Garmin G1000 Pilot’s Guide for the Beechcraft G58

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 older than the indicated weather product age. WARNING: The displayed minimum safe altitude (MSAs) are only advisory in nature and should not be relied upon as the sole source of obstacle and terrain avoidance information. Always refer to current aeronautical charts for appropriate minimum clearance altitudes. WARNING: Always obtain qualified instruction prior to operational use of this equipment. WARNING: Do not use GPS to navigate to any active waypoint identified as a ‘NON WGS84 WPT’ by a system message. ‘NON WGS84 WPT’ waypoints are derived from an unknown map reference datum that may be incompatible with the map reference datum used by GPS (known as WGS84) and may be positioned in error as displayed. WARNING: Do not rely on the autopilot to level the aircraft at the MDA/DH when flying an approach with vertical guidance. The autopilot will not level the aircraft at the MDA/DH even if the MDA/DH is set in the altitude preselect. Garmin G1000 Pilot’s Guide for the Beechcraft G58 190-00629-04 Rev. A WARNINGS, CAUTIONS, AND NOTES 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: Use appropriate primary systems for navigation, and for terrain, obstacle, and traffic avoidance. Garmin SVT is intended as an aid to situational awareness only and may not provide either the accuracy or reliability upon which to solely base decisions and/or plan maneuvers to avoid terrain, obstacles, or traffic. WARNING: Do not use the Garmin SVT runway depiction as the sole means for determining the proximity of the aircraft to the runway or for maintaining the proper approach path angle during landing. 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 operate the weather radar in a transmitting mode when personnel or objects are within the MPEL boundary. WARNING: Always position the weather radar gain setting to Calibrated for viewing the actual intensity of precipitation. Changing the gain in weather mode causes precipitation intensity to be displayed as a color not representative of the true intensity. WARNING: Do not use TAWS information for primary terrain or obstacle avoidance. TAWS is intended only to enhance situational awareness. WARNING : Do not use a QFE altimeter setting with this system. System functions will not operate properly with a QFE altimeter setting. Use only a QNH altimeter setting for height above mean sea level, or the standard pressure setting, as applicable. CAUTION: Do not clean display surfaces with abrasive cloths or cleaners containing ammonia. They will harm the anti-reflective coating. CAUTION: Do not allow repairs to be made by anyone other than an authorized Garmin service center. Unauthorized repairs or modifications could void both the warranty and affect the airworthiness of the aircraft. 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 WARNINGS, CAUTIONS, AND NOTES CAUTION: Never disconnect power to the system when loading a database. Power interruption during the database loading process could result in maintenance being required to reboot the system. 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 system panel and displays, are subject to change and may not reflect the most current system and aviation databases. Depictions of equipment may differ slightly from the actual equipment. NOTE: 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 system utilize GPS as a precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the system can be misused or misinterpreted and, therefore, become unsafe. 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. NOTE: Operating the system in the vicinity of metal buildings, metal structures, or electromagnetic fields can cause sensor differences that may result in nuisance miscompare annunciations during start up, shut down, or while taxiing. If one or more of the sensed values are unavailable, the annunciation indicates no comparison is possible. NOTE: The system responds to a terminal procedure based on data coded within that procedure in the Navigation Database. Differences in system operation may be observed among similar types of procedures due to differences in the Navigation Database coding specific to each procedure. Garmin G1000 Pilot’s Guide for the Beechcraft G58 190-00629-04 Rev. A 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 that have a Type 2 Letter of Authorization (LOA) from the FAA are assured compliance with all data quality requirements (DQRs). A copy of the Type 2 LOA is available for each applicable database and can be viewed at http://fly.garmin.com by selecting ‘Aviation Database Declarations.’ • 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 pertinent aircraft documents 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. 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 ‘Aviation Data Error Report’. NOTE: Electronic aeronautical charts displayed on this system have been shown to meet the guidance in AC 120-76D as a Type B Electronic Flight Bag (EFB) for FliteCharts and ChartView. The accuracy of the charts is subject to the chart data provider. Own-ship position on airport surface charts cannot be guaranteed to meet the accuracy specified in AC 120-76D. Possible additional requirements may make a secondary source of aeronautical charts, such as traditional paper charts or an additional electronic display, necessary on the aircraft and available to the pilot. If the secondary source of aeronautical charts is a Portable Electronic Device (PED), its use must be consistent with the guidance in AC 120-76D. 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 WARNINGS, CAUTIONS, AND NOTES NOTE: The navigation databases used in Garmin navigation systems contain Special Procedures. Prior to flying these procedures, pilots must have specific FAA authorization, training, and possession of the corresponding current, and legitimately-sourced chart (approach plate, etc.). Inclusion of the Special Procedure in the navigation database DOES NOT imply specific FAA authorization to fly the procedure. NOTE: Terrain and obstacle alerting is not available north of 89º North latitude and south of 89º South latitude. This is due to limitations present within the Terrain database and the system’s ability to process the data representing the affected areas. NOTE: The nose of the ‘own ship’ symbol represents the location of the aircraft. The center of any traffic symbol represents the location of that traffic. The traffic and own ship symbols are an abstract representation and do not reflect the physical extent of the aircraft/traffic, and should not replace other methods for identifying traffic. NOTE: Lamp(s) inside this product 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/en-US/ company/environment/recycling 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: Operate G1000 system power through at least one cycle in a period of four days of continuous operation to avoid an autonomous system reboot. Garmin G1000 Pilot’s Guide for the Beechcraft G58 190-00629-04 Rev. A WARNINGS, CAUTIONS, AND NOTES Blank Page 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 SOFTWARE LICENSE AGREEMENT SOFTWARE LICENSE AGREEMENT BY USING THE DEVICE, COMPONENT OR SYSTEM MANUFACTURED OR SOLD BY GARMIN (“THE GARMIN PRODUCT”), YOU AGREE TO BE BOUND BY THE TERMS AND CONDITIONS OF THE FOLLOWING SOFTWARE LICENSE AGREEMENT. PLEASE READ THIS AGREEMENT CAREFULLY. Garmin Ltd. and its subsidiaries (“Garmin”) grants you a limited license to use the software embedded in the Garmin Product (the “Software”) in binary executable form in the normal operation of the Garmin Product. Title, ownership rights, and intellectual property rights in and to the Software remain with Garmin and/or its third-party providers. You acknowledge that the Software is the property of Garmin and/or its third-party providers and is protected under the United States of America copyright laws and international copyright treaties. You further acknowledge that the structure, organization, and code of the Software are valuable trade secrets of Garmin and/or its third-party providers and that the Software in source code form remains a valuable trade secret of Garmin and/or its third-party providers. You agree not to reproduce, decompile, disassemble, modify, reverse assemble, reverse engineer, or reduce to human readable form the Software or any part thereof or create any derivative works based on the Software. You agree not to export or re-export the Software to any country in violation of the export control laws of the United States of America. Garmin G1000 Pilot’s Guide for the Beechcraft G58 190-00629-04 Rev. A SOFTWARE LICENSE AGREEMENT Blank Page 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 REVISION INFORMATION Record of Revisions Part Number Revision Date Page Range Description 190-00629-00 190-00629-00 A B 10/18/05 11/09/05 - All Initial Release ECO 34504: Corrected figure numbering sequence in Section 7 190-00629-01 A B 12/21/07 4/08/08 All All Reformatted PG, Updated to GDU SW version 8.10, and added WAAS Change System Software version, update description of two warning messages, delete PA function, and other minor corrections 190-00629-02 A 6/11/10 All Updated to GDU SW version 11.01, added SVS, added extended squitter, added GTS 820 TAS, and other minor corrections 190-00629-03 A B 4/9/12 11/27/17 All All Updated to GDU SW version 11.12, added profile view, added selected altitude arc, added METARs on active flight plan, and other minor corrections Clerical Added Software License Agreement Updated Warnings, Cautions, and Notes section 190-00629-04 A 6/11/19 All Added support for ADS-B out Added User Defined Holding Patterns Added support for Geo-Referencing on charts Updated Approach types Added Temperature Compensated Altitudes Updated System Setup information Updated TAWS-B information Updated Transponder information Updated Sirius XM radio information Added GDU 13.31 Garmin G1000 Pilot’s Guide for the Beechcraft G58 190-00629-04 Rev. A REVISION INFORMATION Blank Page 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 TABLE OF CONTENTS SECTION 1 SYSTEM OVERVIEW 1.1 System Description ................................................. 