Garmin G1000 Pilot’s Guide for Cessna Nav III

Facsimile: (913)397-8282 Facsimile Toll Free: (800)801-4670 E-mail: orders@garmin.com avionics@garmin.com warranty@garmin.com Garmin (Europe) Ltd. Liberty House, Bulls Copse Road, Southampton, SO40 9RB, UK Telephone: ++44 (0) 870-8501243 Telephone Toll Free: ++44 (0) 0808 238 0000 (option 5) Facsimile: ++44 (0) 238052004 E-mail: avionics.europe@garmin.com Garmin G1000 Pilot’s Guide for Cessna Nav III 190-00498-07 Rev. A ii WARNINGS, CAUTIONS, AND NOTES WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance feature. The terrain avoidance feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight. The terrain avoidance feature is only to be used as an aid for terrain avoidance. Terrain data is obtained from third party sources. Garmin is not able to independently verify the accuracy of the terrain data. WARNING: The displayed minimum safe altitudes (MSAs) are only advisory in nature and should not be relied upon as the sole source of obstacle and terrain avoidance information. Always refer to current aeronautical charts for appropriate minimum clearance altitudes. WARNING: The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and could vary significantly from the altitude displayed by pressure altimeters, such as the GDC 74A Air Data Computer, or other altimeters in aircraft. GPS altitude should never be used for vertical navigation. Always use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft. WARNING: Do not use outdated database information. Databases used in the G1000 system must be updated regularly in order to ensure that the information remains current. Pilots using any outdated database do so entirely at their own risk. WARNING: Do not use basemap (land and water data) information for primary navigation. Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness. WARNING: Traffic information shown on system displays 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: Do not use datalink weather products (e.g., XM WX Satellite Weather, GFDS World Wide Weather, or FIS-B) for hazardous weather penetration. Weather information provided by these products is aged by up to several minutes and may not depict actual weather conditions as they currently appear. 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. 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III iii WARNINGS, CAUTIONS, AND NOTES WARNING: For safety reasons, G1000 operational procedures must be learned on the ground. WARNING: The Garmin G1000, as installed in Cessna Nav III 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: 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. 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 Airman’s Information Manual (AIM) recommend avoiding “by at least 20 miles any thunderstorm identified as severe or giving an intense radar echo.” WARNING: Because of variation in the earth’s magnetic field, operating the system within the following areas could result in loss of reliable attitude and heading indications. North of 72° North latitude at all longitudes. South of 70° South latitude at all longitudes. North of 65° North latitude between longitude 75° W and 120° W. (Northern Canada). North of 70° North latitude between longitude 70° W and 128° W. (Northern Canada). North of 70° North latitude between longitude 85° E and 114° E. (Northern Russia). South of 55° South latitude between longitude 120° E and 165° E. (Region south of Australia and New Zealand). WARNING: Do not use GPS to navigate to any active waypoint identified as a ‘NON WGS84 WPT’ by a system message. ‘NON WGS84 WPT’ waypoints are derived from an unknown map reference datum that may be incompatible with the map reference datum used by GPS (known as WGS84) and may be positioned in error as displayed. Garmin G1000 Pilot’s Guide for Cessna Nav III 190-00498-07 Rev. A iv WARNINGS, CAUTIONS, AND NOTES CAUTION: The PFD and MFD displays use a lens coated with a special anti-reflective coating that is very sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI-REFLECTIVE COATING. It is very important to clean the lens using a clean, lint-free cloth and an eyeglass lens cleaner that is specified as safe for anti-reflective coatings. CAUTION: The Garmin G1000 does not contain any user-serviceable parts. Repairs should only be made by an authorized Garmin service center. Unauthorized repairs or modifications could void both the warranty and the pilot’s authority to operate this device under FAA/FCC regulations. NOTE: When using Stormscope, there are several atmospheric phenomena in addition to nearby thunderstorms that can cause isolated discharge points in the strike display mode. However, clusters of two or more discharge points in the strike display mode do indicate thunderstorm activity if these points reappear after the screen has been cleared. NOTE: 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: 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 : The GDU 1040 PFD/MFD may require a warm-up time of up to 30 minutes when exposed to -40˚C for an extended period. A warm-up time of up to 15 minutes may be required when exposed to -30˚C for an extended period. NOTE : This product, its packaging, and its components contain chemicals known to the State of California to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with California’s Proposition 65. If you have any questions or would like additional information, please refer to our web site at www.garmin.com/prop65. NOTE: Use of polarized eyewear may cause the flight displays to appear dim or blank. 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III v REVISION INFORMATION Record of Revisions Part Number Revision Date Page Range Description 190-00498-00 A 10/27/05 i - I-4 Reformatted for single part number (all previous part numbers incorporated into this part number) Added TAWS-B Added CO Guardian Added new fuel totalizer 190-00498-01 A 9/11/06 i - I-6 Added GFC 700 AFCS Added WAAS and VNAV Added Chartview, Flitecharts, and SafeTaxi Added GDU 7.00 parameters Change manual to larger format 190-00498-02 A 3/8/07 i - I-6 Added Airways Added ADS-B Added GDU 8.02 parameters Various clerical changes 190-00498-03 A 11/6/07 i - I-6 Added GDU 8.20 parameters, including gradient background on the PFD and GFC 700 for the C172. 190-00498-04 A 9/26/08 All Added GDU 9.03 parameters Removed gradient background. Added Synthetic Vision System 190-00498-05 A 8/14/09 All Added GDU 9.14 Added new page navigation Added flight plan import/export Added new EIS displays Added CDI use in Dead Reckoning Mode Various clerical changes 190-00498-06 A B 1/10 4/10 All 484 Added GDU 10.01 Added Auxiliary Video Added AOPA Airport Directory Added Flight Data Logging Removed statement regarding certain SD cards voiding the G1000 warranty. 190-00498-07 A 10/11 All Added Profile View Added FIS-B Weather Added Arrival Alert Added GTS 800 Traffic System Updated database synchronization Added GDU 12.02 parameters Garmin G1000 Pilot’s Guide for Cessna Nav III 190-00498-07 Rev. A vi REVISION INFORMATION B lank Page 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III vii 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 Audio Panel Controls .................................................. 10 1.4 Secure Digital (SD) Cards ..................................... 12 1.5 System Power-up ................................................... 13 1.6 System Operation .................................................. 14 Normal Display Operation ........................................... 14 Reversionary Display Operation ................................... 14 AHRS Operation ......................................................... 15 G1000 System Annunciations ...................................... 17 Softkey Function ......................................................... 17 GPS Receiver Operation .............................................. 25 1.7 Accessing G1000 Functionality............................ 29 Menus ....................................................................... 29 MFD Page Groups ....................................................... 30 MFD System Pages...................................................... 34 1.8 Display Backlighting ............................................. 44 Automatic Adjustment ................................................ 44 Manual Adjustment .................................................... 44 SECTION 2 FLIGHT INSTRUMENTS 2.1 Flight Instruments ................................................. 50 Airspeed Indicator ...................................................... 50 Attitude Indicator ....................................................... 52 Altimeter ................................................................... 53 Vertical Speed Indicator (VSI) ....................................... 55 Horizontal Situation Indicator (HSI) .............................. 57 Course Deviation Indicator (CDI) .................................. 62 2.2 Supplemental Flight Data .................................... 69 Outside Air Temperature .............................................. 69 Wind Data ................................................................. 71 Vertical Navigation (VNV) Indications ........................... 72 2.3 PFD Annunciations and Alerting Functions ........ 73 System Alerting .......................................................... 