Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58

enhance situational awareness. WARNING: Traffic information shown on the G1000 Multi Function Display is provided as an aid in visually acquiring traffic. Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic. WARNING: Use of the Stormscope is not intended for hazardous weather penetration (thunderstorm penetration). Stormscope information, as displayed on the G1000 MFD, is to be used only for weather avoidance, not penetration. WARNING: GDL 69 Weather should not be used for hazardous weather penetration. Weather information provided by the GDL 69 is approved only for weather avoidance, not penetration. WARNING: NEXRAD weather data is to be used for long-range planning purposes only. Due to inherent delays in data transmission and the relative age of the data, NEXRAD weather data should not be used for short-range weather avoidance. 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 iii WARNINGS, CAUTIONS, AND NOTES WARNING: The Garmin G1000, as installed in the Hawker Beechcraft 58/G58 aircraft, has a very high degree of functional integrity. However, the pilot must recognize that providing monitoring and/or self- test capability for all conceivable system failures is not practical. Although unlikely, it may be possible for erroneous operation to occur without a fault indication shown by the G1000. It is thus the responsibility of the pilot to detect such an occurrence by means of cross-checking with all redundant or correlated information available in the cockpit. WARNING: For safety reasons, G1000 operational procedures must be learned on the ground. WARNING: The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment. Portions of the Garmin G1000 utilize GPS as a precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the G1000 can be misused or misinterpreted and, therefore, become unsafe. WARNING: To reduce the risk of unsafe operation, carefully review and understand all aspects of the G1000 Pilot’s Guide documentation and the G1000 Integrated Avionics System and GFC 700 AFCS in Beechcraft 58/G58 Airplane Flight Manual. Thoroughly practice basic operation prior to actual use. During flight operations, carefully compare indications from the G1000 to all available navigation sources, including the information from other NAVAIDs, visual sightings, charts, etc. For safety purposes, always resolve any discrepancies before continuing navigation. WARNING : The illustrations in this guide are only examples. Never use the G1000 to attempt to penetrate a thunderstorm. Both the FAA Advisory Circular, Subject: Thunderstorms, and the Aeronautical Information Manual (AIM) recommend avoiding “by at least 20 miles any thunderstorm identified as severe or giving an intense radar echo.” WARNING : Lamp(s) inside this product may contain mercury (HG) and must be recycled or disposed of according to local, state, or federal laws. For more information, refer to our website at www.garmin.com/ aboutGarmin/environment/disposal.jsp. WARNING : Because of anomalies in the earth’s magnetic field, operating the G1000 within the following areas could result in loss of reliable attitude and heading indications. North of 70° North latitude and south of 70° South latitude. An area north of 65° North latitude between longitude 75º West and 120º West. An area south of 55° South latitude between longitude 120º East and 165º East. CAUTION: The PFD and MFD displays use a lens coated with a special anti-reflective coating that is very sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI-REFLECTIVE COATING. It is very important to clean the lens using a clean, lint-free cloth and an eyeglass lens cleaner that is specified as safe for anti-reflective coatings. Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 190-00629-01 Rev. B iv WARNINGS, CAUTIONS, AND NOTES CAUTION: The Garmin G1000 does not contain any user-serviceable parts. Repairs should only be made by an authorized Garmin service center. Unauthorized repairs or modifications could void both the warranty and the pilot’s authority to operate this device under FAA/FCC regulations. NOTE: When using Stormscope, there are several atmospheric phenomena in addition to nearby thunderstorms that can cause isolated discharge points in the strike display mode. However, clusters of two or more discharge points in the strike display mode do indicate thunderstorm activity if these points reappear after the screen has been cleared. NOTE: All visual depictions contained within this document, including screen images of the G1000 panel and displays, are subject to change and may not reflect the most current G1000 system and aviation databases. Depictions of equipment may differ slightly from the actual equipment. NOTE : This device complies with part 15 of the FCC Rules. Operation is subject to the following two conditions: (1) this device may not cause harmful interference, and (2) this device must accept any interference received, including interference that may cause undesired operation. NOTE : Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of attitude and heading displays while the aircraft is on the ground. Moving the aircraft more than 100 yards away from the source of the interference should alleviate the condition. NOTE : Use of polarized eyewear may cause the flight displays to appear dim or blank. NOTE : This product, its packaging, and its components contain chemicals known to the State of California to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with California’s Proposition 65. If you have any questions or would like additional information, please refer to our web site at www.garmin.com/prop65. 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 v 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 Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 190-00629-01 Rev. B vi 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 ................................................... 13 1.6 System Operation .................................................. 15 Normal Operation ....................................................... 