1 1.2 Line Replaceable Units (LRU) ................................. 2 1.3 G1000 Controls........................................................ 7 PFD/MFD Controls ........................................................ 7 Additional AFCS Controls ............................................ 10 Audio Panel Controls .................................................. 11 1.4 Secure Digital Cards.............................................. 13 1.5 System Power-up ................................................... 14 1.6 System Operation .................................................. 15 Normal Operation ....................................................... 15 Reversionary Mode ..................................................... 15 AHRS Operation ......................................................... 16 G1000 System Annunciations ...................................... 18 Softkey Function ......................................................... 19 GPS Receiver Operation .............................................. 25 1.7 Accessing G1000 Functionality............................ 30 Menus ....................................................................... 30 MFD Page Groups ....................................................... 30 MFD System Pages...................................................... 34 1.8 Display Backlighting ............................................. 53 SECTION 2 FLIGHT INSTRUMENTS 2.1 Flight Instruments ................................................. 58 Airspeed Indicator ...................................................... 58 Attitude Indicator ....................................................... 61 Altimeter ................................................................... 62 Vertical Speed Indicator (VSI) ....................................... 63 Vertical Deviation ....................................................... 64 Horizontal Situation Indicator (HSI) .............................. 65 Course Deviation Indicator (CDI) .................................. 70 2.2 Supplemental Flight Data .................................... 77 Temperature Displays .................................................. 77 Wind Data ................................................................. 78 Vertical Navigation (VNV) Indications ........................... 79 2.3 PFD Annunciations and Alerting Functions ........ 80 G1000 Alerting System ................................................ 80 Marker Beacon Annunciations...................................... 81 Traffic Annunciation .................................................... 82 TAWS Annunciations ................................................... 82 Altitude Alerting ......................................................... 83 Low Altitude Annunciation .......................................... 83 Minimum Descent Altitude/Decision Height Alerting ...... 84 2.4 Abnormal Operations ........................................... 85 Abnormal GPS Conditions ........................................... 85 Unusual Attitudes ....................................................... 86 SECTION 3 ENGINE INDICATION SYSTEM 3.1 Engine Display ....................................................... 89 3.2 Lean Display ........................................................... 91 3.3 System Display ...................................................... 94 SECTION 4 AUDIO PANEL AND CNS 4.1 Overview ................................................................ 97 MFD/PFD Controls and Frequency Display ..................... 98 Audio Panel Controls ................................................ 100 4.2 COM Operation .................................................... 102 COM Transceiver Selection and Activation ................... 102 COM Transceiver Manual Tuning ................................ 103 Quick-Tuning and Activating 121.500 MHz .................. 104 Auto-Tuning the COM Frequency ................................ 105 Frequency Spacing .................................................... 109 Automatic Squelch.................................................... 110 Volume .................................................................... 110 4.3 NAV Operation ..................................................... 111 NAV Radio Selection and Activation ........................... 111 NAV Receiver Manual Tuning ..................................... 112 Auto-Tuning a NAV Frequency from the MFD............... 114 Marker Beacon Receiver ............................................ 119 DME Tuning (Optional) .............................................. 120 4.4 GTX 33 ES Mode S Transponder ........................ 121 Transponder Controls ................................................ 121 Transponder Mode Selection ...................................... 122 Entering a Transponder Code ..................................... 125 IDENT Function ........................................................ 126 Flight ID Reporting.................................................... 127 4.5 Additional Audio Panel Functions ..................... 128 Power-Up ................................................................. 128 Mono/Stereo Headsets .............................................. 128 Speaker ................................................................... 128 Intercom .................................................................. 129 Clearance Recorder and Player................................... 131 Split COM ................................................................ 132 Entertainment Inputs ................................................ 133 Garmin G1000 Pilot’s Guide for the Beechcraft G58 190-00629-04 Rev. A TABLE OF CONTENTS 4.6 Audio Panel Preflight Procedure ....................... 134 4.7 Abnormal Operation ........................................... 135 Stuck Microphone..................................................... 135 COM Tuning Failure................................................... 135 Audio Panel Fail-Safe Operation ................................. 135 Reversionary Mode ................................................... 135 SECTION 5 FLIGHT MANAGEMENT 5.1 Introduction ......................................................... 137 Navigation Status Box............................................... 138 5.2 Using Map Displays ............................................. 140 Map Orientation ....................................................... 140 Map Range .............................................................. 142 Map Panning............................................................ 144 Measuring Bearing and Distance ................................ 149 Topography .............................................................. 150 Map Symbols ........................................................... 153 Airways ................................................................... 159 Track Vector ............................................................. 161 Wind Vector ............................................................. 162 Nav Range Ring........................................................ 163 Fuel Range Ring ....................................................... 164 Field of View (SVS) .................................................... 165 Selected Altitude Intercept Arc ................................... 166 5.3 Waypoints............................................................. 167 Airports ................................................................... 168 Intersections ............................................................ 175 NDBs ....................................................................... 177 VORs ....................................................................... 179 User Waypoints ........................................................ 181 5.4 Airspaces .............................................................. 187 5.5 Direct-to-Navigation .......................................... 191 5.6 Flight Planning..................................................... 197 Flight Plan Creation .................................................. 198 Adding Waypoints to an Existing Flight Plan................ 203 Adding Airways to a Flight Plan ................................. 205 Adding Procedures to a Stored Flight Plan .................. 207 Flight Plan Storage ................................................... 214 Flight Plan Editing .................................................... 