73 Marker Beacon Annunciations...................................... 74 Traffic Annunciation .................................................... 74 TAWS Annunciations ................................................... 75 Altitude Alerting ......................................................... 76 Low Altitude Annunciation .......................................... 76 Minimum Descent Altitude/Decision Height Alerting ...... 77 2.4 Abnormal Operations ........................................... 78 Abnormal GPS Conditions ........................................... 78 Unusual Attitudes ....................................................... 79 SECTION 3 ENGINE INDICATION SYSTEM (EIS) 3.1 Engine Display ....................................................... 83 Normally-Aspirated and Turbocharged Aircraft .............. 83 3.2 Lean Display ........................................................... 86 Normally-Aspirated Aircraft ......................................... 88 Turbocharged Aircraft.................................................. 89 3.3 System Display ...................................................... 90 Normally-Aspirated and Turbocharged Aircraft .............. 90 SECTION 4 AUDIO PANEL AND CNS 4.1 Overview ................................................................ 95 MFD/PFD Controls and Frequency Display ..................... 96 Audio Panel Controls .................................................. 98 4.2 COM Operation .................................................... 100 COM Transceiver Selection and Activation ................... 100 COM Transceiver Manual Tuning ................................ 101 Quick-tuning and Activating 121.500 MHz .................. 102 Auto-tuning the COM Frequency ................................ 103 Frequency Spacing .................................................... 107 Automatic Squelch.................................................... 108 Volume .................................................................... 108 4.3 NAV Operation ..................................................... 109 NAV Radio Selection and Activation ........................... 109 NAV Receiver Manual Tuning ..................................... 110 Auto-tuning a NAV Frequency from the MFD ............... 112 Marker Beacon Receiver ............................................ 117 DME Tuning ............................................................. 118 4.4 GTX 33 Mode S Transponder .............................. 119 Transponder Controls ................................................ 119 Transponder Mode Selection ...................................... 120 Entering a Transponder Code ..................................... 123 IDENT Function ........................................................ 124 4.5 Additional Audio Panel Functions ..................... 125 Power-up ................................................................. 125 Mono/Stereo Headsets .............................................. 125 Speaker ................................................................... 125 Intercom .................................................................. 126 Passenger Address (PA) System .................................. 128 Clearance Recorder and Player................................... 128 Entertainment Inputs ................................................ 129 Garmin G1000 Pilot’s Guide for Cessna Nav III 190-00498-07 Rev. A viii TABLE OF CONTENTS 4.6 Audio Panel Preflight Procedure ....................... 130 4.7 Abnormal Operation ........................................... 131 Stuck Microphone..................................................... 131 COM Tuning Failure................................................... 131 Audio Panel Fail-safe Operation ................................. 131 Reversionary Mode ................................................... 131 SECTION 5 FLIGHT MANAGEMENT 5.1 Introduction ......................................................... 133 Navigation Status Box............................................... 134 5.2 Using Map Displays ............................................. 136 Map Orientation ....................................................... 136 Map Range .............................................................. 138 Map Panning............................................................ 140 Measuring Bearing and Distance ................................ 144 Topography .............................................................. 145 Map Symbols ........................................................... 148 Airways ................................................................... 154 Track Vector ............................................................. 156 Wind Vector ............................................................. 157 Nav Range Ring........................................................ 158 Fuel Range Ring ....................................................... 159 Field of View (SVS) .................................................... 160 Selected Altitude Intercept Arc ................................... 161 5.3 Waypoints............................................................. 162 Airports ................................................................... 163 Intersections ............................................................ 170 NDBs ....................................................................... 172 VORs ....................................................................... 174 User Waypoints ........................................................ 176 5.4 Airspaces .............................................................. 182 5.5 Direct-to-Navigation .......................................... 185 5.6 Flight Planning..................................................... 190 Flight Plan Creation .................................................. 191 Adding Waypoints to an Existing Flight Plan................ 196 Adding Airways to a Flight Plan ................................. 198 Adding Procedures to a Stored Flight Plan .................. 201 Flight Plan Storage ................................................... 207 Flight Plan Editing .................................................... 210 Along Track Offsets ................................................... 214 Parallel Track ............................................................ 215 Activating a Flight Plan Leg ....................................... 218 Inverting a Flight Plan ............................................... 219 Flight Plan Views ...................................................... 220 Closest Point of FPL .................................................. 222 5.7 Vertical Navigation ............................................. 223 Altitude Constraints .................................................. 225 5.8 Procedures ........................................................... 229 Departures ............................................................... 229 Arrivals ................................................................... 232 Approaches ............................................................. 234 5.9 Trip Planning ........................................................ 240 Trip Planning ............................................................ 240 5.10 RAIM Prediction................................................... 244 5.11 Navigating a Flight Plan ..................................... 247 5.12 Abnormal Operation ........................................... 275 SECTION 6 HAZARD AVOIDANCE 6.1 XM WX Satellite Weather ................................... 278 Activating Services.................................................... 278 Using XM WX Satellite Weather Products .................... 279 6.2 GFDS Worldwide Weather .................................. 312 Registering the Iridium Satellite System ...................... 312 Registering the system for Garmin Flight Data Services 313 GFDS Weather Data Requests .................................... 322 Worldwide Weather Products ..................................... 326 Abnormal Operations ................................................ 342 6.3 FIS-B Weather ...................................................... 344 Using FIS-B Weather Products .................................... 344 6.4 WX-500 Stormscope ........................................... 359 Setting Up Stormscope on the Navigation Map ........... 359 6.5 Terrain Proximity ................................................. 364 Displaying Terrain Proximity Data ............................... 364 6.6 Profile View Terrain ............................................. 369 Profile View Display .................................................. 369 6.7 Terrain-SVS ........................................................... 372 Displaying Terrain-SVS Data ....................................... 373 Terrain-SVS Page ...................................................... 375 Terrain-SVS Alerts ..................................................... 377 6.8 TAWS-B ................................................................. 381 Displaying TAWS-B Data ............................................ 382 TAWS-B Page ........................................................... 385 TAWS-B Alerts .......................................................... 387 System Status........................................................... 