15 Reversionary Mode ..................................................... 15 AHRS Operation ......................................................... 16 G1000 System Annunciations ...................................... 18 Softkey Function ......................................................... 19 GPS Receiver Operation .............................................. 24 1.7 Accessing G1000 Functionality ........................... 29 Menus ....................................................................... 29 MFD Page Groups ....................................................... 29 MFD System Pages ..................................................... 33 1.8 Display Backlighting ............................................. 47 SECTION 2 FLIGHT INSTRUMENTS 2.1 Flight Instruments ................................................. 52 Airspeed Indicator ...................................................... 52 Attitude Indicator ....................................................... 55 Altimeter ................................................................... 56 Vertical Speed Indicator (VSI) ....................................... 57 Vertical Deviation ....................................................... 58 Horizontal Situation Indicator (HSI) .............................. 59 Course Deviation Indicator (CDI) .................................. 64 2.2 Supplemental Flight Data .................................... 71 Temperature Displays .................................................. 71 Wind Data ................................................................. 72 Vertical Navigation (VNV) Indications ........................... 73 2.3 PFD Annunciations and Alerting Functions ........ 74 G1000 Alerting System ................................................ 74 Marker Beacon Annunciations ..................................... 75 Traffic Annunciation .................................................... 76 TAWS Annunciations (Optional) ................................... 76 Altitude Alerting ......................................................... 77 Low Altitude Annunciation (WAAS only) ....................... 77 Minimum Descent Altitude/Decision Height Alerting ...... 78 2.4 Abnormal Operations ........................................... 79 Abnormal GPS Conditions ........................................... 79 Unusual Attitudes ....................................................... 80 SECTION 3 ENGINE INDICATION SYSTEM 3.1 Engine Display ....................................................... 83 3.2 Lean Display ........................................................... 85 3.3 System Display ...................................................... 88 SECTION 4 AUDIO PANEL AND CNS 4.1 Overview ................................................................ 91 MFD/PFD Controls and Frequency Display ..................... 92 Audio Panel Controls .................................................. 94 4.2 COM Operation ...................................................... 96 COM Transceiver Selection and Activation ..................... 96 COM Transceiver Manual Tuning .................................. 97 Quick-Tuning and Activating 121.500 MHz .................... 98 Auto-Tuning the COM Frequency .................................. 99 Frequency Spacing .................................................... 103 Automatic Squelch.................................................... 104 Volume .................................................................... 104 4.3 NAV Operation ..................................................... 105 NAV Radio Selection and Activation ........................... 105 NAV Receiver Manual Tuning ..................................... 106 Auto-Tuning a NAV Frequency from the MFD .............. 108 Marker Beacon Receiver ............................................ 113 DME Tuning (Optional) .............................................. 114 4.4 GTX 33 Mode S Transponder .............................. 115 Transponder Controls ................................................ 115 Transponder Mode Selection ...................................... 116 Entering a Transponder Code ..................................... 119 IDENT Function ........................................................ 120 Flight ID Reporting ................................................... 121 4.5 Additional Audio Panel Functions ..................... 122 Power-Up ................................................................. 122 Mono/Stereo Headsets .............................................. 122 Speaker ................................................................... 122 Intercom .................................................................. 123 Passenger Address (PA) System .................................. 125 Clearance Recorder and Player................................... 125 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 vii TABLE OF CONTENTS Split COM ................................................................ 126 Entertainment Inputs ................................................ 127 4.6 Audio Panel Preflight Procedure ....................... 128 4.7 Abnormal Operation ........................................... 129 Stuck Microphone..................................................... 129 COM Tuning Failure................................................... 129 Audio Panel Fail-Safe Operation ................................. 129 Reversionary Mode ................................................... 129 SECTION 5 FLIGHT MANAGEMENT 5.1 Introduction ......................................................... 131 Navigation Status Box............................................... 133 5.2 Using Map Displays ............................................. 134 Map Orientation ....................................................... 134 Map Range .............................................................. 136 Map Panning............................................................ 138 Measuring Bearing and Distance ................................ 143 Topography .............................................................. 