216 Along Track Offsets ................................................... 219 Parallel Track ............................................................ 220 Activating a Flight Plan Leg ....................................... 224 Inverting a Flight Plan ............................................... 225 Flight Plan Views ...................................................... 226 Closest Point of FPL .................................................. 228 User-Defined Holding Patterns ................................... 228 5.7 Vertical Navigation ............................................. 233 Altitude Constraints .................................................. 235 5.8 Procedures ........................................................... 239 Departures ............................................................... 239 Arrivals ................................................................... 243 Approaches ............................................................. 246 5.9 Trip Planning ........................................................ 254 Trip Planning ............................................................ 254 5.10 RAIM Prediction................................................... 258 5.11 Navigating a Flight Plan ..................................... 261 5.12 Abnormal Operation ........................................... 289 SECTION 6 HAZARD AVOIDANCE 6.1 XM WX Satellite Weather ................................... 292 Activating Services.................................................... 292 Using XM WX Satellite Weather Products .................... 294 6.2 Airborne Color Weather Radar .......................... 324 System Description ................................................... 324 Principles of Pulsed Airborne Weather Radar ............... 324 Safe Operating Distance ............................................ 329 Basic Antenna Tilt Setup ............................................ 329 Weather Mapping and Interpretation ......................... 331 Ground Mapping and Interpretation ........................... 344 System Status........................................................... 345 6.3 WX-500 Stormscope ........................................... 346 Setting Up Stormscope on the Navigation Map ........... 346 Selecting the Stormscope Page .................................. 350 6.4 TAWS-B ................................................................. 352 Displaying TAWS-B Data ............................................ 353 TAWS-B Page ........................................................... 355 TAWS-B Alerts .......................................................... 357 System Status........................................................... 363 6.5 Profile View Terrain ............................................. 365 Profile View Display .................................................. 366 6.6 Traffic Information Service (TIS) ........................ 369 Displaying TRAFFIC Data ........................................... 370 Traffic Map Page....................................................... 372 TIS Alerts ................................................................. 373 System Status........................................................... 374 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 TABLE OF CONTENTS 6.7 Garmin GTS 820 Traffic ....................................... 377 Theory of operation .................................................. 377 TAS Alerts ................................................................ 380 System Test .............................................................. 381 Operation ................................................................ 382 6.8 L-3 Skywatch Traffic ............................................ 390 TAS Symbology......................................................... 390 Operation ................................................................ 391 Altitude Display ........................................................ 394 Traffic Map Page Display Range ................................. 394 TAS Alerts ................................................................ 396 System Status........................................................... 396 SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM 7.1 AFCS Overview .................................................... 399 Additional AFCS Controls .......................................... 401 7.2 Flight Director Operation ................................... 402 Activating the Flight Director ..................................... 402 AFCS Status Box ....................................................... 403 Flight Director Modes................................................ 404 Command Bars ......................................................... 404 7.3 Vertical Modes ..................................................... 405 Pitch Hold Mode (PIT) ............................................... 406 Selected Altitude Capture Mode (ALTS) ....................... 407 Altitude Hold Mode (ALT) .......................................... 408 Vertical Speed Mode (VS) .......................................... 409 Flight Level Change Mode (FLC) ................................. 410 Vertical Navigation Modes (VPTH, ALTV) ..................... 412 Glidepath Mode (GP) (SBAS only)............................... 417 Glideslope Mode (GS) ............................................... 419 Go Around Mode (GA) .............................................. 420 7.4 Lateral Modes ...................................................... 421 Roll Hold Mode (ROL) ............................................... 422 Navigation Modes (GPS, VOR, LOC, bc) ....................... 424 Approach Modes (GPS, VAPP, LOC) ............................. 426 Backcourse Mode (BC) .............................................. 427 Intercepting and Flying A DME Arc ............................. 428 7.5 Autopilot and Yaw Damper Operation ............. 429 Flight Control ........................................................... 429 Engagement............................................................. 430 Control Wheel Steering ............................................. 430 Disengagement ........................................................ 431 7.6 Example Flight Plan ............................................ 432 Departure ................................................................ 433 Intercepting a VOR Radial .......................................... 435 Flying a Flight Plan/GPS Course ................................. 436 Descent ................................................................... 437 Approach ................................................................. 441 Go Around/Missed Approach ..................................... 445 7.7 AFCS Annunciations and Alerts ......................... 447 AFCS Status Alerts .................................................... 447 Overspeed Protection ................................................ 448 SECTION 8 ADDITIONAL FEATURES 8.1 Synthetic Vision System (SVS) (Optional) ......... 450 SVS Operation .......................................................... 451 SVS Features ............................................................ 453 Field of View ............................................................ 461 8.2 SafeTaxi ................................................................ 463 8.3 ChartView ............................................................. 469 ChartView Softkeys ................................................... 470 Terminal Procedures Charts ....................................... 471 Chart Options........................................................... 479 Day/Night View ........................................................ 485 ChartView Cycle Number and Expiration Date ............. 487 8.4 FliteCharts ............................................................ 490 FliteCharts Softkeys .................................................. 491 Terminal Procedures Charts ....................................... 492 Chart Options........................................................... 500 Day/Night View ........................................................ 504 FliteCharts Cycle Number and Expiration Date............. 507 8.5 Airport Directory ................................................ 511 Airport Directory Database Cycle Number and Revision 512 8.6 SiriusXM Satellite Radio Entertainment........... 514 Activating SiriusXM Satellite Radio Services ................ 514 Using SiriusXM Satellite Radio ................................... 515 Automatic Audio Muting ........................................... 519 8.7 Scheduler.............................................................. 521 8.8 Flight Data Logging ............................................ 523 8.9 Abnormal Operation ........................................... 525 SVS Troubleshooting ................................................. 525 Reversionary Mode ................................................... 525 Unusual Attitudes ..................................................... 526 Garmin G1000 Pilot’s Guide for the Beechcraft G58 190-00629-04 Rev. A TABLE OF CONTENTS APPENDICES Annunciations and Alerts ............................................. 