392 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III ix TABLE OF CONTENTS 6.9 Traffic Information Service (TIS) ........................ 394 Displaying TRAFFIC Data ........................................... 395 Traffic Map Page....................................................... 397 TIS Alerts ................................................................. 398 System Status........................................................... 399 6.10 Garmin GTS 800 Traffic ....................................... 402 Theory of operation .................................................. 402 TAS Alerts ................................................................ 405 System Test .............................................................. 406 Operation ................................................................ 407 6.11 Honeywell KTA870 Traffic................................... 415 TAS Symbology......................................................... 415 Operation ................................................................ 416 Altitude Display ........................................................ 419 Traffic Map Page Display Range ................................. 419 TAS Alerts ................................................................ 421 System Status........................................................... 422 6.12 ADS-B Traffic ........................................................ 423 SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM 7.1 AFCS Controls ...................................................... 430 7.2 Flight Director Operation ................................... 432 Activating the Flight Director ..................................... 432 AFCS Status Box ....................................................... 433 Command Bars ......................................................... 434 Flight Director Modes................................................ 434 7.3 Vertical Modes ..................................................... 435 Pitch Hold Mode (PIT) ............................................... 436 Selected Altitude Capture Mode (ALTS) ....................... 437 Altitude Hold Mode (ALT) .......................................... 438 Vertical Speed Mode (VS) .......................................... 439 Flight Level Change Mode (FLC) ................................. 440 Vertical Navigation Modes (VPTH, ALTV) ..................... 442 Glidepath Mode (GP) (SBAS Only) .............................. 447 Glideslope Mode (GS) ............................................... 449 Go Around Mode (GA) .............................................. 450 7.4 Lateral Modes ...................................................... 451 Roll Hold Mode (ROL) ............................................... 452 Heading Select Mode (HDG) ...................................... 453 Navigation Modes (GPS, VOR, LOC) ............................ 454 Approach Modes (GPS, VAPP, LOC) ............................. 456 Backcourse Mode (BC) .............................................. 458 7.5 Autopilot Operation............................................ 459 Engaging the Autopilot ............................................. 459 Control Wheel Steering ............................................. 460 Disengaging the Autopilot ......................................... 460 7.6 Example Procedures............................................ 461 Departure ................................................................ 462 Intercepting a VOR Radial .......................................... 464 Flying a Flight Plan/GPS Course ................................. 465 Descent ................................................................... 466 Approach ................................................................. 470 Go Around/Missed Approach ..................................... 474 7.7 AFCS Annunciations and Alerts ......................... 476 AFCS Status Alerts .................................................... 476 Overspeed Protection ................................................ 477 SECTION 8 ADDITIONAL FEATURES 8.1 Synthetic Vision System (SVS) (Optional) ......... 480 SVS Operation .......................................................... 481 SVS Features ............................................................ 483 Field of View ............................................................ 491 8.2 SafeTaxi ................................................................ 493 SafeTaxi Cycle Number and Revision .......................... 496 8.3 ChartView (Optional) .......................................... 499 ChartView Softkeys ................................................... 499 Terminal Procedures Charts ....................................... 500 Chart Options........................................................... 508 Day/Night View ........................................................ 514 ChartView Cycle Number and Expiration Date ............. 516 8.4 FliteCharts ............................................................ 519 FliteCharts Softkeys .................................................. 519 Terminal Procedures Charts ....................................... 520 Chart Options........................................................... 527 Day/Night View ........................................................ 531 FliteCharts Cycle Number and Expiration Date............. 533 8.5 AOPA Airport Directory....................................... 536 AOPA Database Cycle Number and Revision ............... 537 8.6 SiriusXM Satellite Radio (Service Optional) .... 539 Activating SiriusXM Satellite Radio Services ................ 539 Using SiriusXM Radio................................................ 540 Automatic Audio Muting ........................................... 544 8.7 Scheduler.............................................................. 545 8.8 Electronic Checklists ........................................... 547 Garmin G1000 Pilot’s Guide for Cessna Nav III 190-00498-07 Rev. A x TABLE OF CONTENTS 8.9 Flight Data Logging ............................................ 550 8.10 Auxiliary Video (Optional) .................................. 552 Video Setup ............................................................. 553 Display Selection ...................................................... 553 Input Selection ......................................................... 554 Zoom/Range ............................................................ 554 8.11 Abnormal Operation ........................................... 556 SVS Troubleshooting ................................................. 556 Reversionary Mode ................................................... 556 Unusual Attitudes ..................................................... 557 APPENDICES Annunciations and Alerts ............................................. 561 Alert Level Definitions ............................................... 562 Nav III Aircraft Alerts ................................................. 562 CO Guardian Messages ............................................. 563 G1000 System Annunciations .................................... 563 Other G1000 Aural Alerts .......................................... 566 G1000 System Message Advisories............................. 566 Flight Plan Import/Export Messages ........................... 577 AFCS Alerts .............................................................. 578 Terrain-SVS Alerts ..................................................... 579 TAWS-B ALERTS ........................................................ 580 TAWS-B System Status Annunciations ......................... 581 Database Management ................................................ 583 Jeppesen Databases.................................................. 583 Garmin Databases .................................................... 587 Glossary.......................................................................... 593 Frequently Asked Questions ........................................ 599 General TIS Information ............................................... 603 Introduction ............................................................. 603 TIS vs. TAS/TCAS ....................................................... 603 TIS Limitations.......................................................... 603 Map Symbols ................................................................. 605 INDEX Index ................................................................................ I-1 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 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 is designed to provide an overview of the G1000 Integrated Flight Deck as installed in Cessna Nav III aircraft, which include the Cessna 172R, 172S, the normally aspirated Cessna 182 (182), the turbocharged Cessna 182 (T182), the normally aspirated Cessna 206 (206), and the turbocharged Cessna 206 (T206). 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 1040/1044B Primary Flight Display (PFD) • GDU 1040/1044B Multi Function Display (MFD) • GIA 63/63W Integrated Avionics Unit (IAU) • 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 • GTS 800 Traffic Avoidance System (optional) • GDL 90 ADS-B/FIS-B Data Link Transceiver (optional) • GSA 81 AFCS Servos • GSM 85 Servo Gearboxs A top-level G1000 system block diagram is shown in Figure 1-1. See Figure 1-2 for optional/additional equipment. NOTE: Refer to the AFCS section for details on the GFC 700 AFCS. The GFC 700 Automated Flight Control System (AFCS) provides the flight director (FD) and autopilot (AP) functions of the G1000 system. 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 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 1040/1044B – The GDU 1044B features a 10.4-inch LCD display with 1024 x 768 resolution. The left display is configured as a PFD and the right display is configured as an MFD. Both GDU 1044Bs link and display all functions of the G1000 system during flight. The displays communicate with each other through a High-Speed Data Bus (HSDB) Ethernet connection. Each display is also paired via an Ethernet connection with a GIA 63 or 63W Integrated Avionics Unit. Systems that do not use the GFC 700 Automatic Flight Control System use the GDU 1040, which employs the same features as the GDU 1044B without the controls for the Garmin GFC 700 Automatic Flight Control System (AFCS). • GIA 63/63W (2) – Functions as the main communication hub, linking all LRUs with the PFD. Each GIA 63/63W contains a GPS receiver, VHF COM/NAV/GS receivers, a flight director (FD) and system integration microprocessors. The GIA 63W contains a GPS SBAS receiver. Each GIA is paired with a respective GDU 1040/1044B display through Ethernet. The GIAs are not paired together and do not communicate with each other directly. • 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 63/63W, GDU 1040/1044B, and GRS 77, using an ARINC 429 digital interface. The GDC 74A also interfaces directly with the GTP 59. 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 3 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX • GEA 71 (1) – Receives and processes signals from the engine and airframe sensors. This unit communicates with both GIA 63/63Ws using an RS-485 digital interface. • GRS 77 (1) – Provides aircraft attitude and heading information via ARINC 429 to both the GDU 1040/1044B and the GIA 63/63W. The GRS 77 contains advanced sensors (including accelerometers and rate sensors) and interfaces with the on-side GMU 44 to obtain magnetic field information, with the GDC 74A to obtain air data, and with both GIAs 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. • GMA 1347 – The GMA 1347 Audio Panel integrates NAV/COM digital audio, intercom system and marker beacon controls. The GMA 1347 also controls manual display reversionary mode (red DISPLAY BACKUP button) and is installed between the MFD and the PFD. The GMA 1347 communicates with both GIA 63/ 63Ws using an RS-232 digital interface. • GTX 33 (1) – The GTX 33 is a solid-state, Mode-S transponder that provides Modes A, C and S operation. The GTX 33 is controlled through the PFD and communicates with both GIA 63/63Ws through an RS-232 digital interface. 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 4 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX • 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 SiriusXM Satellite Radio service is required to enable the GDL 69A capability. • GTS 800 – The GTS 800 Traffic Advisory System (TAS) uses active interrogations of Mode S and Mode C transponders to provide Traffic Advisories to the pilot independent of the air traffic control system. • GDL 90 (1) – A digital data link transceiver designed to transmit, receive and decode ADS-B traffic information, as well as FIS-B weather information. It broadcasts aircraft position, velocity, projected track, altitude, and flight identification to other equipped aircraft in the vicinity, as well as to FAA ground stations. The GDL 90 receives FIS-B weather information which is displayed on the MFD as NEXRAD radar and METARs. • GSA 81 (3), and GSM 85 (3) – The GSA 81 servos are used for the automatic control of roll, pitch, 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. 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 5 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Figure 1-1 Basic G1000 System No. 1 GIA 63/63W Integrated Avionics Unit System Inegration Processors I/O Processors VHF COM VHF NAV/LOC GPS/WAAS Glideslope GFC 700 Flight Director (172S, 182, & 206) No. 2 GIA 63/63W Integrated Avionics Unit System Integration Processors I/O Processors VHF COM VHF NAV/LOC GPS/WAAS Glideslope GTX 33 Transponder Reversionary Control GEA 71 Engine/Airframe Unit GDC 74A Air Data Computer OAT Airspeed Altitude Vertical Speed GRS 77 AHRS Attitude Rate of Turn Slip/Skid GMU 44 Magnetometer Heading GPS Output GPS Output Reversionary Control GMA 1347 Audio Panel PFD GDU 1040 or GDU 1044B* Honeywell KAP 140 Autopilot MFD GDU 1040 or GDU 1044B* The GDU 1040 is available in systems not using the GFC 700 Automatic Flight Control System. The GDU 1044B is available in systems using the Garmin GFC 700 Automatic Flight Control System. * GSA 81 Pitch Trim Autopilot Calculations (172S/TD,182 & 206) GSA 81 Pitch Servo Autopilot Calculations (172S/TD,182 & 206) GSA 81 Roll Servo Autopilot Calculations (172S/TD,182 & 206) GTS 800 TAS or GDL 90 Data Link ADS-B Traffic Data 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 6 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX No. 2 GIA 63/63W Integrated Avionics Unit System Integration Processors I/O Processors VHF COM VHF NAV/LOC GPS Glideslope L3 Stormscope Lightning Strike and Thunderstorm Detection Honeywell KR 87 ADF Receiver Honeywell KN 63 DME GDL 69/69A Data Link Weather Data Digital Audio Entertainment CO Guardian Carbon Monoxide Detection Honeywell KTA 870 Traffic Avoidance System ELT Emergency Locator Transmitter No. 1 GIA 63/63W Integrated Avionics Unit System Integration Processors I/O Processors VHF COM VHF NAV/LOC GPS Glideslope GFC 700 Flight Director Figure 1-2 Additional Equipment Options 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 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 described in the CNS & Audio Panel and AFCS sections respectively. The G1000 system controls are located on the PFD and MFD bezels and audio panel. The controls for the PFD and MFD are discussed within the following pages of this section. PFD/MFD CONTROLS Figure 1-3 PFD/MFD Controls 4 2 1 6 5 7 9 8 3 17 12 13 11 10 27 25 24 28 16 15 14 20 21 19 23 18 22 26 29 GFC 700 AFCS Only 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 8 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX PFD and MFD control functions are the same. 1 NAV VOL/ID Knob – Controls the NAV audio level. Press to toggle the Morse code identifier ON and OFF. Volume level is shown in the field as a percentage. 2 NAV Frequency Transfer Key – Transfers the standby and active NAV frequencies. 3 Dual NAV Knob – Tunes the MHz (large knob) and kHz (small knob) standby frequencies for the NAV receiver. Press to toggle the tuning cursor (light blue box) between the NAV1 and NAV2 fields. 4 Heading Knob – Turn to manually select a heading on the HSI. When pressed, it synchronizes the heading bug with the compass lubber line. Selected Heading provides the heading reference to the Flight Director while operating in Heading Select mode. 5 Joystick – Changes the map range (distance top to bottom of map display) when rotated. Activates the map pointer when pressed. 6 CRS/BARO Knob – The large knob sets the altimeter barometric pressure and the small knob adjusts the course. The course is only adjustable when the HSI is in VOR1, VOR2, or OBS/SUSP mode. Pressing this knob centers the CDI on the currently selected VOR. Selected Course provides course reference to the Flight Director when operating in Navigation and Approach modes. 7 Dual COM Knob – Tunes the MHz (large knob) and kHz (small knob) standby frequencies for the COM transceiver. Pressing this knob toggles the tuning cursor (light blue box) between the COM1 and COM2 fields. 8 COM Frequency Transfer Key – Transfers the standby and active COM frequencies. Pressing and holding this key for two seconds automatically tunes the emergency frequency (121.5 MHz) in the active frequency field. 9 COM VOL/SQ Knob – Controls COM audio level. Audio volume level is shown in the field as a percentage. Pressing this knob turns the COM automatic squelch ON and OFF. 10 Direct-to Key – Allows the user to enter a destination waypoint and establish a direct course to the selected destination (specified by the identifier, chosen from the active route, or taken from the map pointer position). 11 FPL Key – Displays the active Flight Plan Page for creating and editing the active flight plan, or for accessing stored flight plans. 12 CLR Key (DFLT MAP) – Erases information, cancels an entry, or removes page menus. To display the Navigation Map Page immediately, press and hold CLR (MFD only). 13 Dual FMS Knob – Press to turn the selection cursor ON/OFF. Data Entry: With the cursor ON, turn to enter data in the highlighted field (large knob moves cursor location; small knob selects character for highlighted cursor location). When the cursor is turned ON while viewing the Active Flight Plan Page, the cursor is placed on the line below the Data Insertion Pointer see Figure 1-4. The pointer indicates data entered at the cursor will be inserted above the line selected. 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) 14 MENU Key – Displays a context-sensitive list of options. This list allows the user to access additional features, or to make setting changes that relate to certain pages. 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 9 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Figure 1-4 Data Insertion Pointer Data is Inserted Above the Cursor, Indicated by the Data Insertion Pointer 15 PROC Key – Selects approaches, departures and arrivals from the flight plan. If a flight plan is used, available procedures for the departure and/or arrival airport are automatically suggested. If a flight plan is not used, the desired airport and the desired procedure may be selected. This key selects IFR departure procedures (DPs), arrival procedures (STARs) and approaches (IAPs) from the database and loads them into the active flight plan. 16 ENT Key – Accepts a menu selection or data entry. This key is used to approve an operation or complete data entry. It is also used to confirm selections and information entries. 17 Dual ALT Knob – Sets the selected altitude in the box located above the Altimeter. The large knob selects the thousands (500m for metric), while the small knob selects the hundreds (50m for metric). Altitude Select is used by the Automatic Flight Control System in certain modes, in addition to the standard G1000 Altitude Alerter function. The following are only available with the GFC 700 AFCS. 18 AP Key – Engages/disengages the autopilot and flight director. Pressing the AP Key activates the flight director and engages the autopilot in the default pitch axis and roll axis modes. Pressing the AP Key again disengages the autopilot and deactivates the flight director. 19 HDG Key – Selects/deselects Heading Select Mode. 20 NAV Key – Selects/deselects Navigation Mode. 21 APR Key – Selects/deselects Approach Mode. 22 VS Key – Selects/deselects Vertical Speed Mode. 23 FLC Key – Selects/deselects Flight Level Change Mode. 24 FD Key – Activates/deactivates the flight director only. Pressing the FD Key turns on the flight director in the default pitch axis and roll axis 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. 25 ALT Key – Selects/deselects Altitude Hold Mode. 26 VNV Key – Selects/deselects Vertical Navigation Mode. 27 BC Key – Selects/deselects Back Course Mode. 28 29 NOSE UP/NOSE DN Keys – Controls the active pitch reference for the Pitch Hold, Vertical Speed, and Flight Level Change modes. 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 10 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX AUDIO PANEL CONTROLS Figure 1-5 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 receiver audio 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 is simultaneously selected when this key is pressed allowing received audio from the #2 COM receiver to be heard. COM2 can be deselected by pressing the COM2 Key, or COM1 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 on Cessna Nav III aircraft. 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 11 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 6 COM3 – Not used on Cessna Nav III aircraft. 7 COM 1/2 – Split COM is disabled on Cessna Nav III aircraft. 8 TEL – Not used on Cessna Nav III aircraft. 9 PA – Selects the Passenger Address system. The selected COM transmitter is deselected when the PA Key is pressed. The Passenger Address system is disabled on the Cessna 172R/S. 10 SPKR – Selects and deselects the cabin speaker. COM and NAV receiver audio can be heard on the speaker. 11 MKR/MUTE – Mutes the currently received marker beacon receiver audio. Unmutes when new marker beacon audio is received. Also, stops play of the clearance recorder. 12 HI SENS – Press to increase marker beacon receiver sensitivity. Press again to return to normal. 13 DME – Pressing turns DME audio on or off. 14 NAV1 – When selected, audio from the #1 NAV receiver can be heard. 15 ADF – Pressing turns on or off the audio from the ADF receiver. 16 NAV2 – When selected, audio from the #2 NAV receiver can be heard. 17 AUX – Not used on Cessna Nav III aircraft. 18 MAN SQ – Press to enable manual squelch for the intercom. When 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 audio. Pressing the PLAY Key during play begins playing the previously recorded memory block. Each subsequent press of the PLAY Key begins playing the next previously recorded block. Press the MKR/MUTE Key to stop play. 20 PILOT – Pressing selects the pilot intercom isolation. Press again to deselect pilot isolation. 21 COPLT – Pressing selects the copilot intercom isolation. Press again to deselect copilot isolation. 22 PILOT Knob – Press to switch between volume and squelch control as indicated by the ‘VOL’ or ‘SQ’ being illuminated. 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 Reversionary Mode Button – Pressing manually selects Reversionary Mode. 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 12 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 1.4 SECURE DIGITAL (SD) CARDS NOTE: Ensure the G1000 System is powered off before inserting an SD card. NOTE: Refer to Appendix B for instructions on loading database updates. The PFD and MFD data card slots use Secure Digital (SD) cards and are located on the upper right side of the display bezels. SD cards are used for storing the various databases and system software updates. Each display bezel is equipped with two SD card slots. The top slot is used for importing and exporting flight plans, Flight Data Logging, and loading navigation database updates. The bottom slot of each display contains a Garmin Supplemental Data Card which is used for storing the various databases. Not all SD cards are compatible with the G1000. Use only SD cards supplied by Garmin or the aircraft manufacturer. Installing an SD card: 1) Insert the SD card in the SD card slot, pushing the card in until the spring latch engages. The front of the card should remain flush with the face of the display bezel. 2) To eject the card, gently press on the SD card to release the spring latch. Figure 1-6 Display Bezel SD Card Slots SD Card Slots 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 13 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 1.5 SYSTEM POWER-UP NOTE: See the Aircraft Flight Manual (AFM) for specific procedures concerning avionics power application and emergency power supply operation. NOTE: Refer to Appendix A for system-specific annunciations and alerts. The G1000 System is integrated with the aircraft electrical system and receives power directly from electrical busses. The G1000 PFD, MFD, and supporting sub-systems include both power-on and continuous built-in test features that exercise the processor, RAM, ROM, external inputs, and outputs to provide safe operation. During system initialization, test annunciations are displayed, as shown in Figure 1-7. All system annunciations should disappear typically within the first minute of power-up. Upon power-up, key annunciator lights also become momentarily illuminated on the Audio Panel. On the PFD, the AHRS begins to initialize and displays “AHRS ALIGN: Keep Wings Level”. The AHRS should display valid attitude and heading fields typically within the first minute of power-up. The AHRS can align itself both while taxiing and during level flight. When the MFD powers up, the power-up screen (Figure 1-8) displays the following information: • System version • Copyright • Land database name and version • Safe Taxi database information • Terrain database name and version • Obstacle database name and version • Navigation database name, version, and effective dates • Airport Directory name, version and effective dates • FliteCharts/ChartView database information Current database information includes database type, cycle number, or valid operating dates. Review the listed information for currency (to ensure that no databases have expired). Pressing the ENT Key (or right-most softkey) acknowledges this information, and the Navigation Map Page is displayed upon pressing the key a second time. When the system has acquired a sufficient number of satellites to determine a position, the aircraft’s current position is shown on the Navigation Map Page. Figure 1-7 PFD Initialization Figure 1-8 MFD Power-Up Screen (172R shown) 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 14 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 1.6 SYSTEM OPERATION NOTE: In normal operating mode, backlighting can only be adjusted from the PFD. In reversionary mode, it can be adjusted from the remaining display. The displays are connected together via a single Ethernet bus for high-speed communication. Each IAU is connected to a single display, as shown in Figure 1-1. This allows the units to share information, enabling true system integration.. This section discusses normal and reversionary G1000 display operation, as well as the various AHRS modes and G1000 System Annunciations. NORMAL DISPLAY OPERATION In normal operating mode, the PFD presents graphical flight instrumentation (attitude, heading, airspeed, altitude, vertical speed), replacing the traditional flight instrument cluster (see the Flight Instruments Section for more information). The MFD normally displays a full-color moving map with navigation information (see the Flight Management Section), while the left portion of the MFD is dedicated to the Engine Indication System (EIS; see the EIS Section). Both displays offer control for COM and NAV frequency selection. Figure 1-9 Normal Mode REVERSIONARY DISPLAY OPERATION NOTE: The G1000 System alerts the pilot when backup paths are utilized by the LRUs. Refer to Appendix A for further information regarding system-specific alerts. 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. 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 15 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 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. Figure 1-10 Reversionary Mode (Failed PFD) 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 and CNS 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 AHRS OPERATION NOTE: Refer to Appendix A for specific AHRS alert information. NOTE: Aggressive maneuvering while AHRS is not operating normally may degrade AHRS accuracy. The Attitude and Heading Reference System (AHRS) performs attitude, heading, and vertical acceleration calculations for the G1000 System, utilizing GPS, magnetometer, and air data in addition to information from its internal sensors. Attitude and heading information are updated on the PFD while the AHRS receives appropriate combinations of information from the external sensor inputs. Loss of GPS, magnetometer, or air data inputs is communicated to the pilot by message advisory alerts. Any failure of the internal AHRS inertial sensors results in loss of attitude and heading information (indicated by red ‘X’ flags over the corresponding flight instruments). 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 16 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 1-12 AHRS Operation GPS INPUT FAILURE NOTE: In-flight initialization of AHRS, when operating without any valid source of GPS data and at true air speed values greater than approximately 200 knots, is not guaranteed. Under these rare conditions, it is possible for in-flight AHRS initialization to take an indefinite amount of time which would result in an extended period of time where valid AHRS outputs are unavailable. Two GPS inputs are provided to the AHRS. If GPS information from one of the inputs fails, the AHRS uses the remaining GPS input and an alert message is issued to inform the pilot. If both GPS inputs fail, the AHRS can continue to provide attitude and heading information to the PFD as long as magnetometer and airspeed data are available and valid. MAGNETOMETER FAILURE If the magnetometer input fails, the AHRS continues to output valid attitude information; however, the heading output on the PFD is flagged as invalid with a red ‘X’. AIR DATA INPUT FAILURE Failure of the air data input has no affect on the AHRS output while AHRS is receiving valid GPS information. Invalid/unavailable airspeed data in addition to GPS failure results in loss of all attitude and heading information. 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 17 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX G1000 SYSTEM ANNUNCIATIONS NOTE: For a detailed description of all annunciations and alerts, refer to Appendix A. Refer to the Pilot’s Operating Handbook (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 1-13 displays all possible flags and responsible LRUs). Upon G1000 power-up, certain windows remain invalid as equipment begins to initialize. All windows should be operational within one minute of power-up. If any window remains flagged, the G1000 system should be serviced by a Garmin- authorized repair facility. Figure 1-13 G1000 System Failure Annunciations GDC 74A Air Data Computer GTX 33 Transponder OR GIA 63/W Integrated Avionics Units GDC 74A Air Data Computer GEA 71 Engine Airframe Unit OR GIA 63/W Integrated Avionics Unit GIA 63/W Integrated Avionics Units GRS 77 AHRS OR GMU 44 Magnetometer GIA 63/W Integrated Avionics Units GIA 63/W Integrated Avionics Units Database Mismatch in PFD and MFD SOFTKEY FUNCTION The softkeys are located along the bottoms of the displays. The softkeys shown depend on the softkey level or page being displayed. The bezel keys below the softkeys can be used to select the appropriate softkey. When a softkey is selected, its color changes to black text on gray background and remains this way until it is turned off, at which time it reverts to white text on black background. Softkey Names (Displayed) Figure 1-14 Softkeys (Second-Level PFD Configuration) Bezel-Mounted Softkeys (Press) Softkey On 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 18 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX PFD SOFTKEYS The CDI, IDENT, TMR/REF, NRST, and ALERTS softkeys undergo a momentary change to black text on gray background and automatically switch back to white text on black background when selected. The PFD softkeys provide control over flight management functions, including GPS, NAV, terrain, traffic, and lightning (optional). Each softkey sublevel has a BACK Softkey which can be selected to return to the previous level. The ALERTS Softkey is visible at all softkey levels (label changes if messages are issued). INSET Displays Inset Map in PFD lower left corner OFF Removes Inset Map DCLTR (3) Selects desired amount of map detail; cycles through declutter levels: DCLTR (No Declutter): All map features visible DCLTR-1: Declutters land data DCLTR-2: Declutters land and SUA data DCLTR-3: Removes everything except for the active flight plan WX LGND Displays icon and age on the Inset Map for the selected weather products (optional) TRAFFIC Cycles through traffic display options: TRFC-1: Traffic displayed on inset map TRFC-2: Traffic Map Page is displayed in the inset map window 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 NEXRAD or PRECIP Displays NEXRAD weather and coverage information on Inset Map (optional) Displays GFDS or FIS-B precipitation on Inset Map (optional) XM LTNG or DL LTNG Displays XM WX lightning information on Inset Map (optional) Displays GFDS Worldwide Weather lightning information on Inset Map (optional) METAR Displays METAR flags on airport symbols shown on the Inset Map (optional) PFD Displays second-level softkeys for additional PFD configurations SYN VIS Displays the softkeys for enabling or disabling Synthetic Vision features PATHWAY Displays rectangular boxes representing the horizontal and vertical flight path of the active flight plan SYN TERR Enables synthetic terrain depiction HRZN HDG Displays compass heading along the Zero-Pitch line APTSIGNS Displays position markers for airports within approximately 15 nm of the current aircraft position. Airport identifiers are displayed when the airport is within approximately 9 nm. DFLTS Resets PFD to default settings, including changing units to standard 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 19 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX WIND Displays softkeys to select wind data parameters OPTN 1 Wind direction arrows with headwind and crosswind components OPTN 2 Wind direction arrow and speed OPTN 3 Wind direction arrow with direction and speed OFF Information not displayed DME Displays the DME Information Window BRG1 Cycles the Bearing 1 Information Window through NAV1, GPS/ waypoint identifier and GPS-derived distance information, and ADF/frequency HSI FRMT Provides access to the HSI formatting softkeys 360 HSI Displays the HSI in a 360 degree view ARC HSI Displays the HSI as an arc BRG2 Cycles the Bearing 2 Information Window through NAV2 or GPS waypoint identifier and GPS-derived distance information, and ADF/frequency. ALT UNIT Displays softkeys for setting the altimeter and BARO settings to metric units METERS When enabled, displays altimeter in meters IN Press to display the BARO setting as inches of mercury HPA Press to display the BARO setting as hectopacals STD BARO Sets barometric pressure to 29.92 in Hg (1013 hPa if METRIC Softkey is 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 selection of the DME 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 Allows manual selection of ground mode in certain conditions VFR Automatically enters the VFR code (1200 in the U.S.A. only) CODE Displays transponder code selection softkeys 0-7 0 — 7 Use numbers to enter code IDENT Activates the Special Position Identification (SPI) pulse for 18 seconds, identifying the transponder return on the ATC screen BKSP Removes numbers entered, one at a time IDENT Activates the Special Position Identification (SPI) pulse for 18 seconds, identifying the transponder return on the ATC screen TMR/REF Displays Timer/References Window NRST Displays Nearest Airports Window ALERTS Displays Alerts Window 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 20 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Figure 1-15 Top Level PFD Softkeys Figure 1-16 INSET Softkeys Press the BACK or OFF Softkey to return to the top-level softkeys. ALERTS STRMSCP DME ALERTS TRFC-1 TRFC-2 WX LGND METAR (optional) or (optional) PRECIP (optional) or DL LTNG (optional) (optional) (optional) Figure 1-17 PFD Configuration Softkeys Press the BACK Softkey to return to the top-level softkeys BRG1 (NAV1) BRG1 (GPS) BRG1 (OFF) DME ALT UNIT METERS IN HPA DME ALERTS ALERTS ALERTS ALERTS HSI FRMT ALERTS ARC HSI 360 HSI BRG1 (ADF) BRG2 (NAV2) BRG2 (GPS) BRG2 (OFF) BRG2 (ADF) SYN VIS SYN TERR HRZN HDG PATHWAY APTSIGNS ALERTS 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 21 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Figure 1-18 XPDR (Transponder) Softkeys Press the BACK Softkey to return to the top-level softkeys. Press the BACK Softkey to return to the previous softkey level. ALERTS ALERTS DME ALERTS MFD SOFTKEYS ENGINE Pressing this softkey makes available the LEAN and SYSTEM Softkeys LEAN Pressing makes available the CYL SLCT and ASSIST Softkeys to facilitate engine leaning CYL SLCT The Cylinder Select Softkey cycles through selection of each cylinder indicated by changing the cylinder display to light blue ASSIST Pressing the ASSIST Softkey causes the first cylinder that peaks to become highlighted and information for that cylinder to be displayed BACK Returns to the previous level softkeys SYSTEM Press this softkey to make available the RST FUEL and GAL REM Softkeys RST FUEL Pressing the Rest Fuel Softkey resets fuel used and gallons remaining to zero GAL REM Press this softkey (Gallons Remaining) to display the quantity adjustment softkeys -10 GAL Pressing decreases the fuel remaining quantity in 10 gallon increments -1 GAL Pressing decreases the fuel remaining quantity in 1 gallon increments +1GAL Pressing increases the fuel remaining quantity in 1 gallon increments +10 GAL Pressing decreases the fuel remaining quantity in 10 gallon increments XX GAL Pressing this softkey sets the fuel remaining to the quantity at the filler neck tab where XX is an airframe specific quantity XX GAL Pressing this softkey sets the fuel remaining to the full tank quantity where XX as an airframe specific quantity 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 22 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX MAP Enables second-level Navigation Map softkeys TRAFFIC Displays traffic information on Navigation Map PROFILE Displays/removes Profile View on Navigation Map Page 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 dependant 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 Pressing this softkey displays/removes Stormscope lightning data on the Navigation Map. NEXRAD or PRECIP Displays NEXRAD weather and coverage information on the Navigation Map (optional) Displays GFDS or FIS-B precipitation on Navigation Map (optional) XM LTNG or DL LTNG Displays XM WX lightning information on the Navigation Map (optional) Displays GFDS Worldwide Weather lightning information on the Navigation Map (optional) METAR Displays METAR flags on airport symbols shown on the Navigation Map LEGEND Displays the legend for the selected weather products. Available only when NEXRAD, XM LTNG, METAR and/or PROFILE softkeys are selected. 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 Displays the appropriate chart CHKLIST Displays the Checklist Page 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 23 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX ENGINE Displays the engine checklist CHECK Pressing this softkey checks off a checklist item. If an item is already checked, an UNCHECK Softkey is displayed. EXIT Press to exit the checklist EMERGCY Displays the emergency checklist 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 24 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX BACK RST FUEL SYSTEM ENGINE LEAN ENGINE MAP DCLTR ENGINE LEAN BACK SYSTEM DCLTR-2 DCLTR-3 DCLTR-1 CHKLIST EXIT EMERGCY ENGINE CHECK The CHECK Softkey changes to UNCHECK when the checklist item is already checked. (optional) BACK SYSTEM LEAN ENGINE Press the ENGINE or BACK Softkey to return to the default Engine Page level. ASSIST CYL SLCT GAL REM SHW CHRT (optional) (Default softkey is dependant on the selection made in the map setup options) BACK -10 GAL SYSTEM ENGINE LEAN -1 GAL XX GAL +10 GAL +1 GAL XX GAL Press the ENGINE Softkey to the default Engine Page level. X = airframe specific values Press the BACK Softkey to return to the previous softkey level. (All except Diesel) ENGINE BACK FUEL BACK RST FUEL GAL REM ENGINE ENGINE BACK -10 GAL -1 GAL 44 GAL +10 GAL +1 GAL Press the ENGINE Softkey to return to the default Engine Page level. Press the BACK Softkey to return to the previous softkey level. ENGINE BACK Press the ENGINE or BACK Softkey to return to the default Engine Page level. ENGINE SYSTEM FUEL SYSTEM FUEL SYSTEM Press the ENGINE or BACK Softkey to return to the default Engine Page level. FUEL SYSTEM (Diesel only) AIRWY ON AIRWY LO AIRWAYS AIRWY HI Press the BACK softkey to return to the top-level softkeys. BACK METAR XM LTNG NEXRAD STRMSCP AIRWAYS TERRAIN PROFILE TOPO TRAFFIC LEGEND (optional) or PRECIP (optional) or DL LTNG (optional) (optional) (optional) Figure 1-19 MFD Softkeys 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 25 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX GPS RECEIVER OPERATION Each GIA 63/63W Integrated Avionics Unit (IAU) contains a GPS receiver. 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 in SBAS (Satellite Based Augmentation System) capable systems, one of the GPS receivers has not yet acquired an SBAS signal. While the aircraft is on the ground, the SBAS signal may be blocked by obstructions causing one GPS receiver to have difficulty acquiring a good signal. Also, while airborne, turning the aircraft may result in one of the GPS receivers temporarily losing the SBAS signal. If the sensor annunciation persists, check for a system failure message in the Messages Window on the PFD. If no failure message exists, check the GPS Status Page and compare the information for GPS1 and GPS2. Discrepancies may indicate a problem. Viewing GPS receiver status information 1) Use the large FMS Knob on the MFD to select the Auxiliary Page Group (see Section 1.7 for information on navigating MFD page groups). 2) Use the small FMS Knob to select GPS Status Page. Selecting the GPS receiver for which data may be reviewed 1) Use the FMS Knob to select the AUX - GPS Status Page. 2) To change the selected GPS receiver: a) Press the desired GPS Softkey. Or: a) Press the MENU Key. b) Use the FMS Knob to highlight the receiver which is not selected and press the ENT Key. 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 26 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Figure 1-20 GPS Status Page (RAIM or SBAS Selected) Satellite Signal Strength Bars Satellite Constellation Diagram Satellite Signal Information Status RAIM Availability Prediction GPS Receiver Status RAIM Softkey Selected SBAS Softkey Selected Enabled SBAS Options The GPS Status Page provides the following information: • Satellite constellation diagram Satellites currently in view are shown at their respective positions on a sky view diagram. The sky view is always in a north-up orientation, with the outer circle representing the horizon, the inner circle representing 45° above the horizon, and the center point showing the position directly overhead. Each satellite is represented by an oval containing the Pseudo-random noise (PRN) number (i.e., satellite identification number). Satellites whose signals are currently being used are represented by solid ovals. • Satellite signal information status The accuracy of the aircraft’s GPS fix is calculated using Estimated Position Uncertainty (EPU), Dilution of Precision (DOP), and horizontal and vertical figures of merit (HFOM and VFOM). EPU is the radius of a circle centered on an estimated horizontal position in which actual position has 95% probability of laying. EPU is a statistical error indication and not an actual error measurement. DOP measures satellite geometry quality (i.e., number of satellites received and where they are relative to each other) on a range from 0.0 to 9.9, with lower numbers denoting better accuracy. HFOM and VFOM, measures of horizontal and vertical position uncertainty, are the current 95% confidence horizontal and vertical accuracy values reported by the GPS receiver. The current calculated GPS position, time, altitude, ground speed, and track for the aircraft are displayed below the satellite signal accuracy measurements. • GPS receiver status 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 27 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX The GPS solution type (ACQUIRING, 2D NAV, 2D DIFF NAV, 3D NAV, 3D DIFF NAV) for the active GPS receiver (GPS1 or GPS2) is shown in the upper right of the GPS Status Page. When the receiver is in the process of acquiring enough satellite signals for navigation, the receiver uses satellite orbital data (collected continuously from the satellites) and last known position to determine the satellites that should be in view. ACQUIRING is indicated as the solution until a sufficient number of satellites have been acquired for computing a solution. When the receiver is in the process of acquiring a 3D navigational GPS solution, 3D NAV is indicated as the solution until the 3D differential fix has finished acquisition. SBAS (Satellite-Based Augmentation System) indicates INACTIVE. When acquisition is complete, the solution status indicates 3D DIFF NAV and SBAS indicates ACTIVE. • RAIM (Receiver Autonomous Integrity Monitoring) Prediction (RAIM Softkey is selected) In most cases performing a RAIM prediction is not necessary. However, in some cases, the selected approach may be outside the SBAS coverage area and it may be necessary to perform a RAIM prediction for the intended approach. Receiver Autonomous Integrity Monitoring (RAIM) is a GPS receiver function that performs a consistency check on all tracked satellites. RAIM ensures that the available satellite geometry allows the receiver to calculate a position within a specified RAIM protection limit (2.0 nautical miles for oceanic and enroute, 1.0 nm for terminal, and 0.3 nm for non-precision approaches). During oceanic, enroute, and terminal phases of flight, RAIM is available nearly 100% of the time. The RAIM prediction function also indicates whether RAIM is available at a specified date and time. RAIM computations predict satellite coverage within ±15 min of the specified arrival date and time. Because of the tighter protection limit on approaches, there may be times when RAIM is not available. The G1000 automatically monitors RAIM and warns with an alert message when it is not available. If RAIM is not predicted to be available for the final approach course, the approach does not become active, as indicated by the messages “Approach is not active” and “RAIM not available from FAF to MAP”. If RAIM is not available when crossing the FAF, the missed approach procedure must be flown. Predicting RAIM availability 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) Use the large FMS Knob to scroll to the Most Recent Waypoints List. b) Use the small FMS Knob to highlight the desired waypoint in the list and press the ENT Key. The G1000 automatically fills in the identifier, facility, and city fields with the information for the selected waypoint. c) Press the ENT Key to accept the waypoint entry. 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 28 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Or: a) To use the present position, press the MENU Key. b) With ‘Set WPT to Present Position’ highlighted, press the ENT Key. c) Press the ENT Key to accept the waypoint entry. 6) 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 • SBAS Selection (SBAS Softkey is pressed)(WAAS, EGNOS, or MSAS capable systems only) In certain situations, such as when the aircraft is outside or on the fringe of the WAAS, EGNOS, or MSAS coverage area, it may be desirable to disable the reception of the applicable SBAS signal (although it is not recommended). When disabled, the SBAS field in the GPS Status box indicates DISABLED. There may be a small delay for the GPS Status box to be updated upon WAAS, EGNOS, and MSAS enabling/disabling. Disabling WAAS, EGNOS or MSAS 1) Select the GPS Status Page. 2) If necessary, press the SBAS Softkey. 3) Press the FMS Knob, and turn the large FMS Knob to hightlight the desired SBAS system. 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). 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 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 1-21 Page Menu Examples No Options with NRST Window Displayed on the PFD Options with FPL Window Displayed 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 30 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX MFD PAGE GROUPS NOTE: Refer to the Flight Management, Hazard Avoidance, and Additional Features sections for details on specific pages. Information on the MFD is presented on pages which are grouped according to function. The page group and active page title are displayed in the upper center of the screen, below the Navigation Status Box. In the bottom right corner of the screen, the page group tabs are displayed along the bottom Available pages in the group are displayed in a list above the page groups. The current page group and current page within the group are shown in cyan. For some of these pages (Airport/Procedures/Weather Information, XM WX Satellite Weather, Procedure Loading), the active title of the page changes while the page name in the list remains the same. Figure 1-22 Page Title and Page Groups Page Group Active Page Title MFD Page Groups Pages in Current Group Selecting a page using the FMS Knob: 1) Turn either FMS Knob one click to display the pop-up page selection window. 2) Turn the large FMS Knob until the desired page group is selected. For example, the MAP page group is selected in Figure 1-22. 3) 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. 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 31 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Figure 1-23 Map Pages Map Pages (MAP) Navigation Map Traffic Map Stormscope ® Weather Data Link (service optional) - XM WX Satellite Weather - FIS-B Weather - GFDS Worldwide Weather Terrain Proximity/Terrain-SVS/ TAWS-B Figure 1-24 Waypoint Pages Airport Information Pages Waypoint Pages (WPT) Airport Information pages - Airport Information (INFO-1 Softkey) - Airport Directory (INFO-2 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 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 32 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Auxiliary Pages (AUX) Trip Planning Utility GPS Status System Setup SiriusXM Satellite pages - XM Information (INFO Softkey) - XM Radio (RADIO Softkey) System Status Video (Optional) Figure 1-25 Auxiliary Pages SiriusXM Satellite Pages Figure 1-26 Flight Plan Pages Flight Plan Pages (FPL) Active Flight Plan - Wide View, Narrow View (VIEW Softkey) Flight Plan Catalog or Stored Flight Plan (NEW Softkey) The Flight Plan Pages may also be accessed using the FPL Key. Main pages within this group are selected by turning the small FMS Knob. The Checklist Page may be accessed from the page group tab or the CHKLIST Softkey. See the Additional Features section for a discussion on checklists. 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 33 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Figure 1-27 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 bezel key. In some instances, softkeys may be used to access the Procedure Pages. The Flight Plan Pages are accessed using the FPL Key on the MFD. Main pages within this group are selected by turning the small FMS Knob. The Procedure pages may be accessed at any time on the MFD by pressing the PROC Key. A menu is initialized, and when a departure, approach, or arrival is selected, the appropriate Procedure Loading Page is opened. Turning the FMS Knob does not scroll through the Procedure pages (note the single page icon in the lower right corner). Figure 1-28 Procedure Pages Procedure Pages (PROC) Departure Loading Arrival Loading Approach Loading For some of these pages (Airport Information pages, SiriusXM Satellite pages, Procedure pages), the title of the page may change while the page icon remains the same. 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 34 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX MFD SYSTEM PAGES In the Auxiliary (AUX) Page Group, there are two system pages: System Setup and System Status. The System Setup Page allows management of various system parameters, while the System Status Page displays the status of all G1000 system LRUs. SYSTEM SETUP PAGE The System Setup Page allows management of the following system parameters: • Time display format (local or UTC ) • Displayed measurement units • Baro transition alert (see Flight Instruments Section) • Arrival Alerts • Airspace alerts • Audio alert voice • Flight director format (only the single que option is available in the Cessna Nav III) • Page Navigation • MFD Data Bar (Navigation Status Box) fields • GPS Course Deviation Indicator (CDI) range • COM transceiver channel spacing • Displayed nearest airports Selecting the System Setup Page: 1) Turn the large FMS Knob to select the AUX Page group. 2) Turn the small FMS Knob to display the System Setup Page. Figure 1-29 System Setup Page 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 35 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Date/time The Date/Time Box on the System Setup Page displays the current date and time and allows the pilot to set the time format (local 12-hr, local 24-hr, or UTC) and offset. The time offset is used to define current local time. UTC (also called GMT or Zulu) date and time are calculated directly from the GPS satellites signals and cannot be changed. When using a local time format, designate the offset by adding or subtracting the desired number of hours. Set the system time format: 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 time format field in the Date/Time Box. 3) Turn the small FMS Knob to select the desired system time format (local 12hr, local 24hr, UTC) and press the ENT Key. Set the current time offset: 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 time offset field in the Date/Time Box. 3) Turn the FMS Knobs to enter the time offset and press the ENT Key. DisPlay Units The Display Units Box on the System Setup Page allows configuration of the measurement units used for the following displayed data: • Nav angle (magnetic, true) When set to ‘MAGNETIC’, magnetic variation is figured into the displayed value. When ‘TRUE’ is selected, no magnetic variation is calculated and a ‘T’ is displayed next to the value. Affects the BRG field in the PFD Navigation Status Box. Affects Current Heading, Selected Heading, and Selected Course boxes on the PFD. Affects the BRG, DTK, TKE, TRK, and XTK fields in the MFD Navigation Status Box. • Distance and speed (metric, nautical) Affects the DIS field in the PFD Navigation Status Box and the range setting of the Inset Map. Affects all distance and speed displays on the MFD with the exception of the displayed wind speed displayed on the Navigation Map Page. Wind speed is affected on the Trip Planning Page. • Altitude and vertical speed (feet, meters) Affects all altitude and elevation displays on the MFD, with the exception of VNAV altitudes on the Active Flight Plan Page. • Temperature (Celsius, Fahrenheit) Affects all temperature displays on the PFD. Affects the temperature display on the Trip Planning Page. Does not affect the Engine Indicating System display. 190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 36 SYSTEM OVERVIEW SYSTEM