144 Map Symbols ........................................................... 147 Airways ................................................................... 153 Track Vector ............................................................. 155 Wind Vector ............................................................. 156 Nav Range Ring ....................................................... 157 Fuel Range Ring ....................................................... 158 5.3 Waypoints............................................................. 159 Airports ................................................................... 160 Intersections ............................................................ 166 NDBs ....................................................................... 168 VORs ....................................................................... 170 User Waypoints ........................................................ 172 5.4 Airspaces .............................................................. 177 5.5 Direct-to-Navigation .......................................... 181 5.6 Flight Planning..................................................... 187 Flight Plan Creation .................................................. 188 Adding Waypoints to an Existing Flight Plan................ 191 Adding Airways to a Flight Plan ................................. 193 Adding Procedures to a Stored Flight Plan .................. 196 Flight Plan Storage ................................................... 203 Flight Plan Editing .................................................... 205 Along Track Offsets ................................................... 208 Parallel Track ............................................................ 210 Activating a Flight Plan Leg ....................................... 213 Inverting a Flight Plan ............................................... 214 Flight Plan Views ...................................................... 215 Closest Point of FPL .................................................. 217 5.7 Vertical Navigation ............................................. 218 Altitude Constraints .................................................. 220 5.8 Procedures ........................................................... 224 Departures ............................................................... 224 Arrivals ................................................................... 227 Approaches ............................................................. 229 5.9 Trip Planning ........................................................ 235 Trip Planning ............................................................ 235 5.10 RAIM Prediction .................................................. 239 5.11 Navigating a Flight Plan ..................................... 243 5.12 Abnormal Operation ........................................... 270 SECTION 6 HAZARD AVOIDANCE 6.1 XM Satellite Weather .......................................... 273 Activating Services.................................................... 274 Using XM Satellite Weather Products.......................... 275 6.2 Airborne Color Weather Radar .......................... 297 System Description ................................................... 297 Principles of Pulsed Airborne Weather Radar ............... 297 Safe Operating Distance ............................................ 302 Basic Antenna Tilt Setup ............................................ 302 Weather Mapping and Interpretation ......................... 304 Ground Mapping and Interpretation ........................... 317 6.3 WX-500 Stormscope ........................................... 318 Setting Up Stormscope on the Navigation Map ........... 318 Selecting the Stormscope Page .................................. 322 6.4 Terrain Awareness and Warning System........... 323 Displaying TAWS Data ............................................... 324 TAWS Page .............................................................. 326 TAWS Alerts ............................................................. 328 System Status........................................................... 334 6.5 Traffic Information Service (TIS) ........................ 335 Displaying TRAFFIC Data ........................................... 336 Traffic Map Page....................................................... 338 TIS Alerts ................................................................. 339 System Status........................................................... 340 Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 190-00629-01 Rev. B viii TABLE OF CONTENTS 6.6 L-3 Skywatch Traffic Advisory System (TAS)..... 343 TAS Symbology......................................................... 343 Operation ................................................................ 344 Altitude Display ........................................................ 346 Traffic Map Page Display Range ................................. 347 TAS Alerts ................................................................ 348 System Status........................................................... 349 SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM 7.1 AFCS Overview .................................................... 351 Additional AFCS Controls .......................................... 353 7.2 Flight Director Operation ................................... 354 Activating the Flight Director ..................................... 354 AFCS Status Box ....................................................... 355 Flight Director Modes................................................ 356 Command Bars ......................................................... 356 7.3 Vertical Modes ..................................................... 357 Pitch Hold Mode (PIT) ............................................... 358 Selected Altitude Capture Mode (ALTS) ....................... 359 Altitude Hold Mode (ALT) .......................................... 360 Vertical Speed Mode (VS) .......................................... 