529 Alert Level Definitions ............................................... 530 Aircraft Alerts ........................................................... 531 G1000 System Annunciations .................................... 533 G1000 System Message Advisories............................. 536 Pilot Profile Import/Export Messages .......................... 546 Database Management ................................................ 547 Jeppesen Databases.................................................. 547 Garmin Databases .................................................... 551 Glossary.......................................................................... 557 Frequently Asked Questions ........................................ 565 Map Symbols ................................................................. 569 INDEX Index ................................................................................ I-1 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 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 This section provides an overview of the G1000 Integrated Flight Deck as installed in the Beechcraft G58 Baron. The G1000 system is an integrated flight control system that presents flight instrumentation, position, navigation, communication, and identification information to the pilot through large-format displays. The system consists of the following Line Replaceable Units (LRUs): • GDU 1040 Primary Flight Display (PFD) • GDU 1043/1045 Multi Function Display (MFD) • GIA 63W Integrated Avionics Unit • GDC 74A Air Data Computer (ADC) • GEA 71 Engine/Airframe Unit • GRS 77 Attitude and Heading Reference System (AHRS) • GMU 44 Magnetometer • GMA 1347 Audio System with Integrated Marker Beacon Receiver • GTX 33 Mode S Transponder with Extended Squitter • GDL 69A Satellite Data Link Receiver • GWX 68 Weather Radar • GTP 59 Outside Air Temperature (OAT) Probe • GSA 81 AFCS Servos • GSM 85 Servo Gearboxes • GTS 820 Traffic Advisory System (if installed) A top-level G1000 system block diagram is shown in Figure 1-1 (it does not include the GSM 85A). NOTE: Refer to the AFCS section for details on the GFC 700 AFCS. In the Beechcraft G58 Baron, the GFC 700 Automated Flight Control System (AFCS) provides the flight director (FD), autopilot (AP), and yaw damper (YD) functions of the G1000 system. 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 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 (LRU) • GDU 1040 (1) – The GDU 1040 is configured as a Primary Flight Display (PFD) that features a 10.4-inch LCD with 1024 x 768 resolution. The display communicates with the MFD and with the #1 GIA 63W Integrated Avionics Unit through a High-Speed Data Bus (HSDB) Ethernet connection. • GDU 1043/1045 (1) – The GDU 1043 or GDU 1045 is configured as an MFD that features a 10.4-inch LCD with 1024 x 768 resolution. The display communicates with the PFD and with the #2 GIA 63W Integrated Avionics Unit through a High-Speed Data Bus (HSDB) Ethernet connection. The GDU 1045 has a VNV Button, which is needed to enable optional coupled Baro-VNAV AFCS mode. • GIA 63W (2) – Functions as the main communication hub, linking all LRUs with the PFD and MFD. Each GIA 63W contains a GPS receiver, VHF COM/NAV/GS receivers, a flight director (FD) and system integration microprocessors. Each GIA 63W contains a GPS SBAS receiver. Each GIA 63W is paired with a display via HSDB connection. The GIA 63Ws are not paired together and do not communicate with each other directly. 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 3 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX • GDC 74A (1) – Processes data from the pitot/static system as well as the OAT probe. This unit provides pressure altitude, airspeed, vertical speed and OAT information to the G1000 system, and it communicates with the GIA 63Ws, the displays, and the GRS 77, using an ARINC 429 digital interface (it also interfaces directly with the GTP 59). • GEA 71 (2) – Receives and processes signals from the engine and airframe sensors. This unit communicates with both GIA 63Ws using an RS-485 digital interface. • GRS 77 (1) – Provides aircraft attitude and heading information via ARINC 429 to both displays and both GIA 63Ws. The GRS 77 contains advanced sensors (including accelerometers and rate sensors) and interfaces with the GMU 44 to obtain magnetic field information, with the GDC 74A to obtain air data, and with both GIA 63Ws to obtain GPS information. AHRS modes of operation are discussed later in this document. • GMU 44 (1) – Measures local magnetic field. Data is sent to the GRS 77 for processing to determine aircraft magnetic heading. This unit receives power directly from the GRS 77 and communicates with the GRS 77 using an RS-485 digital interface. 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 4 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX • GMA 1347 (1) – Integrates NAV/COM digital audio, intercom system and marker beacon controls. This unit also enables the manual control of the display reversionary mode (red DISPLAY BACKUP button) and communicates with both GIA 63W units, using an RS-232 digital interface. • GTX 33 with Extended Squitter(1) – Solid-state transponder that provides Modes A, C, S, and ADS-B Out capability. The transponder can be controlled from the PFD. The transponder communicates with the GIA 63Ws through an RS-232 digital interface. • GDL 69A (1) – A satellite radio receiver that provides real-time weather information to the G1000 MFD (and, indirectly, to the inset map of the PFD) as well as digital audio entertainment. The GDL 69A communicates with the MFD via HSDB connection. A subscription to the XM Satellite Radio service is required to enable the GDL 69A capability. • GWX 68 (1) – Provides airborne weather and ground mapped radar data to the MFD, through the GDL 69A, via HSDB connection. 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 5 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX • GTP 59 (1) – Provides Outside Air Temperature (OAT) data to the GDC 74A. • GSA 81 (4), and GSM 85 (4) – The GSA 81 servos are used for the automatic control of roll, pitch, yaw, and pitch trim. These units interface with each GIA 63W. The GSM 85 servo gearbox is responsible for transferring the output torque of the GSA 81 servo actuator to the mechanical flight-control surface linkage. • GTS 820 – The GTS 820 Traffic Advisory System (TAS) uses active interrogations of Mode S, Mode A, and Mode C transponders to provide Traffic Advisories to the pilot independent of the air traffic control system. • GA 58 (2) – The GA 58 is a directional antenna for the Traffic Avoidance System. One top-mounted directional antenna and one bottom mounted antenna are required. 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 6 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX GTX 33 Transponder Reversionary Control GEA 71(2) Engine/Airframe Units GDC 74A Air Data Computer OAT Airspeed Altitude Vertical Speed GMU 44 Magnetometer Heading Reversionary Control GMA 1347 Audio Panel G C Ve A r ed No. 2 GIA 63W Integrated Avionics Unit System Integration Processors I/O Processors VHF COM VHF NAV/LOC GPS Glideslope GPS Output No. 1 GIA 63W Integrated Avionics Unit System Integration Processors I/O Processors VHF COM VHF NAV/LOC GPS Glideslope GPS Output GRS 77 AHRS Attitude Rate of Turn Slip/Skid GDU 1040 Primary Flight Display GDU 1043/1045 Multi Function Display L-3 Skywatch SKY497 Traffic Advisory System (if installed) Honeywell KN 63 DME (optional) L-3 WX-500 Stormscope Lightning Sensor (optional) GSA 81 (4) Servos GDL 69A Data Link Weather and Digital Audio Entertainment GWX 68 Weather Radar GTS 820 Traffic Advisory System (if installed) Figure 1-1 G1000 System Block Diagram 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 7 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 1.3 G1000 CONTROLS NOTE: The Audio Panel (GMA 1347) and AFCS controls are also described in the CNS & Audio Panel and AFCS sections respectively. The G1000 system controls are located on the PFD and MFD bezels, and the audio panel. The controls for the PFD and MFD are discussed within the following pages of this section. PFD/MFD CONTROLS Figure 1-2 PFD/MFD Controls 4 2 1 6 5 7 9 8 3 12 16 11 10 15 14 13 20 21 19 18 26 25 24 22 23 29 28 MFD Only 17 27 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 8 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 1 NAV VOL/ID Knob Turn to control NAV audio volume (shown in the NAV Frequency Box as a percentage) Press to toggle Morse code identifier audio ON/OFF 2 NAV Frequency Trans- fer 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. When operating in Heading Select mode, this knob pro- vides the heading reference to the flight director. Press to display a digital heading momentarily to the left of the HSI and synchronize the Selected Heading to the current heading 5 Joystick Turn to change map range Press to activate Map Pointer for map panning 6 CRS/BARO Knob Turn large knob for altimeter barometric pressure setting Turn the small knob to set the pilot-selected course on the HSI when the VOR1, VOR2, or OBS/SUSP mode is selected. Pressing this knob centers the CDI on the currently selected VOR. The pilot-selected course provides course reference to the pilot-side flight director when operating in Navigation and Approach modes. 