selected) Displays airways on the map; cycles through the following: AIRWAYS: No airways are displayed AIRWY ON: All airways are displayed AIRWY LO: Only low altitude airways are displayed AIRWY HI: Only high altitude airways are displayed STRMSCP Displays/removes Stormscope information on Navigation Map (optional) NEXRAD Displays/removes NEXRAD weather and coverage information on Navigation Map Page (optional) XM LTNG Displays/removes XM lightning information on Navigation Map Page (optional) XM LTNG Displays/removes XM lightning information on Navigation Map (optional) METAR Displays/removes METAR information on Navigation Map (optional) BACK Returns to top-level softkeys 190-00647-03 Rev. A Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 21 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 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 When available, displays optional airport and terminal procedure charts CHKLIST When available, displays optional checklists Press the ENGINE Softkey to return to the top-level softkeys. ENGINE ENGINE BACK (optional) (optional) NEXRAD TERRAIN AIRWAYS (optional) (optional) (optional) XM LTNG METAR LEGEND TOPO MAP TRAFFIC PROFILE MAP ENGINE CHKLIST CHKLIST The DONE Softkey label changes to UNDO when the checklist item is already checked. EXIT DONE ENGINE CHKLIST EMERGCY CHKLIST DCLTR SHW CHRT DCLTR-2 DCLTR-3 DCLTR-1 Press the BACK Softkey to return to the top-level softkeys. LEAN INC FUEL RST FUEL DEC FUEL STRMSCP Figure 1-19 ENGINE Softkeys Press the ENGINE Softkey to return to the top-level softkeys. ENGINE ENGINE BACK (optional) (optional) NEXRAD TERRAIN AIRWAYS (optional) (optional) (optional) XM LTNG METAR LEGEND TOPO MAP TRAFFIC PROFILE MAP ENGINE CHKLIST CHKLIST The DONE Softkey label changes to UNDO when the checklist item is already checked. EXIT DONE ENGINE CHKLIST EMERGCY CHKLIST DCLTR SHW CHRT DCLTR-2 DCLTR-3 DCLTR-1 Press the BACK Softkey to return to the top-level softkeys. LEAN INC FUEL RST FUEL DEC FUEL STRMSCP Figure 1-20 MAP Softkeys Press the ENGINE Softkey to return to the top-level softkeys. ENGINE ENGINE BACK (optional) (optional) NEXRAD TERRAIN AIRWAYS (optional) (optional) (optional) XM LTNG METAR LEGEND TOPO MAP TRAFFIC PROFILE MAP ENGINE CHKLIST CHKLIST The DONE Softkey label changes to UNDO when the checklist item is already checked. EXIT DONE ENGINE CHKLIST EMERGCY CHKLIST DCLTR SHW CHRT DCLTR-2 DCLTR-3 DCLTR-1 Press the BACK Softkey to return to the top-level softkeys. LEAN INC FUEL RST FUEL DEC FUEL STRMSCP Figure 1-21 Checklist Softkeys Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 190-00647-03 Rev. A 22 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 1.7 ACCESSING G1000 FUNCTIONALITY MENUS NOTE: No other window can be displayed on the PFD while the PFD Setup Menu is displayed. Pressing the MENU Key while any other PFD window is displayed does not display the PFD Setup Menu. 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 settings 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 1-22 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 will try 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. 190-00647-03 Rev. A Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 23 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 by turning the small FMS Knob to select a character for the first placeholder. Turning the knob to the right scrolls through the alphabet (where appropriate) toward the letter Z, starting in the middle at K, and the digits zero through nine. Turning the knob to the left scrolls in the opposite direction. 4) Use the large FMS Knob to move the cursor to the next placeholder in the field. 5) Repeat, using the small FMS Knob to select a character and the large FMS Knob to move the cursor, until the field is complete. 6) Press the ENT Key to confirm entry. 7) Press the FMS Knob or CLR Key to cancel data entry (the field reverts back to its previous information). 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 in light blue. 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/Procedure/Weather Information, XM, Procedure Loading), the title of the page changes while the page icon remains the same. Pages for optional functions (e.g. Stormscope) will not be displayed if the function is not configured. Figure 1-23 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. Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 190-00647-03 Rev. A 24 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Figure 1-24 Map Pages • Map Page Group (MAP) Navigation Map Traffic Map Stormscope Weather Data Link Installed Terrain Function • Waypoint Page Group (WPT) Airport/Procedures/Weather Information Pages - Airport Information (INFO Softkey) - Departure Information (DP Softkey) - Arrival Information (STAR Softkey) - Approach Information (APR Softkey) - Weather Information (WX Softkey) Intersection Information NDB Information VOR Information User Waypoint Information Figure 1-25 Waypoint Pages Airport/Procedures/ Weather Information Pages 190-00647-03 Rev. A Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 25 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 XM Satellite screens - XM Information (INFO Softkey) - XM Radio (RADIO Softkey) System Status Figure 1-26 Auxiliary Pages XM Pages Maintenance data is continuously recorded by the Central Maintenance Computer (CMC). At the discretion of the Aircraft Manufacturer, this data may be displayed on an OEM DIAGNOSTICS Page accessible from within the AUX Page Group. • Nearest Page Group (NRST) Nearest Airports Nearest Intersections Nearest NDB Nearest VOR Nearest User Waypoints Nearest Frequencies Nearest Airspaces Figure 1-27 Nearest Pages Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 190-00647-03 Rev. A 26 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 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. In this case, the page remains set to the selected page until a different page softkey is pressed, even if a different page group is selected. 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 1-28 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 1-29 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. 190-00647-03 Rev. A Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 27 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX SYSTEM SETUP AND STATUS In the Auxiliary (AUX) Page Group, there are two system pages: System Setup and System Status. The System Setup Page allows management of various system parameters, while the System Status Page displays the status of all G1000 System LRUs. AUX - SYSTEM SETUP PAGE The System Setup Page allows management of the following system parameters: • Time display format (local or UTC ) • Flight Director Format (see the Flight Instruments Section) • Displayed measurement units • MFD Data Bar (Navigation Status Box) fields (see the Flight Management Section) • Barometric Transition Alert (see the Flight Instruments Section) • GPS Course Deviation Indicator (CDI) range (see the Flight Instruments Section) • Airspace alerts (see the Flight Management Section) • COM transceiver channel spacing (see the Audio Panel and CNS Section) • Arrival alert • Displayed nearest airports (see the Flight Management Section) • Audio alert voice Figure 1-30 System Setup Page Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 190-00647-03 Rev. A 28 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 Splash Screen. 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 1-31 Display Unit Settings (System Setup Page) Creating a profile: 1) 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. 190-00647-03 Rev. A Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 29 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 7) Press the ENT Key. 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) 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) 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) 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 Mooney M20M/M20R/M20TN 190-00647-03 Rev. A 30 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX If an SD card is inserted into the top slot of the MFD, pilot profiles may imported from the SD card into the system, or exported from the system to the SD card. Because system settings may vary from one airframe to another, always verify system settings from an imported profile are consistent with the desired settings. Importing a profile from an SD card: 1) Insert an SD card containing the pilot profile(s) into the top card slot on the MFD. 2) Turn the FMS Knob to select the AUX - System Setup Page. 3) Select the IMPORT Softkey. Or: a) Press the MENU Key. b) Turn the FMS Knob to highlight ‘Import Pilot Profile’ and press the ENT Key. 4) The system displays the Pilot Profile Importing window with ‘IMPORT’ highlighted. To change the selected profile to be imported from the SD card (shown as ‘SELECT FILE’), turn the large FMS Knob to highlight the profile file name, then turn the small FMS Knob to highlight a profile from the list, and press the ENT Key. 5) If desired, the profile name to be used after profile has been imported can be changed by turning the FMS Knob to highlight the ‘PROFILE NAME’ field, then use the large and small FMS Knobs to enter the name, and press the ENT Key. Imported profile names cannot begin with a blank space or be named ‘DEFAULT’, ‘GARMIN DEFAULTS’ or ‘DEFAULT SETTINGS’. 6) With ‘IMPORT’ highlighted, press the ENT Key. 7) If the imported profile name is the same as an existing profile on the system, the system displays an ‘Overwrite existing file? OK or CANCEL’ prompt. Press the ENT Key to replace profile on the system with the profile imported from the SD card, or turn the FMS Knob to highlight ‘CANCEL’ and press the ENT Key to return to the Pilot Profile Importing window. 