361 Flight Level Change Mode (FLC) ................................. 362 Vertical Navigation Modes (VPTH, ALTV) ..................... 364 Glidepath Mode (GP) (waas only)............................... 369 Glideslope Mode (GS) ............................................... 371 Go Around Mode (GA) .............................................. 372 7.4 Lateral Modes ...................................................... 373 Roll Hold Mode (ROL) ............................................... 374 Navigation Modes (GPS, VOR, LOC, bc) ....................... 376 Approach Modes (GPS, VAPP, LOC) ............................. 378 7.5 Autopilot and Yaw Damper Operation ............. 380 Flight Control ........................................................... 380 Engagement............................................................. 381 Control Wheel Steering ............................................. 381 Disengagement ........................................................ 382 7.6 Example Flight Plan ............................................ 383 Departure ................................................................ 384 Intercepting a VOR Radial .......................................... 386 Flying a Flight Plan/GPS Course ................................. 387 Descent ................................................................... 388 Approach ................................................................. 392 Go Around/Missed Approach ..................................... 394 7.7 AFCS Annunciations and Alerts ......................... 396 AFCS Status Alerts .................................................... 396 Overspeed Protection ................................................ 397 SECTION 8 ADDITIONAL FEATURES 8.1 SafeTaxi ................................................................ 399 SafeTaxi Cycle Number and Revision .......................... 402 8.2 ChartView ............................................................. 405 ChartView Softkeys ................................................... 405 Terminal Procedures Charts ....................................... 406 Chart Options........................................................... 416 Day/Night View ........................................................ 422 ChartView Cycle Number and Expiration Date ............. 424 8.3 FliteCharts ............................................................ 428 FliteCharts Softkeys .................................................. 428 Terminal Procedures Charts ....................................... 429 Chart Options........................................................... 437 Day/Night View ........................................................ 441 FliteCharts Cycle Number and Expiration Date............. 443 8.4 XM Radio Entertainment (Optional) ................. 447 Activating XM Satellite Radio Services ........................ 447 Using XM Radio ....................................................... 449 8.5 Scheduler.............................................................. 453 8.6 Abnormal Operation ........................................... 455 APPENDICES Annunciations and Alerts ............................................. 457 Alert Level Definitions ............................................... 459 Aircraft Alerts ........................................................... 459 G1000 System Annunciations .................................... 461 G1000 System Message Advisories............................. 464 AFCS Alerts .............................................................. 475 TAWS ALERTS ........................................................... 476 SD Card Use ................................................................... 479 Jeppesen Databases.................................................. 479 Garmin Databases .................................................... 480 Glossary.......................................................................... 483 Frequently Asked Questions ........................................ 491 Map Symbols ................................................................. 497 INDEX Index ................................................................................ I-1 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/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 58/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 63/63W 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 • 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 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 58/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. 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/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 Displays (PFD) that features a 10.4-inch LCD with 1024 x 768 resolution. The display communicates with the MFD and with the #1 GIA 63/63W 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 63/63W 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 63/63W (2) – Functions as the main communication hub, linking all LRUs with the PFD and MFD. Each GIA 63/63W contains a GPS receiver, VHF COM/NAV/GS receivers, a flight director (FD) and system integration microprocessors. Each GIA 63/63W contains a GPS WAAS receiver. Each GIA 63/63W is paired with a display via HSDB connection. The GIA 63/63Ws are not paired together and do not communicate with each other directly. 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/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 63(W)s, the displays, and the GRS 77, using an ARINC 429 digital interface (it also interfaces directly with the GTP 59). The GDC 74A is designed to operate in Reduced Vertical Separation Minimum (RVSM) airspace. • GEA 71 (2) – Receives and processes signals from the engine and airframe sensors. This unit communicates with both GIA 63(W)s 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. 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/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 the #1 GIA 63(W), using an RS-232 digital interface. • GTX 33 (1) – Solid-state transponder that provides Modes A, C and S capability. The transponder can be controlled from the PFD. The transponder communicates with the GIA 63/63Ws 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. 