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 Trans- fer 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 es- tablish 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 menu selection or data entry 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 9 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 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 ALT Knob Sets the selected altitude in the Selected Altitude Box (the large knob selects the thousands, the small knob selects the hundreds). In addition to providing the standard G1000 altitude alerter function, selected altitude provides an altitude setting for the Altitude Capture/Hold mode of the AFCS. 18 AP Key Engages/disengages the Autopilot and Flight Director in the default vertical and lateral modes. 19 FD Key Activates/deactivates the Flight Director only. Pressing the FD key turns on the Flight Direc- tor in the default vertical and lateral modes. Pressing the FD key again deactivates the Flight Director and removes the command bars, unless the Autopilot is engaged. If the Autopilot is engaged, the FD key is disabled. 20 NAV Key Selects/deselects the Navigation mode. 21 ALT Key Selects/deselects the Altitude Hold mode. 22 VS Key Selects/deselects the Vertical Speed mode. 23 FLC Key Selects/deselects the Flight Level Change mode. 24 YD Key Engages/disengages the Yaw Damper. 25 HDG Key Selects/deselects the Heading Select mode. 26 APR Key Selects/deselects the Approach mode. 27 VNV Key (if equipped) Selects/deselects Vertical Navigation mode 28 NOSE UP Key Controls the active pitch reference for the Pitch Hold, Vertical Speed, and Flight Level Change modes. 29 NOSE DN Key Controls the active pitch reference for the Pitch Hold, Vertical Speed, and Flight Level Change modes. 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 10 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 1-3 Dual Concentric Knob The bottom portion of the MFD bezel features 12 softkeys that are designed to perform various functions depending upon the specific page being displayed. These softkeys are discussed throughout the Pilot’s Guide documentation. ADDITIONAL AFCS CONTROLS The AP DISC (Autopilot Disconnect) Switch, CWS (Control Wheel Steering) Button, GO AROUND Switch, and MEPT (Manual Electric Pitch Trim) Switch are additional AFCS controls and are located in the cockpit, separately from the AFCS Control Unit. These are discussed in detail in the AFCS section. 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 11 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX AUDIO PANEL CONTROLS Figure 1-4 Audio Panel Controls (GMA 1347) 17 18 15 13 11 9 20 7 5 3 1 14 2 16 4 6 8 10 12 22 24 23 21 19 NOTE: When a key is selected, a triangular annunciator above the key is illuminated. 1 COM1 MIC – Selects the #1 transmitter for transmitting. COM1 receive is simultaneously selected when this key is pressed allowing received audio from the #1 COM receiver to be heard. COM2 receive can be added by pressing the COM2 Key. 2 COM1 – When selected, audio from the #1 COM receiver can be heard. 3 COM2 MIC – Selects the #2 transmitter for transmitting. COM2 receive is simultaneously selected when this key is pressed allowing received audio from the #2 COM receiver to be heard. COM1 receive can be added by pressing the COM1 Key. 4 COM2 – When selected, audio from the #2 COM receiver can be heard. 5 COM3 MIC – Not used in Beechcraft G58 aircraft. 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 12 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 6 COM3 – Not used in Beechcraft G58 aircraft. 7 COM 1/2 – Split COM Key. Allows simultaneous transmission on COM1 and COM2 by the pilot and copilot. 8 TEL – Not used in Beechcraft G58 aircraft. 9 PA – Not used in Beechcraft G58 aircraft. 10 SPKR – Selects and deselects the cabin speaker. COM and NAV receiver audio can be heard on the speaker. 11 MKR/MUTE – Selects marker beacon receiver audio. Mutes the currently received marker beacon receiver audio. Unmutes automatically when new marker beacon audio is received. Also, stops play of recorded COM audio. 12 HI SENS – Press to increase marker beacon receiver sensitivity. Press again to return to low sensitivity. 13 DME – Pressing turns optional DME audio on or off. 14 NAV1 – When selected, audio from the #1 NAV receiver can be heard. 15 ADF – Not used in Beechcraft G58 aircraft. 16 NAV2 – When selected, audio from the #2 NAV receiver can be heard. 17 AUX – Not used in Beechcraft G58 aircraft. 18 MAN SQ – Enables manual squelch for the intercom. When the intercom is active, press the PILOT Knob to illuminate SQ. Turn the PILOT/PASS Knobs to adjust squelch. 19 PLAY – Press once to play the last recorded COM audio. Press again while audio is playing and the previous block of recorded audio is played. Each subsequent press plays each previously recorded block. Pressing the MKR/MUTE Key during play of a memory block stops play. 20 PILOT – Selects and deselects the pilot intercom isolation. 21 COPLT – Selects and deselects the copilot intercom isolation. 22 PILOT Knob – Press to switch between volume and squelch control as indicated by illumination of VOL or SQ. Turn to adjust intercom volume or squelch. The MAN SQ Key must be selected to allow squelch adjustment. 23 PASS Knob – Turn to adjust Copilot/Passenger intercom volume or squelch. The MAN SQ Key must be selected to allow squelch adjustment. 24 DISPLAY BACKUP Button – Manually selects Reversionary Mode. 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 13 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 1.4 SECURE DIGITAL CARDS NOTE: Refer to the Appendices for instructions on updating the aviation database. NOTE: Ensure that the G1000 system is powered off before inserting the SD card. The GDU 1040 and GDU 1043/1045 data card slots use Secure Digital (SD) cards and are located on the top right portion 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. Install an SD card Insert the SD card in the SD card slot, pushing the card in until the spring latch engages. The front of the card should remain flush with the face of the display bezel. Remove an SD card Gently press on the SD card to release the spring latch and eject the card. Figure 1-5 Display Bezel SD Card Slots SD Card Slots 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 14 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 1.5 SYSTEM POWER-UP NOTE: Refer to the Appendices for AHRS initialization bank angle limitations. NOTE: See the Appendices for additional information regarding system-specific annunciations and alerts. NOTE: See the Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual (AFM/POH) for specific procedures concerning avionics power application and emergency power supply operation. The G1000 system is integrated with the aircraft electrical system and receives power directly from electrical busses. The G1000 PFDs, 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 1-6. All system annunciations should disappear typically within one minute of power-up. Upon power-up, key annunciator lights also become momentarily illuminated on the audio panels, the control units 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 one minute of power-up. The AHRS can align itself both while taxiing and during level flight. When the MFD powers up (Figure 1-7), the MFD Power-up Page displays the following information: • System version • Copyright • Land database name and version • Safe Taxi database information • Terrain database name and version • Obstacle database name and version • Navigation database name, version, and effective dates • Airport Directory name, version and effective dates • FliteCharts/ChartView database information Current database information includes the valid operating dates, cycle number and database type. When this information has been reviewed for currency (to ensure that no databases have expired), the pilot is prompted to continue. Pressing the ENT Key acknowledges this information and displays the Navigation Map Page. Figure 1-7 MFD Power-up Page Figure 1-6 PFD Initialization 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 15 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 1.6 SYSTEM OPERATION The displays are connected together via multiple data busses, thus allowing for high-speed communication. As shown in Figure 1-1, each GIA 63W is connected to one display. This section discusses the normal and reversionary modes of operation as well as the various AHRS modes of the G1000 system. NORMAL OPERATION PFD In normal mode, the PFD presents graphical flight instrumentation (attitude, heading, airspeed, altitude and vertical speed), thereby replacing the traditional flight instrument cluster. The PFD also offers control for COM and NAV frequency selection. MFD In normal mode, the right portion of the MFD displays a full-color moving map with navigation information, while the left portion of the MFD is dedicated to the Engine Indication System (EIS). Figure 1-8 gives an example of the G1000 displays in normal mode. Figure 1-8 Normal Operation Audio Panel Primary Flight Display Multi Function Display REVERSIONARY MODE 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. 