8) If successful, the system displays ‘Pilot profile import succeeded.’ in the IMPORT RESULTS window below. With ‘OK’ highlighted, press the ENT or CLR Keys or press the FMS Knob to return to the AUX - System Setup Page. The imported profile becomes the active profile. Pilot Profile Importing and Import Results Window Pilot Profiles Available for Import from SD Card (‘STEVE’S PROFILE’ Selected) Import Successful Figure 1-32 Pilot Profile Import (AUX - System Setup Page) 190-00647-03 Rev. A Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 31 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Exporting a profile to an SD card: 1) Insert the SD card for storing the Pilot Profile into the top card slot on the MFD. 2) Turn the FMS Knob to select the AUX - System Setup Page. 3) If necessary, activate the desired pilot profile to export. Only the currently active Pilot Profile can be exported. 4) Select the EXPORT Softkey. The system displays the Pilot Profile Exporting window. Or: a) Press the MENU Key. b) Turn the FMS Knob to highlight ‘Export Pilot Profile’ and press the ENT Key. 5) To export the pilot profile using the current supplied name, press the ENT Key with ‘EXPORT’ highlighted. To change the profile file name turn the large FMS Knob to highlight the ‘SELECT FILE’ field, then enter the new name with the large and small FMS Knobs, then press the ENT Key. Then press the ENT Key with ‘EXPORT’ highlighted. 6) If the profile name to be exported is the same as an existing profile file name on the SD card, the system displays an ‘Overwrite existing file? OK or CANCEL’ prompt. Press the ENT Key to replace the profile on the SD card with the profile to be exported, or turn the FMS Knob to highlight ‘CANCEL’ and press the ENT Key to return to the Pilot Profile Exporting window without exporting the profile. 7) If successful, the EXPORT RESULTS window displays ‘Pilot profile export succeeded.’ With ‘OK’ highlighted, press the ENT or CLR Keys, or press the FMS Knob to return to the AUX - System Setup Page. Pilot Profile Exporting Window, Enter a Name to Use for Exported Profile Export Successful Figure 1-33 Pilot Profile Export on the AUX - System Setup Page Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 190-00647-03 Rev. A 32 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). 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 1-34 System Time (Local 24-hr Format) Configuring the system time: 1) Select the AUX - System Setup Page. 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 1-35 Date/Time Settings (System Setup Page) 190-00647-03 Rev. A Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 33 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, the Temperature units, and the Position units can be set from here. 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) Fuel and Fuel Flow Gallons* Imperial Gallons Kilograms Liters Pounds Fuel parameters (Trip Planning Page) Engine Indication System (EIS) Weight Pounds* Kilograms N/A N/A Position HDDD°MM.MM’* All positions N/A * Default setting Table 1-1 Display Units Settings (System Setup Page) Changing a display unit setting 1) While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor. 2) Turn the large FMS Knob to highlight the desired field in the Display Units Box. 3) Turn the small FMS Knob to select the desired units. 4) Press the ENT Key. Press the CLR Key to cancel the action without changing the units. Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 190-00647-03 Rev. A 34 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX arrival alerts The Arrival Alert Box on the System Setup Page allows arrival alerts to be turned on/off and the alert trigger distance set. An arrival alert can be set to notify the pilot with a message upon reaching a user- specified distance from the final destination (the direct-to waypoint or the last waypoint in a flight plan). Once the set distance (up to 99.9 units) has been reached, an “Arrival at [waypoint]” message is displayed in the PFD Navigation Status Box. Figure 1-36 Arrival Alert Settings (System Setup Page) Enabling/disabling an arrival alert: 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 select the ON/OFF field in the Arrival Alert Box. 4) Turn the small FMS Knob clockwise to turn the airspace alert ON or counterclockwise to turn the alert OFF. Changing the arrival alert trigger distance: 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 distance field in the Arrival Alert Box. 4) Use the FMS Knob to enter a trigger distance and press the ENT Key. aUDio alerts The Audio Alert Box on the System Setup Page allows the audio alert voice to be set to male or female. Changing the audio alert voice: 1) Use the FMS Knob to select the System Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight the voice in the Audio Alert Box. 190-00647-03 Rev. A Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 35 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 4) Turn the small FMS Knob to display and highlight the desired voice. 5) Press the ENT Key. AUX - SYSTEM STATUS PAGE The System Status Page displays the status and software version numbers for all detected system LRUs. Pertinent information on all system databases is also displayed. Active LRUs are indicated by green check marks and failed LRUs are indicated by red ‘X’s. Failed LRUs should be noted and a Mooney service center or Garmin-authorized dealer informed. Figure 1-37 Example System Status Page The LRU and ARFRM Softkeys on the System Status Page select the applicable list (LRU INFO or AIRFRAME window) through which the FMS Knob can be used to scroll information within the selected window. Selecting the MFD1 DB Softkey (label background changes to grey indicting the softkey is selected) places the cursor in the database window. Use the FMS Knob to scroll through database information for the MFD. Selecting the softkey again will change the softkey label to PFD1 DB. PFD 1 database information is now displayed in the database window. Selecting the softkey a third time will change the softkey label to PFD2 DB. PFD 2 database information is now displayed in the database window. The ANN TEST Softkey, when selected, causes an annunciation test tone to be played. Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 190-00647-03 Rev. A 36 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX UTILITY PAGE For flight planning purposes, timers, trip statistics, and a scheduler feature are provided on the AUX - Utility Page. The timers available include a stopwatch-like generic timer, a total time in flight timer, and a record of the time of departure. Trip statistics—odometer, trip odometer, and average trip and maximum groundspeeds—are displayed from the time of the last reset. Refer to the Additional Features section for a dicussion on the Scheduler and Flight Data Logger features. Figure 1-38 Utility Page timers The G1000 timers available include: • Stopwatch-like generic timers (available from the PFD Timer/References Window and on the MFD AUX - Utility Page) • Total-time-in-flight timer (MFD AUX - Utility Page) • Time since departure (MFD AUX - Utility Page) The generic timer can be set to count up or down from a specified time (HH:MM:SS). When the countdown on the timer reaches zero the digits begin to count up from zero. If the timer is reset before reaching zero on a countdown, the digits are reset to the initial value. If the timer is counting up when reset, the digits are zeroed. 190-00647-03 Rev. A Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 37 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Setting the generic timer (PFD): 1) Press the TMR/REF Softkey. 2) Turn the large FMS Knob to select the timer field (hh/mm/ss). 3) Use the FMS Knob to enter the desired time and press the ENT Key. 4) With the UP/DN field highlighted, turn the small FMS Knob to select the timer counting direction (UP/DN) and press the ENT Key. 6) With ‘START?’ highlighted, press the ENT Key to start the timer. The field changes to ‘STOP?’. 7) To stop the timer, press the ENT Key with ‘STOP?’ highlighted. The field changes to ‘RESET?’. 8) To reset the timer, press the ENT Key with ‘RESET?’ highlighted. The field changes back to ‘START?’ and the digits are reset. 9) To remove the window, press the CLR Key or the TMR/REF Softkey. Figure 1-39 Generic Timer (PFD Timer/References Window) Setting the generic timer (MFD AUX - Utility Page) 1) Use the FMS Knob to select the AUX - Utility Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the small FMS Knob to select the timer counting direction (UP/DN) and press the ENT Key. 4) If a desired starting time is desired: a) Use the large FMS Knob to highlight the HH:MM:SS field. b) Use the FMS Knob to enter the desired time and press the ENT Key. 5) Turn the large FMS Knob to highlight ‘START?’ and press the ENT Key to start the timer. The field changes to ‘STOP?’. 6) To stop the timer, press the ENT Key with ‘STOP?’ highlighted. The field changes to ‘RESET?’. 7) To reset the timer, press the ENT Key with ‘RESET?’ highlighted. The field changes back to ‘START?’ and the digits are reset. Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 190-00647-03 Rev. A 38 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Figure 1-40 Timers (MFD AUX - Utility Page) The flight timer can be set to count up from zero starting at system power-up or from the time that the aircraft lifts off; the timer can also be reset to zero at any time. Setting the flight timer starting criterion 1) Use the FMS Knob to select the AUX - Utility Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight the field next to the flight timer. 4) Turn the small FMS Knob to select the starting criterion (PWR-ON or IN-AIR) and press the ENT Key. Resetting the flight timer 1) U