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 5 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & cNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX • GTP 59 (2) – 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 63/63W. 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. 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/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 Engine/Airframe Unit GDC 74A Air Data Computer OAT Airspeed Altitude Vertical Speed GMU 44 Magnetometer Heading Reversionary Control GMA 1347 Audio Panel No. 2 GIA 63/63W Integrated Avionics Unit System Integration Processors I/O Processors VHF COM VHF NAV/LOC GPS Glideslope GPS Output No. 1 GIA 63/63W 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 (optional) 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 Figure 1-1 G1000 System Block Diagram 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/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 27 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/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 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/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. 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/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. 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/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 58/B58 aircraft. 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/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 58/B58 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 58/B58 aircraft. 9 PA – Not used in Beechcraft 58/B58 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 58/B58 aircraft. 16 NAV2 – When selected, audio from the #2 NAV receiver can be heard. 17 AUX – Not used in Beechcraft 58/B58 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. 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/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 1-6 Display Bezel SD Card Slots SD Card Slots 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. 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 14 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 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 1-7. 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 1-8), the MFD Power-up Page displays the following information: • System version • Copyright • Land database name and version • Terrain database name and version • Airport Terrain database name and version • Obstacle database name and version • Aviation database name, version, and effective dates • ChartView or FliteCharts database information • Safe Taxi database information Current database information includes 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 1-8 MFD Power-up Page Figure 1-7 PFD Initialization 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/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 63/63W 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 1-9 gives an example of the G1000 displays in normal mode. Figure 1-9 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. 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 16 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Figure 1-10 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 1-11 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 63/63W become inoperative, the on-side GIA 63/63W 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 63/63W are flagged as invalid (red “X”) on the remaining PFD (see Figure 1-12). Figure 1-12 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 1-13) 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. 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 17 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & cNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 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 1-13 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. 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). 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 18 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 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 14 G1000 System Failure Annunciations GDC 74A Air Data Computer GTX 33 Transponder Or GIA 63/63W Integrated Avionics Units GDC 74A Air Data Computer GEA 71 Engine Airframe Unit Or GIA 63/63W Integrated Avionics Unit GIA 63/63W Integrated Avionics Units GRS 77 AHRS Or GMU 44 Magnetometer GIA 63/63W Integrated Avionics Units GIA 63/63W Integrated Avionics Units 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/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 1-15 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 TRAFFIC Displays traffic information on Inset Map 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) PFD Displays second-level softkeys for additional PFD configurations DFLTS Resets PFD to default settings, including changing units to standard WIND Displays softkeys to select wind data parameters OPTN 1 Longitudinal and lateral components OPTN 2 Total direction and speed OPTN 3 Total direction with head and crosswind speed components OFF Information not displayed 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 20 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 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 Selects Mode A (transponder replies to interrogations) ALT Selects Mode C – altitude reporting mode (transponder replies to identification and altitude interrogations) GND Manually selects Ground Mode, the transponder does not allow Mode A and Mode C replies, but it does permit acquisition squitter and replies to discretely addressed Mode S interrogations VFR Automatically enters the VFR code (1200 in the U.S.A. only) CODE Displays transponder code selection softkeys 0-7 0 — 7 Use numbers to enter code BKSP Removes numbers entered, one at a time 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 