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 Ethernet interface to the display is cut off. Thus, the IAU can no longer communicate with the remaining display (refer to Figure 1-1), and the NAV and COM functions provided to the failed display by the IAU are flagged as invalid on the remaining display. The system reverts to backup paths for the AHRS, ADC, Engine/Airframe Unit, and Transponder, as required. The change to backup paths is completely automated for all LRUs and no pilot action is required. 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 16 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Figure 1-9 Reversionary Mode Operation Audio Panel Primary Flight Display Failed Multi Function Display 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 (refer to the Audio Panel section for further details). Pressing this button again deactivates reversionary mode. Figure 1-10 DISPLAY BACKUP Button Pressing the DISPLAY BACKUP button activates/deactivates reversionary mode for both the PFD and the MFD. Should the connection between a PFD and the on-side GIA 63W become inoperative, the on-side GIA 63W can no longer communicate with the remaining PFD (refer to Figure 1-1). As a result, the NAV and COM functions provided to the failed PFD by the on-side GIA 63W are flagged as invalid (red “X”) on the remaining PFD (see Figure 1-11). Figure 1-11 Inoperative Input (NAV1 Shown) AHRS OPERATION NOTE: Refer to the Appendices for specific AHRS alert information. 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 1-12) 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. 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 17 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 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. Attitude/Heading Invalid AHRS no-GPS Mode AHRS Normal Operation AHRS no- Mag Mode AHRS no-Mag/ no-Air Mode Heading Invalid available available unavailable unavailable available unavailable unavailable available Air Data Magnetometer Data unavailable available GPS Data Magnetometer Data Air Data Figure 1-12 AHRS Operation GPS INPUT FAILURE NOTE: In-flight initialization of AHRS, when operating without any valid source of GPS data and at true air speed values greater than approximately 200 knots, is not guaranteed. Under these rare conditions, it is possible for in-flight AHRS initialization to take an indefinite amount of time which would result in an extended period of time where valid AHRS outputs are unavailable. The G1000 system provides two sources of GPS information. If a single GPS receiver fails, or if the information provided from one of the GPS receivers is unreliable, the AHRS seamlessly transitions to using the other GPS receiver. An alert message informs the pilot of the use of the backup GPS path. If both GPS inputs fail, the AHRS continues to operate in reversionary No-GPS mode so long as the air data and magnetometer inputs are available and valid. 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 18 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX AIR DATA INPUT FAILURE A failure of the air data input has no effect on AHRS output while AHRS is operating in normal mode. A failure of the air data input while the AHRS is operating in reversionary No-GPS mode results in invalid attitude and heading information on the PFD (as indicated by red “X” flags). MAGNETOMETER FAILURE If the magnetometer input fails, the AHRS transitions to one of the reversionary No-Magnetometer modes and continues to output valid attitude information. However, if the aircraft is airborne, the heading output on the PFD does become invalid (as indicated by a red “X”). G1000 SYSTEM ANNUNCIATIONS NOTE: For a detailed description of all annunciations and alerts, refer to Appendix A. Refer to the (AFM/ POH) for additional information regarding pilot responses to these annunciations. When an LRU or an LRU function fails, a large red “X” is typically displayed on windows associated with the failed data (Figure 1-14 displays all possible flags and responsible LRUs). Upon G1000 power-up, certain windows remain invalid as equipment begins to initialize. All windows should be operational within one minute of power-up. If any window remains flagged, the G1000 system should be serviced by a Garmin- authorized repair facility. Figure 1-13 G1000 System Failure Annunciations GDC 74A Air Data Computer GTX 33 Transponder Or GIA 63W Integrated Avionics Units GDC 74A Air Data Computer GEA 71 Engine Airframe Unit Or GIA 63W Integrated Avionics Unit GIA 63W Integrated Avionics Units GRS 77 AHRS Or GMU 44 Magnetometer GIA 63W Integrated Avionics Units GIA 63W Integrated Avionics Units 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 19 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 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 1-14 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. If messages remain after acknowledgement, the ALERTS Softkey is black on white. The PFD softkeys provide control over flight management functions, including GPS, NAV, terrain, traffic, and lightning. Each softkey sublevel has a BACK Softkey which can be pressed to return to the previous level. The ALERTS Softkey is visible in all softkey levels. For the top level softkeys and the transponder (XPDR) levels, the IDENT Softkey remains visible. 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 icons and age on the Inset Map for 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) 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 20 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 Headwind/tailwind and crosswind arrows with numeric speed components OPTN 2 Wind direction arrow and numeric speed OPTN 3 Wind direction arrow with numeric direction and speed OFF Information not displayed DME Displays/removes the DME Information Window (optional) BRG1 Cycles the Bearing 1 Information Window between NAV1, and GPS/ waypoint identifier and GPS-derived distance information 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 1 Information Window between NAV2, and GPS/ waypoint identifier and GPS-derived distance information 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 DME Displays the DME Tuning Window, allowing tuning and selection of the DME (optional) XPDR Displays transponder mode selection softkeys STBY Selects standby mode (transponder does not reply to any interrogations) ON White (On-Ground) - Transponder generates Mode A and Mode S replies, as well as transmission of acquisition and extended squitters, including ADS-B out. Green (Airborne) - Transponder generates Mode A and Mode S replies, as well as transmission of acquisition and extended squitters, including ADS-B out. 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 21 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX ALT Selects Altitude Mode (selection is usually automatic) White (On-Ground) - Transponder does not allow Mode A or Mode C replies to interrogations, , but it does permit acquisition and extended squitters including ADS-B out, and replies to discretely addressed Mode S interrogations. Green (Airborne) - Transponder generates Mode A, Mode C, and Mode S replies to interrogations, as well as transmissions of acquisition and extended squitters including ADS-B out. VFR Automatically enters the VFR code (1200 in the U.S.A. only) CODE Displays transponder code selection softkeys 0-7 0 — 7 Use numbers to enter code IDENT Activates the Special Position Identification (SPI) pulse for 18 seconds, identifying the transponder return on the ATC screen BKSP Removes numbers entered, one at a time IDENT Activates the Special Position Identification (SPI) pulse for 18 seconds, identifying the transponder return on the ATC screen ADS-B TX Enables/disables automatic transmission of ADS-B position and speed. IDENT Activates the Special Position Identification (SPI) pulse for 18 seconds, identifying the transponder return on the ATC screen TMR/REF Displays Timer/References Window NRST Displays Nearest Airports Window ALERTS Displays Alerts Window Figure 1-15 Top Level PFD Softkeys ALERTS (optional) 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 22 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Figure 1-16 INSET Softkeys Select the BACK Softkey to return to the top-level softkeys. STRMSCP ALERTS ALERTS (optional) (optional) TRFC-1 TRFC-2 METAR (optional) (optional) (optional) WX LGND (optional) Figure 1-17 PFD Configuration Softkeys Select the BACK Softkey to return to the top-level softkeys ALT UNIT METERS IN HPA ALERTS ALERTS ALERTS ALERTS HSI FRMT 360 HSI ARC HSI ALERTS (optional) ALERTS SYN VIS SYN TERR HRZN HDG PATHWAY APTSIGNS 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 23 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Figure 1-18 XPDR Softkeys Select the BACK Softkey to return to the top-level softkeys. Select the BACK Softkey to return to the previous level softkeys. ALERTS ALERTS ALERTS (optional) ADS-B TX 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 24 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX MFD SOFTKEYS ENGINE Displays second-level softkeys for additional EIS configuration ENGINE Displays default EIS display LEAN Displays EIS lean display CYL SLCT Allows selection of engine cylinder to view additional information ASSIST Enables/disables leaning assist mode SYSTEM Displays system oil pressure and temperature, fuel calculations, and electrical system information 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 166 GAL Resets calculated fuel remaining to 166 gallons and resets fuel used to zero 194 GAL Resets calculated fuel remaining to 194 gallons and resets fuel used to zero MAP Enables second-level Navigation Map softkeys TRAFFIC Displays traffic information on Navigation Map PROFILE Displays the profile view on Navigation Map TOPO Displays topographical data (e.g., coastlines, terrain, rivers, lakes) and elevation scale on Navigation Map TERRAIN Displays terrain information on Navigation Map 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 Stormscope information on Navigation Map (optional) NEXRAD Displays NEXRAD weather and coverage information on Navigation Map XM LTNG Displays XM lightning information on Navigation Map METAR Displays METAR information on Navigation Map (optional) LEGEND Displays selected XM weather product legends on Navigation Map BACK Returns to top-level softkeys DCLTR (3) Selects desired amount of map detail; cycles through declutter levels: DCLTR (No Declutter): All map features visible DCLTR-1: Declutters land data DCLTR-2: Declutters land and SUA data DCLTR-3: Removes everything except for the active flight plan SHW CHRT When available, displays optional airport and terminal procedure charts CHKLIST When available, displays optional checklists 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 25 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Figure 1-19 MFD Softkeys MAP DCLTR TOPO PROFILE BACK TERRAIN DCLTR-2 DCLTR-3 DCLTR-1 Select the BACK Softkey on this level to return to the top softkey level. NEXRAD XM LTNG SHW CHRT CHKLIST AIRWAYS AIRWY LO AIRWAY HI AIRWY ON STRMSCP TRAFFIC (optional) ENGINE BACK ENGINE SYSTEM BACK ENGINE SYSTEM 166 GAL 194 GAL DEC FUEL INC FUEL LEAN LEAN BACK ENGINE SYSTEM CYL SLCT ASSIST LEAN METAR LEGEND (optional) (optional) (optional) GPS RECEIVER OPERATION Each Integrated Avionics Unit (IAU) contains a GPS receiver. Internal system checking is performed to ensure both GPS receivers are providing accurate data to the PFD. When both GPS receivers are providing accurate data, the GPS receiver producing the better solution is used by the system. Information collected by the specified receiver (GPS1 for the #1 IAU or GPS2 for the #2 IAU) may be viewed on the AUX - GPS Status Page. These GPS sensor annunciations are most often seen after system power-up when one GPS receiver has acquired satellites before the other, or one of the GPS receivers has not yet acquired a SBAS signal. While the aircraft is on the ground, the SBAS signal may be blocked by obstructions causing one GPS receiver to have difficulty acquiring a good signal. Also, while airborne, turning the aircraft may result in one of the GPS receivers temporarily losing the SBAS signal. If the sensor annunciation persists, check for a system failure message in the Messages Window on the PFD. If no failure message exists, check the GPS Status Page and compare the information for GPS1 and GPS2. Discrepancies may indicate a problem. 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 26 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Viewing GPS receiver status information 1) Use the large FMS Knob to select the Auxiliary Page Group (see Section 1.7 for information on navigating MFD page groups). 2) Use the small FMS Knob to select GPS Status Page. Selecting the GPS receiver for which data may be reviewed 1) Use the FMS Knob to select the AUX - GPS STATUS Page. 2) To change the selected GPS receiver: a) Press the desired GPS Softkey. Or: a) Press the MENU Key. b) Use the FMS Knob to highlight the receiver which is not selected and press the ENT Key. Figure 1-20 GPS Status Page (RAIM or SBAS Selected) Satellite Signal Strength Bars Satellite Constellation Diagram Satellite Signal Information Status RAIM Availability Prediction GPS Receiver Status SBAS Selected RAIM Softkey Selected SBAS Softkey Selected GPS Selection Softkeys 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 27 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX The GPS Status Page provides the following information: • Satellite constellation diagram Satellites currently in view are shown at their respective positions on a sky view diagram. The sky view is always in a north-up orientation, with the outer circle representing the horizon, the inner circle representing 45° above the horizon, and the center point showing the position directly overhead. Each satellite is represented by an oval containing the Pseudo-random noise (PRN) number (i.e., satellite identification number). Satellites whose signals are currently being used are represented by solid ovals. • Satellite signal information status The accuracy of the aircraft’s GPS fix is calculated using Estimated Position Uncertainty (EPU), Dilution of Precision (DOP), and horizontal and vertical figures of merit (HFOM and VFOM). EPU is the radius of a circle centered on an estimated horizontal position in which actual position has 95% probability of laying. EPU is a statistical error indication and not an actual error measurement. DOP measures satellite geometry quality (i.e., number of satellites received and where they are relative to each other) on a range from 0.0 to 9.9, with lower numbers denoting better accuracy. HFOM and VFOM, measures of horizontal and vertical position uncertainty, are the current 95% confidence horizontal and vertical accuracy values reported by the GPS receiver. The current calculated GPS position, time, altitude, ground speed, and track for the aircraft are displayed below the satellite signal accuracy measurements. • GPS receiver status The GPS solution type (ACQUIRING, 2D NAV, 2D DIFF NAV, 3D NAV, 3D DIFF NAV) for the active GPS receiver (GPS1 or GPS2) is shown in the upper right of the GPS Status Page. When the receiver is in the process of acquiring enough satellite signals for navigation, the receiver uses satellite orbital data (collected continuously from the satellites) and last known position to determine the satellites that should be in view. ACQUIRING is indicated as the solution until a sufficient number of satellites have been acquired for computing a solution. When the receiver is in the process of acquiring a 3D differential GPS solution, 3D NAV is indicated as the solution until the 3D differential fix has finished acquisition. SBAS (Satellite-Based Augmentation System) indicates INACTIVE. When acquisition is complete, the solution status indicates 3D DIFF NAV and SBAS indicates ACTIVE. • RAIM (Receiver Autonomous Integrity Monitoring) Prediction (RAIM Softkey is selected) In most cases performing a RAIM prediction is not necessary. However, in some cases, the selected approach may be outside the SBAS coverage area and it may be necessary to perform a RAIM prediction for the intended approach. Receiver Autonomous Integrity Monitoring (RAIM) is a GPS receiver function that performs a consistency check on all tracked satellites. RAIM ensures that the available satellite geometry allows the receiver to calculate a position within a specified RAIM protection limit (2.0 nautical miles for oceanic and enroute, 1.0 nm for terminal, and 0.3 nm for non-precision approaches). During oceanic, enroute, and terminal phases of flight, RAIM is available nearly 100% of the time. The RAIM prediction function also indicates whether RAIM is available at a specified date and time. RAIM computations predict satellite coverage within ±15 min of the specified arrival date and time. 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 28 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Because of the tighter protection limit on approaches, there may be times when RAIM is not available. The G1000 automatically monitors RAIM and warns with an alert message when it is not available. If RAIM is not predicted to be available for the final approach course, the approach does not become active, as indicated by the messages “Approach is not active” and “RAIM not available from FAF to MAP”. If RAIM is not available when crossing the FAF, the missed approach procedure must be flown. Predicting RAIM availability at a selected waypoint 1) Select the GPS Status Page. 2) If necessary, press the RAIM Softkey. 3) Press the FMS Knob. The ‘WAYPOINT’ field is highlighted. 4) Turn the small FMS Knob to display the Waypoint Information Window. 5) Enter the desired waypoint: a) Use the FMS Knob to enter the desired waypoint by identifier, facility, or city name and press the ENT Key. Refer to Section 1.7 for instructions on entering alphanumeric data into the G1000. Or: a) Turn the small FMS Knob counter-clockwise to display a list of flight plan waypoints (the FPL list is populated only when navigating a flight plan). b) Turn the small FMS Knob clockwise to display the NRST, RECENT, or AIRWAY waypoints, if required. c) Turn the large FMS Knob clockwise to select the desired waypoint. The G1000 automatically fills in the identifier, facility, and city fields with the information for the selected waypoint. d) Press the ENT Key to accept the waypoint entry. 6) Use the FMS Knob to enter an arrival time and press the ENT Key. 7) Use the FMS Knob to enter an arrival date and press the ENT Key. 8) With the cursor highlighting ‘COMPUTE RAIM?’, press the ENT Key. Once RAIM availability is computed, one of the following is displayed: • ‘COMPUTE RAIM?’