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 21 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & cNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Figure 1-16 Top Level PFD Softkeys ALERTS (optional) Figure 1-17 INSET Softkeys Select the BACK Softkey to return to the top-level softkeys. STRMSCP ALERTS ALERTS (optional) (optional) 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 22 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Figure 1-18 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) Figure 1-19 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) 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 23 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 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 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 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 24 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Figure 1-20 MFD Softkeys MAP DCLTR TOPO 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 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 WAAS signal. While the aircraft is on the ground, the WAAS 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 WAAS 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. 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. 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 25 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & cNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 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 1-21 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 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. 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 26 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX • 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 WAAS 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. 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. 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 27 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & cNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 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. 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: 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 28 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX • ‘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 WAAS coverage area, it may be desireable to disable WAAS (although it is not recommended). When disabled, the SBAS field in the GPS Status box indicates DISABLED. Disabling WAAS 1) Select the GPS Status Page. 2) If necessary, press the SBAS Softkey. 3) Press the FMS Knob. ‘WAAS’ is highlighted. 4) Press the ENT Key to uncheck the box. 5) 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 WAAS) 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). 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 29 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 1-22 Page Menu Examples No Options with NRST Window Displayed on the PFD Options with FPL Window Displayed MFD PAGE GROUPS NOTE: Refer to the Flight Management, Hazard Avoidance, and Additional Features sections for details on specific pages. The page group and active page title box are displayed in the upper center of the screen. Page Group Active Page Title Figure 1-23 Page Title Box 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 30 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 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. Figure 1-24 Page Group Icons Page Groups Selected Page Pages in Current Group The MFD displays information in four main page groups; specific pages within each group can vary depending on the configuration of optional equipment. Selecting a page using the FMS Knob 1) Turn the large FMS Knob until the desired page group is selected. 2) Turn the small FMS Knob until the desired page is selected. There are also several pages (Airport Information and XM Information pages) which are selected first from within a main page group with the FMS Knobs, then with the appropriate softkey at the bottom of the page. In this case, the page remains set to the selected screen until a different screen softkey is pressed. Figure 1-25 Map Pages Map Pages (MAP) Navigation Map Traffic Map Weather Radar Stormscope®(optional) Weather Data Link (service optional) Terrain 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 31 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & cNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Figure 1-26 Waypoint Pages Airport Information Pages Waypoint Pages (WPT) Airport Information pages - Airport Information (INFO Softkey) - Departure Information (DP Softkey) - Arrival Information (STAR Softkey) - Approach Information (APR Softkey) - Weather Information (WX Softkey) Intersection Information NDB Information VOR Information User Waypoint Information Figure 1-27 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 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 32 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Figure 1-28 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 1-29 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 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 33 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 1-30 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 • Airspace alerts (see the Flight Management Section) • Arrival alerts (see the Flight Management Section) • Audio alerts • 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) 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 34 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 1-31 System Setup Page 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 35 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & cNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX DATE/TIME The G1000 obtains the current Universal Coordinated Time (UTC) date and time directly from the GPS satellite signals (shown on the AUX - GPS Status Page, Figure 1-22). System time (displayed in the lower right corner of the PFD) can be displayed in three formats: local 12-hr, local 24-hr, or UTC. Local time is set by adding/subtracting an offset (hours:minutes) to/from UTC. Figure 1-32 System Time (Local 24-hr Format) Configuring the system time: 1) Select the AUX - System Setup Page. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the ‘Time Format’ field. 4) Turn the small FMS Knob to select the desired format and press the ENT Key to confirm selection. The ‘Time Offset’ field is highlighted. 5) Use the FMS Knob to enter the desired time offset (±HH:MM) and press the ENT Key to confirm selection. Figure 1-33 Date/Time Settings (System Setup Page) 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 36 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX PILOT PROFILES System settings may be saved under a pilot profile. When the system is powered on, the last selected pilot profile is shown on the MFD Power-up Splash Screen (Figure 1-8). The G1000 can store up to 25 profiles; the currently active profile, the amount of memory used, and the amount of memory available are shown at the top of the System Setup Page in the box labeled ‘Pilot Profile’. From here, pilot profiles may be created, selected, renamed, or deleted. Figure 1-34 Display Unit Settings (System Setup Page) Creating a profile: 1) Select the AUX - System Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight ‘CREATE’ in the Pilot Profile Box. 4) Press the ENT Key. A ‘Create Profile’ window is displayed. 5) Use the FMS Knob to enter a profile name up to 16 characters long and press the ENT Key. Pilot profile names cannot begin with a blank as the first letter. 6) In the next field, use the small FMS Knob to select the desired settings upon which to base the new profile. Profiles can be created based on Garmin factory defaults, default profile settings (initially based on Garmin factory defaults unless edited by the pilot), or current system settings. 7) Press the ENT Key. 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 37 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & cNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 8) With ‘CREATE’ highlighted, press the ENT Key to create the profile Or: Use the large FMS Knob to select ‘CREATE and ACTIVATE’ and press the ENT Key to activate the new profile. 9) To cancel the process, select ‘CANCEL’ with the large FMS Knob and press the ENT Key. Selecting an active profile: 1) Select the AUX - System Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight the active profile field in the Pilot Profile Box. 4) Turn the small FMS Knob to display the pilot profile list and highlight the desired profile. 5) Press the ENT Key. The G1000 loads and displays the system settings for the selected profile. Renaming a profile: 1) Select the AUX - System Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight ‘RENAME’ in the Pilot Profile Box. 4) Press the ENT Key. 5) In the ‘Rename Profile’ window, turn the FMS Knob to select the profile to rename. 6) Press the ENT Key. 7) Use the FMS Knob to enter a new profile name up to 16 characters long and press the ENT Key. 8) With ‘RENAME’ highlighted, press the ENT Key. 9) To cancel the process, use the large FMS Knob to select ‘CANCEL’ and press the ENT Key. Deleting a profile: 1) Select the AUX - System Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight ‘DELETE’ in the Pilot Profile Box. 4) Press the ENT Key. 5) In the ‘Delete Profile’ window, turn the FMS Knob to select the profile to delete. 6) Press the ENT Key. 7) With ‘DELETE’ highlighted, press the ENT Key. 8) To cancel the process, use the large FMS Knob to select ‘CANCEL’ and press the ENT Key. 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 38 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX DISPLAY UNITS Units in which various quantities are displayed on the G1000 screens are listed on the System Setup Page. The Navigation Angle reference, the Temperature units, and the Position units can be set from here. Category Settings Affected Quantities Exceptions Navigation Angle Magnetic (North)* True (North) Heading Course Bearing Track Desired Track Wind direction (Trip Planning Page) Distance and Speed Metric Nautical* Crosstrack error (HSI) Bearing distances (information windows) DME distance (information window) Flight plan distances Map ranges DIS, GS, TAS, XTK fields (Navigation Status Box) All distances on MFD Altitude buffer distance (System Setup) Arrival Alert trigger distance (System Setup) All speeds on MFD Airspeed Indicator True Airspeed (PFD) Wind speed vector Map range (Traffic Page, Terrain Proximity/TAWS Page) CDI scaling (System Setup) Fuel range calculation (EIS) Altitude and Vertical Speed Feet* Meters All altitudes on MFD All elevations on MFD Altimeter Vertical Speed Indicator VNV altitudes (Active Flight Plan) Temperature Celsius* Fahrenheit All temperatures on PFD Total Air Temperature (Trip Planning Page) Engine Indication System (EIS) Fuel and Fuel Flow Gallons* Imperial Gallons Kilograms Liters Pounds Fuel parameters (Trip Planning Page) Engine Indication System (EIS) Weight** Pounds* Kilograms N/A N/A Position HDDD°MM.MM’* HDDD°MM’SS.S” All positions N/A * Default setting ** Contact a Garmin-authorized service center to change this setting Table 1-1 Display Units Settings (System Setup Page) Changing a display unit setting 1) While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor. 2) Turn the large FMS Knob to highlight the desired field in the Display Units Box. 3) Turn the small FMS Knob to select the desired units. 4) Press the ENT Key. Press the CLR Key to cancel the action without changing the units. 