—RAIM has not been computed for the current waypoint, time, and date combination • ‘COMPUTING AVAILABILITY’—RAIM calculation in progress • ‘RAIM AVAILABLE’—RAIM is predicted to be available for the specified waypoint, time, and date • ‘RAIM NOT AVAILABLE’—RAIM is predicted to be unavailable for the specified waypoint, time, and date Predicting RAIM availability at present position 1) Select the GPS Status Page. 2) If necessary, press the RAIM Softkey. 3) Press the FMS Knob. The ‘WAYPOINT’ field is highlighted. 4) Press the MENU Key. 5) With ‘Set WPT to Present Position’ highlighted, press the ENT Key. 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 29 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 6) Press the ENT Key to accept the waypoint entry. 7) Use the FMS Knob to enter an arrival time and press the ENT Key. 8) Use the FMS Knob to enter an arrival date and press the ENT Key. 9) With the cursor highlighting ‘COMPUTE RAIM?’, press the ENT Key. Once RAIM availability is computed, one of the following is displayed: • ‘COMPUTE RAIM?’—RAIM has not been computed for the current waypoint, time, and date combination • ‘COMPUTING AVAILABILITY’—RAIM calculation in progress • ‘RAIM AVAILABLE’—RAIM is predicted to be available for the specified waypoint, time, and date • ‘RAIM NOT AVAILABLE’—RAIM is predicted to be unavailable for the specified waypoint, time, and date • SBAS Selection (SBAS Softkey is selected) In certain situations, such as when the aircraft is outside or on the fringe of the SBAS coverage area, it may be desireable to disable SBAS (although it is not recommended). When disabled, the SBAS field in the GPS Status box indicates DISABLED. Disabling SBAS 1) Select the GPS Status Page. 2) If necessary, press the SBAS Softkey. 3) Press the FMS Knob to activate the cursor. 4) Turn either FMS Knob to select ‘EGNOS’ or ‘MSAS’ or ‘WAAS’, as necessary. 5) Press the ENT Key to uncheck the box. 6) Repeat steps 4 & 5 as necessary, then press the FMS Knob to remove the cursor. • GPS Satellite Signal Strengths The GPS Status Page can be helpful in troubleshooting weak (or missing) signal levels due to poor satellite coverage or installation problems. As the GPS receiver locks onto satellites, a signal strength bar is displayed for each satellite in view, with the appropriate satellite PRN number (01-32 or 120-138 for SBAS) below each bar. The progress of satellite acquisition is shown in three stages, as indicated by signal bar appearance: - No bar—Receiver is looking for the indicated satellite - Hollow bar—Receiver has found the satellite and is collecting data - Light blue bar—Receiver has collected the necessary data and the satellite signal can be used - Green bar—Satellite is being used for the GPS solution - Checkered bar—Receiver has excluded the satellite (Fault Detection and Exclusion) - “D” indication—Denotes the satellite is being used as part of the differential computations Each satellite has a 30-second data transmission that must be collected (signal strength bar is hollow) before the satellite may be used for navigation (signal strength bar becomes solid). 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 30 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 The G1000 has a 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 options for the window/page selected. The main controls used in association with all window/page group operations are described in section 1.3. Softkey selection does not display menus or submenus. Navigating the Page Menu Window 1) Press the MENU Key to display the Page Menu Window. 2) Turn the FMS Knob to scroll through a list of available options (a scroll bar appears to the right of the window when the option list is longer than the window). 3) Press the ENT Key to select the desired option. 4) The CLR Key may be pressed to remove the menu and cancel the operation. Pressing the FMS Knob also removes the displayed menu. Figure 1-21 Page Menu Examples No Options with NRST Window Displayed on the PFD Options with FPL Window Displayed MFD PAGE GROUPS NOTE: Refer to other supporting sections in this Pilot’s Guide for details on specific pages. 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 31 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Information on the MFD is presented on pages which are grouped according to function. The page group and active page title are displayed in the upper center of the screen, below the Navigation Status Box. In the bottom right corner of the screen, the current page group, number of pages available in the group, and placement of the current page within the group are indicated. The MFD displays information in four main page groups; specific pages within each group can vary depending on the configuration of optional equipment. Figure 1-22 Page Title and Page Groups Page Group Active Page Title MFD Page Groups Pages in Current Group Selected Page Selecting a page using the FMS Knob 1) Turn the large FMS Knob until the desired page group is selected. 2) Turn the small FMS Knob until the desired page is selected. There are also several pages (Airport/Procedures/Weather Information and XM pages) which are selected first from within a main page group with the FMS Knob, then with the appropriate softkey at the bottom of the page (or from the page menu). In this case, the page remains set to the selected page until a different page softkey is selected, even if a different page group is selected. Figure 1-23 Map Pages Map Pages (MAP) Navigation Map Traffic Map Weather Radar Stormscope®(optional) Weather Data Link (service optional) Terrain 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 32 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Figure 1-24 Waypoint Pages Airport Information Pages Waypoint Page Group (WPT) Airport/Procedures/Weather Information Pages - Airport Information (INFO-1 Softkey) - Airport Directory Information (INFO-2 Softkey) - Departure Information (DP Softkey) - Arrival Information (STAR Softkey) - Approach Information (APR Softkey) - Weather Information (optional) (WX Softkey) Intersection Information NDB Information VOR Information User Waypoint Information Figure 1-25 Auxiliary Pages Auxiliary Pages (AUX) Trip Planning Utility GPS Status System Setup XM Satellite pages - XM Information (INFO Softkey) - XM Radio (RADIO Softkey) System Status XM Satellite Pages 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 33 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Figure 1-26 Nearest Pages Nearest Pages (NRST) Nearest Airports Nearest Intersections Nearest NDB Nearest VOR Nearest User Waypoints Nearest Frequencies Nearest Airspaces In addition to the main page groups accessed exclusively using the FMS Knobs, there are pages for flight planning (FPL) and loading procedures (PROC) which are accessed by a dedicated key. In some instances, softkeys may be used to access the Procedure Pages. The Flight Plan Pages are accessed using the FPL Key.. Main pages within this group are selected by turning the small FMS Knob. Figure 1-27 Flight Plan Pages Flight Plan Pages (FPL) Active Flight Plan - Wide View, Narrow View (VIEW Softkey) Flight Plan Catalog Stored Flight Plan (NEW Softkey) Narrow and Wide View 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 34 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX The Procedure 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. Turning the FMS Knob does not scroll through the Procedure pages (note the single page icon in the lower right corner). Figure 1-28 Procedure Pages Procedure Pages (PROC) Departure Loading Arrival Loading Approach Loading For some of these pages (Airport Information pages, XM Satellite pages, Procedure pages), the title of the page may change while the page icon remains the same. MFD SYSTEM PAGES In the Auxiliary (AUX) Page Group, there are two system pages: System Setup (page 4 of 6) and System Status (page 6 of 6). The System Setup Page allows management of various system parameters, while the System Status Page displays the status of all G1000 system LRUs. SYSTEM SETUP PAGE G1000 system settings are managed from the System Setup Page. The following settings can be changed: • Date/time • Displayed navigation angle reference, temperature, and position settings • Baro transition alert (see the Flight Instruments Section) • Airspace alerts (see the Flight Management Section) • Arrival alerts (see the Flight Management Section) • Audio alerts • Flight Director (see the AFCS Section) • Page Navigation • MFD Navigation Status Box fields (see the Flight Management Section) • CDI scaling for GPS navigation source (see the Flight Instruments Section) • COM channel spacing (see the Audio Panel and CNS Section) • Criteria for displaying nearest airports (see the Flight Management Section) 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 35 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Restoring system setup defaults: 1) Select the AUX - SYSTEM SETUP Page. 2) Press the DFLTS Softkey; or press the MENU Key, highlight ‘Restore Defaults’, and press the ENT Key. Figure 1-29 System Setup Page 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 (Figure 1-7). 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. 190-00629-04 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft G58 36 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Figure 1-30 Pilot Profile Management (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 pro