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 39 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & cNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX ARRIVAL ALERTS The Arrival Alert Box on the System Setup Page allows arrival alerts to be turned on/off and the alert trigger distance set. An arrival alert can be set to notify the pilot with a message upon reaching a user- specified distance from the final destination (the direct-to waypoint or the last waypoint in a flight plan). Once the set distance (up to 99.9 units) has been reached, an “Arrival at [waypoint]” message is displayed in the PFD Navigation Status Box. Figure 1-35 Arrival Alert Settings (System Setup Page) Enabling/disabling an arrival alert: 1) Use the FMS Knob to select the AUX - System Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to select the ON/OFF field in the Arrival Alert Box. 4) Turn the small FMS Knob clockwise to turn the airspace alert ON or counterclockwise to turn the alert OFF. Changing the arrival alert trigger distance: 1) Use the FMS Knob to select the AUX - System Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight the distance field in the Arrival Alert Box. 4) Use the FMS Knob to enter a trigger distance and press the ENT Key. AUDIO ALERTS The Audio Alert Box on the System Setup Page allows the audio alert voice to be set to male or female. Changing the audio alert voice 1) While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor. 2) Turn the large FMS Knob to highlight the voice in the Audio Alert Box. 3) Turn the small FMS Knob to display and highlight the desired voice and press the ENT Key. 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 40 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX SYSTEM STATUS PAGE The System Status Page displays the status and software version numbers for all detected system LRUs. Pertinent information on all system databases is also displayed. Active LRUs are indicated by green check marks and failed LRUs are indicated by red “X”s. Failed LRUs should be noted and a service center or Garmin dealer informed. Figure 1-36 Example System Status Page The LRU, ARFRM, and DBASE Softkeys on the System Status Page select the list (LRU Info, Airframe, or Database) through which the FMS Knob can be used to scroll if all the information cannot appear on the screen. The ANN TEST Softkey, when pressed, causes an annunciation test tone to be played. 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 41 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & cNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX UTILITY PAGE For flight planning purposes, timers, trip statistics, and a scheduler feature are provided on the AUX - Utility Page. The timers available include a stopwatch-like generic timer, a total time in flight timer, and a record of the time of departure. Trip statistics—odometer, trip odometer, and average trip and maximum groundspeeds—are displayed from the time of the last reset. Refer to the Additional Features section for a dicussion on the Scheduler feature. Figure 1-37 Utility Page TIMERS The G1000 timers available include: • Stopwatch-like generic timers (available from the PFD Timer/References Window and on the MFD AUX - Utility Page) • Total-time-in-flight timer (MFD AUX - Utility Page) • Time since departure (MFD AUX - Utility Page) The generic timer can be set to count up or down from a specified time (HH:MM:SS). When the countdown on the timer reaches zero the digits begin to count up from zero. If the timer is reset before reaching zero on a countdown, the digits are reset to the initial value. If the timer is counting up when reset, the digits are zeroed. 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 42 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Setting the generic timer (PFD): 1) Press the TMR/REF Softkey. 2) Turn the large FMS Knob to select the timer field (hh/mm/ss). 3) Use the FMS Knob to enter the desired time and press the ENT Key. 4) With the UP/DN field highlighted, turn the small FMS Knob to select the timer counting direction (UP/DN) and press the ENT Key. 6) With ‘START?’ highlighted, press the ENT Key to start the timer. The field changes to ‘STOP?’. 7) To stop the timer, press the ENT Key with ‘STOP?’ highlighted. The field changes to ‘RESET?’. 8) To reset the timer, press the ENT Key with ‘RESET?’ highlighted. The field changes back to ‘START?’ and the digits are reset. 9) To remove the window, press the CLR Key or the TMR/REF Softkey. Figure 1-38 Generic Timer (PFD Timer/References Window) Setting the generic timer (MFD AUX - Utility Page) 1) Use the FMS Knob to select the AUX - Utility Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the small FMS Knob to select the timer counting direction (UP/DN) and press the ENT Key. 4) If a desired starting time is desired: a) Use the large FMS Knob to highlight the HH:MM:SS field. b) Use the FMS Knob to enter the desired time and press the ENT Key. 5) Turn the large FMS Knob to highlight ‘START?’ and press the ENT Key to start the timer. The field changes to ‘STOP?’. 6) To stop the timer, press the ENT Key with ‘STOP?’ highlighted. The field changes to ‘RESET?’. 7) To reset the timer, press the ENT Key with ‘RESET?’ highlighted. The field changes back to ‘START?’ and the digits are reset. 190-00629-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft 58/G58 43 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & cNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Figure 1-39 Timers (MFD AUX - Utility Page) The flight timer can be set to count up from zero starting at system power-up or from the time that the aircraft lifts off; the timer can also be reset to zero at any time. Setting the flight timer starting criterion 1) Use the FMS Knob to select the AUX - Utility Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight the field next to the flight timer. 4) Turn the small FMS Knob to select the starting criterion (PWR-ON or IN-AIR) and press the ENT Key. Resetting the flight timer 1) Use the FMS Knob to select the AUX - Utility Page. 2) Press the MENU Key. 3) With ‘Reset Flight Timer’ highlighted, press the ENT Key. The G1000 records the time at which departure occurs, depending on whether the pilot prefers the time to be recorded from system power-up or from aircraft lift off. The displayed departure time can also be reset to display the current time at the point of reset. The format in which the time is displayed is controlled from the System Setup Page. Setting the departure timer starting criterion 1) Use the FMS Knob to select the AUX - Utility Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight th