G1000 ® Integrated Avionics System Pilot’s Guide ® G1000 Pilot’s Guide Garmin International, Inc. 1200 East 151st Street Olathe, KS 66062, U.S.A. p:913.397.8200 f:913.397.8282 Garmin AT, Inc. 2345 Turner Road SE Salem, OR 97302, U.S.A. p:503.391.3411 f:503.364.2138 Garmin Corporation No. 68, Jangshu 2nd Road Shijr, Taipei County, Taiwan p:886/02.2642.9199 f:886/02.2642.9099 www.garmin.com Quest KODIAK® 100 Garmin (Europe) Ltd. Liberty House, Hounsdown Business Park Southampton, Hampshire SO40 9LR U.
SYSTEM OVERVIEW FLIGHT INSTRUMENTS ENGINE INDICATION SYSTEM AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AUTOMATIC FLIGHT CONTROL SYSTEM ADDITIONAL FEATURES APPENDICES INDEX
Copyright © 2006-2012, 2014 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0552.22 or later for the Quest KODIAK® 100. Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions. Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A. Tel: 913/397.8200 Fax: 913/397.8282 Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.
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.
WARNINGS, CAUTIONS, AND NOTES WARNING: For safety reasons, G1000 operational procedures must be learned on the ground. WARNING: The Garmin system, as installed in this aircraft, has a very high degree of functional integrity. However, the pilot must recognize that providing monitoring and/or self-test capability for all conceivable system failures is not practical. WARNING: The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance.
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.
WARNINGS, CAUTIONS, AND NOTES NOTE: The FAA has asked Garmin to remind pilots who fly with Garmin database-dependent avionics of the following: • It is the pilot’s responsibility to remain familiar with all FAA regulatory and advisory guidance and information related to the use of databases in the National Airspace System. • Garmin equipment will only recognize and use databases that are obtained from Garmin or Jeppesen.
REVISION INFORMATION Record of Revision Part Number 190-00590-00 190-00590-00 190-00590-00 190-00590-01 Revision A B C A Date 3/21/07 4/3/07 6/22/07 10/13/08 Page Range All All All All 190-00590-02 A 7/31/09 All 190-00590-03 A 5/7/10 All 190-00590-04 A 11/5/10 All 190-00590-05 A 1/6/12 All 190-00590-06 A 3/12/14 All 190-00590-07 Rev. A Description Initial Release Added Print Specification Reference to Cover Sheet Revised AMPS Engine Gauge Added GDU 8.
REVISION INFORMATION vi 190-00590-06 B 5/1/14 All 190-00590-07 A 8/29/14 All Changed KODIAK™ to KODIAK® Incorporated Quest comments on the Garmin AFCS - Removed automatic activation of Low Bank Mode - GA switch does not uncouple autopilot - Roll Trim does not uncouple autopilot Corrections to USP and ESP Added Database notes Updated System Software Number for GDU 14.
TABLE OF CONTENTS 1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.8 SECTION 1 SYSTEM OVERVIEW System Description.................................................. 1 Line Replaceable Units............................................ 2 G1000 Controls......................................................... 6 PFD/MFD Controls......................................................... 6 Controls Associated With the MFD.................................. 8 Audio Panel Controls............................................
TABLE OF CONTENTS Simultaneous COM Operation..................................... 129 Clearance Recorder and Player.................................... 130 Entertainment Inputs................................................. 131 4.6 Audio Panels Preflight Procedure....................... 132 4.7 Abnormal Operation............................................ 134 Stuck Microphone...................................................... 134 COM Tuning Failure...................................................
TABLE OF CONTENTS 6.5 Profile View Terrain.............................................. 365 Profile View Display................................................... 366 6.6 Traffic Information Service (TIS)......................... 369 Displaying Traffic Data............................................... 370 Traffic Map Page........................................................ 372 TIS Alerts.................................................................. 373 System Status............................
TABLE OF CONTENTS Comparator Annunciations......................................... 542 G1000 System Annunciations..................................... 544 G1000 System Message Advisories.............................. 546 AFCS Alerts............................................................... 560 TAWS-B ALERTS......................................................... 561 TAWS-B System Status Annunciations.......................... 562 Flight Plan Import/Export Messages............................
SYSTEM OVERVIEW SYSTEM OVERVIEW SECTION 1 SYSTEM OVERVIEW 1.1 SYSTEM DESCRIPTION FLIGHT INSTRUMENTS This section is designed to provide an overview of the G1000 Integrated Flight Deck installed in the Quest KODIAK® 100. The G1000 is an integrated flight deck system that presents flight instrumentation, position, navigation, communication, and identification information to the pilot using flat-panel color displays.
SYSTEM OVERVIEW SYSTEM OVERVIEW 1.2 LINE REPLACEABLE UNITS EIS FLIGHT INSTRUMENTS • GDU 1040 (3) – The GDU 1040 is configured as two Primary Flight Displays (PFD) and one Multi Function Display (MFD). The displays communicate with each other through a High-Speed Data Bus (HSDB) Ethernet connection. Each display is also paired with an Ethernet connection to an IAU.
SYSTEM OVERVIEW SYSTEM OVERVIEW • GEA 71 (1) – The Engine Airframe Unit receives and processes signals from the engine and airframe sensors. This unit communicates with both IAUs using an RS-485 digital interface. FLIGHT INSTRUMENTS • GTX 33 (1) – The solid-state Transponder provides Modes A, C, and S capability and communicates with both IAUs through an RS-232 digital interface.
SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS • GWX 68 (1)(optional) – Provides airborne weather and ground mapped radar data to the MFD via HSDB connection. AUDIO PANEL & CNS EIS • GTS 800 (optional) – 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.
SYSTEM OVERVIEW SYSTEM OVERVIEW GMC 710 AFCS Control Unit (optional) PFD #1 GMA 1347 Audio Panel #1 GDU 1040 MFD GMA 1347 Audio Panel #2 GDU 1040 FLIGHT INSTRUMENTS GDU 1040 PFD #2 EIS GWX 68 GDL 69A Air Airborne Weather and Ground Mapped Radar Data (optional) Real-time Weather and Digital Audio Entertainment (optional) Weather Radar We Integrated Avionics Unit GDC 74A #2 Air Data Computer Air Data Computer OAT Airspeed Altitude Vertical Speed ed GRS 77 #1 G AHRS GRS 77 #2 AHRS Att
SYSTEM OVERVIEW SYSTEM OVERVIEW 1.3 G1000 CONTROLS FLIGHT INSTRUMENTS NOTE: The Audio Panel (GMA 1347) is described in the CNS & Audio Panel section. The G1000 system controls are located on the PFD and MFD bezels and the audio panel. The controls for the PFD and MFD are discussed within the following pages of this section.
SYSTEM OVERVIEW NAV VOL/ID Knob Turn to control NAV audio volume (shown in the NAV Frequency Box as a percentage) NAV Frequency Transfer Key 3 NAV Knob Heading Knob Press to toggle cyan tuning box between NAV1 and NAV2 Turn to manually select a heading Joystick Press to display a digital heading momentarily to the left of the HSI and synchronize the Selected Heading to the and current heading Turn to change map range CRS/BARO Knob Press to activate Map Pointer for map panning Turn large knob for altim
SYSTEM OVERVIEW SYSTEM OVERVIEW 15 ENT Key Validates/confirms menu selection or data entry 16 FMS Knob Press to turn the selection cursor ON/OFF. FLIGHT INSTRUMENTS (Flight Management Data Entry: With cursor ON, turn to enter data in the highlighted field (large knob moves cursor location; small knob selects character for highlighted cursor System Knob) location) EIS Scrolling: When a list of information is too long for the window/box, a scroll bar appears, indicating more items to view.
SYSTEM OVERVIEW SYSTEM OVERVIEW AUDIO PANEL CONTROLS 4 5 6 7 8 9 10 11 12 13 14 15 16 AUDIO PANEL & CNS cNS 3 EIS 2 FLIGHT INSTRUMENTS 1 17 20 21 22 23 HAZARD AVOIDANCE 19 FLIGHT MANAGEMENT 18 24 Figure 1-4 Audio Panel Controls (GMA 1347) AFCS NOTE: When a key is selected, a triangular annunciator above the key is illuminated. COM1 – When selected, audio from the #1 COM receiver can be heard. 3 COM2 MIC – Selects the #2 transmitter for transmitting.
6 COM3 – Not used in KODIAK 100 aircraft. 7 COM 1/2 – Not used in KODIAK 100 aircraft. 8 TEL – Not used in KODIAK 100 aircraft. 9 PA – Selects the passenger address system. The selected COM transmitter is deselected when the PA Key is pressed. 10 SPKR – Selects and deselects the cabin speaker. COM and NAV receiver audio can be heard on the speaker. 11 MKR/MUTE – Selects marker beacon receiver audio. Mutes the currently received marker beacon receiver audio.
SYSTEM OVERVIEW SYSTEM OVERVIEW 1.4 SECURE DIGITAL (SD) CARDS FLIGHT INSTRUMENTS NOTE: Ensure the G1000 System is powered off before inserting an SD card. NOTE: Refer to Appendix B for instructions on updating the aviation databases. EIS The PFD and MFD data card slots use Secure Digital (SD) cards and are located on the upper right side of the display bezels. Each display bezel is equipped with two SD card slots.
SYSTEM OVERVIEW SYSTEM OVERVIEW 1.5 SYSTEM POWER-UP FLIGHT INSTRUMENTS 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. EIS The G1000 System is integrated with the aircraft electrical system and receives power directly from electrical busses.
SYSTEM OVERVIEW SYSTEM OVERVIEW 1.6 SYSTEM OPERATION FLIGHT INSTRUMENTS 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 the on-side display. This section discusses normal and reversionary G1000 display operation, as well as the various AHRS modes and G1000 System Annunciations.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW SYSTEM OVERVIEW Primary Flight Display #1 Multi-Function Display Primary Flight Display #2 EIS Figure 1-9 G1000 Reversionary Mode (Failed PFD #1) AUDIO PANEL & CNS Pressing the DISPLAY BACKUP Button activates/deactivates reversionary mode for both the on-side PFD and the MFD.
SYSTEM OVERVIEW SYSTEM OVERVIEW NO EIS YES GPS Data Available and Reliable? FLIGHT INSTRUMENTS The AHRS (GRS 77) corrects for shifts and variations in the Earth’s magnetic field by applying the Magnetic Field Variation Database. The Magnetic Field Variation Database is derived from the International Geomagnetic Reference Field (IGRF). The IGRF is a mathematical model that describes the Earth’s main magnetic field and its annual rate of change. The database is updated approximately every 5 years.
SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS If both the heading and track are unavailable, the HSI displays a yellow ‘HDG’ annunciation with a red X over the heading readout box. The system also removes directional numbers and letters from the HSI.
SYSTEM OVERVIEW SYSTEM OVERVIEW SOFTKEY FUNCTION FLIGHT INSTRUMENTS 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.
AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW SYSTEM OVERVIEW SENSOR ADC1 ADC2 AHRS1 AHRS2 PFD SYN VIS Displays softkeys for selecting the #1 and #2 AHRS and Air Data Computers Selects the #1 Air Data Computer Selects the #2 Air Data Computer Selects the #1 AHRS Selects the #2 AHRS Displays second-level softkeys for additional PFD configurations Displays the softkeys for enabling or disabling Synthetic Vision features PATHWAY SYN TERR Displays rectangular boxes representing the h
SYSTEM OVERVIEW SYSTEM OVERVIEW GND VFR CODE 0—7 BKSP IDENT AUDIO PANEL & CNS cNS TMR/REF NRST ALERTS EIS IDENT FLIGHT INSTRUMENTS Manually selects Ground Mode, the transponder does not allow Mode A and Mode C replies, but it does permit acquisition squitter and replies to discretely addressed Mode S interrogations Automatically enters the VFR code (1200 in the U.S.A.
SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS ALERTS ADC1 ADC2 AHRS1 BACK AHRS2 ALERTS Select the BACK Softkey to return to the top level softkeys.
SYSTEM OVERVIEW SYSTEM OVERVIEW ALERTS FLIGHT INSTRUMENTS ALERTS Select the BACK Softkey to return to the top-level softkeys. EIS ALERTS Select the BACK Softkey to return to the previous level softkeys. AUDIO PANEL & CNS cNS Figure 1-20 XPDR Softkeys MFD SOFTKEYS APPENDICES Displays/removes XM lightning information on Navigation Map (optional) Displays/removes METAR information on Navigation Map (optional) Garmin G1000 Pilot’s Guide for the Quest KODIAK® 100 INDEX 190-00590-07 Rev.
SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS LEGEND WX RADAR BACK DCLTR (3) Displays/removes METAR legend on Navigation Map Page (optional) Displays/removes airborne weather radar information on Navigation Map Page Returns to top-level softkeys 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 pl
SYSTEM OVERVIEW SYSTEM OVERVIEW GPS RECEIVER OPERATION Each GIA 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. FLIGHT INSTRUMENTS EIS GPS1 provides information to the pilot-side PFD, and GPS2 provides data to the copilot-side PFD. Internal system checking is performed to ensure both GPS receivers are providing accurate data to the PFDs.
SYSTEM OVERVIEW SYSTEM OVERVIEW Satellite Constellation Diagram GPS Receiver Status RAIM Availability Prediction FLIGHT INSTRUMENTS Satellite Signal Information Status AUDIO PANEL & CNS EIS SBAS Selected FLIGHT MANAGEMENT Satellite Signal Strength Bars GPS Selection Softkeys RAIM Softkey Selected SBAS Softkey Selected Figure 1-22 GPS Status Page (RAIM or SBAS Selected) HAZARD AVOIDANCE The GPS Status Page provides the following information: • Satellite constellation diagram Satellites curren
SYSTEM OVERVIEW SYSTEM OVERVIEW • GPS receiver status FLIGHT INSTRUMENTS 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.
SYSTEM OVERVIEW SYSTEM OVERVIEW a) Turn the small FMS Knob counter-clockwise to display a list of flight plan waypoints (the FPL list is populated only when navigating a flight plan). b) Turn the small FMS Knob clockwise to display the NRST, RECENT, or AIRWAY waypoints, if required. FLIGHT INSTRUMENTS c) Turn the large FMS Knob clockwise to select the desired waypoint. The G1000 automatically fills in the identifier, facility, and city fields with the information for the selected waypoint.
SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS • SBAS Selection (SBAS Softkey is selected) In certain situations, such as when the aircraft is outside or on the fringe of the SBAS coverage area, it may be desireable to disable SBAS (although it is not recommended). When disabled, the SBAS field in the GPS Status box indicates DISABLED. Disabling SBAS 1) Select the GPS Status Page. 2) If necessary, press the SBAS Softkey. 3) Press the FMS Knob to activate the cursor.
SYSTEM OVERVIEW SYSTEM OVERVIEW 1.7 ACCESSING G1000 FUNCTIONALITY FLIGHT INSTRUMENTS MENUS EIS The G1000 has a dedicated MENU Key that when pressed displays a context-sensitive list of options. This options list allows the user to access additional features or make settings changes which specifically relate to the currently displayed window/page. There is no all-encompassing menu. Some menus provide access to additional submenus that are used to view, edit, select, and review options.
SYSTEM OVERVIEW SYSTEM OVERVIEW MFD PAGE GROUPS NOTE: Refer to other supporting sections in this Pilot’s Guide for details on specific pages. EIS Page Group MFD FLIGHT INSTRUMENTS Information on the MFD is presented on pages 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, a page group window is displayed by turning either FMS Knob.
SYSTEM OVERVIEW SYSTEM OVERVIEW • Map Page Group (MAP) Navigation Map Traffic Map FLIGHT INSTRUMENTS Weather Radar (optional) Stormscope Map Weather Data Link (optional) AUDIO PANEL & CNS EIS TAWS Figure 1-25 Map Pages FLIGHT MANAGEMENT • Waypoint Page Group (WPT) Airport/Procedures/Weather Information Pages - Airport Information (INFO-1 Softkey) HAZARD AVOIDANCE - Airport Directory Information (INFO-2 Softkey) - Departure Information (DP Softkey) AFCS - Arrival Information (STAR Softkey) -
SYSTEM OVERVIEW SYSTEM OVERVIEW • Auxiliary Page Group (AUX) Weight Planning Trip Planning FLIGHT INSTRUMENTS Utility GPS Status System Setup 1 System Setup 2 (optional) EIS XM Satellite screens (optional) - XM Information (INFO Softkey) AUDIO PANEL & CNS cNS XM Pages - XM Radio (RADIO Softkey) System Setup Pages Maintenance Logs Video FLIGHT MANAGEMENT System Status Figure 1-27 Auxiliary Pages HAZARD AVOIDANCE Maintenance data is continuously recorded by the Central Maintenance Computer (CM
SYSTEM OVERVIEW SYSTEM OVERVIEW • Flight Plan Page Group (FPL) Active Flight Plan FLIGHT INSTRUMENTS Flight Plan Catalog EIS - Stored Flight Plan (NEW Softkey) AUDIO PANEL & CNS Figure 1-29 Flight Plan Pages FLIGHT MANAGEMENT There are also several pages (Airport/Procedures/Weather Information and XM pages) selected first from within a main page group with the FMS Knob, then with the appropriate softkey at the bottom of the page.
SYSTEM OVERVIEW SYSTEM OVERVIEW AUX - SYSTEM SETUP 1 PAGE The System Setup 1 Page allows management of the pilot profiles and the following system parameters: • Displayed measurement units • Barometric Transition Alert (see the Flight Instruments Section) AUDIO PANEL & CNS cNS • Audio alert voice • COM transceiver channel spacing (see the Audio Panel and CNS Section) • Displayed nearest airports (see the Flight Management Section) • CDI/Baro Synchronization) (see the Flight Instruments Section) EIS •
SYSTEM OVERVIEW SYSTEM OVERVIEW Or: 1) Use the FMS Knob to select the AUX - System Setup 1 Page. FLIGHT INSTRUMENTS 2) Press the MENU Key. 3) Highlight ‘Restore Defaults’ and press the ENT Key. Pilot Profiles AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS System settings may be saved under a pilot profile. When the system is powered on, the last selected pilot profile is shown on the MFD Power-up Splash Screen.
SYSTEM OVERVIEW SYSTEM OVERVIEW 6) In the next field, use the small FMS Knob to select the desired settings upon which to base the new profile. Profiles can be created based on Garmin factory defaults, default profile settings (initially based on Garmin factory defaults unless edited by the pilot), or current system settings. FLIGHT INSTRUMENTS 7) Press the ENT Key.
SYSTEM OVERVIEW SYSTEM OVERVIEW If an SD card is inserted into the top slot of the MFD, pilot profiles may imported from the SD card into the system, or exported from the system to the SD card. FLIGHT INSTRUMENTS Because system settings may vary from one airframe to another, always verify system settings from an imported profile are consistent with the desired settings. Importing a profile from an SD card: 1) Insert an SD card containing the pilot profile(s) into the top card slot on the MFD.
SYSTEM OVERVIEW SYSTEM OVERVIEW Exporting a profile to an SD card: 1) Insert the SD card for storing the Pilot Profile into the top card slot on the MFD. 2) Turn the FMS Knob to select the AUX - System Setup 1 Page. FLIGHT INSTRUMENTS 3) If necessary, activate the desired pilot profile to export. Only the currently active Pilot Profile can be exported. 4) Select the EXPORT Softkey. The system displays the Pilot Profile Exporting window. Or: a) Press the MENU Key.
SYSTEM OVERVIEW SYSTEM OVERVIEW Date/Time FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS The G1000 obtains the current Universal Coordinated Time (UTC) date and time directly from the GPS satellite signals (shown on the AUX - GPS Status Page). System time (displayed in the lower right corner of the PFD) can be displayed in three formats: local 12-hr, local 24-hr, or UTC. Local time is set by adding/ subtracting an offset (hours:minutes) to/from UTC.
SYSTEM OVERVIEW SYSTEM OVERVIEW Display Units Category Navigation Angle Engine Indication System (EIS) N/A N/A All positions N/A AFCS Position** Altimeter Vertical Speed Indicator VNV altitudes (Active Flight Plan) Engine Indication System (EIS) HAZARD AVOIDANCE Weight** All temperatures on PFD Total Air Temperature (Trip Planning Page) Fuel parameters (Trip Planning Page) FLIGHT MANAGEMENT Fuel and Fuel Flow ADDITIONAL FEATURES Celsius* Fahrenheit Pounds* Gallons Pounds* Kilograms HDDD°MM.
SYSTEM OVERVIEW SYSTEM OVERVIEW 4) Turn the small FMS Knob to select from a list of measurement units. 5) Press the ENT Key when the desired unit is highlighted. FLIGHT INSTRUMENTS 6) To cancel the process without changing the units, press the CLR Key. Arrival Alerts HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS The Arrival Alert Box on the System Setup 1 Page allows the Alerts Window arrival alerts to be turned ON/OFF, and the alert trigger distance (up to 99.
SYSTEM OVERVIEW SYSTEM OVERVIEW Audio Alerts The Audio Alert Box on the System Setup 1 Page allows the audio alert voice to be set to male or female. FLIGHT INSTRUMENTS Changing the audio alert voice: 1) Use the FMS Knob to select the System Setup 1 Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight the voice in the Audio Alert Box. 4) Turn the small FMS Knob to display and highlight the desired voice. EIS 5) Press the ENT Key.
AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW SYSTEM OVERVIEW Figure 1-37 Page Navigation Settings (AUX - System Setup 1 Page) FLIGHT MANAGEMENT AUX - SYSTEM STATUS PAGE APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE The System Status Page displays the status and software version numbers for all detected system LRUs. Pertinent information on all system databases is also displayed. Active LRUs are indicated by green check marks and failed LRUs are indicated by red ‘X’s.
SYSTEM OVERVIEW SYSTEM OVERVIEW The LRU and ARFRM Softkeys on the System Status Page select the applicable list (LRU INFO or AIRFRAME window) through which the FMS Knob can be used to scroll information within the selected window. FLIGHT INSTRUMENTS Selecting the MFD1 DB Softkey (label background changes to grey indicting the softkey is selected) places the cursor in the database window. Use the FMS Knob to scroll through database information for the MFD.
SYSTEM OVERVIEW SYSTEM OVERVIEW Setting the generic timer (PFD): 1) Press the TMR/REF Softkey. FLIGHT INSTRUMENTS 2) Turn the large FMS Knob to select the timer field (hh/mm/ss). 3) Use the FMS Knob to enter the desired time and press the ENT Key. 4) With the UP/DN field highlighted, turn the small FMS Knob to select the timer counting direction (UP/DN) and press the ENT Key. 6) With ‘START?’ highlighted, press the ENT Key to start the timer. The field changes to ‘STOP?’.
SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS cNS Figure 1-41 Timers (MFD AUX - Utility Page) FLIGHT MANAGEMENT The flight timer can be set to count up from zero starting at system power-up or from the time that the aircraft lifts off; the timer can also be reset to zero at any time. Setting the flight timer starting criterion 1) Use the FMS Knob to select the AUX - Utility Page. 2) Press the FMS Knob momentarily to activate the flashing cursor.
SYSTEM OVERVIEW SYSTEM OVERVIEW Resetting the departure time 1) Use the FMS Knob to select the AUX - Utility Page. FLIGHT INSTRUMENTS 2) Press the MENU Key. 3) Use the FMS Knob to highlight ‘Reset Departure Time’ and press the ENT Key. Trip Statistics EIS The odometer and trip odometer record the total mileage traveled from the last reset; these odometers can be reset independently. Resetting the trip odometer also resets the average trip groundspeed.
SYSTEM OVERVIEW SYSTEM OVERVIEW Entering a scheduler message: 1) Select the AUX - Utility Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. FLIGHT INSTRUMENTS 3) Turn the large FMS Knob to highlight the first empty scheduler message naming field. 4) Use the FMS Knob to enter the message text to be displayed in the Alerts Window and press the ENT Key. 5) Press the ENT Key again or use the large FMS Knob to move the cursor to the field next to ‘Type’.
EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW SYSTEM OVERVIEW AUDIO PANEL & CNS Figure 1-43 PFD Alerts Window GPS POSITION HAZARD AVOIDANCE FLIGHT MANAGEMENT The Timer/References Window on the PFD shows the current GPS position at the bottom of the window using the selected display format (HHDDºMM.MM’ or HDDDºMM’SS.S”). AFCS GPS Position Figure 1-44 GPS Position (Timer/References Window) Viewing the GPS Position in the Timer/References Window: ADDITIONAL FEATURES 1) Press the TMR/REF Softkey.
SYSTEM OVERVIEW SYSTEM OVERVIEW 1.8 DISPLAY BACKLIGHTING FLIGHT INSTRUMENTS The PFD and MFD display backlighting, the PFD and MFD bezel, and the Audio Panel keys can be adjusted manually in one of two ways: • Using the individual dimmer bus control for the desired display, or • Using the PFD Setup Menu and the following procedures. In normal operating mode, backlighting can only be adjusted from the PFDs. In reversionary mode, adjustments can be made from any remaining displays.
INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW SYSTEM OVERVIEW Blank Page 50 Garmin G1000 Pilot’s Guide for the Quest KODIAK® 100 190-00590-07 Rev.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW SECTION 2 FLIGHT INSTRUMENTS FLIGHT INSTRUMENTS WARNING: If the airspeed, attitude, altitude, or heading indications become unusable, refer to the backup instruments. Increased situational awareness is provided by replacing the traditional instruments on the panel with two easyto-scan Primary Flight Displays (PFDs) that feature large horizons, airspeed, attitude, altitude, vertical speed, and course deviation information.
SYSTEM OVERVIEW FLIGHT INSTRUMENTS FLIGHT INSTRUMENTS 21 20 19 1 18 17 16 2 EIS 15 14 AUDIO PANEL & CNS 3 13 4 12 5 11 6 FLIGHT MANAGEMENT 10 9 7 APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE 8 1 NAV Frequency Box 12 Turn Rate Indicator 2 Airspeed Indicator 13 Barometric Altimeter Setting 3 Ground Speed 14 Vertical Speed Indicator (VSI) 4 True Airspeed 15 Reference Altitude Bug 5 Current Heading 16 Altimeter 6 Horizontal Situation Indicator (HSI) 17 Ref
FLIGHT INSTRUMENTS SYSTEM OVERVIEW 15 16 FLIGHT INSTRUMENTS 14 1 13 12 11 EIS 10 2 9 AUDIO PANEL & CNS 8 3 7 4 FLIGHT MANAGEMENT 5 6 9 Selected Course 2 Selected Heading 10 3 Wind Data Box Required Vertical Speed Indicator 11 Vertical Deviation Indication 4 Inset Map 12 Reversionary Sensor Window 5 Bearing Information Windows 13 Comparator Window 6 14 VNV Target Altitude 7 Minimum Descent Altitude/ Decision Height Flight Plan Window 15 Terrain Annunciation 8 Annunciati
SYSTEM OVERVIEW FLIGHT INSTRUMENTS 2.1 FLIGHT INSTRUMENTS FLIGHT INSTRUMENTS AIRSPEED INDICATOR NOTE: Refer to the Aircraft Flight Manual (AFM) for airspeed criteria and Vspeed values. AUDIO PANEL & CNS EIS The Airspeed Indicator displays airspeed on a moving tape rolling number gauge. The true airspeed is displayed in knots below the Airspeed Indicator. The ground speed is displayed in knots to the left of the true airspeed.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW Vspeeds (Vref and Vclimb) can be changed and their bugs enabled (on) or disabled (off) from the Timer/References Window. When enabled, the Vspeed bugs are displayed to the right of the airspeed scale. All Vspeed values are reset and all Vspeed bugs are disabled during power up. FLIGHT INSTRUMENTS Changing Vspeeds and enabling/disabling Vspeed bugs: 1) Press the TMR/REF Softkey. 2) Turn the large FMS Knob to highlight the field of the desired Vspeed to be changed.
SYSTEM OVERVIEW FLIGHT INSTRUMENTS ATTITUDE INDICATOR FLIGHT INSTRUMENTS Attitude information is displayed over a virtual blue sky and brown ground with a white horizon line. The Attitude Indicator displays the pitch, roll, and slip/skid information.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW ALTIMETER FLIGHT INSTRUMENTS The Altimeter displays 600 feet of barometric altitude values at a time on a moving tape rolling number gauge. Numeric labels and major tick marks are shown at intervals of 100 feet. Minor tick marks are at intervals of 20 feet. The indicated altitude is displayed inside the black pointer. The Selected Altitude is displayed above the Altimeter in the box indicated by a selection bug symbol.
SYSTEM OVERVIEW FLIGHT INSTRUMENTS Altitudes can also be displayed in meters as an overlay (Figure 2-7). Note that the altitude tape does not change scale. FLIGHT INSTRUMENTS Displaying the metric altitude overlay: 1) Press the PFD Softkey to display the second-level softkeys. 2) Press the ALT UNIT Softkey. 3) Press the METERS Softkey to turn on metric altitude readouts. 4) Press the BACK Softkey to return to the top-level softkeys.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW If the barometric altimeter settings differ between PFDs by more than 0.02 in Hg, the readouts turn yellow. Once the settings are synchronized (BARO turned on), they remain synchronized until the setting is turned off. FLIGHT INSTRUMENTS Synchronizing the altimeter barometric pressure settings: 1) Select the AUX - System Setup Page using the FMS Knob. 2) Press the FMS Knob to activate the cursor.
SYSTEM OVERVIEW FLIGHT INSTRUMENTS FLIGHT INSTRUMENTS The Baro Transition Alert flashes the barometric pressure setting. The Baro Transition Alert serves as a reminder to the pilot to change the barometric pressure setting to standard when climbing through the barometric transition altitude, or to change the barometric pressure setting from standard to the local altimeter setting when descending through the barometric transition altitude.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW descent rate is greater than 100 fpm. If the rate of ascent/descent exceeds 2000 fpm, the pointer appears at the edge of the tape and the rate appears inside the pointer. FLIGHT INSTRUMENTS A magenta chevron is displayed on the VSI to indicate the Required Vertical Speed for reaching a VNV target altitude once the “TOD [Top of Descent] within 1 minute” alert has generated.
SYSTEM OVERVIEW FLIGHT INSTRUMENTS HORIZONTAL SITUATION INDICATOR (HSI) FLIGHT INSTRUMENTS The Horizontal Situation Indicator (HSI) displays a rotating compass card in a heading-up orientation. Letters indicate the cardinal points with numeric labels every 30˚. Major tick marks are at 10˚ intervals and minor tick marks are at 5˚ intervals.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW Course Pointer FLIGHT INSTRUMENTS The Arc HSI is a 140˚ expanded section of the compass rose. The Arc HSI contains a Course Pointer, combined To/From Indicator and a sliding deviation indicator, and a deviation scale. Upon station passage, the To/From Indicator flips and points to the tail of the aircraft, just like a conventional To/From flag.
SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS FLIGHT INSTRUMENTS Navigation angles (track, heading, course, bearing) are corrected to the computed magnetic variation (Mag Var) or referenced to true north (T), set on the AUX - System Setup Page. When an approach referenced to true north has been loaded into the flight plan, the system generates a message to change the navigation angle setting to True at the appropriate time.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW TURN RATE INDICATOR FLIGHT INSTRUMENTS The Turn Rate Indicator is located directly above the rotating compass card. Tick marks to the left and right of the lubber line denote half-standard and standard turn rates. A magenta Turn Rate Trend Vector shows the current turn rate. The end of the trend vector gives the heading predicted in 6 seconds, based on the present turn rate.
SYSTEM OVERVIEW FLIGHT INSTRUMENTS When a bearing pointer is displayed, the associated information window is also displayed.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW COURSE DEVIATION INDICATOR (CDI) NOTE: During a heading change of greater than 105˚ with respect to the course, the CDI on the Arc HSI FLIGHT INSTRUMENTS switches to the opposite side of the deviation scale and displays reverse sensing. The Course Deviation Indicator (CDI) moves left or right from the course pointer along a lateral deviation scale to display aircraft position relative to the course. If the course deviation data is not valid, the CDI is not displayed.
SYSTEM OVERVIEW Changing navigation sources: FLIGHT INSTRUMENTS FLIGHT INSTRUMENTS 2) Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2. This places the cyan tuning box over the NAV2 standby frequency. 1) Press the CDI Softkey to change from GPS to VOR1 or LOC1. This places the cyan tuning box over the NAV1 standby frequency in the upper left corner of the PFD. 3) Press the CDI Softkey a third time to return to GPS.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW If the same VOR/LOC navigation source is selected on both PFDs, the navigation source annunciation becomes yellow on both displays if not synchronized. Once the CDIs are synchronized (CDI Synchronization turned on), they remain synchronized until the selection is turned off. FLIGHT INSTRUMENTS Synchronizing the CDIs: 1) Select the AUX - System Setup Page using the FMS Knob. 2) Press the FMS Knob to activate the cursor.
SYSTEM OVERVIEW FLIGHT INSTRUMENTS GPS CDI SCALING FLIGHT INSTRUMENTS When GPS is the selected navigation source, the flight plan legs are sequenced automatically and annunciations appear on the HSI for the flight phase. Flight phase annunciations are normally shown in magenta, but when cautionary conditions exist the color changes to yellow. If the current leg in the flight plan is a heading leg, HDG LEG is annunciated in magenta beneath the aircraft symbol.
Enroute (Oceanic if >200 nm from nearest airport) Terminal Approach 0.3 nm 1.0 nm 1.0 nm 2.0 nm 0.3 nm 1.0 nm Terminal Refer to accompanying approach CDI scaling figures FLIGHT INSTRUMENTS Departure SYSTEM OVERVIEW CDI Full-scale Deflection FLIGHT INSTRUMENTS Missed Approach EIS AUDIO PANEL & CNS Figure 2-26 Automatic CDI Scaling • Once a departure procedure is activated, the CDI is scaled for departure (0.3 nm). • The system switches from departure to terminal CDI scaling (1.
2 nm FAF EIS CDI scale varies if VTF is activated 0.3 nm 1.0 nm 2 nm FAF Landing Threshold CDI scale varies if VTF is activated Figure 2-27 Typical LNAV and LNAV+V Approach CDI Scaling AUDIO PANEL & CNS angle based on database information course width angle set by system CDI Full-scale Deflection 0.3 nm 1.0 nm CDI scale is set to the smaller of 0.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW OBS MODE NOTE: VNV is inhibited while automatic waypoint sequencing has been suspended. FLIGHT INSTRUMENTS Enabling Omni-bearing Selector (OBS) Mode suspends the automatic sequencing of waypoints in a GPS flight plan (GPS must be the selected navigation source), but retains the current Active-to waypoint as the navigation reference even after passing the waypoint. OBS is annunciated to the lower right of the aircraft symbol when OBS Mode is selected.
SYSTEM OVERVIEW FLIGHT INSTRUMENTS AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS As the aircraft crosses the missed approach point (MAP), automatic approach waypoint sequencing is suspended. SUSP appears on the HSI at the lower right of the aircraft symbol. The OBS Softkey label changes to indicate the suspension is active as shown in Figure 2-30. Pressing the SUSP Softkey deactivates the suspension and resumes automatic sequencing of approach waypoints.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW 2.2 SUPPLEMENTAL FLIGHT DATA FLIGHT INSTRUMENTS NOTE: Pressing the DFLTS Softkey turns off metric Altimeter display, the Inset Map and wind data display. In addition to the flight instruments, the PFDs also display various supplemental information, including temperatures, wind data, and Vertical Navigation (VNV) indications.
SYSTEM OVERVIEW FLIGHT INSTRUMENTS WIND DATA Option 1 Option 2 Option 3 No Data FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Wind direction and speed in knots can be displayed relative to the aircraft in a window to the upper left of the HSI. When the window is selected for display, but wind information is invalid or unavailable, the window displays NO WIND DATA. Wind data can be displayed in three different ways.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW VERTICAL NAVIGATION (VNV) INDICATIONS FLIGHT INSTRUMENTS When a VNV flight plan has been activated, VNV indications (VNV Target Altitude, RVSI, VDI) appear on the PFD in conjunction with the “TOD within 1 minute” message and “Vertical track” voice alert. See the Flight Management and AFCS sections for details on VNV features. VNV indications are removed from the PFD according to the criteria listed in the table.
SYSTEM OVERVIEW FLIGHT INSTRUMENTS 2.3 PFD ANNUNCIATIONS AND ALERTING FUNCTIONS FLIGHT INSTRUMENTS The following annunciations and alerting functions are displayed on the PFD. Refer to Appendix A for more information on alerts and annunciations. SYSTEM ALERTING EIS Messages appear in the Alerts Window in the lower right corner of the PFD (Figure 2-34) when a warning, caution, advisory alert, or G1000 message advisory occurs.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW in white, and safe operating annunciations in green. New alerts are displayed at the top of the Annunciation Window, regardless of priority. Once acknowledged, they are sequenced based on priority. FLIGHT INSTRUMENTS Critical values generated by redundant sensors are monitored by comparators.
SYSTEM OVERVIEW FLIGHT INSTRUMENTS TRAFFIC ANNUNCIATION FLIGHT INSTRUMENTS Traffic is displayed symbolically on the PFD Inset Map, the MFD Navigation Map Page, and various other MFD page maps. Refer to the Hazard Avoidance Section and Appendix F for more details about the Traffic Information Service (TIS) and optional Traffic Advisory Systems (TAS).
FLIGHT INSTRUMENTS SYSTEM OVERVIEW TAWS ANNUNCIATIONS Terrain Awareness and Warning System (TAWS) annunciations appear on the PFD at the top left of the Altimeter. Refer to the Hazard Avoidance Section and Appendix A for information on TAWS alerts and annunciations.
SYSTEM OVERVIEW FLIGHT INSTRUMENTS LOW ALTITUDE ANNUNCIATION NOTE: A Low Altitude Annunciation is available only when SBAS is available. This annunciation is only FLIGHT INSTRUMENTS available when TAWS-B alerting has been inhibited. When the Final Approach Fix (FAF) is the active waypoint in a GPS SBAS approach using vertical guidance, a Low Altitude Annunciation may appear if the current aircraft altitude is at least 164 feet below the prescribed altitude at the FAF.
FLIGHT INSTRUMENTS Within 100 feet SYSTEM OVERVIEW Within 2500 feet Altitude Reached FLIGHT INSTRUMENTS Barometric Minimums Bug EIS Barometric Minimums Box Figure 2-40 Barometric MDA/DH Alerting Visual Annunciations AUDIO PANEL & CNS Alerting is inhibited while the aircraft is on the ground and until the aircraft reaches 150 feet above the MDA. If the aircraft proceeds to climb after having reached the MDA, once it reaches 50 feet above the MDA, alerting is disabled.
SYSTEM OVERVIEW FLIGHT INSTRUMENTS 2.4 ABNORMAL OPERATIONS FLIGHT INSTRUMENTS ABNORMAL GPS CONDITIONS The annunciations listed in Table 2-3 can appear on the HSI when abnormal GPS conditions occur (Figure 2-42). Refer to the Flight Management Section for more information on Dead Reckoning Mode.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW HEADING FAILURE MODES FLIGHT INSTRUMENTS If the system is unable to determine the aircraft heading, but GPS-based track information is available, the HSI displays the ground track instead of heading using HSI Track Mode. In this mode, a magenta ‘TRK’ annunciation and track readout appear on the HSI. In addition, a yellow ‘HDG’ annunciation with a red X appear above the ‘TRK’ annunciation to indicate the HSI is displaying track instead of heading.
SYSTEM OVERVIEW FLIGHT INSTRUMENTS • Traffic Annunciations • System Time • AFCS Annunciations • PFD Setup Menu • Minimum Descent Altitude/ Decision Height readout • Flight director Command Bars • Inset Map • Windows displayed in the lower right corner of the PFD: • Vertical Deviation, Glideslope, and Glidepath Indicators • Outside air temperature (OAT) – Timer/References • Altimeter Barometric Setting • Wind data – Nearest Airports • Selected Altitude • Selected Heading readout – Flight P
ENGINE INDICATION SYSTEM SYSTEM OVERVIEW SECTION 3 ENGINE INDICATION SYSTEM (EIS) NOTE: Refer to the Aircraft Flight Manual (AFM) for limitations. FLIGHT INSTRUMENTS The G1000 Engine Indication System (EIS) for the Quest KODIAK 100 displays critical engine, electrical, fuel, and other system parameters on the left side of the Multi Function Display (MFD) during normal operations.
SYSTEM OVERVIEW ENGINE INDICATION SYSTEM FLIGHT INSTRUMENTS The KODIAK 100’s EIS instrument types include vertical slider gauges, horizontal bar indicators, digital MAP DCLTR SHW CHRT CHKLIST readouts,ENGINE and slide bars. Green bands and readouts indicate normal ranges of operation; yellow and red bands and readouts indicate caution and warning, respectively. When unsafe operating conditions occur, readouts, pointers, and labels may change color and flash corresponding to the level of the condition.
ENGINE INDICATION SYSTEM • SYSTEM Accesses the System Display • FUEL Accesses the Fuel Display INC FUEL Increases totalizer-based fuel remaining in 10-lb increments RST FUEL Resets totalizer-based fuel remaining to the aircraft’s fuel capacity and resets the displayed fuel used to zero Returns to the previous level of softkeys • BACK AUDIO PANEL & CNS Decreases totalizer-based fuel remaining in 10-lb increments EIS DEC FUEL FLIGHT INSTRUMENTS Accesses the Engine Display and EIS softkeys SYST
SYSTEM OVERVIEW ENGINE INDICATION SYSTEM 3.1 ENGINE DISPLAY FLIGHT INSTRUMENTS The Engine Display is shown by default. If another EIS display is currently shown, the Engine Display may be selected by pressing the ENGINE or BACK Softkey. At the top of all three EIS displays, the Torque, Interstage Turbine Temperature (ITT), Propeller Speed, and Gas Generator Speed gauges are present. Trim and flap indications are also shown on all EIS displays.
ENGINE INDICATION SYSTEM 4 6 8 10 12 Engine Start Displays engine oil temperature in °C Displays DC current in amperes (amps) for the generator (G) and the alternator (A) Displays DC bus voltages for the main bus (M) and essential bus (E) Displays quantities of fuel in pounds (lb) in the left (L) and right (R) tanks Aileron and rudder trim are indicated with pointers along slide bars; the white bars indicate takeoff trim positions Elevator trim is indicated with a pointer along a slide bar; takeoff t
SYSTEM OVERVIEW ENGINE INDICATION SYSTEM 3.2 SYSTEM DISPLAY FLIGHT INSTRUMENTS The System Display is accessed by pressing the SYSTEM Softkey. The instruments presented here, in addition to the gauges and trim slide bars, are separated into three categories: Oil (pressure and temperature), Ice Protection (quantity), and Electrical (currents and voltages). Accessing the EIS System Display: 1) Press the ENGINE Softkey. 2) Press the SYSTEM Softkey.
ENGINE INDICATION SYSTEM 2 4 6 8 Displays gas generator speed as a percentage Displays engine oil pressure in pounds per square inch (psi) Displays engine oil temperature in °C Displays quantity of ice protection fluid in gallons (gal) Displays DC current in amperes (amps) for the generator (G) and the alternator (A) Displays DC bus voltages for the main bus and essential bus FLIGHT MANAGEMENT 9 Displays propeller speed in revolutions per minute (rpm) AUDIO PANEL & CNS 7 Displays Interstage Turbi
SYSTEM OVERVIEW ENGINE INDICATION SYSTEM 3.3 FUEL DISPLAY NOTE: Fuel calculations do not use the aircraft fuel quantity indicators and are calculated from the last time FLIGHT INSTRUMENTS the fuel was reset. The Fuel Display is accessed by pressing the FUEL Softkey.
ENGINE INDICATION SYSTEM SYSTEM OVERVIEW NOTE: Fuel indications can be configured to display pounds or gallons.
INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW ENGINE INDICATION SYSTEM Blank Page 96 Garmin G1000 Pilot’s Guide for the Quest KODIAK® 100 190-00590-07 Rev.
AUDIO PANEL AND CNS SYSTEM OVERVIEW SECTION 4 AUDIO PANEL AND CNS FLIGHT INSTRUMENTS 4.1 OVERVIEW The Communication/Navigation/Surveillance (CNS) system includes the Audio Panels, communication radios, navigation radios, and Mode S transponder. The System Overview Section provides a block diagram description of the Audio Panels and CNS system interconnection.
SYSTEM OVERVIEW AUDIO PANEL AND CNS MFD/PFD CONTROLS AND FREQUENCY DISPLAY 2 3 4 5 6 7 8 FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS 1 9 10 HAZARD AVOIDANCE 11 12 INDEX APPENDICES ADDITIONAL FEATURES AFCS Figure 4-1 MFD/PFD Controls, COM/NAV Frequency Tuning Boxes, and NRST Window (PFD Shown) 98 Garmin G1000 Pilot’s Guide for the Quest KODIAK® 100 190-00590-07 Rev.
AUDIO PANEL AND CNS NAV Frequency Box – Displays NAV standby and active frequency fields, volume, and station ID. The frequency of the NAV radio selected for navigation is displayed in green. 5 COM Frequency Box – Displays COM standby and active frequency fields and volume. The selected COM transceiver frequency is displayed in green. 6 COM Knob – Tunes the standby frequencies for the COM transceiver (large knob for MHz; small knob for kHz).
SYSTEM OVERVIEW AUDIO PANEL AND CNS 3 4 5 6 7 8 9 10 11 12 14 15 16 AUDIO PANEL & CNS 2 13 FLIGHT MANAGEMENT 1 18 19 20 21 HAZARD AVOIDANCE EIS FLIGHT INSTRUMENTS AUDIO PANEL CONTROLS 22 23 17 24 AFCS Figure 4-2 Audio Panel Controls INDEX APPENDICES ADDITIONAL FEATURES NOTE: When a key is selected, a triangular annunciator above the key is illuminated. 100 1 COM1 MIC – Selects the #1 transmitter for transmitting.
AUDIO PANEL AND CNS SPKR – Selects and deselects the cabin speaker. COM and NAV receiver audio can be heard on the speaker. 11 MKR/MUTE – Selects marker beacon receiver audio. Mutes the currently received marker beacon receiver audio. Unmutes automatically when new marker beacon audio is received. Also, stops play of recorded COM audio. 12 HI SENS – Press to increase marker beacon receiver sensitivity. Press again to return to low sensitivity. 13 DME – Not used in KODIAK 100 aircraft.
SYSTEM OVERVIEW AUDIO PANEL AND CNS 4.2 COM OPERATION FLIGHT INSTRUMENTS COM TRANSCEIVER SELECTION AND ACTIVATION NOTE: During PA Mode, the COM MIC Annunciator is extinguished and the COM active frequency color changes to white, indicating that neither COM transmitter is active. NOTE: When turning on the G1000 for use, the system remembers the last frequencies used and the active EIS COM transceiver state prior to shutdown.
AUDIO PANEL AND CNS SYSTEM OVERVIEW TRANSMIT/RECEIVE INDICATIONS FLIGHT INSTRUMENTS During COM transmission, a white TX appears by the active COM frequency replacing the Frequency Transfer Arrow. On the Audio Panel, when the active COM is transmitting, the active transceiver COM MIC Key Annunciator flashes approximately once per second. During COM signal reception, a white RX appears by the active COM frequency replacing the Frequency Transfer Arrow.
SYSTEM OVERVIEW AUDIO PANEL AND CNS SELECTING THE RADIO TO BE TUNED FLIGHT INSTRUMENTS Press the small COM Knob to transfer the frequency tuning box and Frequency Transfer Arrow between the upper and lower radio frequency fields. EIS Press the COM Knob to Switch the Tuning Box From One COM Radio to the Other AUDIO PANEL & CNS Figure 4-6 Switching COM Tuning Boxes QUICK-TUNING AND ACTIVATING 121.
AUDIO PANEL AND CNS SYSTEM OVERVIEW AUTO-TUNING THE COM FREQUENCY COM frequencies can be automatically tuned from the following: • Nearest Airports Window (PFD) • NRST – Nearest Frequencies Page (ARTCC, FSS, WX) FLIGHT INSTRUMENTS • WPT – Airport Information Page • NRST – Nearest Airspaces Page • NRST – Nearest Airports Page AUTO-TUNING FROM THE PFD EIS COM frequencies for the nearest airports can be automatically tuned from the Nearest Airports Window on the PFD.
SYSTEM OVERVIEW AUDIO PANEL AND CNS AUTO-TUNING FROM THE MFD FLIGHT INSTRUMENTS Frequencies can be automatically loaded into the COM Frequency Box from pages in the NRST or WPT page group by highlighting the frequency and pressing the ENT Key (Figures 4-9, 4-10, and 4-11). Auto-tuning a COM frequency from the WPT and NRST Pages: 1) From any page that the COM frequency can be auto-tuned, activate the cursor by pressing the FMS Knob or the appropriate softkey.
AUDIO PANEL AND CNS SYSTEM OVERVIEW On the WPT - Airport Information Page, the cursor can be placed on the frequency field by pressing the FMS Knob and scrolling through the list. The frequency is transferred to the COM Standby Field with the ENT Key.
SYSTEM OVERVIEW AUDIO PANEL AND CNS ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS COM frequencies can also be auto-tuned from the NRST – Nearest Airspaces, NRST – Nearest Frequencies, and NRST – Nearest Airports Pages on the MFD in a similar manner using the appropriate softkeys or MENU Key, the FMS Knob, and the ENT Key.
AUDIO PANEL AND CNS SYSTEM OVERVIEW FREQUENCY SPACING FLIGHT INSTRUMENTS The G1000 COM radios can tune either 25-kHz spacing (118.000 to 136.975 MHz) or 8.33-kHz spacing (118.000 to 136.990 MHz) for 760-channel or 3040-channel configuration. When 8.33-kHz channel spacing is selected, all of the 25-kHz channel spacing frequencies are also available in the complete 3040-channel list. COM channel spacing is set on the System Setup Page of the AUX Page Group. 25-kHz Channel Spacing EIS 8.
SYSTEM OVERVIEW AUDIO PANEL AND CNS AUTOMATIC SQUELCH FLIGHT INSTRUMENTS Automatic Squelch quiets unwanted static noise when no audio signal is received, while still providing good sensitivity to weak COM signals. To disable Automatic Squelch, press the VOL/SQ Knob. When Automatic Squelch is disabled, COM audio reception is always on. Continuous static noise is heard over the headsets and speaker, if selected. Pressing the VOL/SQ Knob again enables Automatic Squelch.
AUDIO PANEL AND CNS SYSTEM OVERVIEW 4.3 NAV OPERATION NAV RADIO SELECTION AND ACTIVATION FLIGHT INSTRUMENTS The NAV Frequency Box is composed of four fields: two standby fields and two active fields. The active frequencies are on the right side and the standby frequencies are on the left. EIS A NAV radio is selected for navigation by pressing the CDI Softkey located on the PFD. The active NAV frequency selected for navigation is displayed in green.
SYSTEM OVERVIEW AUDIO PANEL AND CNS EIS FLIGHT INSTRUMENTS NAV radios are selected for listening by pressing the corresponding keys on the Audio Panel. Pressing the NAV1 or NAV2 Key selects and deselects the navigation radio source. Selected audio can be heard over the headset and the speakers (if selected). All radios can be selected individually or simultaneously.
AUDIO PANEL AND CNS SYSTEM OVERVIEW SELECTING THE RADIO TO BE TUNED Press the small NAV Knob to transfer the frequency tuning box and Frequency Transfer Arrow between the upper and lower radio frequency fields. FLIGHT INSTRUMENTS Press the NAV Knob to Switch the Tuning Box From One NAV Radio to the Other EIS Figure 4-20 Switching NAV Tuning Boxes AUDIO PANEL & CNS VOR/LOC ID When the Morse code Identifier audio is on for a NAV radio, a white ID appears to the left of the active NAV frequency.
SYSTEM OVERVIEW AUTO-TUNING A NAV FREQUENCY FROM THE MFD FLIGHT INSTRUMENTS AUDIO PANEL AND CNS • WPT – VOR Information • NRST – Nearest Frequencies (FSS, WX) • NRST – Nearest Airports • NRST – Nearest Airspaces NAV frequencies can be selected and loaded from the following MFD pages: • WPT – Airport Information • NRST – Nearest VOR EIS The MFD provides auto-tuning of NAV frequencies from waypoint and nearest pages.
AUDIO PANEL AND CNS SYSTEM OVERVIEW Or: 1) When on the NRST pages, press the MENU Key to display the page menu. 2) Turn the large FMS Knob to scroll through the menu options. FLIGHT INSTRUMENTS 3) Press the ENT Key to place the cursor in the desired window. 4) Scroll through the frequency selections with the FMS Knob. 5) Press the ENT Key to load the NAV frequency into the standby field of the selected NAV radio.
SYSTEM OVERVIEW AUDIO PANEL AND CNS FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS In the example shown, the VOR list is selected with the VOR Softkey or from the page menu. The FMS Knob or ENT Key is used to scroll through the list. The cursor is placed on the frequency with the FREQ Softkey and loaded into the NAV Tuning Box with the ENT Key. HAZARD AVOIDANCE Press the ENT Key to Load the Frequency into the NAV Standby Field.
AUDIO PANEL AND CNS SYSTEM OVERVIEW While enroute, NAV frequencies can also be auto-tuned from the NRST – Nearest Airports, WPT – Airport Information, WPT – VOR Information, and NRST – Nearest Frequencies Pages on the MFD in a similar manner using the appropriate softkeys or MENU Key, the FMS Knob, and the ENT Key. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES 190-00590-07 Rev.
SYSTEM OVERVIEW AUDIO PANEL AND CNS AUTO-TUNING NAV FREQUENCIES ON APPROACH ACTIVATION FLIGHT INSTRUMENTS NOTE: The primary NAV frequency is auto-tuned upon loading a VOR or ILS/Localizer approach. NOTE: When an ILS/LOC approach has been activated in GPS Mode, the system switches to NAV Mode as the final approach course is intercepted (within 15 nm of the FAF). See the Flight Management Section for details. NAV frequencies are automatically loaded into the NAV Frequency Box on approach activation.
AUDIO PANEL AND CNS SYSTEM OVERVIEW MARKER BEACON RECEIVER NOTE: The marker beacon indicators operate independently of marker beacon audio and cannot be turned FLIGHT INSTRUMENTS off. The marker beacon receiver is used as part of the ILS. The marker beacon receiver is always on and detects any marker beacon signals within the reception range of the aircraft.
SYSTEM OVERVIEW AUDIO PANEL AND CNS 4.4 GTX 33 MODE S TRANSPONDER FLIGHT INSTRUMENTS The GTX 33 Mode S Transponder provides Mode A, Mode C, and Mode S interrogation and reply capabilities.
AUDIO PANEL AND CNS ALT GND VFR CODE IDENT BACK FLIGHT INSTRUMENTS ON IDENT SYSTEM OVERVIEW STBY XPDR ALERTS Pressing the BACK Softkey returns to the top-level softkeys. EIS 0 1 2 3 4 5 6 7 IDENT BKSP BACK ALERTS AUDIO PANEL & CNS Pressing the BACK Softkey returns to the mode selection softkeys.
SYSTEM OVERVIEW STANDBY MODE (MANUAL) FLIGHT INSTRUMENTS AUDIO PANEL AND CNS Standby Mode can be selected at any time by pressing the STBY Softkey. In Standby, the transponder does not reply to interrogations, but new codes can be entered. When Standby is selected, a white STBY indication and transponder code appear in the mode field of the Transponder Data Box. In all other modes, these fields appear in green. NOTE: In Standby Mode, the IDENT function is inoperative.
AUDIO PANEL AND CNS SYSTEM OVERVIEW ALTITUDE MODE (AUTOMATIC OR MANUAL) Altitude Mode is automatically selected when the aircraft becomes airborne. Altitude Mode may also be selected manually by pressing the ALT Softkey. FLIGHT INSTRUMENTS If Altitude Mode is selected, a green ALT indication and transponder code appear in the mode field of the Transponder Data Box, and all transponder replies requesting altitude information are provided with pressure altitude information.
SYSTEM OVERVIEW AUDIO PANEL AND CNS ENTERING A TRANSPONDER CODE Entering a transponder code with softkeys: FLIGHT INSTRUMENTS 1) Press the XPDR Softkey to display the Transponder Mode Selection Softkeys. 2) Press the CODE Softkey to display the Transponder Code Selection Softkeys, for digit entry. EIS 3) Press the digit softkeys to enter the code in the code field.
AUDIO PANEL AND CNS SYSTEM OVERVIEW VFR CODE FLIGHT INSTRUMENTS The VFR code can be entered either manually or by pressing the XPDR Softkey, then the VFR Softkey. When the VFR Softkey is pressed, the pre-programmed VFR code is automatically displayed in the code field of the Transponder Data Box. Pressing the VFR Softkey again restores the previous identification code. The pre-programmed VFR Code is set at the factory to 1200.
SYSTEM OVERVIEW AUDIO PANEL AND CNS 4.5 ADDITIONAL AUDIO PANEL FUNCTIONS FLIGHT INSTRUMENTS POWER-UP The Audio Panel performs a self-test during power-up. During the self-test all Audio Panel annunciator lights illuminate for approximately two seconds. Once the self-test is completed, most of the settings are restored to those in use before the unit was last turned off. MONO/STEREO HEADSETS EIS Stereo headsets are recommended for use in this aircraft.
AUDIO PANEL AND CNS SYSTEM OVERVIEW INTERCOM The two Audio Panels include a ten-position intercom system (ICS) for the pilot, copilot, and up to eight passengers. The intercom provides pilot and copilot isolation from the passengers and aircraft radios. FLIGHT INSTRUMENTS Pressing an ICS key on either Audio Panel selects and deselects the same key on both Audio Panels. Either the pilot or copilot may select or deselect the intercom.
SYSTEM OVERVIEW AUDIO PANEL AND CNS INTERCOM VOLUME AND SQUELCH NOTE: The pilot side Audio Panel adjusts the passenger volume and squelch on the pilot’s side of the FLIGHT INSTRUMENTS aircraft. The copilot side Audio Panel adjusts the passenger volume and squelch on the copilot’s side of the aircraft. EIS The PILOT/PASS Knob on each Audio Panel controls volume or manual squelch adjustment for the pilot and passengers on each side of the aircraft.
AUDIO PANEL AND CNS SYSTEM OVERVIEW PASSENGER ADDRESS (PA) SYSTEM FLIGHT INSTRUMENTS A passenger address system is available for delivering voice messages over the cabin speaker. When the PA Key is selected on either Audio Panel, the COM MIC Annunciator on that side is extinguished, and the active COM frequency on the associated PFD changes to white, indicating that there is no COM selected. A Push-toTalk (PTT) must be pressed to deliver PA announcements.
SYSTEM OVERVIEW AUDIO PANEL AND CNS CLEARANCE RECORDER AND PLAYER NOTE: Pressing the play key on the pilot’s Audio Panel plays recorded audio to the pilot. Pressing the play FLIGHT INSTRUMENTS key on the copilot’s Audio Panel plays recorded audio to the copilot. The Audio Panel contains a digital clearance recorder that records up to 2.5 minutes of the selected COM radio signal. Recorded COM audio is stored in separate memory blocks. Once 2.
AUDIO PANEL AND CNS SYSTEM OVERVIEW ENTERTAINMENT INPUTS XM RADIO ENTERTAINMENT FLIGHT INSTRUMENTS XM Radio audio from the Data Link Receiver may be heard by the pilot and passengers simultaneously (optional: requires subscription to XM Radio Service). Refer to the Additional Features Section for more details on the Data Link Receiver. ENTERTAINMENT AUDIO MUTING EIS Entertainment audio muting occurs when aircraft radio or marker beacon activity is heard.
SYSTEM OVERVIEW AUDIO PANEL AND CNS 4.6 AUDIO PANELS PREFLIGHT PROCEDURE FLIGHT INSTRUMENTS NOTE: If the pilot and/or copilot are using headsets that have a high/low switch or volume control knob, verify that the switch is in the high position and the volume control on the headsets is at maximum volume setting. On single‑pilot flights, verify that all other headsets are not connected to avoid excess noise in the audio system.
AUDIO PANEL AND CNS SYSTEM OVERVIEW Independent radio volume adjustments made using the MFD/PFD controls affect only the audio output for each radio selected for adjustment. Radio volume adjustment affects both crew positions equally for each radio that is adjusted. FLIGHT INSTRUMENTS Setting the Audio Panel during preflight: 1) Verify that the PILOT and COPLT Annunciators are extinguished. 2) Verify manual squelch is set to full open. 3) Turn the PILOT/PASS Knobs clockwise two full turns.
SYSTEM OVERVIEW AUDIO PANEL AND CNS 4.7 ABNORMAL OPERATION FLIGHT INSTRUMENTS Abnormal operation of the G1000 includes equipment failures of the G1000 components and failure of associated equipment, including switches and external devices. STUCK MICROPHONE If the push-to-talk (PTT) Key becomes stuck, the COM transmitter stops transmitting after 35 seconds of continuous operation. An alert appears on the PFD to advise the crew of a stuck microphone.
AUDIO PANEL AND CNS SYSTEM OVERVIEW PFD FAILURE, DUAL SYSTEM FLIGHT INSTRUMENTS If PFD1 fails, COM1 and NAV1 display a red X on both remaining displays. NAV1 is unavailable. COM1 automatically tunes 121.500 MHz, but the frequency is not shown. The COM1 emergency frequency is available to both the copilot and pilot.
SYSTEM OVERVIEW AUDIO PANEL AND CNS AUDIO PANEL FAIL-SAFE OPERATION FLIGHT INSTRUMENTS If there is a failure of both Audio Panels, a fail-safe circuit connects the pilot’s headset and microphone directly to the COM1 transceiver and the copilot’s headset directly to the COM2 transceiver. Audio is not available on the speaker. If there is a failure of one Audio Panel, that side only has access to their respective on-side fail-safe COM.
FLIGHT MANAGEMENT SYSTEM OVERVIEW SECTION 5 FLIGHT MANAGEMENT FLIGHT INSTRUMENTS 5.1 INTRODUCTION The G1000 is an integrated flight, engine, communication, navigation and surveillance system. This section of the Pilot’s Guide explains flight management using the G1000. EIS The most prominent parts of the G1000 are the three full color displays: two Primary Flight Displays (PFD) and one Multi Function Display (MFD).
SYSTEM OVERVIEW FLIGHT MANAGEMENT FLIGHT INSTRUMENTS Navigation Status Box Current Track Indicator Navigation Mode Inset Map AUDIO PANEL & CNS EIS Location of: - Direct To Window - Flight Plan Window - Procedures Window - Nearest Airports Window - Timer/References Window Figure 5-1 GPS Navigation Information on the PFD FLIGHT MANAGEMENT Navigation Status Box Map Orientation Navigation Page Title Navigation Map HAZARD AVOIDANCE - Aviation Data - Geographic Data - Topographic Data - Hazard Data Ai
FLIGHT MANAGEMENT SYSTEM OVERVIEW • Active flight plan leg (e.g., ‘D-> KICT’ or ‘KIXD -> KCOS’) or flight plan annunciations (e.g., ‘Turn right to 021˚ in 8 seconds’) FLIGHT INSTRUMENTS • Distance (DIS) and Bearing (BRG) to the next waypoint or flight plan annunciations (e.g.
SYSTEM OVERVIEW FLIGHT MANAGEMENT 5.2 USING MAP DISPLAYS FLIGHT INSTRUMENTS Map displays are used extensively in the G1000 to provide situational awareness in flight. Most G1000 maps can display the following information: AUDIO PANEL & CNS EIS • Airports, NAVAIDs, airspaces, airways, land data • Aircraft icon (representing present position) (highways, cities, lakes, rivers, borders, etc.
FLIGHT MANAGEMENT SYSTEM OVERVIEW • Desired track up (DTK UP) aligns the top of the map display to the desired course. • Heading up (HDG UP) aligns the top of the map display to the current aircraft heading. FLIGHT INSTRUMENTS NOTE: When panning or reviewing active flight plan legs in a non-North Up orientation, the map does not show the map orientation nor the wind direction and speed. NOTE: Map orientation can only be changed on the Navigation Map Page.
SYSTEM OVERVIEW FLIGHT MANAGEMENT The map can be configured to switch automatically to a north up orientation when the map range reaches a minimum range. FLIGHT INSTRUMENTS Enabling/disabling Auto North Up and selecting the minimum switching range: 1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Menu is displayed. 3) Select the ‘Map’ group. 4) Press the ENT Key.
FLIGHT MANAGEMENT SYSTEM OVERVIEW FLIGHT INSTRUMENTS If a terrain caution or warning occurs, all navigation maps automatically adjust to the smallest map range clearly showing the potential impact points If a new traffic advisory alert occurs, any map page capable of displaying traffic advisory alerts automatically adjusts to the smallest map range clearly showing the traffic advisory. When terrain or traffic alerts clear, the map returns to the previous auto zoom range based on the active waypoint.
SYSTEM OVERVIEW FLIGHT MANAGEMENT Configuring automatic zoom: 1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option. FLIGHT INSTRUMENTS 2) Press the ENT Key. The Map Setup Menu is displayed. 3) Select the ‘Map’ group. 4) Press the ENT Key. 5) Highlight the ‘AUTO ZOOM’ field. 6) Select ‘Off’, ‘MFD Only’, ‘PFD Only’, or ‘ALL On’. EIS 7) Press the ENT Key to accept the selected option. The flashing cursor highlights the ‘MAX LOOK FWD’ field.
FLIGHT MANAGEMENT SYSTEM OVERVIEW Map Pointer Information FLIGHT INSTRUMENTS Map Pointer EIS AUDIO PANEL & CNS Figure 5-8 Navigation Map - Map Pointer Activated FLIGHT MANAGEMENT NOTE: The map is normally centered on the aircraft’s position. If the map has been panned and there has HAZARD AVOIDANCE been no pointer movement for about 60 seconds, the map reverts back to centered on the aircraft position and the flashing pointer is removed.
SYSTEM OVERVIEW FLIGHT MANAGEMENT FLIGHT INSTRUMENTS When the Map Pointer crosses an airspace boundary, the boundary is highlighted and airspace information is shown at the top of the display. The information includes the name and class of airspace, the ceiling in feet above Mean Sea Level (MSL), and the floor in feet MSL.
FLIGHT MANAGEMENT SYSTEM OVERVIEW NAVAID Information FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS GO BACK Softkey Figure 5-11 Navigation Map - Information Window - NAVAID FLIGHT MANAGEMENT Viewing airspace information for a special-use or controlled airspace: 1) Place the Map Pointer on an open area within the boundaries of an airspace. HAZARD AVOIDANCE 2) Press the ENT Key to display an options menu. 3) ‘Review Airspaces’ should already be highlighted, if not select it.
SYSTEM OVERVIEW FLIGHT MANAGEMENT MEASURING BEARING AND DISTANCE FLIGHT INSTRUMENTS Distance and bearing from the aircraft’s present position to any point on the viewable navigation map may be calculated using the ‘Measure Bearing and Distance’ selection from Navigation Map page menu. The bearing and distance tool displays a dashed Measurement Line and a Measure Pointer to aid in graphically identifying points with which to measure.
FLIGHT MANAGEMENT SYSTEM OVERVIEW TOPOGRAPHY FLIGHT INSTRUMENTS All navigation maps can display various shades of topography colors representing land elevation, similar to aviation sectional charts. Topographic data can be displayed or removed as described in the following procedures.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW FLIGHT MANAGEMENT TOPO DATA Range AUDIO PANEL & CNS EIS TOPO DATA On/Off FLIGHT MANAGEMENT Figure 5-15 Navigation Map Setup Menu - TOPO DATA Setup The topographic data range is the maximum map range on which topographic data is displayed. NOTE: Since the PFD Inset Map is much smaller than the MFD navigation maps, items are removed on the HAZARD AVOIDANCE PFD Inset Map two range levels smaller than the range selected in the Map Setup pages (e.g.
FLIGHT MANAGEMENT SYSTEM OVERVIEW Maximum Displayed Elevation Minimum Displayed Elevation FLIGHT INSTRUMENTS Aircraft Altitude (MSL) Range of Displayed Elevations EIS Ground Elevation at Map Pointer Location (only visible when Map Pointer is displayed) AUDIO PANEL & CNS Figure 5-16 Navigation Map - TOPO SCALE FLIGHT MANAGEMENT Displaying/removing the topographic scale (TOPO SCALE): 1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option.
SYSTEM OVERVIEW FLIGHT MANAGEMENT MAP SYMBOLS FLIGHT INSTRUMENTS This section discusses the types of land and aviation symbols that can be displayed. Each listed type of symbol can be turned on or off, and the maximum range to display each symbol can be set. The decluttering of the symbols from the map using the DCLTR Softkey is also discussed.
FLIGHT MANAGEMENT SYSTEM OVERVIEW AVIATION SYMBOLS The following items are configured on the aviation menu: Aviation Symbols Symbol Default Maximum Range (nm) Range (nm) 2000 500 300 100 20 100 30 Non-directional Beacon (NDB WAYPOINT) 15 30 VOR (VOR WAYPOINT) 150 300 Class B Airspace/TMA (CLASS B/TMA) 200 500 Class C Airspace/TCA (CLASS C/TCA) 200 500 Class D Airspace (CLASS D) 150 300 Restricted Area (RESTRICTED) 200 500 Military Operations Area [MOA(MILITARY)] 200 500 Other/Air D
SYSTEM OVERVIEW FLIGHT MANAGEMENT SYMBOL SETUP FLIGHT INSTRUMENTS All pages with maps can display land symbols (roads, lakes, borders, etc). Land symbols can be removed totally (turned off). Displaying/removing all land symbols: 1) Press the MENU Key with the Navigation Map Page displayed. The Page Menu is displayed and the cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Group Menu is displayed and the cursor flashes on the ‘Map’ option.
FLIGHT MANAGEMENT SYSTEM OVERVIEW 7) Press the ENT Key to accept the selected size. 8) Select the desired range. 9) Press the ENT Key to accept the selected range. FLIGHT INSTRUMENTS 10) Press the FMS Knob to return to the Navigation Map Page.
SYSTEM OVERVIEW FLIGHT MANAGEMENT MAP DECLUTTER FLIGHT INSTRUMENTS The declutter feature allows the pilot to progressively step through four levels of removing map information. The declutter level is displayed in the DCLTR Softkey and next to the Declutter Menu Option. EIS Declutter Level Navigation Map Page Menu DCLTR Softkey Figure 5-21 Navigation Map - Declutter Level Indications AUDIO PANEL & CNS Decluttering the map: Press the DCLTR Softkey with the Navigation Map Page displayed.
FLIGHT MANAGEMENT SYSTEM OVERVIEW Table 5-3 lists the items that are decluttered at each map detail level. The ‘X’ represents map items decluttered for each level of detail.
SYSTEM OVERVIEW FLIGHT MANAGEMENT AIRWAYS FLIGHT INSTRUMENTS This airways discussion is based upon the North American airway structure. The airway structure in places other than North America vary by location, etc. and are not discussed in this book. Low Altitude Airways (or Victor Airways) primarily serve smaller piston-engine, propeller-driven airplanes on shorter routes and at lower altitudes.
FLIGHT MANAGEMENT SYSTEM OVERVIEW 3) Select the softkey again to display Low Altitude Airways only (AIRWY LO). 4) Select the softkey again to display High Altitude Airways only (AIRWY HI). 5) Select the softkey again to remove High Altitude Airways. No airways are displayed (AIRWAYS). FLIGHT INSTRUMENTS Or: 1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Menu is displayed.
SYSTEM OVERVIEW FLIGHT MANAGEMENT TRACK VECTOR FLIGHT INSTRUMENTS The Navigation Map can display a track vector that is useful in minimizing track angle error. The track vector is a solid cyan line segment extended to a predicted location. The track vector look-ahead time is selectable (30 sec, 60 sec (default), 2 min, 5 min, 10 min, 20 min) and determines the length of the track vector. The track vector shows up to 90 degrees of a turn for the 30 and 60 second time settings.
FLIGHT MANAGEMENT SYSTEM OVERVIEW WIND VECTOR Wind Direction FLIGHT INSTRUMENTS The map displays a wind vector arrow in the upper right-hand portion of the screen. Wind vector information is displayed as a white arrow pointing in the direction in which the wind is moving for wind speeds greater than or equal to 1 kt. Wind Speed Figure 5-26 Navigation Map - Wind Vector EIS NOTE: The wind vector is not displayed until the aircraft is moving. It is not displayed on the Waypoint Information pages.
SYSTEM OVERVIEW FLIGHT MANAGEMENT NAV RANGE RING FLIGHT INSTRUMENTS The Nav Range Ring shows the direction of travel (ground track) on a rotating compass card. The range is determined by the map range. The range is 1/4 of the map range (e.g., 37.5 nm on a 150 nm map).
FLIGHT MANAGEMENT SYSTEM OVERVIEW FUEL RANGE RING Time to Reserve Fuel FLIGHT INSTRUMENTS The map can display a fuel range ring which shows the remaining flight distance. A dashed green circle indicates the selected range to reserve fuel. A solid green circle indicates the total endurance range. If only reserve fuel remains, the range is indicated by a solid yellow circle.
SYSTEM OVERVIEW FLIGHT MANAGEMENT FIELD OF VIEW (SVS) FLIGHT INSTRUMENTS The map can display the boundaries of the PFD Synthetic Vision System (SVS) lateral field of view. The field of view is shown as two dashed lines forming a V shape in front of the aircraft symbol on the map. This is only available if SVS is installed on the aircraft.
FLIGHT MANAGEMENT SYSTEM OVERVIEW SELECTED ALTITUDE INTERCEPT ARC The map can display the location along the current track where the aircraft will intercept the selected altitude. The location will be shown as a cyan arc when the aircraft is actuallly climbing or descending.
SYSTEM OVERVIEW FLIGHT MANAGEMENT 5.3 WAYPOINTS FLIGHT INSTRUMENTS Waypoints are predetermined geographical positions (internal database) or pilot-entered positions, and are used for all phases of flight planning and navigation. Communication and navigation frequencies can be tuned “automatically” from various Waypoint Information (WPT) pages, Nearest (NRST) pages, and the Nearest Airports Window (on PFD). This auto-tuning feature simplifies frequency entry over manual tuning.
FLIGHT MANAGEMENT SYSTEM OVERVIEW Identifier with Duplicates FLIGHT INSTRUMENTS Duplicate Waypoints EIS AUDIO PANEL & CNS Duplicate Message FLIGHT MANAGEMENT Figure 5-32 Waypoint Information Window - Duplicate Identifier AIRPORTS HAZARD AVOIDANCE NOTE: ‘North Up’ orientation on the Airport Information Page cannot be changed; the pilot needs to be aware of proper orientation if the Navigation Map orientation is different from the Airport Information Page Map.
SYSTEM OVERVIEW FLIGHT MANAGEMENT Airport Information - ID/Facility/City - Usage Type/Region - Lat/Long/Elev - Fuel Available - Time Zone (UTC Offset) FLIGHT INSTRUMENTS Navigation Map Showing Selected Airport Runway Information - Designation - Length/Width/Surface - Lighting Available Airport METAR EIS Airport/Runway Diagram COM/NAV Freq. Info.
FLIGHT MANAGEMENT SYSTEM OVERVIEW The airport directory information is viewed on the Airport Directory Page by pressing the INFO softkey until INFO-2 is displayed.
SYSTEM OVERVIEW FLIGHT MANAGEMENT The Airport Frequencies Box uses the descriptions and abbreviations listed in the following table: AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Communication Frequencies Approach * Control Pre-Taxi Arrival * CTA * Radar ASOS Departure * Ramp ATIS Gate Terminal * AWOS Ground TMA * Center Helicopter Tower Class B * Multicom TRSA * Class C * Other Unicom Clearance Navigation Frequencies ILS LOC * May include Additional Information Table 5-5 Airport Frequency Abbreviations
FLIGHT MANAGEMENT SYSTEM OVERVIEW Pressing the ENT Key displays the PFD Airport Information Window for the highlighted airport. Pressing the ENT Key again returns to the Nearest Airports Window with the cursor on the next airport in the list. Continued presses of the ENT Key sequences through the information pages for all airports in the Nearest Airports list.
SYSTEM OVERVIEW FLIGHT MANAGEMENT Nearest Airports FLIGHT INSTRUMENTS - ID/Type - Bearing/Distance Airport Information - Facility/City/Elevation Nearest Airport Runway Information - Designation/Surface - Length/Width EIS Navigation Map Showing Nearest Airport COM/NAV Freq. Info.
FLIGHT MANAGEMENT SYSTEM OVERVIEW Viewing runway information for a specific airport: 1) With the Nearest Airports Page displayed, press the RNWY Softkey; or press the MENU Key, highlight ‘Select Runway Window’; and press the ENT Key. The cursor is placed in the ‘RUNWAYS’ Box. FLIGHT INSTRUMENTS 2) Turn the small FMS Knob to select the desired runway. 3) Press the FMS Knob to remove the flashing cursor.
SYSTEM OVERVIEW FLIGHT MANAGEMENT INTERSECTIONS NOTE: The VOR displayed on the Intersection Information Page is the nearest VOR, not necessarily the VOR FLIGHT INSTRUMENTS used to define the intersection. The Intersection Information Page is used to view information about intersections.
FLIGHT MANAGEMENT SYSTEM OVERVIEW The Nearest Intersections Page can be used to quickly find an intersection close to the flight path. In addition to displaying a map of the surrounding area, the page displays information for up to 25 nearest intersections in three boxes labeled ‘NEAREST INT’, ‘INFORMATION’, and ‘REFERENCE VOR’. FLIGHT INSTRUMENTS The selected intersection is indicated by a white arrow. Up to eleven intersections are visible at a time.
SYSTEM OVERVIEW FLIGHT MANAGEMENT NDBS FLIGHT INSTRUMENTS The NDB Information Page is used to view information about NDBs. In addition to displaying a map of the currently selected NDB and surrounding area, the page displays NDB information in four boxes labeled ‘NDB’, ‘INFORMATION’, ‘FREQUENCY’, and ‘NEAREST AIRPORT’.
FLIGHT MANAGEMENT SYSTEM OVERVIEW The Nearest NDB Page can be used to quickly find a NDB close to the flight path. In addition to displaying a map of the surrounding area, the page displays information for up to 25 nearest NDBs in three boxes labeled ‘NEAREST NDB’, ‘INFORMATION’, and ‘FREQUENCY’. FLIGHT INSTRUMENTS A white arrow before the NDB identifier indicates the selected NDB. Up to eleven NDBs are visible at a time. If there are more than can be shown, each list can be scrolled.
SYSTEM OVERVIEW FLIGHT MANAGEMENT VORS FLIGHT INSTRUMENTS The VOR Information Page can be used to view information about VOR and ILS signals (since ILS signals can be received on a NAV receiver), or to quickly auto-tune a VOR or ILS frequency. Localizer information cannot be viewed on the VOR Information Page. If a VOR station is combined with a TACAN station it is listed as a VORTAC on the VOR Information Page, and if it includes only DME, it is displayed as VOR-DME.
FLIGHT MANAGEMENT SYSTEM OVERVIEW 1) With the Nearest VOR Page displayed, press the MENU Key. 2) Highlight ‘Select VOR Window’, and press the ENT Key. 3) Press the ENT Key or turn either FMS Knob to select an identifier in the Nearest VOR Box. FLIGHT INSTRUMENTS 4) Press the FMS Knob to remove the flashing cursor. EIS The Nearest VOR Page can be used to quickly find a VOR station close to the aircraft. Also, a NAV frequency from a selected VOR station can be loaded from the Nearest VOR Page.
SYSTEM OVERVIEW FLIGHT MANAGEMENT USER WAYPOINTS FLIGHT INSTRUMENTS The G1000 can create and store up to 1,000 user-defined waypoints. User waypoints can be created from any map page (except PFD Inset Map, AUX-Trip Planning Page, or Procedure Pages) by selecting a position on the map using the Joystick, or from the User Waypoint Information Page by referencing a bearing/distance from an existing waypoint, bearings from two existing waypoints, or latitude and longitude.
FLIGHT MANAGEMENT SYSTEM OVERVIEW Nearest User Wpt List Navigation Map Showing Selected User Waypoint FLIGHT INSTRUMENTS - Identifier - Bearing/Distance from aircraft position EIS User Waypoint Info - Comment - Lat/Long Selected User Waypoint AUDIO PANEL & CNS Reference Wpt Info - Identifier - Radial/Distance Figure 5-46 Nearest User Waypoint Page FLIGHT MANAGEMENT CREATING USER WAYPOINTS User waypoints can be created from the User Waypoint Information Page in the following ways: Creating user w
SYSTEM OVERVIEW FLIGHT MANAGEMENT 1) Press the FMS Knob to activate the cursor. 2) Enter a user waypoint name (up to six characters). FLIGHT INSTRUMENTS 3) Press the ENT Key. The message ‘Are you sure you want to create the new User Waypoint AAAAAA?’ is displayed. 4) With ‘YES’ highlighted, press the ENT Key.
FLIGHT MANAGEMENT SYSTEM OVERVIEW 3) Enter a user waypoint name (up to six characters). 4) Press the ENT Key to accept the selected name. The first reference waypoint box is highlighted. 5) If desired, define the type and location of the waypoint in one of the following ways: FLIGHT INSTRUMENTS a) Select “RAD/RAD” using the small FMS Knob, press the ENT Key, and enter the two reference waypoint identifiers and radials into the REFERENCE WAYPOINTS window using the FMS Knobs.
SYSTEM OVERVIEW FLIGHT MANAGEMENT Changing the location of an existing waypoint to the aircraft present position: 1) Enter a waypoint name or select the waypoint in the User Waypoint List, then press the ENT Key. FLIGHT INSTRUMENTS 2) Press the MENU Key. 3) Select ‘Use Present Position’. 4) Press the ENT Key twice. The new waypoint’s location is saved. 5) Press the FMS Knob to remove the flashing cursor.
FLIGHT MANAGEMENT SYSTEM OVERVIEW DELETING USER WAYPOINTS Deleting a single user waypoint: FLIGHT INSTRUMENTS 1) Highlight a User Waypoint in the User Waypoint List, or enter a waypoint in the User Waypoint field. 2) Press the DELETE Softkey or press the CLR Key. ‘Yes’ is highlighted in the confirmation window. 3) Press the ENT Key. 4) Press the FMS Knob to remove the flashing cursor. Or: EIS 1) Highlight a User Waypoint in the User Waypoint List, or enter a waypoint in the User Waypoint field.
SYSTEM OVERVIEW FLIGHT MANAGEMENT 5.4 AIRSPACES FLIGHT INSTRUMENTS The G1000 can display the following types of airspaces: Class B/TMA, Class C/TCA, Class D, Restricted, MOA (Military), Other Airspace, Air Defense Interdiction Zone (ADIZ), and Temporary Flight Restriction (TFR).
FLIGHT MANAGEMENT SYSTEM OVERVIEW The Airspace Alerts Box allows the pilot to turn the controlled/special-use airspace message alerts on or off. This does not affect the alerts listed on the Nearest Airspaces Page or the airspace boundaries depicted on the Navigation Map Page. It simply turns on/off the warning provided when the aircraft is approaching or near an airspace. FLIGHT INSTRUMENTS An altitude buffer is also provided which “expands” the vertical range above or below an airspace.
SYSTEM OVERVIEW FLIGHT MANAGEMENT Map ranges for the airspace boundaries are selected from the Aviation Group in the Map Setup Menu. See Table 5-2 for the default and maximum ranges for each type of airspace and the symbol used to define the airspace area. FLIGHT INSTRUMENTS The Nearest Airspaces Page can be used to quickly find airspaces close to the flight path. In addition, a selected frequency associated with the airspace can be loaded from the Nearest Airspaces Page.
FLIGHT MANAGEMENT SYSTEM OVERVIEW Pressing the ALERTS Softkey displays the message window on the PFD. The following airspace alerts are displayed in the message window: Comments The aircraft is inside the special use airspace. FLIGHT INSTRUMENTS Special use airspace is ahead of aircraft. The aircraft penetrates the airspace within 10 minutes. Special use airspace is near and ahead of the aircraft position. Special use airspace is within 2 nm of the aircraft position.
SYSTEM OVERVIEW FLIGHT MANAGEMENT 5.5 DIRECT-TO-NAVIGATION FLIGHT INSTRUMENTS The Direct-to method of navigation, initiated by pressing the Direct-to Key on either the MFD or PFD, is quicker to use than a flight plan when the desire is to navigate to a single point such as a nearby airport. Once a direct-to is activated, the G1000 establishes a point-to-point course line from the present position to the selected direct-to destination.
FLIGHT MANAGEMENT SYSTEM OVERVIEW Any waypoint can be entered as a direct-to destination from the Direct-to Window. Entering a waypoint identifier, facility name, or city as a direct-to destination: FLIGHT INSTRUMENTS 1) Press the Direct-to Key. The Direct-to Window is displayed (with the active flight plan wayoint as the default selection or a blank waypoint field if no flight plan is active).
SYSTEM OVERVIEW FLIGHT MANAGEMENT Any NRST, RECENT, USER, or AIRWAY waypoints can be selected as a direct-to destination in the Direct-to Window. FLIGHT INSTRUMENTS Selecting a NRST, RECENT, USER, or AIRWAY waypoint as a direct-to destination: 1) Press the Direct-to Key. The Direct-to Window is displayed (with the active flight plan destination as the default selection or a blank destination if no flight plan is active).
FLIGHT MANAGEMENT SYSTEM OVERVIEW 4) Press the Direct-to Key to display the Direct-to Window with the selected point entered as the direct-to destination. 5) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’. FLIGHT INSTRUMENTS 6) Press the ENT Key again to activate the direct-to. Cancelling a Direct-to: 1) Press the Direct-to Key to display the Direct-to Window. 2) Press the MENU Key. EIS 3) With ‘Cancel Direct-To NAV’ highlighted, press the ENT Key.
SYSTEM OVERVIEW FLIGHT MANAGEMENT FLIGHT INSTRUMENTS A direct-to with altitude constraints creates a descent path (and provides guidance to stay on the path) from the aircraft’s current altitude to the altitude of the direct-to waypoint. The altitude is reached at the waypoint, or at the specified distance along the flight path if an offset distance has been entered. All VNV altitudes prior to the direct-to destination are removed from the active flight plan upon successful activation of the direct-to.
FLIGHT MANAGEMENT SYSTEM OVERVIEW 5.6 FLIGHT PLANNING Flight Plan Leg Type FLIGHT INSTRUMENTS Flight planning on the G1000 consists of building a flight plan by entering waypoints one at a time, adding waypoints along airways, and inserting departures, airways, arrivals, or approaches as needed. The G1000 allows flight planning information to be entered from either the MFD or PFD.
SYSTEM OVERVIEW FLIGHT MANAGEMENT The following could cause the airway update to fail: • Airway identifier, entry waypoint, or exit waypoint not found in the new database. FLIGHT INSTRUMENTS • Airway entry/exit waypoint is not an acceptable waypoint for the airway – either the waypoint is no longer on the airway, or there is a new directional restriction that prevents it being used. • Loading the new airway sequence would exceed the capacity of the flight plan.
FLIGHT MANAGEMENT SYSTEM OVERVIEW Catalog Contents - # Used - # Empty FLIGHT INSTRUMENTS Flight Plan List - Comment Selected Flight Plan Map EIS Selected FPL Info Softkeys AUDIO PANEL & CNS - Departure Waypoint - Destination Waypoint - Total Flight Plan Distance - Enroute Safe Altitude Figure 5-58 Flight Plan Catalog Page FLIGHT MANAGEMENT The active flight plan is listed on the active Flight Plan Page on the MFD, and in the Active Flight Plan Window on the PFD.
SYSTEM OVERVIEW FLIGHT MANAGEMENT Creating a stored flight plan: 1) Press the FPL Key. FLIGHT INSTRUMENTS 2) Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page. 3) Press the NEW Softkey; or press the MENU Key, highlight ‘Create New Flight Plan’, and press the ENT Key to display a blank flight plan for the first empty storage location. EIS 4) Turn the small FMS Knob to display the Waypoint Information Window.
FLIGHT MANAGEMENT SYSTEM OVERVIEW Flight plans can be imported from an SD Card or exported to an SD Card from the Stored Flight Plan Page. Importing a Flight Plan from an SD Card FLIGHT INSTRUMENTS 1) Insert the SD card containing the flight plan in the top card slot on the MFD. 2) Press the FPL Key to display the Active Flight Plan Page on the MFD. 3) Turn the small FMS Knob to select the Flight Plan Catalog Page. 4) Press the FMS Knob to activate the cursor.
SYSTEM OVERVIEW FLIGHT MANAGEMENT NOTE: If the imported flight plan contains a waypoint with a name that duplicates the name of a waypoint FLIGHT INSTRUMENTS already stored on the system, the system compares the coordinates of the imported waypoint with those of the existing waypoint. If the coordinates are different, the imported waypoint is automatically renamed by adding characters to the end of the name.
FLIGHT MANAGEMENT SYSTEM OVERVIEW ADDING WAYPOINTS TO AN EXISTING FLIGHT PLAN FLIGHT INSTRUMENTS Waypoints can be added to the active flight plan or any stored flight plan. Choose the flight plan, select the desired point of insertion, enter the waypoint, and it is added in front of the selected waypoint. Flight plans are limited to 99 waypoints (including waypoints within airways and procedures). If the number of waypoints in the flight plan exceeds 99, the message “Flight plan is full.
SYSTEM OVERVIEW FLIGHT MANAGEMENT Adding a waypoint to a stored flight plan: 1) On the Flight Plan Catalog Page, press the FMS Knob to activate the cursor. FLIGHT INSTRUMENTS 2) Highlight the desired flight plan. 3) Press the EDIT Softkey; or press the ENT Key, turn the large FMS Knob clockwise to select “EDIT” and press the ENT Key. The Stored Flight Plan Page is displayed. 4) Select the point in the flight plan to add the new waypoint.
FLIGHT MANAGEMENT SYSTEM OVERVIEW Creating and adding user waypoints to the active flight plan: 1) Press the Joystick to activate the panning function on the Active Flight Plan Page and pan to the map location of the desired user waypoint. FLIGHT INSTRUMENTS 2) Press the LD WPT Softkey; or press the MENU Key, select ‘Load Waypoint’, and press the ENT Key. The user waypoint is created with a name of USRxxx (using the next available in sequence) and is added to the end of the active flight plan.
SYSTEM OVERVIEW FLIGHT MANAGEMENT 5) Turn the FMS Knob to select the desired airway from the list, and press the ENT Key. Low altitude airways are shown first in the list, followed by “all” altitude airways, and then high altitude airways. FLIGHT INSTRUMENTS 6) Turn the FMS Knob to select the desired airway exit point from the list, and press the ENT Key. ‘LOAD?’ is highlighted. 7) Press the ENT Key. The system returns to editing the flight plan with the new airway inserted.
FLIGHT MANAGEMENT SYSTEM OVERVIEW RESTRICTIONS ON ADDING AIRWAYS Some airways have directional restrictions on all or part of the route. Airway “A2” in Europe has a directional restriction over the whole route such that it can be flown only in the direction MTD-ABB-BNE-DEVAL.
SYSTEM OVERVIEW FLIGHT MANAGEMENT DEPARTURE (DP) FLIGHT INSTRUMENTS A Departure Procedure (DP) is loaded at the departure airport in the flight plan. Only one departure can be loaded at a time in a flight plan. The route is defined by selection of a departure, the transition waypoints, and a runway.
FLIGHT MANAGEMENT SYSTEM OVERVIEW Departure Airport FLIGHT INSTRUMENTS Selected Departure Selected Runway Preview of Selected Departure Selected Transition Departure Transition Points Available EIS Selected Departure End Point AUDIO PANEL & CNS Figure 5-69 Departure Loading Page - Selecting Transition FLIGHT MANAGEMENT Inserted Departure Header HAZARD AVOIDANCE - Departure Identifier: [departure airport]-[departure runway]. [departure transition]. [departure end point] (e.g., KMKC-ALL.WLDCT2.
SYSTEM OVERVIEW FLIGHT MANAGEMENT ARRIVAL (STAR) FLIGHT INSTRUMENTS A Standard Terminal Arrival (STAR) is loaded at the destination airport in the flight plan. Only one arrival can be loaded at a time in a flight plan. The route is defined by selection of an arrival, the transition waypoints, and a runway.
FLIGHT MANAGEMENT SYSTEM OVERVIEW Destination Airport FLIGHT INSTRUMENTS Selected Arrival Selected Transition Transitions Available with DBRY1 EIS Arrival Waypoint Sequence Preview of Selected Arrival AUDIO PANEL & CNS Figure 5-72 Arrival Loading Page - Selecting the Transition FLIGHT MANAGEMENT HAZARD AVOIDANCE Inserted Arrival Header AFCS - Arrival Identifier: [arrival airport]-[arrival transition]. [arrival].[arrival runway] (e.g., KCOS-ALS.DBRY1.
SYSTEM OVERVIEW FLIGHT MANAGEMENT APPROACH (APPR) FLIGHT INSTRUMENTS An Approach Procedure (APPR) can be loaded at any airport that has an approach available. Only one approach can be loaded at a time in a flight plan. The route for a selected approach is defined by designating transition waypoints.
FLIGHT MANAGEMENT SYSTEM OVERVIEW Destination Airport FLIGHT INSTRUMENTS Selected Approach Selected Transition EIS Transitions Available with Selected Approach Approach Waypoint Sequence AUDIO PANEL & CNS Preview of Selected Approach Load Approach? FLIGHT MANAGEMENT Figure 5-75 Approach Loading Page - Selecting the Transition HAZARD AVOIDANCE Inserted Approach Header - Approach Identifier: [approach airport].
SYSTEM OVERVIEW FLIGHT MANAGEMENT FLIGHT PLAN STORAGE FLIGHT INSTRUMENTS The G1000 can store up to 99 flight plans, numbered 1 through 99. The active flight plan is erased when the G1000 is powered off or when another flight plan is activated. Details about each stored flight plan can be viewed on the Flight Plan Catalog Page and on the Stored Flight Plan Page. Viewing information about a stored flight plan: 1) Press the FPL Key on the MFD to display the Active Flight Plan Page.
FLIGHT MANAGEMENT SYSTEM OVERVIEW ACTIVATE A FLIGHT PLAN FLIGHT INSTRUMENTS Activating a stored flight plan erases the active flight plan and replaces it with the flight plan being activated. Inverting a stored flight plan reverses the waypoint order, erases the active flight plan, and replaces it with the flight plan being activated (the stored flight plan is not changed).
SYSTEM OVERVIEW FLIGHT MANAGEMENT DELETE A STORED FLIGHT PLAN Individual or all stored flight plans can be deleted from the G1000 memory. FLIGHT INSTRUMENTS Deleting a stored flight plan: 1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page. 2) Press the FMS Knob to activate the cursor, and turn the FMS Knob to highlight the desired flight plan.
FLIGHT MANAGEMENT SYSTEM OVERVIEW Deleting an individual waypoint from the active flight plan: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). FLIGHT INSTRUMENTS 2) Press the FMS Knob to activate the cursor (not required on the PFD) and turn the large FMS Knob to highlight the waypoint to be deleted. 3) Press the CLR Key. The ‘Remove XXXXX?’ window is displayed. 4) With ‘OK’ highlighted, press the ENT Key.
SYSTEM OVERVIEW FLIGHT MANAGEMENT 4) Press the EDIT Softkey; or press the MENU Key, select ‘Edit Flight Plan’ and press the ENT Key. The Stored Flight Plan Page is displayed. 5) Turn the large FMS Knob to highlight the waypoint to be deleted. FLIGHT INSTRUMENTS 6) Press the CLR Key. The ‘Remove XXXXX?’ window is displayed. 7) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key.
FLIGHT MANAGEMENT SYSTEM OVERVIEW 4) Press the EDIT Softkey; or press the MENU Key, select ‘Edit Flight Plan’ and press the ENT Key. The Stored Flight Plan Page is displayed. 5) Press the MENU Key to display the Page Menu and turn the FMS Knob to highlight ‘Remove ’. FLIGHT INSTRUMENTS 6) Press the ENT Key. The ‘Remove from flight plan?’ window is displayed. 7) With ‘OK’ highlighted, press the ENT Key.
SYSTEM OVERVIEW FLIGHT MANAGEMENT FLIGHT INSTRUMENTS A waypoint must be adjacent to its parent waypoint in the flight plan, so the system limits the along-track distance to less than the length of the leg before or after the selected waypoint. If the selected waypoint is the active waypoint, the distance is limited to less than the distance to go to the active waypoint. Assigning an along track offset to a leg with indeterminate length is not permitted.
FLIGHT MANAGEMENT SYSTEM OVERVIEW PARALLEL TRACK FLIGHT INSTRUMENTS The Parallel Track (PTK) feature allows creation of a parallel course offset of 1 to 50 nm left or right of the current flight plan. When Parallel Track is activated, the course line drawn on the map pages shows the parallel course, and waypoint names have a lower case “p” placed after the identifier. Using direct-to, loading an approach, a holding pattern, or editing and activating the flight plan automatically cancels Parallel Track.
SYSTEM OVERVIEW FLIGHT MANAGEMENT Offset Direction Offset Distance FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Activation Prompt HAZARD AVOIDANCE Figure 5-80 Parallel Track Window Parallel Track Waypoints - TIFTO-p - TOP-p - ...
FLIGHT MANAGEMENT SYSTEM OVERVIEW indicates that the system is unable to activate the parallel track with the message ‘Parallel Track Unavailable Approach Leg Active’. If the offset direction and distance results in an unreasonable route geometry the status indicates that the system is unable to activate the parallel track because of invalid geometry.
SYSTEM OVERVIEW ACTIVATING A FLIGHT PLAN LEG FLIGHT INSTRUMENTS FLIGHT MANAGEMENT Activating a flight plan leg: The G1000 allows selection of a highlighted leg as the “active leg” (the flight plan leg which is currently used for navigation guidance). 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD).
FLIGHT MANAGEMENT SYSTEM OVERVIEW FLIGHT INSTRUMENTS New Active Flight Plan Leg EIS Confirmation Window AUDIO PANEL & CNS Figure 5-85 Active Flight Plan Page - New Active Leg FLIGHT MANAGEMENT INVERTING A FLIGHT PLAN Any flight plan may be inverted (reversed) for navigation back to the original departure point. Inverting the active flight plan: HAZARD AVOIDANCE 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD).
SYSTEM OVERVIEW FLIGHT MANAGEMENT FLIGHT PLAN VIEWS FLIGHT INSTRUMENTS Information about flight plans can be viewed in more than one way. The active flight plan can be configured to show cumulative distance over the length of the flight plan or the distance for each leg of the flight plan; and the active flight plan can be viewed in a narrow or wide view.
FLIGHT MANAGEMENT SYSTEM OVERVIEW Active Flight Plan Leg to Leg Distance Active Flight Plan Cumulative Distance FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS WIDE Softkey, NARROW Softkey, LEG-LEG Softkey, CUM Softkey FLIGHT MANAGEMENT Figure 5-87 Active Flight Plan - Wide vs. Narrow View COLLAPSING AIRWAYS HAZARD AVOIDANCE The G1000 allows airways on the active flight plan to be collapsed or expanded from the Active Flight Plan Page/Window.
SYSTEM OVERVIEW FLIGHT MANAGEMENT Collapsing/expanding the airways in the active flight plan: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). FLIGHT INSTRUMENTS 2) Press the MENU Key, highlight ‘Collapse Airways’ or ‘Expand Airways’, and press the ENT Key. The airways are collapsed/expanded.
FLIGHT MANAGEMENT SYSTEM OVERVIEW FLIGHT INSTRUMENTS Waypoint Selected Hold At Wpt Menu Selection EIS AUDIO PANEL & CNS Location of Hold Hold Entry Course Course Direction (INBOUND or OUTBOUND) (TIME or DIST)) FLIGHT MANAGEMENT Leg Length Mode Button Leg Length (Time in nm or Distance in minutes) Turn Direction (RIGHT or LEFT) HAZARD AVOIDANCE Map of Hold Location AFCS ADDITIONAL FEATURES Expect Further Clearance Time APPENDICES Load Hold in Active Flight Plan Figure 5-89 Creating a User De
SYSTEM OVERVIEW FLIGHT MANAGEMENT Creating a user-defined hold at the aircraft present position: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). FLIGHT INSTRUMENTS 2) Press the MENU Key, highlight ‘Hold At Present Position’, and press the ENT Key. The HOLD AT window appears with the course field highlighted. 3) If desired, use the FMS Knobs to edit the entry course, and press the ENT Key.
FLIGHT MANAGEMENT SYSTEM OVERVIEW Removing a user-defined hold at an off-route direct-to: 1) Press a Direct To Key to display the DIRECT TO Window (PFD or MFD). 2) Press the MENU Key to display the PAGE MENU with the cursor on the ‘Cancel Direct-To NAV’ selection. FLIGHT INSTRUMENTS 3) Press the ENT Key. The holding pattern is removed.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW FLIGHT MANAGEMENT EIS Waypoint Selected AUDIO PANEL & CNS Hold Entry Course Location of Hold Course Direction FLIGHT MANAGEMENT Leg Length HAZARD AVOIDANCE (INBOUND or OUTBOUND) Leg Length Mode Button (Time in nm or Distance in minutes) Turn Direction (RIGHT or LEFT) (TIME or DIST)) ADDITIONAL FEATURES AFCS Map of Hold Location APPENDICES Expect Further Clearance Time Load Hold and Activate Direct To Hold At Direct To Waypoint Selection INDEX Figure 5-9
FLIGHT MANAGEMENT SYSTEM OVERVIEW 5.7 VERTICAL NAVIGATION FLIGHT INSTRUMENTS NOTE: The system supports vertical navigation for all lateral leg types except for CA, FA, FM, HA, HF, IF, HM, VA, VD, VI, VR, and VM. Vertical constraints are not retained in stored flight plans. Current Vertical Navigation Profile EIS The G1000 system Vertical Navigation (VNV) feature provides vertical profile guidance during the enroute and teminal phases of flight.
SYSTEM OVERVIEW FLIGHT MANAGEMENT FLIGHT INSTRUMENTS Canceling vertical navigation results in vertical deviation (V DEV), vertical speed required (VS REQ), and time to top of descent/bottom of descent (TIME TO TOD/BOD) going invalid. The Vertical Deviation Indicator (VDI) and Required Vertical Speed Indicator (RVSI) on the PFD are removed, and the V DEV, VS REQ, and TIME TO TOD items displayed in the CURRENT VNV PROFILE box are dashed. VNV remains disabled until manually enabled.
FLIGHT MANAGEMENT SYSTEM OVERVIEW 4) Press the ENT Key. Vertical guidance begins to the altitude constraint for the selected waypoint. 5) Press the FMS Knob to remove the flashing cursor. FLIGHT INSTRUMENTS The vertical navigation profile can be modified by directly entering a vertical speed target (VS TGT) and/or flight path angle (FPA) in the CURRENT VNV PROFILE box. Modifying the VS TGT and FPA: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD.
SYSTEM OVERVIEW FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS White Text Cyan Text Cyan Subdued Text Large Altitude calculated by the system Text estimating the altitude of the aircraft as it passes over the navigation point. This altitude is provided as a reference and is not designated to be used in determining vertical speed and deviation guidance. Altitude has been entered manually. Altitude is designated for use in giving vertical speed and deviation guidance.
FLIGHT MANAGEMENT SYSTEM OVERVIEW FLIGHT INSTRUMENTS Altitude constraints are displayed and entered in feet mean sea level (MSL) values to the nearest hundred. An altitude constraint in feet above ground level (AGL) format is supported for airports. When a database altitude restriction is displayed, the G1000 allows entry of a different altitude when creating a waypoint, effectively overriding the database restriction (only before the FAF).
SYSTEM OVERVIEW FLIGHT MANAGEMENT Deleting an altitude constraint that has been manually entered: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. FLIGHT INSTRUMENTS 2) Press the FMS Knob, and turn to highlight the desired waypoint altitude constraint. 3) Press the CLR Key. A ‘Remove or Revert to published VNV altitude of nnnnnFT?’ confirmation window is displayed. 4) Select ‘REMOVE’ and press the ENT Key.
FLIGHT MANAGEMENT SYSTEM OVERVIEW 5.8 PROCEDURES FLIGHT INSTRUMENTS The G1000 can access the whole range of instrument procedures available. Departures (DPs), arrivals (STARs), and non-precision and precision approaches (APPRs) are stored within the database and can be loaded using the Procedures (PROC) Key. EIS The selected procedure for the departure or arrival airport is added to the active flight plan.
SYSTEM OVERVIEW FLIGHT MANAGEMENT Departure Airport AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Available Procedure Actions Loaded Procedures Departure Preview Departure Choices FLIGHT MANAGEMENT Figure 5-95 Departure Selection Loaded Departure ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Selected Departure Procedure Loading Page Selection Softkeys INDEX APPENDICES Figure 5-96 Departure Loading 238 Garmin G1000 Pilot’s Guide for the Quest KODIAK® 100 190-00590-07 Rev.
FLIGHT MANAGEMENT SYSTEM OVERVIEW Viewing available departures at an airport: 1) From the Airport Information Page (first page in the WPT group), press the DP Softkey. The Departure Information Page is displayed, defaulting to the airport displayed on the Airport information Page. FLIGHT INSTRUMENTS 2) To select another airport, press the FMS Knob to activate the cursor, enter an identifier/facility name/city, and press the ENT Key. 3) Turn the large FMS Knob to highlight the Departure.
SYSTEM OVERVIEW FLIGHT MANAGEMENT ARRIVALS FLIGHT INSTRUMENTS A Standard Terminal Arrival (STAR) can be loaded at any airport that has one available. Only one arrival can be loaded at a time in a flight plan. If an arrival is loaded when another arrival is already in the active flight plan, the new arrival replaces the previous arrival. The route is defined by selection of an arrival, the transition waypoints, and a runway.
FLIGHT MANAGEMENT SYSTEM OVERVIEW Selected Arrival Loaded Arrival FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS Procedure Loading Page Selection Softkeys Figure 5-98 Arrival Loading FLIGHT MANAGEMENT Viewing available arrivals at an airport: 1) From the Airport Information Page (first page in the WPT group), press the STAR Softkey. The Arrival Information Page is displayed, defaulting to the airport displayed on the Airport Information Page.
SYSTEM OVERVIEW FLIGHT MANAGEMENT Or: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). FLIGHT INSTRUMENTS 2) Press the FMS Knob, and turn to highlight the arrival header in the active flight plan. 3) Press the CLR Key. A confirmation window is displayed listing the arrival procedure. 4) With ‘OK’ highlighted, press the ENT Key. To cancel the removal request, highlight ‘CANCEL’ and press the ENT Key.
FLIGHT MANAGEMENT SYSTEM OVERVIEW Example on HSI FLIGHT INSTRUMENTS EIS Approach Service Level - LNAV, LNAV+V, L/VNAV, LP, LP+V, LPV AUDIO PANEL & CNS HSI Annunciation Description LNAV RNAV GPS approach using published LNAV minima LNAV+V RNAV GPS approach using published LNAV minima.
SYSTEM OVERVIEW FLIGHT MANAGEMENT a) To skip setting minimums, press the ENT Key. FLIGHT INSTRUMENTS 6) Press the ENT Key with ‘LOAD?’ highlighted to load the approach procedure; or turn the large FMS Knob to highlight ‘ACTIVATE’ and press the ENT Key to load and activate the approach procedure. NOTE: When GPS is not approved for the selected final approach course, the message ‘NOT APPROVED FOR GPS’ is displayed.
FLIGHT MANAGEMENT SYSTEM OVERVIEW Viewing available approaches at an airport: 1) From the Airport Information Page (first page in the WPT group), press the APR Softkey. The Approach Information Page is displayed, defaulting to the airport displayed on the Airport information Page. FLIGHT INSTRUMENTS 2) To select another airport, press the FMS Knob to activate the cursor, enter an identifier/facility name/city, and press the ENT Key.
SYSTEM OVERVIEW FLIGHT MANAGEMENT a) To skip setting minimums, press the ENT Key. The ‘LOAD?’ field is highlighted. FLIGHT INSTRUMENTS 8) Press the ENT Key with ‘LOAD?’ highlighted to load the approach procedure; or turn the large FMS Knob to highlight ‘ACTIVATE’ and press the ENT Key to load and activate the approach procedure. The system continues navigating the current flight plan until the approach is activated.
FLIGHT MANAGEMENT SYSTEM OVERVIEW 3) Press the CLR Key. A confirmation window is displayed listing the approach procedure. 4) With ‘OK’ highlighted, press the ENT Key. To cancel the removal, highlight ‘CANCEL’ and press the ENT Key. 5) Press the FMS Knob to remove the flashing cursor. FLIGHT INSTRUMENTS MISSED APPROACH Activating a missed approach in the active flight plan: 1) Press the PROC Key. 2) Turn the FMS Knob to highlight ‘ACTIVATE MISSED APPROACH’. EIS 3) Press the ENT Key.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW FLIGHT MANAGEMENT Selected Temperature FAF Altitude Compensated Altitude AUDIO PANEL & CNS EIS Temperature Compensation Selected FLIGHT MANAGEMENT Figure 5-101 Temperature Compensation HAZARD AVOIDANCE ACTIVATE COMPENSATION? Highlighted CANCEL COMPENSATION? Highlighted ADDITIONAL FEATURES AFCS Figure 5-102 Activating/Cancelling Temperature Compensation APPENDICES Compensated Altitudes Uncompensated Altitudes INDEX Figure 5-103 Temperature Compensation in
FLIGHT MANAGEMENT SYSTEM OVERVIEW Cancelling temperature compensated altitude: 1) From the Active Flight Plan Page, press the MENU Key. The Page Menu is displayed. 2) Turn the FMS Knob to highlight ‘Temperature Compensation’. FLIGHT INSTRUMENTS 3) Press the ENT Key. The TEMPERATURE COMPENSATION Window is displayed. 4) Press the ENT Key. ‘CANCEL COMPENSATION?’ is highlighted. 5) Press the ENT Key. The temperature compensated altitude at the FAF is cancelled.
SYSTEM OVERVIEW FLIGHT MANAGEMENT 5.9 TRIP PLANNING FLIGHT INSTRUMENTS The G1000 allows the pilot to view trip planning information, fuel information, and other information for a specified flight plan or flight plan leg based on automatic data, or based on manually entered data. Weight planning is also available, based on fuel sensor data and the active flight plan (to estimate remaining fuel).
FLIGHT MANAGEMENT SYSTEM OVERVIEW TRIP STATISTICS The trip statistics are calculated based on the selected starting and ending waypoints and the trip planning inputs. FLIGHT INSTRUMENTS In flight plan mode (FPL) with a stored flight plan selected (NN), and the entire flight plan (CUM) selected, the waypoints are the starting and ending waypoints of the selected flight plan.
SYSTEM OVERVIEW FLIGHT MANAGEMENT FUEL STATISTICS FLIGHT INSTRUMENTS The fuel statistics are calculated based on the selected starting and ending waypoints and the trip planning inputs. Some of the calculated trip statistics are dashed when the selected leg of the active flight plan has already been flown. • Fuel efficiency (EFFICIENCY) - This value is calculated by dividing the current ground speed by the current fuel flow. • Time of fuel endurance (TOTAL ENDUR) - This time is shown as hours:minutes.
FLIGHT MANAGEMENT SYSTEM OVERVIEW Selecting automatic or manual page mode: Press the AUTO Softkey or the MANUAL Softkey; or press the MENU Key, highlight ‘Auto Mode’ or ‘Manual Mode’, and press the ENT Key. FLIGHT INSTRUMENTS Selecting flight plan or waypoint mode: Press the FPL Softkey or the WPTS Softkey; or press the MENU Key, highlight ‘Flight Plan Mode’ or ‘Waypoints Mode’, and press the ENT Key.
WEIGHT PLANNING NOTE: All weight planning page data fields display data rounded to the nearest 10 pounds or 5 kilograms.
FLIGHT MANAGEMENT SYSTEM OVERVIEW 3) Press the ENT Key to confirm the entry. 4) Press the FMS Knob to remove the flashing cursor. Entering the average passenger weight: FLIGHT INSTRUMENTS 1) Press the FMS Knob to activate the cursor and highlight the passenger weight field. 2) Turn the small FMS Knob to enter the average passenger weight. 3) Press the ENT Key to confirm the entry. 4) Press the FMS Knob to remove the flashing cursor.
SYSTEM OVERVIEW When the aircraft is in the air and a destination waypoint has been entered, the fuel calculations can be completed. FLIGHT INSTRUMENTS FLIGHT MANAGEMENT • Estimated landing fuel weight = fuel on board weight - (fuel flow x ETE) • Estimated landing weight = zero fuel weight + estimated landing fuel weight.
FLIGHT MANAGEMENT SYSTEM OVERVIEW 5.10 RAIM PREDICTION FLIGHT INSTRUMENTS RAIM (Receiver Autonomous Integrity Monitoring) 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 nm for oceanic, 2.0 nm for enroute, 1.0 nm for terminal, and 0.3 nm for non-precision approaches).
SYSTEM OVERVIEW FLIGHT MANAGEMENT 5) Turn the FMS Knobs to enter an arrival time and press the ENT Key. 6) Turn the FMS Knobs to enter an arrival date and press the ENT Key. FLIGHT INSTRUMENTS 7) Press the ENT Key with ‘COMPUTE RAIM?’ highlighted to begin the computation. Predicting RAIM availability at the aircraft present position: 1) Select the AUX-GPS Status Page. 2) Press the FMS Knob. The RAIM Prediction ‘WAYPOINT’ field is highlighted.
FLIGHT MANAGEMENT SYSTEM OVERVIEW Enabling/Disabling SBAS: 1) Select the AUX-GPS Status Page. 2) Press the SBAS Softkey. FLIGHT INSTRUMENTS 3) Press the FMS Knob, and turn the large FMS Knob to highlight ‘EGNOS’, ‘MSAS’ or ‘WAAS’. 4) Press the ENT Key to disable SBAS. Press the ENT Key again to enable SBAS.
SYSTEM OVERVIEW FLIGHT MANAGEMENT 5.11 NAVIGATING A FLIGHT PLAN FLIGHT INSTRUMENTS The following discussion is an example of navigating a flight plan with the SBAS capable GPS system while the G1000 provides vertical guidance through descents. A lateral flight plan (LNAV) would be navigated in much the same way, but would not include vertical guidance when the final approach course is active. NOTE: The following example flight plan is for instructional purposes only.
FLIGHT MANAGEMENT SYSTEM OVERVIEW 3) ATC now assigns routing to join V4. A heading of 290º is assigned to intercept V4. The aircraft turns to heading 290° as seen in Figure 5-113. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-113 Assigned Heading of 290º 4) Enter V4 into the flight plan. HAZARD AVOIDANCE a) Press the FMS Knob to activate the cursor. AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00590-07 Rev.
SYSTEM OVERVIEW FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS b) The desired entry point for V4 (TOP) must be entered. Turn the large FMS Knob to highlight the desired flight plan insertion point (SLN) as shown in Figure 5-114. When the V4 entry point (TOP) is inserted, it is placed immediately above the highlighted waypoint (SLN).
FLIGHT MANAGEMENT SYSTEM OVERVIEW d) Press the ENT Key. TOP is inserted into the flight plan as in Figure 5-116. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS Figure 5-116 TOP Inserted into the Flight Plan FLIGHT MANAGEMENT e) With SLN still highlighted as in Figure 5-116, turn the small FMS Knob clockwise. The Waypoint Information Page is displayed and the LD AIRWY Softkey is now available. f) Press the LD AIRWY Softkey to display the list of available airways for TOP as seen in Figure 5-117.
SYSTEM OVERVIEW FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS h) Press the ENT Key. The list of available exits for V4 is now displayed as in Figure 5-118. FLIGHT MANAGEMENT Figure 5-118 List of Available Exits for V4 i) If necessary, turn either FMS Knob to select the desired exit. In this case Salina VOR (SLN) is selected as in Figure 5-118. APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE j) Press the ENT Key.
FLIGHT MANAGEMENT SYSTEM OVERVIEW l) V4 is now loaded into the flight plan as shown in Figure 5-120. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS Figure 5-120 V4 is Loaded in the Flight Plan FLIGHT MANAGEMENT 5) Making V4 the active leg of the flight plan. a) Press the FMS Knob to activate the cursor. b) Turn the large FMS Knob to highlight SLN. The TO waypoint of the leg is selected in order to activate the leg. HAZARD AVOIDANCE c) Press the ACT LEG Softkey.
SYSTEM OVERVIEW FLIGHT MANAGEMENT FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS d) Verify the displayed leg is the desired leg and press the ENT Key. Note in Figure 5-122, the magenta arrow in the flight plan window and magenta line on the map indicating V4 is now the active flight plan leg. Note the phase of flight remained in Terminal (TERM) mode up to this point because a departure leg was active.
FLIGHT MANAGEMENT SYSTEM OVERVIEW 7) As the CDI approaches center, the aircraft turns onto the active leg as seen in Figure 5-123. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-123 Turn on to Active Leg 8) At SLN, Victor Airway 244 (V244) is intercepted. Turn prompts are displayed in the PFD Navigation Status Box as seen in Figure 5-124. HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES Figure 5-124 Turn to Intercept V244 APPENDICES INDEX 190-00590-07 Rev.
SYSTEM OVERVIEW FLIGHT MANAGEMENT FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS 9) As seen in Figure 5-125, V244 is now the active flight plan leg. INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Figure 5-125 V244 Now Active Leg 268 Garmin G1000 Pilot’s Guide for the Quest KODIAK® 100 190-00590-07 Rev.
FLIGHT MANAGEMENT SYSTEM OVERVIEW 10) At Lamar VOR (LAA) V263 is intercepted. See Figure 5-126. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-126 HYS to LAA Leg Active HAZARD AVOIDANCE 11) ATC grants clearance to proceed direct to the OPSHN intersection to begin the arrival procedure. ATC advises to expect an altitude of 10,000 feet at OPSHN. a) Press the FMS Knob to activate the cursor. b) Turn the large FMS Knob to select OPSHN in the flight plan list.
SYSTEM OVERVIEW FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS d) Turn the large FMS Knob to place the cursor in the VNV altitude field as shown in Figure 5-128. FLIGHT MANAGEMENT Figure 5-128 Enter VNV Altitude e) An altitude of 10,000 feet is entered as requested by ATC. APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE f) Press the ENT Key. The cursor is now displayed in the VNV offset field as shown in Figure 5-129.
FLIGHT MANAGEMENT SYSTEM OVERVIEW FLIGHT INSTRUMENTS h) Press the ENT Key twice to activate the direct-to. Note, in Figure 5-130, the magenta arrow indicating the direct-to OPSHN after the offset waypoint for OPSHN. The preceding offset waypoint indicates the offset distance and altitude that were previously entered. The remaining waypoints in the loaded arrival procedure have no database specified altitudes; therefore, dashes are displayed.
SYSTEM OVERVIEW FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS b) ‘SELECT APPROACH’ should be highlighted as shown in Figure 5-131. FLIGHT MANAGEMENT Figure 5-131 Procedures Window APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE c) Press the ENT Key. A list of available approaches for the destination airport is displayed as in Figure 5-131.
FLIGHT MANAGEMENT SYSTEM OVERVIEW e) Press the ENT Key. A list of available transitions for the selected approach is displayed as in Figure 5-133. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-133 List of Available Transitions f) Turn either FMS Knob to select the desired transition. In this case, the Initial Approach Fix (IAF) at HABUK is used. g) Press the ENT Key.
AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW FLIGHT MANAGEMENT FLIGHT MANAGEMENT Figure 5-134 Barometric Minimums Set APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE i) With ‘LOAD?’ highlighted, again press the ENT Key. The selected approach is added to the flight plan as seen in Figure 5-135. INDEX Figure 5-135 Loaded Approach 274 Garmin G1000 Pilot’s Guide for the Quest KODIAK® 100 190-00590-07 Rev.
FLIGHT MANAGEMENT SYSTEM OVERVIEW 13) Note the altitude constraints associated with each of the approach waypoints as seen in Figure 5-136. These altitudes are loaded from the database and are displayed as white text, indicating these values are “not designated” for use in computing vertical deviation guidance. FLIGHT INSTRUMENTS Note: To use the displayed altitude for calculating vertical deviation guidance, perform the following: a) Press the FMS Knob to activate the cursor.
SYSTEM OVERVIEW FLIGHT MANAGEMENT 14) As the aircraft approaches OPSHN, it may be desirable to adjust the speed or steepness of the upcoming descent. The default Flight Path Angle (FPA) is -3.0 degrees and a required vertical speed is computed to maintain the -3.0 FPA. To change the vertical flight path, perform the following steps. FLIGHT INSTRUMENTS a) Press the VNV PROF Softkey to place the cursor in the target vertical speed field (VS TGT) as shown in Figure 5-137.
FLIGHT MANAGEMENT SYSTEM OVERVIEW 15) As seen in Figure 5-138, the aircraft is approaching TOD. Note the target vertical speed required to reach the selected altitude. The Vertical Deviation Indicator (VDI) and the Required Vertical Speed Indicator (RVSI) are now displayed on the PFD as shown in Figure 5-138. When the aircraft is within one minute of the TOD, it is annunciated as shown in Figure 5-139, and an aural alert ‘Vertical track’ will be heard.
SYSTEM OVERVIEW FLIGHT MANAGEMENT FLIGHT INSTRUMENTS 16) Upon reaching TOD, a descent vertical speed is established by placing the VSI pointer in line with the RVSI as shown in Figure 5-140.
FLIGHT MANAGEMENT SYSTEM OVERVIEW 18) The aircraft is approaching OPSHN. The upcoming turn and next heading are annunciated at the top left of the PFD as seen in Figure 5-142. Initiate the turn and maneuver the aircraft on a track through the turn radius to intercept the magenta line for the OPSHN to FSHER leg and center the CDI.
SYSTEM OVERVIEW FLIGHT MANAGEMENT FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS 19) After passing OPSHN, the next leg of the arrival turns magenta as shown in Figure 5-143. The magenta arrow in the flight plan list now indicates the OPSHN to FSHER leg of the arrival procedure is now active. Figure 5-143 Tracking the OPSHN to FSHER Leg HAZARD AVOIDANCE 20) The flight continues through the arrival procedure to PYNON (see Figure 5-144).
FLIGHT MANAGEMENT SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Figure 5-144 Approaching PYNON INDEX 190-00590-07 Rev.
SYSTEM OVERVIEW FLIGHT MANAGEMENT FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS 21) Upon passing PYNON the approach procedure automatically becomes active. The approach may be activated at any point to proceed directly to the IAF. In this example, the aircraft has progressed through the final waypoint of the arrival and the flight plan has automatically sequenced to the IAF as the active leg, activating the approach procedure (see Figure 5-145).
FLIGHT MANAGEMENT SYSTEM OVERVIEW 22) The IAF is the next waypoint. At the TOD, establish a descent vertical speed as previously discussed in Step 16. The aircraft altitude is 9,000 feet upon reaching HABUK. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-147 Descending Turn to the Initial Approach Fix (IAF) HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00590-07 Rev.
SYSTEM OVERVIEW FLIGHT MANAGEMENT FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS 23) After crossing FALUR the next waypoint is the FAF. The flight phase changes to LPV on the HSI indicating the current phase of flight is in Approach Mode and the approach type is RNAV LPV. CDI scaling changes accordingly and is used much like a localizer when flying an ILS approach.
FLIGHT MANAGEMENT SYSTEM OVERVIEW 24) After crossing CEGIX, the aircraft continues following the glidepath to maintain the descent to “AT or ABOVE” 6,370 feet at the Missed Approach Point (MAP) (RW35R) as seen in Figure 5-149. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-149 Descending to the Missed Approach Point HAZARD AVOIDANCE In this missed approach procedure, the altitude immediately following the MAP (in this case ‘6368ft’) is not part of the published procedure.
SYSTEM OVERVIEW A direct-to is initiated to MOGAL, which is the Missed Approach Hold Point (MAHP) as seen in Figure 5-150. The aircraft is climbing to 10,000 feet. The CDI flight phase now changes from LPV to MAPR as seen on the HSI. APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS 25) Upon reaching the MAP, it is decided to execute a missed approach. Automatic waypoint sequencing is suspended past the MAP.
FLIGHT MANAGEMENT SYSTEM OVERVIEW 26) The aircraft continues climbing to “AT or ABOVE” 10,000 feet at MOGAL. A holding pattern is established at the MAHP (MOGAL) as shown in Figure 5-151. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-151 Establishing the Holding Pattern 27) The aircraft maintains 10,000 feet while following the magenta line through the hold as in Figure 5-152.
SYSTEM OVERVIEW FLIGHT MANAGEMENT 5.12 ABNORMAL OPERATION FLIGHT INSTRUMENTS This section discusses the Dead Reckoning mode of operation and the subsequent indications. NOTE: Dead Reckoning Mode only functions in Enroute (ENR) or Oceanic (OCN) phase of flight. In all other phases, an invalid GPS solution produces a “NO GPS POSITION” annunciation on the map and the G1000 stops using GPS.
FLIGHT MANAGEMENT SYSTEM OVERVIEW Distance & Estimated Time Enroute FLIGHT INSTRUMENTS Ground Speed Dead Reckoning Annunciaion Wind Data Current Track Indicator EIS GPS Navigation Lost Message AUDIO PANEL & CNS Bearing Pointer/ Distance Wind Data Navigation Data Bar FLIGHT MANAGEMENT All data except Active Leg, TAS, and DTK are in yellow Dead Reckoning Annunciation HAZARD AVOIDANCE Subdued Aircraft Symbol AFCS Figure 5-153 Dead Reckoning Mode - GPS Derived Data Shown in Yellow ADDITIONAL FE
INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW FLIGHT MANAGEMENT Blank Page 290 Garmin G1000 Pilot’s Guide for the Quest KODIAK® 100 190-00590-07 Rev.
HAZARD AVOIDANCE SYSTEM OVERVIEW SECTION 6 HAZARD AVOIDANCE FLIGHT INSTRUMENTS Hazard avoidance features available for the G1000 are designed to aid situational awareness and provide advisory information with regard to potential hazards to flight safety associated with weather, terrain, and air traffic.
SYSTEM OVERVIEW HAZARD AVOIDANCE 6.1 SIRIUSXM WEATHER WARNING: Do not use data link weather information for maneuvering in, near, or around areas of hazardous FLIGHT INSTRUMENTS WARNING: Do not use the indicated data link weather product age to determine the age of the weather EIS weather. Information contained within data link weather products may not accurately depict current weather conditions. information shown by the data link weather product.
HAZARD AVOIDANCE SYSTEM OVERVIEW FLIGHT INSTRUMENTS Audio Radio ID (for SiriusXM Satellite Radio) Data Radio ID (for SiriusXM Weather data) Figure 6-1 XM Information Page AUDIO PANEL & CNS Select to Display XM Information page EIS Weather Products (Available Products for Service Class Indicated in Green) Select to Lock Subscription Information FLIGHT MANAGEMENT ACCESSING SIRIUSXM WEATHER PRODUCTS The principal map for viewing SiriusXM Weather information is the Weather Data Link (XM) Page in the M
SYSTEM OVERVIEW HAZARD AVOIDANCE FLIGHT INSTRUMENTS For each enabled SiriusXM Weather product, the system displays a weather product icon and product age. The product age is the elapsed time (in minutes) since the weather data provider compiled the weather product. The product age display does not indicate the age of the information contained within the weather product, which can be significantly older than the displayed weather product age.
HAZARD AVOIDANCE Symbol 30 60 12 90 12 90 12 60 12 120 12 90 12 60 5 60 12 90 22 90 12 90 12 180 12 no product image 30 5 Temporary Flight Restrictions (TFRs) Terminal Aerodrome Reports (TAFs) no product image 60 12 no product image 60 12 INDEX 12 APPENDICES 30 ADDITIONAL FEATURES 5 AFCS 30 SiriusXM Lightning (XM LTNG) Cell Movement (CELL MOV) SIGMETs/AIRMETs (SIG/AIR) Meteorological Aerodrome Report (METARs) City Forecast (CITY) Surface Analysis (SFC) Freezing L
SYSTEM OVERVIEW HAZARD AVOIDANCE AUDIO PANEL & CNS Cloud Top (CLD TOP) + Echo Top (ECHO TOP) + + + + + + + + + + + Cell Movement (CELL MOV) + + + + + + + + + + + + + + + + + + + FLIGHT MANAGEMENT City Forecast (CITY) + Surface Analysis (SFC) + Freezing Levels (FRZ LVL) + HAZARD AVOIDANCE + METARs Winds Aloft (WIND) + County Warnings (COUNTY) + Cyclone Warnings (CYCLONE) + Icing Potential (ICNG) + PIREPs + AIREPs + Turbulence (TURB) + AFCS + Siri
HAZARD AVOIDANCE SYSTEM OVERVIEW Softkeys control the display of weather information on most MFD pages and the PFD Inset Map (Figure 6-3 shows the weather product softkeys for the Weather Data Link (XM) Page). When a weather product is selected for display, the corresponding softkey label changes to gray to indicate the product is enabled.
SYSTEM OVERVIEW HAZARD AVOIDANCE Setting up and customizing the Weather Data Link (XM) Page: 1) Select the Weather Data Link (XM) Page. FLIGHT INSTRUMENTS 2) Press the MENU Key. 3) With ‘Weather Setup’ highlighted, press the ENT Key (Figure 6-4). 4) Turn the small FMS Knob to select ‘PRODUCT GROUP 1’ or ‘PRODUCT GROUP 2’, and press the ENT Key (Figure 6-5). 5) Turn the large FMS Knob or press the ENT Key to scroll through product selections.
HAZARD AVOIDANCE SYSTEM OVERVIEW Setting up and customizing weather data for the Navigation Map Page: 1) Select the Navigation Map Page. 2) Press the MENU Key. FLIGHT INSTRUMENTS 3) With ‘Map Setup’ highlighted, press the ENT Key (Figure 6-6). 4) Turn the small FMS Knob to select the ‘Weather’ Group and press the ENT Key (Figure 6-7). 5) Turn the large FMS Knob or press the ENT Key to scroll through product selections (Figure 6-8).
SYSTEM OVERVIEW HAZARD AVOIDANCE Viewing legends for displayed weather products (on the Weather Data Link (XM) Page): 1) Select the Weather Data Link (XM) Page. FLIGHT INSTRUMENTS 2) Press the LEGEND Softkey to display the legends for the displayed weather products. Or: a) Press the MENU Key. b) Select ‘Weather Legend’ and press the ENT Key. 3) Turn the FMS Knob to scroll through the legends for enabled weather products.
HAZARD AVOIDANCE SYSTEM OVERVIEW NEXRAD NOTE: The NEXRAD weather product cannot be displayed at the same time as terrain, echo tops, turbulence, FLIGHT INSTRUMENTS icing data, or airborne weather radar is displayed on navigation maps. The National Weather Service (NWS) operates the WSR-88D, or NEXRAD (NEXt-generation RADar) system, an extensive network of 156 high-resolution Doppler radar systems.
SYSTEM OVERVIEW Displaying NEXRAD weather information: FLIGHT INSTRUMENTS HAZARD AVOIDANCE 2) Press the NEXRAD Softkey. 1) Press the MAP Softkey (for the PFD Inset Map, press the INSET Softkey). This step is not necessary on the Weather Data Link (XM) Page. FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS Composite data from all the NEXRAD radar sites in the United States is shown. This data is composed of the maximum reflectivity from the individual radar sweeps.
HAZARD AVOIDANCE SYSTEM OVERVIEW NEXRAD Limitations NEXRAD radar images may have certain limitations: FLIGHT INSTRUMENTS • NEXRAD base reflectivity does not provide sufficient information to determine cloud layers or precipitation characteristics (wet hail vs. rain). For example, it is not possible to distinguish between wet snow, wet hail, and rain. • NEXRAD base reflectivity is sampled at the minimum antenna elevation angle. An individual NEXRAD site cannot depict high altitude storms at close ranges.
SYSTEM OVERVIEW HAZARD AVOIDANCE NEXRAD Limitations (Canada) • Radar coverage extends to 55ºN. FLIGHT INSTRUMENTS • Any precipitation displayed between 52ºN and 55ºN is displayed as mixed regardless of actual propitiation type.
HAZARD AVOIDANCE SYSTEM OVERVIEW ECHO TOPS NOTE: Echo tops cannot be displayed at the same time as NEXRAD or Cloud Tops are selected for display. FLIGHT INSTRUMENTS The Echo Tops weather product (Figure 6-14) shows the location and elevation of the highest radar echo. The highest radar echo does not indicate the top of a storm or clouds; rather it indicates the highest altitude at which the NEXRAD system detected precipitation.
SYSTEM OVERVIEW HAZARD AVOIDANCE The display of radar coverage is always active when either NEXRAD or Echo Tops is selected. Areas where NEXRAD radar coverage and Echo Tops information is not currently available or is not being collected are indicated in gray shade of purple. FLIGHT INSTRUMENTS CLOUD TOPS NOTE: Cloud Tops and Echo Tops cannot be displayed at the same time.
HAZARD AVOIDANCE SYSTEM OVERVIEW SIRIUSXM LIGHTNING NOTE: SiriusXM Lightning data cannot be displayed at the same time as optional WX-500 Stormscope FLIGHT INSTRUMENTS lightning is selected for display. The SiriusXM Lightning weather product (Figure 6-18) shows the approximate location of cloud-to-ground lightning strikes. A strike icon represents a strike that has occurred within a two-kilometer region. The exact location of the lightning strike is not displayed.
SYSTEM OVERVIEW HAZARD AVOIDANCE CELL MOVEMENT FLIGHT INSTRUMENTS The Cell Movement weather product (Figure 6-20) shows the location and movement of storm cells as identified by the ground-based system. Cells are represented by yellow squares, with direction of movement indicated with short, orange arrows. FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS Storm Cells HAZARD AVOIDANCE Figure 6-20 Cell Movement Data On most applicable maps, Cell Movement data is selected for display along with NEXRAD.
HAZARD AVOIDANCE SYSTEM OVERVIEW SIGMETS AND AIRMETS FLIGHT INSTRUMENTS SIGMETs (SIGnificant METeorological Information) and AIRMETs (AIRmen’s METeorological Information) are broadcast for potentially hazardous weather conditions. A Convective SIGMET is issued for hazardous convective weather. A localized SIGMET is a significant weather condition occurring at a localized geographical position.
SYSTEM OVERVIEW HAZARD AVOIDANCE METARS AND TAFS NOTE: Atmospheric pressure as reported for METARs is given in hectopascals (hPa), except for in the United FLIGHT INSTRUMENTS States, where it is reported in inches of mercury (in Hg). Temperatures are reported in Celsius. NOTE: METAR information is only displayed within the installed navigation database service area.
HAZARD AVOIDANCE SYSTEM OVERVIEW 4) Use the FMS Knob or the ENT Key to scroll through the METAR and TAF text. METAR text must be completely scrolled through before scrolling through the TAF text. 5) Press the FMS Knob or the CLR Key to return to the Weather Data Link (XM) Page. FLIGHT INSTRUMENTS Or: 1) Select the Weather Information Page. a) Turn the large FMS Knob to select the Waypoint Page Group. b) Press the WX Softkey to select the Weather Information Page.
SYSTEM OVERVIEW HAZARD AVOIDANCE To display the METAR legend on the Weather Data Link (XM) Page (Figure 6-27), press the LEGEND Softkey when METARs are selected for display. EIS FLIGHT INSTRUMENTS The METAR flag color is determined by the information in the METAR text. A gray METAR flag is displayed when the METAR text does not contain adequate information to determine the METAR category.
HAZARD AVOIDANCE SYSTEM OVERVIEW To display the Surface Analysis and City Forecast legend (Figure 6-29), press the LEGEND Softkey when Surface Analysis and City Forecast are selected to be displayed. FLIGHT INSTRUMENTS EIS Figure 6-29 Surface Analysis Legend FREEZING LEVELS AUDIO PANEL & CNS The Freezing Level weather product shows the color-coded contour lines for the altitude and location at which the first isotherm is found (Figure 6-30).
FLIGHT INSTRUMENTS SYSTEM OVERVIEW HAZARD AVOIDANCE Figure 6-31 Freezing Level Legend EIS WINDS ALOFT AUDIO PANEL & CNS Displaying Winds Aloft data: FLIGHT MANAGEMENT The Winds Aloft weather product (Figure 6-32) shows the predicated wind speed and direction at the surface and at selected altitudes. Winds Aloft altitudes can be displayed in 3,000-foot increments from the surface up to 42,000 feet MSL. 3) Press the WIND Softkey. 1) Select the Weather Data Link (XM) Page.
HAZARD AVOIDANCE SYSTEM OVERVIEW FLIGHT INSTRUMENTS Figure 6-33 Winds Aloft Data with Legend EIS Headwind and tailwind components aloft are available inside the Profile View on the Navigation Map Page (Figure 6-34). The displayed components are relative to current aircraft altitude and track, but not to aircraft speed.
SYSTEM OVERVIEW HAZARD AVOIDANCE Showing/Hiding Profile View (containing winds aloft data) 1) Select the Navigation Map Page. FLIGHT INSTRUMENTS 2) Select the MAP Softkey. 3) Select the PROFILE Softkey. Or: 1) Select the Navigation Map Page 2) Press the MENU Key. EIS 3) Turn the large FMS Knob to highlight ‘Show Profile View’ or ‘Hide Profile View’ (choice dependent on current state) and press the ENT Key.
HAZARD AVOIDANCE SYSTEM OVERVIEW COUNTY WARNINGS FLIGHT INSTRUMENTS The County Warning weather product (Figure 6-38) provides specific public awareness and protection weather warnings from the National Weather Service (NWS). This can include information on severe thunderstorms, tornadoes, and flood conditions.
SYSTEM OVERVIEW HAZARD AVOIDANCE CYCLONE EIS FLIGHT INSTRUMENTS The Cyclone weather product (Figure 6-40) shows the current location of cyclones (hurricanes), tropical storms, and depressions using the symbol shown below (Figure 6-41). Storm tracks include the predicted date and time of arrival inside orange boxes.
HAZARD AVOIDANCE SYSTEM OVERVIEW ICING (CIP & SLD) NOTE: Icing data cannot be displayed at the same time as NEXRAD data is selected for display. FLIGHT INSTRUMENTS Current Icing Product (CIP) data (Figure 6-42) shows a graphical view of the current icing environment. Icing severity is displayed in four categories: light, moderate, severe, and extreme (not specific to aircraft type). The CIP product is not a forecast, but a presentation of the current conditions at the time of the analysis.
SYSTEM OVERVIEW HAZARD AVOIDANCE TURBULENCE NOTE: Turbulence data cannot be displayed at the same time the NEXRAD weather product is selected for FLIGHT INSTRUMENTS display. The Turbulence weather product (Figure 6-44) identifies the potential for erratic movement of high-altitude air mass associated winds. Turbulence is classified as light, moderate, severe or extreme, at altitudes between 21,000 and 45,000 feet. The Turbulence weather product is intended to supplement AIRMETs, SIGMETs, and PIREPS.
HAZARD AVOIDANCE SYSTEM OVERVIEW PIREPS AND AIREPS FLIGHT INSTRUMENTS Pilot Weather Reports (PIREPs) are airborne weather reports collected from pilots. When significant weather conditions are reported or forecast, Air Traffic Control (ATC) facilities are required to solicit PIREPs. A PIREP may contain adverse weather conditions, such as low in-flight visibility, icing conditions, wind shear, and turbulence. PIREPs are issued as either Routine (UA) or Urgent (UUA).
FLIGHT INSTRUMENTS SYSTEM OVERVIEW HAZARD AVOIDANCE EIS Decoded Urgent PIREP Text AUDIO PANEL & CNS Original Urgent PIREP Text FLIGHT MANAGEMENT Figure 6-47 Urgent PIREP Text on the Weather Data Link (XM) Page To display the PIREP or AIREP legend (Figure 6-48), press the LEGEND Softkey when PIREPs or AIREPs are selected for display. HAZARD AVOIDANCE The PIREP color is determined by the type (routine or urgent).
HAZARD AVOIDANCE SYSTEM OVERVIEW 6.2 AIRBORNE COLOR WEATHER RADAR SYSTEM DESCRIPTION FLIGHT INSTRUMENTS The optional Garmin GWX 68 Airborne Color Weather Radar is a four-color digital pulsed radar with 6.5 kilowatts of output power. It combines excellent range and adjustable scanning profiles with a high-definition target display. The pulse width is four microseconds (µs) on all ranges except the 2.5 nm range.
SYSTEM OVERVIEW HAZARD AVOIDANCE NEXRAD AND AIRBORNE WEATHER RADAR FLIGHT INSTRUMENTS Both Airborne Weather Radar and NEXRAD measure weather reflectivity in decibels (dB). A decibel is a logarithmic expression of the ratio of two quantities. Airborne Weather Radar measures the ratio of power against the gain of the antenna, while NEXRAD measures the energy reflected back to the radar, or the radar reflectivity ratio.
HAZARD AVOIDANCE SYSTEM OVERVIEW FLIGHT INSTRUMENTS 320 nm Figure 6-50 Radar Beam in Relation to the Curvature of the Earth EIS RADAR SIGNAL ATTENUATION AUDIO PANEL & CNS The phenomenon of radar signal attenuation affects the operation of weather radar. When the radar signal is transmitted, it is progressively absorbed and scattered, making the signal weaker. This weakening, or attenuation, is caused by two primary sources, distance and precipitation.
SYSTEM OVERVIEW HAZARD AVOIDANCE RADAR SIGNAL REFLECTIVITY Precipitation HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Precipitation or objects more dense than water, such as the surface of the earth or solid structures, are detected by the weather radar. The weather radar does not detect clouds, thunderstorms, or turbulence directly. It detects precipitation associated with clouds, thunderstorms, and turbulence.
HAZARD AVOIDANCE SYSTEM OVERVIEW Ground Returns FLIGHT INSTRUMENTS The intensity of ground target returns depends upon the angle at which the radar beam strikes the ground target (Angle of Incidence) and the reflective properties of that target. The gain can be adjusted so shorelines, rivers, lakes, and cities are well-defined. Increasing the gain too much causes the display to fill in between targets, thus obscuring some landmarks. Cities normally provide a strong return signal.
SYSTEM OVERVIEW HAZARD AVOIDANCE SAFE OPERATING DISTANCE FLIGHT INSTRUMENTS The following information establishes a minimum safe distance from the antenna for personnel near operating weather radar. The minimum safe distance is based on the FCC’s exposure limit at 9.3 to 9.5 GHz for general population/uncontrolled environments, which is 1 mW/cm2. See Advisory Circular 20-68B for more information on safe distance determination.
HAZARD AVOIDANCE SYSTEM OVERVIEW PRACTICAL APPLICATION USING THE BASIC TILT SETUP FLIGHT INSTRUMENTS With the antenna tilt set as previously described, any displayed target return should be scrutinized when flying at altitudes between 2,000 and 30,000 feet AGL. If the displayed target advances on the screen to within 5 nautical miles of the aircraft, avoid it. This may be either weather or ground returns that are 2,000 feet or less below the aircraft.
SYSTEM OVERVIEW HAZARD AVOIDANCE WEATHER MAPPING AND INTERPRETATION WEATHER DISPLAY INTERPRETATION AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS When evaluating various target returns on the weather radar display, the colors denote precipitation intensity and rates shown in the table. Weather Mode Color Intensity Black Green Yellow Red Magenta < 23 dBZ 23 dBZ to < 32 dBZ 32 dBZ to < 41 dBZ 41 dBZ to < 50 dBZ 50 dBZ and greater Approximate Precipitation Rate (in/ hr.) < .01. .01 - 0.1. 0.1 - 0.5 0.
HAZARD AVOIDANCE SYSTEM OVERVIEW Along squall lines (multiple cells or clusters of cells in a line) individual cells may be in different stages of development. Areas between closely spaced, intense targets may contain developing clouds not having enough moisture to produce a return. However, these areas could have strong updrafts or downdrafts. Targets showing wide areas of green are generally precipitation without severe turbulence.
SYSTEM OVERVIEW HAZARD AVOIDANCE EIS FLIGHT INSTRUMENTS In areas of multiple heavy cells, use the Vertical Scan feature along with antenna tilt management to examine the areas. Remember to avoid shadowed areas behind targets. AUDIO PANEL & CNS The Blind Alley at Close Range The Large Storm Behind Figure 6-57 The Blind Alley FLIGHT MANAGEMENT Tornadoes There are no conclusive radar target return characteristics which identify a tornado.
HAZARD AVOIDANCE SYSTEM OVERVIEW Hail shafts are associated with the same radar target return characteristics as tornados. U-shaped cloud edges three to seven miles across can also indicate hail. These target returns appear quite suddenly along any edge of the cell outline. They also change in intensity and shape in a matter of seconds, making vigilant monitoring essential. FLIGHT INSTRUMENTS OPERATION IN WEATHER MODE WARNING: Begin transmitting only when it is safe to do so.
SYSTEM OVERVIEW HAZARD AVOIDANCE Displaying weather on the Weather Radar Page: 1) Select the Weather Radar Page in the Map Page Group with the FMS Knob. FLIGHT INSTRUMENTS 2) Press the MODE Softkey. 3) While on the ground, press the STANDBY Softkey. A one-minute warm-up period is initiated (countdown is displayed on the screen). After the warm-up is complete, the radar enters the Standby Mode. Press the WEATHER Softkey. A confirmation window is displayed.
HAZARD AVOIDANCE SYSTEM OVERVIEW Vertically scanning a storm cell: NOTE: Vertical scanning of a storm cell should be done with the aircraft wings level to avoid constant FLIGHT INSTRUMENTS adjustment of the Bearing Line. 1) While in the Horizontal Scan view, press the BRG Softkey. This places the cursor in the BEARING field and displays the Bearing Line. If the Bearing Line is not displayed, press the MENU Key and turn the large FMS Knob to select Show Bearing Line. Press the ENT Key.
AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW HAZARD AVOIDANCE Figure 6-61 Vertical Scan Display FLIGHT MANAGEMENT Adjusting Antenna Tilt Angle HAZARD AVOIDANCE In order to make an accurate interpretation of a storm cell, the radar beam should be pointed at the wet part of the weather cell to record the proper rainfall intensity (color level). The ideal aiming point is just below the freezing level of the storm. The best way to find this point is to use the Vertical Scan feature.
HAZARD AVOIDANCE SYSTEM OVERVIEW Adjusting antenna tilt on the Vertical Scan display: 1) Press the TILT Softkey to activate the cursor in the TILT field and display the Tilt Line. FLIGHT INSTRUMENTS If the Tilt Line is not displayed, press the MENU Key and turn the large FMS Knob to select Show Tilt Line. Press the ENT Key. 2) Turn the small FMS Knob to adjust the antenna tilt angle. The selected tilt angle is implemented when Horizontal Scan is selected again.
SYSTEM OVERVIEW HAZARD AVOIDANCE Adjusting Gain WARNING: Changing the gain in weather mode causes precipitation intensity to be displayed as a color FLIGHT INSTRUMENTS not representative of the true intensity. Remember to return the gain setting to Calibrated for viewing the actual intensity of precipitation. 1) Press the GAIN Softkey to activate the cursor in the GAIN field. 2) Turn the small FMS Knob to adjust the gain for the desirable level.
HAZARD AVOIDANCE SYSTEM OVERVIEW Sector Scan FLIGHT INSTRUMENTS 1) While in horizontal scan mode, press the BRG Softkey to display the Bearing Line and place the cursor in the BEARING field. If the Bearing Line is not displayed, press the MENU Key and turn the large FMS Knob to select Show Bearing Line. 2) Press the ENT Key.
SYSTEM OVERVIEW HAZARD AVOIDANCE Antenna Stabilization 1) To activate or deactivate the antenna stabilization, press the MODE Softkey. FLIGHT INSTRUMENTS 2) Press the STAB ON Softkey to activate antenna stabilization or press the STAB OFF Softkey to deactivate. The current stabilization condition is shown in the upper right of the weather radar display.
HAZARD AVOIDANCE SYSTEM OVERVIEW Weather Alert Target Bands and Message Advisory FLIGHT INSTRUMENTS The Weather Alert feature indicates the presence of heavy precipitation between the ranges of 80 and 320 nm regardless of the currently displayed range. Weather Alert targets appear as red bands along the outer range ring at the approximate azimuth of the detected returns.
SYSTEM OVERVIEW HAZARD AVOIDANCE GROUND MAPPING AND INTERPRETATION FLIGHT INSTRUMENTS A secondary use of the weather radar system is for the presentation of terrain. This can be a useful tool for verifying aircraft position. A picture of the ground is represented much like a topographical map that can be used as a supplement to the navigation map on the MFD. EIS Ground Map mode uses a different gain range than Weather mode. Different colors are also used to represent the intensity levels.
HAZARD AVOIDANCE SYSTEM OVERVIEW WEATHER RADAR OVERLAY ON THE NAVIGATION MAP PAGE FLIGHT INSTRUMENTS The Map - Weather Radar Page is the principal map page for viewing airborne weather radar information. Weather radar information may also be shown as an overlay on the Navigation Map Page on the MFD as an additional reference. EIS When the airborne weather radar overlay is enabled, a weather radar information box appears in the upperright corner of the Navigation Map Page.
SYSTEM OVERVIEW 4) Turn the large FMS Knob to scroll through the product selections and highlight the WX RADAR overlay selection (‘On’ or ‘Off’). Turn the small FMS knob to highlight the desired selection. FLIGHT INSTRUMENTS HAZARD AVOIDANCE Weather radar controls on the Navigation Map Page are limited to adjustment of the radar range, bearing, and antenna tilt angle. The airborne weather radar overlay is viewable at Navigation Map Ranges between five and 800 nautical miles (ten to 1,500 kilometers).
HAZARD AVOIDANCE SYSTEM OVERVIEW SYSTEM STATUS The radar mode is annunciated in the upper left corner of the Weather Radar Page. Additional information may be displayed in the center of the Weather Radar Page as a banner annunciation.
SYSTEM OVERVIEW HAZARD AVOIDANCE 6.3 WX-500 STORMSCOPE FLIGHT INSTRUMENTS WARNING: Do not rely on information from a lightning detection system display as the sole basis for hazardous weather avoidance. Range limitations and interference may cause the system to display inaccurate or incomplete information. Refer to documentation from the lightning detection system manufacturer for detailed information about the system.
HAZARD AVOIDANCE SYSTEM OVERVIEW The following options are available (Figure 6-71): • STRMSCP LTNG – Turns the display of Stormscope data on or off. FLIGHT INSTRUMENTS • STRMSCP MODE – Selects the CELL or STRIKE mode of lightning activity. Cell mode identifies clusters or cells of electrical activity. Strike mode indicates the approximate location of lightning strikes. • STRMSCP SMBL – Selects the range at which Stormscope data displays.
SYSTEM OVERVIEW HAZARD AVOIDANCE CELL AND STRIKE MODE ON THE NAVIGATION MAP FLIGHT INSTRUMENTS On the Navigation Map, cell mode identifies cells of lightning activity (Figure 6-72). Stormscope identifies clusters of electrical activity that indicate cells. Strike mode indicates the approximate location of lightning strikes. Selecting the ‘cell’ or ‘strike’ mode on the Navigation Map: 1) Press the MENU Key. 2) With ‘Map Setup’ selected, press the ENT Key. EIS 3) Select the ‘Weather’ group.
HAZARD AVOIDANCE SYSTEM OVERVIEW If heading input is lost, strikes and/or cells must be cleared manually after the execution of each turn (Figure 6-73). This is to ensure that the strike and/or cell positions are depicted accurately in relation to the nose of the aircraft. FLIGHT INSTRUMENTS Manually clearing Stormscope data on the Navigation Map: 1) Press the MENU Key. 2) Select ‘Clear Stormscope Lightning®’. 3) Press the ENT Key.
SYSTEM OVERVIEW HAZARD AVOIDANCE SELECTING THE STORMSCOPE PAGE Stormscope lightning data can be displayed at the ranges of 25 nm, 50 nm, 100 nm, and 200 nm. FLIGHT INSTRUMENTS Adjusting the Stormscope Map Range: 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Stormscope Page. HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS 3) To change the map range, turn the RANGE Knob clockwise to zoom out or counter-clockwise to zoom in.
HAZARD AVOIDANCE SYSTEM OVERVIEW 6.4 TAWS-B FLIGHT INSTRUMENTS WARNING: Do not use TAWS information for primary terrain avoidance. TAWS is intended only to enhance situational awareness. NOTE: The data contained in the TAWS databases comes from government agencies. Garmin accurately processes and cross-validates the data but cannot guarantee the accuracy and completeness of the data.
SYSTEM OVERVIEW from the altimeter) to differ from the GSL altitude. This variation results in the aircraft’s GSL altitude differing from the baro-corrected altitude. FLIGHT INSTRUMENTS HAZARD AVOIDANCE TAWS-B uses yellow (caution) and red (warning) to depict terrain and obstacles (with heights greater than 200 feet above ground level, AGL) alerts relative to aircraft altitude. Colors are adjusted automatically as the aircraft altitude changes.
HAZARD AVOIDANCE SYSTEM OVERVIEW Displaying terrain and obstacle information (maps other than the TAWS-B Page): 1) Press the MAP Softkey (for the PFD Inset Map, press the INSET Softkey). 2) Press the TERRAIN Softkey to display terrain and obstacle data. FLIGHT INSTRUMENTS When TAWS-B is selected on maps other than the TAWS-B Page, an icon is shown to indicate that the feature is enabled for display.
SYSTEM OVERVIEW HAZARD AVOIDANCE Customizing terrain and obstacle display on the Navigation Map Page: 1) Select the Navigation Map Page. FLIGHT INSTRUMENTS 2) Press the MENU Key. 3) With ‘Map Setup’ highlighted, press the ENT Key (Figure 6-77). 4) Turn the small FMS Knob to select the ‘Map’ Group and press the ENT Key (Figure 6-78). 5) Turn the large FMS Knob or press the ENT Key to scroll through product selections (Figure 6-79).
HAZARD AVOIDANCE SYSTEM OVERVIEW TAWS-B PAGE FLIGHT INSTRUMENTS The TAWS-B Page is specialized to show terrain, obstacle, and potential impact point data in relation to the aircraft’s current altitude, without clutter from the basemap. Aviation data (airports, VORs, and other NAVAIDs) can be displayed for reference. If an obstacle and the projected flight path of the aircraft intersect, the display automatically zooms in to the closest potential point of impact on the TAWS-B Page.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW HAZARD AVOIDANCE Map Orientation Current Aircraft GPS-derived GSL Altitude Red Terrain (Above or Within 100’ Below the Aircraft Altitude) Map Range Rings Black Terrain (More than 1000’ Below the Aircraft Altitude) AUDIO PANEL & CNS EIS Red Lighted Obstacle (Above or Within 100’ Below Aircraft Altitude) Yellow Terrain (Between 100’ and 1000’ Below the Aircraft Altitude) FLIGHT MANAGEMENT Yellow Lighted Obstacles (Between 100’ and 1000’ Below Aircraft Altitude) T
HAZARD AVOIDANCE SYSTEM OVERVIEW TAWS-B ALERTS FLIGHT INSTRUMENTS Alerts are issued when flight conditions meet parameters that are set within TAWS-B software algorithms. TAWS-B alerts typically employ a CAUTION or a WARNING alert severity level, or both. When an alert is issued, visual annunciations are displayed and voice alerts are simultaneously issued. Table 6-11 shows TAWS-B alert types with corresponding annunciations and voice alerts.
SYSTEM OVERVIEW HAZARD AVOIDANCE Alert Type PFD/MFD** MFD Pop-Up Alert Alert (except TAWS-B Page) Annunciation Voice Alert EIS FLIGHT INSTRUMENTS Excessive Descent Rate Warning (EDR) “Pull Up” or Imminent Terrain Impact Warning (ITI) or AUDIO PANEL & CNS FLIGHT MANAGEMENT Imminent Obstacle Impact Warning (IOI) HAZARD AVOIDANCE Imminent Terrain Impact Caution (ITI) AFCS or “Caution, Terrain; Caution, Terrain” or “Terrain Ahead; Terrain Ahead”* or “Caution, Obstacle; Caution, Obstacle”* or
HAZARD AVOIDANCE SYSTEM OVERVIEW EXCESSIVE DESCENT RATE ALERT FLIGHT INSTRUMENTS The purpose of the Excessive Descent Rate (EDR) alert is to provide suitable notification when the aircraft is determined to be closing (descending) upon terrain at an excessive speed. Figure 6-84 shows the parameters for the alert as defined by TSO-C151b.
SYSTEM OVERVIEW HAZARD AVOIDANCE FORWARD LOOKING TERRAIN AVOIDANCE FLIGHT INSTRUMENTS The Forward Looking Terrain Avoidance (FLTA) feature of TAWS-B compares the aircraft’s projected flight path with known terrain and obstacles in their respective databases and issues four types of alerts as either a caution or a warning: Reduced Required Terrain Clearance (RTC) and Reduced Required Obstacle Clearance (ROC) alerts are issued when the aircraft flight path is above terrain, yet is projected to come within
HAZARD AVOIDANCE SYSTEM OVERVIEW PREMATURE DESCENT ALERTING A Premature Descent Alert (PDA) is issued when the system detects that the aircraft is significantly below the normal approach path to a runway (Figure 6-86). FLIGHT INSTRUMENTS PDA alerting begins when the aircraft is below 700 feet AGL within 15 nm of the destination airport and ends when the aircraft is 0.5 nm from the runway threshold.
SYSTEM OVERVIEW HAZARD AVOIDANCE FIVE-HUNDRED VOICE CALLOUT (VCO) ALERT FLIGHT INSTRUMENTS The “Five-hundred” voice alert occurs when the aircraft descends to within 500 feet above the terrain or runway threshold. When the aircraft is within five nautical miles of an airport, the “Five Hundred” voice alert is based on the nearest runway threshold elevation.
HAZARD AVOIDANCE SYSTEM OVERVIEW 1000 800 700 FLIGHT INSTRUMENTS Height Above Terrain (Feet) 900 600 “DON’T SINK” or “TOO LOW, TERRAIN” 500 400 300 EIS 200 100 0 0 500 1000 1500 2000 2500 3000 3500 4000 4500 5000 5500 6000 6500 7000 AUDIO PANEL & CNS Sink Rate (FPM) Figure 6-89 Negative Climb Rate (NCR) Sink Rate FLIGHT MANAGEMENT SYSTEM STATUS During G1000 power-up, TAWS-B conducts a system test of its alerting capabilities. The system test can also be manually initiated.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW HAZARD AVOIDANCE EIS TAWS-B requires a 3-D GPS navigation solution along with specific vertical accuracy minimums. Should the navigation solution become degraded or if the aircraft is out of the database coverage area, the annunciation ‘TAWS N/A’ is generated in the annunciation window and on the TAWS-B Page. If the aircraft is in the air, the voice alert “TAWS Not Available” is also generated.
HAZARD AVOIDANCE SYSTEM OVERVIEW 6.5 PROFILE VIEW TERRAIN FLIGHT INSTRUMENTS The system offers a Profile View of terrain and obstacles relative to the aircraft’s current flight path and altitude on the Navigation Map Page of the MFD. Profile View does not provide terrain or obstacle caution or warning annunciations or voice alerts, nor does it display potential impact points inside the Profile View. The colors and symbols in Figure 6-91 and Table 6-14 are used to represent terrain and obstacles.
SYSTEM OVERVIEW HAZARD AVOIDANCE PROFILE VIEW DISPLAY FLIGHT INSTRUMENTS When the Profile View is enabled, it is displayed in a window below the Navigation Map. Altitude is shown along a vertical scale, with an aircraft icon positioned at the current altitude. Distance is represented horizontally along the bottom of the Profile View, and increases from left (present position) to right.
HAZARD AVOIDANCE Approach 0.6 nm Departure 0.6 nm Terminal 2.0 nm Enroute 4.0 nm Oceanic 4.0 nm FLIGHT INSTRUMENTS Total Profile View Width SYSTEM OVERVIEW Flight Phase EIS Table 6-15 Profile View Width Scale AUDIO PANEL & CNS PROFILE PATH FLIGHT MANAGEMENT The Profile Path displays the horizontal and lateral boundaries of the Profile View. The path is shown as a white rectangle on the Navigation Map Page (Figure 6-92) and is only available when Profile View is enabled.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS Figure 6-93 Navigation Map Page Menu Figure 6-95 Navigation Map Page Setup Menu, Profile Group INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Figure 6-94 Navigation Map Page Setup Menu 368 Garmin G1000 Pilot’s Guide for the Quest KODIAK® 100 190-00590-07 Rev.
HAZARD AVOIDANCE SYSTEM OVERVIEW 6.6 TRAFFIC INFORMATION SERVICE (TIS) FLIGHT INSTRUMENTS WARNING: The Traffic Information Service (TIS) is intended for advisory use only. TIS is intended to help the pilot locate traffic visually. It is the responsibility of the pilot to see and maneuver to avoid traffic. NOTE: TIS is available only when the aircraft is within the service volume of a TIS-capable terminal radar EIS site.
SYSTEM OVERVIEW HAZARD AVOIDANCE DISPLAYING TRAFFIC DATA FLIGHT INSTRUMENTS The Map - Traffic Map Page is the principal page for viewing traffic information. Additional displays of traffic information are available as map overlays while TIS is operating, and serve as additional reference to the Traffic Map Page.
HAZARD AVOIDANCE SYSTEM OVERVIEW FLIGHT INSTRUMENTS The Navigation Map Page Setup Menu provides a means in addition to the softkey for enabling/disabling display of traffic. The setup menu also controls the map range settings above which traffic data (symbols and labels) are decluttered from the display. If a map range larger than the map range setting is selected, the data is removed from the map. Maps besides the Traffic Map Page use settings based on those selected for the Navigation Map Page.
SYSTEM OVERVIEW HAZARD AVOIDANCE TRAFFIC MAP PAGE FLIGHT INSTRUMENTS The Traffic Map Page is specialized to show surrounding TIS traffic data in relation to the aircraft’s current position and altitude, without clutter from the basemap. Aircraft orientation on this map is always heading up unless there is no valid heading. Map range is adjustable with the RANGE Knob from 2 to 12 nm, as indicated by the map range rings.
HAZARD AVOIDANCE SYSTEM OVERVIEW TIS ALERTS When the number of TAs on the Traffic Map Page increases from one scan to the next, the following occur: • A single “Traffic” voice alert is generated. FLIGHT INSTRUMENTS • A ‘TRAFFIC’ Annunciation appears to the top left of the Attitude Indicator on the PFD, flashing for 5 seconds and remaining displayed until no TAs are detected in the area. • The PFD Inset Map is automatically displayed with traffic.
SYSTEM OVERVIEW HAZARD AVOIDANCE Muting the “TIS Not Available” voice alert: 1) Select the Traffic Map Page. FLIGHT INSTRUMENTS 2) Press the TNA MUTE Softkey. The status is displayed in the upper left corner of the Traffic Map Page. Or: a) Press the MENU Key. b) Select ‘‘’Not Available” Mute On’ (shown if TNA muting is currently off) and press the ENT Key. EIS SYSTEM STATUS AUDIO PANEL & CNS The G1000 performs an automatic test of TIS during power-up.
HAZARD AVOIDANCE SYSTEM OVERVIEW Mode Traffic Mode Annunciation (Traffic Map Page) TIS Operating OPERATING TIS Failed* FAIL AUDIO PANEL & CNS STANDBY (also shown in white in center of page) Traffic Display Status Icon (Other Maps) EIS TIS Standby FLIGHT INSTRUMENTS The traffic mode is annunciated in the upper left corner of the Traffic Map Page. When the aircraft is on the ground, TIS automatically enters Standby Mode.
SYSTEM OVERVIEW HAZARD AVOIDANCE The annunciations to indicate the status of traffic information appear in a banner at the lower left corner of maps on which traffic can be displayed (Table 6-17). FLIGHT INSTRUMENTS Traffic Status Banner Annunciation TA OFF SCALE EIS TA X.
HAZARD AVOIDANCE SYSTEM OVERVIEW 6.7 GARMIN GTS 800 TRAFFIC FLIGHT INSTRUMENTS WARNING: Do not rely solely upon the display of traffic information to accurately depict all of the traffic information within range of the aircraft. Due to lack of equipment, poor signal reception, and/or inaccurate information from other aircraft, traffic may be present but not represented on the displays. NOTE: TIS is disabled if a Traffic Advisory System (TAS) is installed.
SYSTEM OVERVIEW HAZARD AVOIDANCE TAS SYMBOLOGY The GTS 800 uses symbology to depict intruding traffic using the symbols shown in Table 6-20. FLIGHT INSTRUMENTS Symbol Description Traffic Advisory EIS Traffic Advisory out of the selected display range. Displayed at outer range ring at proper bearing.
HAZARD AVOIDANCE SYSTEM OVERVIEW TA ALERTING CONDITIONS Sensitivity Intruder Altitude Level Available B Yes B No HAZARD AVOIDANCE No FLIGHT MANAGEMENT A Intruder closing rate provides less than 20 seconds of vertical and horizontal separation. Or: Intruder closing rate provides less than 20 seconds of horizontal separation and vertical separation is within 600 feet. Or: Intruder range is within 0.2 nm and vertical separation is within 600 feet.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW HAZARD AVOIDANCE AUDIO PANEL & CNS EIS Inset Map Displays When TA is Detected FLIGHT MANAGEMENT Figure 6-103 Traffic Annunciation (PFD) Bearing Relative Altitude Distance (nm) “One o’clock” through “Twelve o’clock” or “No Bearing” “High”, “Low”, “Same Altitude” (if within 200 feet of own altitude), or “Altitude not available” “Less than one mile”, “One Mile” through “Ten Miles”, or “More than ten miles” HAZARD AVOIDANCE Table 6-22 TA Descriptive Voice Announ
HAZARD AVOIDANCE SYSTEM OVERVIEW Test Mode Annunciation Operating Mode Non-Threat Traffic at 11 o’clock, Distance 3.6 nm, 1000’ Above, Level FLIGHT INSTRUMENTS Proximity Traffic at 1 o’clock, Distance 3.6 nm, 1000’ Below, Descending EIS TA at 9 o’clock, Distance 2.
SYSTEM OVERVIEW HAZARD AVOIDANCE TRAFFIC MAP PAGE FLIGHT INSTRUMENTS The Traffic Map Page shows surrounding TAS traffic data in relation to the aircraft’s current position and altitude, without basemap clutter. It is the principal map page for viewing traffic information. Aircraft orientation is always heading up unless there is no valid heading. Map range is adjustable with the RANGE Knob, as indicated by the map range rings.
HAZARD AVOIDANCE SYSTEM OVERVIEW Altitude Display The pilot can select the volume of airspace in which non-threat and proximity traffic is displayed. TAs occurring outside of these limits will always be shown. FLIGHT INSTRUMENTS Changing the altitude range: 1) On the Traffic Map Page, select the ALT MODE Softkey. 2) Press one of the following Softkeys: EIS • ABOVE: Displays non-threat and proximity traffic from 9000 feet above the aircraft to 2700 feet below the aircraft.
SYSTEM OVERVIEW HAZARD AVOIDANCE Flight ID Display FLIGHT INSTRUMENTS The Flight IDs of other aircraft (when available) can be enabled for display on the Traffic Map Page (Figure 6-106). When a flight ID is received, it will appear above or below the corresponding traffic symbol on the Traffic Map Page when this option is enabled.
HAZARD AVOIDANCE SYSTEM OVERVIEW Traffic Map Page Display Range The display range on the Traffic Map Page can be changed at any time. Map range is adjustable with the RANGE Knob, as indicated by the map range rings. FLIGHT INSTRUMENTS Changing the display range on the Traffic Map Page: 1) Turn the RANGE Knob.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW HAZARD AVOIDANCE Non-Threat Traffic Traffic Advisory EIS Proximity Traffic TA Off Scale Banner Annunciation Traffic Status Icon AUDIO PANEL & CNS “No Bearing” Traffic Advisory Banner Annunciation Figure 6-108 TAS Traffic on Navigation Map Page FLIGHT MANAGEMENT Customizing the traffic display on the Navigation Map Page: 1) Select the Navigation Map Page. 2) Press the MENU Key. 3) With Map Setup highlighted, press the ENT Key (Figure 6-109).
HAZARD AVOIDANCE SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS Figure 6-109 Navigation Map Page Menu AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 6-110 Navigation Map Page Setup Menu Figure 6-111 Navigation Map Page Setup Menu, Traffic Group HAZARD AVOIDANCE The Navigation Map Page Setup Menu also controls the display of traffic. The setup menu controls the map range settings. Traffic data symbols and labels can be decluttered from the display.
SYSTEM OVERVIEW HAZARD AVOIDANCE SYSTEM STATUS The traffic mode is annunciated in the upper left corner of the Traffic Map Page.
HAZARD AVOIDANCE SYSTEM OVERVIEW 6.8 SKY497 TRAFFIC FLIGHT INSTRUMENTS WARNING: Do not rely solely upon the display of traffic information to accurately depict all of the traffic information within range of the aircraft. Due to lack of equipment, poor signal reception, and/or inaccurate information from other aircraft, traffic may be present but not represented on the displays. NOTE: Refer to the SKY497 Pilot’s Guide for a detailed discussion of this Traffic Advisory System (TAS).
SYSTEM OVERVIEW HAZARD AVOIDANCE OPERATION FLIGHT INSTRUMENTS The unit must be in operating mode for traffic to be displayed. The ability to switch from standby to operating mode on the ground is especially useful for scanning the airspace around the airport before takeoff. Switching from standby mode to operating mode: 1) On the Traffic Page, press the OPERATE Softkey or press the MENU Key and turn the small FMS knob to select Operating Mode.
HAZARD AVOIDANCE SYSTEM OVERVIEW Operating Mode Altitude Mode Traffic Display Range Ring Traffic Advisory, 500’ Below, Climbing EIS “Non-Bearing” Traffic (Bearing Undetermined), Distance 4.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW HAZARD AVOIDANCE Non-Threat Traffic Traffic Advisory EIS Proximity Traffic TA Off Scale Banner Annunciation Traffic Status Icon AUDIO PANEL & CNS “No Bearing” Traffic Advisory Banner Annunciation Figure 6-113 TAS Traffic on Navigation Map Page FLIGHT MANAGEMENT Displaying traffic information (PFD Inset Map): 1) Press the INSET Softkey. 2) Press the TRAFFIC Softkey to display traffic data on the inset map (TRFC-1).
HAZARD AVOIDANCE SYSTEM OVERVIEW ALTITUDE DISPLAY Changing the altitude display mode: FLIGHT INSTRUMENTS 1) On the Traffic Page, press the ALT MODE Softkey. 2) Press one of the following Softkeys: • BELOW • NORMAL • ABOVE EIS • UNREST (unrestricted) 3) To return to the Traffic Page, press the BACK Softkey. AUDIO PANEL & CNS Or: 1) Press the MENU Key.
SYSTEM OVERVIEW HAZARD AVOIDANCE Customizing the traffic display on the Navigation Map Page: 1) Select the Navigation Map Page. FLIGHT INSTRUMENTS 2) Press the MENU Key. 3) With Map Setup highlighted, press the ENT Key (Figure 6-114). 4) Turn the small FMS Knob to select the Traffic Group and press the ENT Key (Figure 6-115). 5) Turn the large FMS Knob or press the ENT Key to scroll through the selections (Figure 6-116).
HAZARD AVOIDANCE SYSTEM OVERVIEW TAS ALERTS NOTE: Refer to the TAS documentation for information on alerts generated by the TAS equipment. FLIGHT INSTRUMENTS When the number of TAs on the Traffic Map Page increases from one scan to the next, the following occur: • A “Traffic, Traffic” voice alert is generated. • A TRAFFIC Annunciation appears at the top right of the airspeed on the PFD, flashing for 5 seconds and remaining displayed until no TAs are detected in the area.
SYSTEM OVERVIEW HAZARD AVOIDANCE If the unit fails, an annunciation as to the cause of the failure is shown in the center of the Traffic Map Page.
AUTOMATIC FLIGHT CONTROL SYSTEM SYSTEM OVERVIEW SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM 7.1 GARMIN AFCS FLIGHT INSTRUMENTS NOTE: The approved Pilot’s Operating Handbook (POH) always supersedes this Pilot’s Guide. The digital Garmin Automatic Flight Control System (AFCS) is fully integrated within the G1000 System avionics architecture. The System Overview section provides a block diagram to support this system description.
SYSTEM OVERVIEW AUTOMATIC FLIGHT CONTROL SYSTEM BASIC AUTOPILOT OPERATION FLIGHT INSTRUMENTS This section provides an overview for autopilot engagement and disengagement. A more detailed description follows in the Autopilot and Yaw Damper Operation section. • Autopilot Engagement — The autopilot may be engaged by pushing the AP Key on the AFCS Control Unit. Annunciations regarding the engagement are indicated on the PFD.
AUTOMATIC FLIGHT CONTROL SYSTEM SYSTEM OVERVIEW GARMIN AFCS CONTROLS The AFCS Control Unit is positioned below the MFD, and has the following controls: Selects/deselects Heading Select Mode 4 NAV Key FD Key 5 XFR Key Selects/deselects Navigation Mode Activates/deactivates the flight director only Pressing once turns on the selected flight director in the default vertical and lateral modes. Pressing again deactivates the flight director and removes the Command Bars.
SYSTEM OVERVIEW AUTOMATIC FLIGHT CONTROL SYSTEM The following AFCS controls are located separately from the AFCS Control Unit: FLIGHT INSTRUMENTS AP DISC Switch (Autopilot Disconnect) EIS CWS Button (Control Wheel Steering) Disengages the autopilot, yaw damper, and flight director and interrupts pitch trim operation. An AP DISC Switch is located on each control wheel. This switch may be used to acknowledge an autopilot disconnect alert and mute the associated aural tone.
AUTOMATIC FLIGHT CONTROL SYSTEM SYSTEM OVERVIEW FLIGHT DIRECTOR OPERATION FLIGHT INSTRUMENTS The flight director function provides pitch and roll commands to the AFCS and displays them on the PFDs. With the flight director active, the aircraft can be hand-flown to follow the path shown by the Command Bars. Maximum commanded pitch (-15°, +16°) and roll (22°) angles, vertical acceleration, and roll rate are limited to values established during AFCS certification.
SYSTEM OVERVIEW AUTOMATIC FLIGHT CONTROL SYSTEM AFCS STATUS BOX FLIGHT INSTRUMENTS Flight director mode annunciations are displayed on the PFDs when the flight director is active. Flight director selection and autopilot and yaw damper statuses are shown in the center of the AFCS Status Box. Lateral flight director modes are displayed on the left and vertical on the right. Armed modes are displayed in white and active in green.
AUTOMATIC FLIGHT CONTROL SYSTEM SYSTEM OVERVIEW FLIGHT INSTRUMENTS If the information required to compute a flight director mode becomes invalid or unavailable, the flight director automatically reverts to the default mode for that axis. A flashing yellow mode annunciation and annunciator light indicate loss of sensor (ADC) or navigation data (VOR, LOC, GPS, VNV, SBAS) required to compute commands.
SYSTEM OVERVIEW AUTOMATIC FLIGHT CONTROL SYSTEM VERTICAL MODES FLIGHT INSTRUMENTS Table 7-2 lists the vertical modes with their corresponding controls and annunciations. The mode reference is displayed next to the active mode annunciation for Altitude Hold, Vertical Speed, and Flight Level Change modes. The NOSE UP/DN Wheel can be used to change the vertical mode reference while operating under Pitch Hold, Vertical Speed, or Flight Level Change Mode.
AUTOMATIC FLIGHT CONTROL SYSTEM SYSTEM OVERVIEW PITCH HOLD MODE (PIT) FLIGHT INSTRUMENTS When the flight director is activated (the FD Key is pressed) or switched (the XFR Key is pressed), Pitch Hold Mode is selected by default. Pitch Hold Mode is indicated as the active vertical mode by the ‘PIT’ annunciation. This mode may be used for climb or descent to the Selected Altitude (shown above the Altimeter), since Selected Altitude Capture Mode is automatically armed when Pitch Hold Mode is activated.
SYSTEM OVERVIEW AUTOMATIC FLIGHT CONTROL SYSTEM SELECTED ALTITUDE CAPTURE MODE (ALTS) FLIGHT INSTRUMENTS Selected Altitude Capture Mode is automatically armed with activation of the following modes: • Pitch Hold • Go Around • Vertical Speed • Vertical Path Tracking (if the Selected Altitude is to be captured instead of the VNV Target Altitude) • Flight Level Change EIS The white ‘ALTS’ annunciation indicates Selected Altitude Capture Mode is armed (see Figure 7-6 for example).
AUTOMATIC FLIGHT CONTROL SYSTEM SYSTEM OVERVIEW ALTITUDE HOLD MODE (ALT) FLIGHT INSTRUMENTS Altitude Hold Mode can be activated by pressing the ALT Key; the flight director maintains the current aircraft altitude (to the nearest 10 feet) as the Altitude Reference. The flight director’s Altitude Reference, shown in the AFCS Status Box, is independent of the Selected Altitude, displayed above the Altimeter. Altitude Hold Mode active is indicated by a green ‘ALT’ annunciation in the AFCS Status Box.
SYSTEM OVERVIEW AUTOMATIC FLIGHT CONTROL SYSTEM FLIGHT INSTRUMENTS When Vertical Speed Mode is activated by pressing the VS Key, ‘VS’ is annunciated in green in the AFCS Status Box along with the Vertical Speed Reference. The Vertical Speed Reference is also displayed above the Vertical Speed Indicator. A Vertical Speed Reference Bug corresponding to the Vertical Speed Reference is shown on the indicator.
AUTOMATIC FLIGHT CONTROL SYSTEM SYSTEM OVERVIEW The Airspeed Reference is set to the current airspeed upon mode activation. Flight Level Change Mode is indicated by a green ‘FLC’ annunciation beside the Airspeed Reference in the AFCS Status Box. The Airspeed Reference is also displayed directly above the Airspeed Indicator, along with a bug corresponding to the Airspeed Reference along the tape.
SYSTEM OVERVIEW AUTOMATIC FLIGHT CONTROL SYSTEM VERTICAL NAVIGATION MODES (VPTH, ALTV) NOTE: VNV is disabled when parallel track or Dead Reckoning Mode is active. Refer to the Flight Management FLIGHT INSTRUMENTS Section for more information on VNV flight plans. NOTE: The Selected Altitude takes precedence over any other vertical constraints. Vertical Navigation (VNV) flight control is available for enroute/terminal cruise and descent operations when VNV flight planning is available.
AUTOMATIC FLIGHT CONTROL SYSTEM SYSTEM OVERVIEW Prior to descent path interception, the Selected Altitude must be set below the current aircraft altitude by at least 75 feet.
SYSTEM OVERVIEW AUTOMATIC FLIGHT CONTROL SYSTEM When a descent leg is captured (i.e., vertical deviation becomes valid), Vertical Path Tracking becomes active and tracks the descent profile (Figure 7-13). An altitude capture mode (‘ALTS’ or ‘ALTV’) is armed as appropriate.
AUTOMATIC FLIGHT CONTROL SYSTEM SYSTEM OVERVIEW Non-Path Descents FLIGHT INSTRUMENTS Pitch Hold, Vertical Speed, and Flight Level Change modes can also be used to fly non-path descents while VNV flight control is selected. If the VS or FLC Key is pressed while Vertical Path Tracking Mode is selected, Vertical Path Tracking Mode reverts to armed along with the appropriate altitude capture mode to allow profile re-capture.
SYSTEM OVERVIEW AUTOMATIC FLIGHT CONTROL SYSTEM FLIGHT INSTRUMENTS At 50 feet from the VNV Target Altitude, the flight director automatically transitions from VNV Target Altitude Capture to Altitude Hold Mode and tracks the level leg. As Altitude Hold Mode becomes active, the white ‘ALT’ annunciation moves to the active vertical mode field and flashes green for 10 seconds to indicate the automatic transition.
AUTOMATIC FLIGHT CONTROL SYSTEM SYSTEM OVERVIEW Upon reaching the glidepath, the flight director transitions to Glidepath Mode and begins to capture and track the glidepath. FLIGHT INSTRUMENTS Figure 7-16 Glidepath Mode Armed Once the following conditions have been met, the glidepath can be captured: • The active waypoint is at or after the final approach fix (FAF). • Vertical deviation is valid.
SYSTEM OVERVIEW AUTOMATIC FLIGHT CONTROL SYSTEM GLIDESLOPE MODE (GS) NOTE: Pressing the CWS Button while Glideslope Mode is active does not cancel the mode. The autopilot FLIGHT INSTRUMENTS guides the aircraft back to the glideslope upon release of the CWS Button. Glideslope Mode is available for LOC/ILS approaches to capture and track the glideslope. When Glideslope Mode is armed (annunciated as ‘GS’ in white), LOC Approach Mode is armed as the lateral flight director mode.
AUTOMATIC FLIGHT CONTROL SYSTEM SYSTEM OVERVIEW TAKEOFF (TO) AND GO AROUND (GA) MODES FLIGHT INSTRUMENTS In Takeoff and Go Around modes, the flight director commands a constant set pitch attitude. The GA Switch is used to select both modes. The mode entered by the flight director depends on whether the aircraft is on the ground. Selected Altitude Capture Mode is automatically armed when the aircraft is at least 400 feet below the Selected Altitude at the time Takeoff or Go Around Mode is selected.
SYSTEM OVERVIEW AUTOMATIC FLIGHT CONTROL SYSTEM LATERAL MODES FLIGHT INSTRUMENTS The following table relates each AFCS lateral mode to its respective control and annunciation. Refer to the vertical modes section for information regarding Takeoff and Go Around modes. NOTE: The AFCS may generate a lower bank angle than the maximum roll command limit in degrees indicated in Table 7-3 by the amount needed to produce a turn rate equal to or less than standard rate.
AUTOMATIC FLIGHT CONTROL SYSTEM SYSTEM OVERVIEW ROLL HOLD MODE (ROL) NOTE: If Roll Hold Mode is activated as a result of a mode reversion, the flight director rolls wings level. FLIGHT INSTRUMENTS When the flight director is activated or switched, Roll Hold Mode is selected by default. This mode is annunciated as ‘ROL’ in the AFCS Status Box. The current aircraft bank angle is held, subject to the bank angle condition.
SYSTEM OVERVIEW AUTOMATIC FLIGHT CONTROL SYSTEM HEADING SELECT MODE (HDG) FLIGHT INSTRUMENTS Heading Select Mode is activated by pressing the HDG Key. Heading Select Mode acquires and maintains the Selected Heading. The Selected Heading is shown by a cyan bug on the HSI and in the box to the upper left of the HSI. NOTE: Pressing the HDG Knob synchronizes the Selected Heading to the current heading. EIS The Selected Heading is adjusted using the HDG Knob.
AUTOMATIC FLIGHT CONTROL SYSTEM SYSTEM OVERVIEW If the Course Deviation Indicator (CDI) shows greater than one dot when the NAV Key is pressed, the selected mode is armed. If the CDI is less than one dot, Navigation Mode is automatically captured when the NAV Key is pressed. The armed annunciation appears in white to the left of the active lateral mode.
SYSTEM OVERVIEW AUTOMATIC FLIGHT CONTROL SYSTEM APPROACH MODES (GPS, VAPP, LOC) NOTE: The selected navigation receiver must have a valid VOR or LOC signal or active GPS course for the FLIGHT INSTRUMENTS flight director to enter Approach Mode. EIS Approach Mode is activated when the APR Key is pressed. Approach Mode acquires and tracks the selected navigation source (GPS, VOR, or LOC), depending on loaded approach.
AUTOMATIC FLIGHT CONTROL SYSTEM SYSTEM OVERVIEW 2) Ensure a LOC/ILS approach is loaded into the active flight plan. 3) Ensure the corresponding LOC frequency is tuned. 4) Press the APR Key.
SYSTEM OVERVIEW AUTOMATIC FLIGHT CONTROL SYSTEM If the navigation source is VOR or localizer or OBS Mode has been enabled when using GPS, the Selected Course is controlled using the CRS Knob corresponding to the selected flight director (CRS1 for the pilot side, CRS2 for the copilot side). FLIGHT INSTRUMENTS Pressing the CWS Button and hand-flying the aircraft does not reset any reference data while in Backcourse Mode.
AUTOMATIC FLIGHT CONTROL SYSTEM SYSTEM OVERVIEW When the autopilot is not engaged, the pitch trim servo may be used to provide manual electric pitch trim (MEPT). This allows the aircraft to be trimmed using a control wheel switch rather than the trim wheel. Manual trim commands are generated only when both halves of the MEPT Switch are operated simultaneously. Trim speeds are scheduled with airspeed to provide more consistent response.
SYSTEM OVERVIEW DISENGAGEMENT FLIGHT INSTRUMENTS AUTOMATIC FLIGHT CONTROL SYSTEM The autopilot may be manually disengaged by pushing the AP DISC, MEPT Switch, or the AP Key on the AFCS Control Unit. Manual disengagement is indicated by a five-second flashing yellow ‘AP’ annunciation and a three-second autopilot disconnect aural alert. The AP DISC or MEPT Switch may be used to cancel the aural alert. NOTE: Pressing the AP Key does not disengage the yaw damper.
AUTOMATIC FLIGHT CONTROL SYSTEM SYSTEM OVERVIEW director revert to LVL mode for pitch and roll (Figure 7-34). While in level mode, all other modes are available by pressing the corresponding button. Roll Pitch FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Command Bars Indicate Level with the Horizon Figure 7-34 Level Mode Annunciation HAZARD AVOIDANCE UNDERSPEED PROTECTION Underspeed Protection is available when the autopilot is on.
SYSTEM OVERVIEW AUTOMATIC FLIGHT CONTROL SYSTEM ALTITUDE-CRITICAL MODES (ALT, GS, GP, TO, GA, FLC) FLIGHT INSTRUMENTS If the aircraft decelerates to stall warning, the lateral and vertical flight director modes will change from active to armed (Figure 7-36), and the autopilot will provide input causing the aircraft to pitch down and the wings to level.
AUTOMATIC FLIGHT CONTROL SYSTEM SYSTEM OVERVIEW FLAP CONFIGURATION TRIM (FCT) FLIGHT INSTRUMENTS The Flap Configuration Trim (FCT) feature automatically adjusts Pitch Trim when flap settings are changed. FCT becomes operational when the aircraft is in the air, autopilot is disengaged, and the flap setting is more than 2 degrees. FCT can be inhibited by pressing and holding the AP DISC Switch. FCT will again become active when the AP DISC Switch is released.
SYSTEM OVERVIEW c) Press the AP Key to engage the autopilot in a climb, holding the pitch angle commanded in Takeoff Mode and wings level. FLIGHT INSTRUMENTS AUTOMATIC FLIGHT CONTROL SYSTEM 2) In this example, Vertical Speed Mode is used to capture the Selected Altitude (Pitch Hold, Vertical Speed, or Flight Level Change Mode may be used). a) Press the VS Key to activate Vertical Speed Mode.
AUTOMATIC FLIGHT CONTROL SYSTEM SYSTEM OVERVIEW INTERCEPTING A VOR RADIAL FLIGHT INSTRUMENTS During climb-out, the autopilot continues to fly the aircraft in Heading Select Mode. Airway V4 to Salina VOR (SLN) should now be intercepted. Since the enroute flight plan waypoints correspond to VORs, flight director Navigation Mode using either VOR or GPS as the navigation source may be used. In this scenario, VOR Navigation Mode is used for navigation to the first VOR waypoint in the flight plan.
SYSTEM OVERVIEW AUTOMATIC FLIGHT CONTROL SYSTEM FLYING A FLIGHT PLAN/GPS COURSE NOTE: Changing the navigation source cancels Navigation Mode and causes the flight director to revert FLIGHT INSTRUMENTS back to Roll Hold Mode (wings rolled level). As the aircraft closes on Salina VOR, GPS is used to navigate the next leg, airway V244. The aircraft is currently tracking inbound on Airway V4.
AUTOMATIC FLIGHT CONTROL SYSTEM SYSTEM OVERVIEW Flight Level Change descent: 1) Select Flight Level Change Mode: FLIGHT INSTRUMENTS a) Use the ALT SEL Knob on the AFCS Controller, or the ALT Knob on the PFD, to set the Selected Altitude to 10,000 feet. b) Press the FLC Key to activate Flight Level Change Mode. The annunciation ‘FLC’ appears next to the Airspeed Reference, which defaults to the current aircraft airspeed. Selected Altitude Capture Mode is armed automatically.
SYSTEM OVERVIEW AUTOMATIC FLIGHT CONTROL SYSTEM c) If Vertical Path Tracking Mode is armed more than 5 minutes prior to descent path capture, acknowledgment is required for the flight director to transition from Altitude Hold to Vertical Path Tracking Mode.
AUTOMATIC FLIGHT CONTROL SYSTEM SYSTEM OVERVIEW 2) Reduce power to allow descent in Flight Level Change Mode. The autopilot maintains the Airspeed Reference. 3) As the aircraft nears the Selected Altitude, the flight director transitions to Selected Altitude Capture Mode, indicated by the green ‘ALTS’ annunciation flashing for up to 10 seconds.
SYSTEM OVERVIEW AUTOMATIC FLIGHT CONTROL SYSTEM APPROACH NOTE: If an approach contains a DME arc, the arc must be flown in Navigation Mode with the AFCS. When FLIGHT INSTRUMENTS receiving vectors from ATC, Navigation Mode must be selected prior to intercepting the ARC. Flying an ILS approach: 1) Transition from GPS Navigation Mode to Heading Select Mode. EIS a) Select the Runway 35L ILS approach for KCOS and select ‘VECTORS’ for the transition. Load and activate the approach into the flight plan.
AUTOMATIC FLIGHT CONTROL SYSTEM SYSTEM OVERVIEW KCOS FLIGHT INSTRUMENTS LOC APR/ GS Mode 3 PETEY 2 G EIS HD e od M PYNON 1 AUDIO PANEL & CNS FLIGHT MANAGEMENT GPS NAV Mode HAZARD AVOIDANCE Figure 7-46 ILS Approach to KCOS Flying an RNAV GPS approach with vertical guidance: AFCS 1) Arm flight director modes for a RNAV GPS approach with vertical guidance: a) Make sure the navigation source is set to GPS (use CDI Softkey to change navigation source).
SYSTEM OVERVIEW AUTOMATIC FLIGHT CONTROL SYSTEM 4) There are two options available at this point, as the autopilot flies the approach: • Push the AP DISC Switch at the decision height and land the aircraft. FLIGHT INSTRUMENTS • Use the GA Switch to execute a missed approach.
AUTOMATIC FLIGHT CONTROL SYSTEM SYSTEM OVERVIEW GO AROUND/MISSED APPROACH NOTE: As a result of calculations performed by the system while flying the holding pattern, the display may FLIGHT INSTRUMENTS re-size automatically and the aircraft may not precisely track the holding pattern as depicted on the PFD and MFD. Flying a missed approach: EIS 1) Push the GA Switch at the Decision height and apply go around power to execute a missed approach.
SYSTEM OVERVIEW AUTOMATIC FLIGHT CONTROL SYSTEM FLIGHT INSTRUMENTS 4 MOGAL EIS GPS NAV Mode AUDIO PANEL & CNS 3 2 FLIGHT MANAGEMENT GA Mode KCOS HAZARD AVOIDANCE 1 INDEX APPENDICES ADDITIONAL FEATURES AFCS Figure 7-48 Go Around/Missed Approach 440 Garmin G1000 Pilot’s Guide for the Quest KODIAK® 100 190-00590-07 Rev.
AUTOMATIC FLIGHT CONTROL SYSTEM SYSTEM OVERVIEW AFCS ANNUNCIATIONS AND ALERTS AFCS STATUS ALERTS FLIGHT INSTRUMENTS The annunciations in Table 7-5 (listed in order of increasing priority) can appear on the PFDs above the Airspeed and Attitude indicators. Only one annunciation may occur at a time, and messages are prioritized by criticality.
SYSTEM OVERVIEW OVERSPEED PROTECTION FLIGHT INSTRUMENTS While Pitch Hold, Vertical Speed, Flight Level Change, Vertical Path Tracking, or an altitude capture mode is active, airspeed is monitored by the flight director. Pitch commands are not changed until overspeed protection becomes active. Overspeed protection is provided in situations where the flight director cannot acquire and maintain the mode reference for the selected vertical mode without exceeding Vmo.
AUTOMATIC FLIGHT CONTROL SYSTEM SYSTEM OVERVIEW ABNORMAL OPERATION SUSPECTED AUTOPILOT MALFUNCTION FLIGHT INSTRUMENTS NOTE: Consult the aircraft documentation for the location of circuit breakers as well as specifics that may supplement or amplify this procedure. If an autopilot failure or trim failure is suspected to have occurred, perform the following steps: 1) Firmly grasp the control wheel. EIS 2) Press and hold the AP DISC Switch.
SYSTEM OVERVIEW AUTOMATIC FLIGHT CONTROL SYSTEM 7.2 S-TEC FIFTY FIVE X AUTOPILOT (OPTIONAL) FLIGHT INSTRUMENTS NOTE: This section covers only the additional ‘AP’, ‘YD’, and ‘FD’ status annunciations that may appear in the G1000 AFCS Status Box. These status annunciations are not analogous to both the G1000 and the S-TEC Fifty Five X. Refer to the approved S-TEC Fifty Five X Pilot’s Operating Handbook (POH) for a comprehensive list of annunciations and operating instructions.
ADDITIONAL FEATURES SYSTEM OVERVIEW SECTION 8 ADDITIONAL FEATURES NOTE: With the availability of SafeTaxi®, ChartView, or FliteCharts®, it may be necessary to carry another FLIGHT INSTRUMENTS source of charts on-board the aircraft.
SYSTEM OVERVIEW ADDITIONAL FEATURES 8.1 SYNTHETIC VISION TECHNOLOGY (SVT™) FLIGHT INSTRUMENTS WARNING: Use appropriate primary systems for navigation, and for terrain, obstacle, and traffic avoidance. SVT is intended as an aid to situational awareness only and may not provide either the accuracy or reliability upon which to solely base decisions and/or plan maneuvers to avoid terrain, obstacles, or traffic.
ADDITIONAL FEATURES SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 8-1 Synthetic Vision Imagery SVT OPERATION HAZARD AVOIDANCE SVT is activated from the PFD using the softkeys located along the bottom edge of the display. Pressing the softkeys turns the related function on or off. When SVT is enabled, the pitch scale increments are reduced to 10 degrees up and 7.5 degrees down. AFCS SVT functions are displayed on three levels of softkeys.
SYSTEM OVERVIEW ADDITIONAL FEATURES FLIGHT INSTRUMENTS PFD SYN VIS BACK Pressing the BACK Softkey returns to the top-level softkeys. BACK EIS PATHWAY SYN TERR HRZN HDG APTSIGNS AUDIO PANEL & CNS Pressing the BACK Softkey returns to the previous level of softkeys. Figure 8-2 SVT Softkeys Enabling and disabling SVT: FLIGHT MANAGEMENT 1) Press the PFD Softkey. 2) Press the SYN VIS Softkey. 3) Press the SYN TERR Softkey. The SVT display will cycle on or off with the SYN TERR Softkey.
ADDITIONAL FEATURES SYSTEM OVERVIEW SVT FEATURES Pathways Color Matches CDI Indicating NAV Source Flight Path Marker Airplane Symbol EIS Zero Pitch Line (ZPL) with Compass Heading Marks AUDIO PANEL & CNS Synthetic Terrain FLIGHT MANAGEMENT Figure 8-3 SVT on the Primary Flight Display HAZARD AVOIDANCE SVT Softkeys FLIGHT INSTRUMENTS Selected Altitude Airport Runway NOTE: Pathways and terrain features are not a substitute for standard course and altitude deviation information provided by the
SYSTEM OVERVIEW ADDITIONAL FEATURES FLIGHT INSTRUMENTS Selected Altitude FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS Programmed Altitudes HAZARD AVOIDANCE Figure 8-4 Programmed and Selected Altitude AFCS Pathways provide supplemental glidepath/glideslope information on an active ILS, LPV, LNAV/VNAV, LP, and some LNAV approaches. Pathways are intended as an aid to situational awareness and should not be used independent of the CDI, VDI, glide path indicator, and glide slope indicator.
ADDITIONAL FEATURES SYSTEM OVERVIEW Descent and Approach FLIGHT INSTRUMENTS Pathways are shown descending only for a programmed descent (Figures 8-5, 8-6). When the flight plan includes programmed descent segments, pathways are displayed along the descent path provided that the selected altitude is lower than the programmed altitude.
SYSTEM OVERVIEW ADDITIONAL FEATURES Missed Approach FLIGHT INSTRUMENTS Upon activating the missed approach, pathways lead to the Missed Approach Holding Point (MAHP) and are displayed as a level path at the published altitude for the MAHP, or the selected altitude, whichever is the highest. If the initial missed approach leg is a Course-to-Altitude (CA) leg, the pathways boxes will be displayed level at the altitude published for the MAHP.
ADDITIONAL FEATURES SYSTEM OVERVIEW FLIGHT PATH MARKER FLIGHT INSTRUMENTS The Flight Path Marker (FPM), also known as a Velocity Vector, is displayed on the PFD at groundspeeds above 30 knots. The FPM depicts the approximate projected path of the aircraft accounting for wind speed and direction relative to the three-dimensional terrain display. The FPM is always available when the Synthetic Terrain feature is in operation.
SYSTEM OVERVIEW ADDITIONAL FEATURES HORIZON HEADING FLIGHT INSTRUMENTS The Horizon Heading is synchronized with the HSI and shows approximately 60 degrees of compass heading in 30‑degree increments on the Zero Pitch Line. Horizon Heading tick marks and digits appearing on the zero pitch line are not visible behind either the airspeed or altitude display. Horizon Heading is used for general heading awareness, and is activated and deactivated by pressing the HRZN HDG Softkey.
ADDITIONAL FEATURES SYSTEM OVERVIEW RUNWAYS WARNING: Do not use SVT runway depiction as the sole means for determining the proximity of the aircraft FLIGHT INSTRUMENTS to the runway or for maintaining the proper approach path angle during landing. NOTE: Not all airports have runways with endpoint data in the database, therefore, these runways are not displayed. EIS Runway data provides improved awareness of runway location with respect to the surrounding terrain.
SYSTEM OVERVIEW ADDITIONAL FEATURES TAWS ALERTING FLIGHT INSTRUMENTS Terrain alerting on the synthetic terrain display is triggered by Forward-looking Terrain Avoidance (FLTA) alerts, and corresponds to the red and yellow X symbols on the Inset Map and MFD map displays. For more detailed information regarding TAWS, refer to the Hazard Avoidance Section. In some instances, a terrain or obstacle alert may be issued with no conflict shading displayed on the synthetic terrain.
ADDITIONAL FEATURES SYSTEM OVERVIEW FLIGHT INSTRUMENTS Obstacles are represented on the synthetic terrain display by standard two-dimensional tower symbols found on the Inset map and MFD maps and charts. Obstacle symbols appear in the perspective view with relative height above terrain and distance from the aircraft.
SYSTEM OVERVIEW ADDITIONAL FEATURES FIELD OF VIEW FLIGHT INSTRUMENTS The PFD field of view can be represented on the MFD Navigation Map Page. Two dashed lines forming a V‑shape in front of the aircraft symbol on the map represent the forward viewing area shown on the PFD. Configuring field of view: 1) While viewing the Navigation Map Page, press the MENU Key to display the PAGE MENU. FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS 2) Turn the large FMS Knob to highlight Map Setup and press the ENT Key.
ADDITIONAL FEATURES SYSTEM OVERVIEW The following figure compares the PFD forward looking depiction with the MFD plan view and FIELD OF VIEW turned on. FLIGHT INSTRUMENTS Lines Depict PFD Field of View EIS AUDIO PANEL & CNS SVT View on the PFD Field of View on the MFD Figure 8-13 PFD and MFD Field of View Comparison FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00590-07 Rev.
SYSTEM OVERVIEW ADDITIONAL FEATURES 8.2 SAFETAXI FLIGHT INSTRUMENTS SafeTaxi® is an enhanced feature that gives greater map detail when viewing airports at close range. The maximum map ranges for enhanced detail are pilot configurable. When viewing at ranges close enough to show the airport detail, the map reveals taxiways with identifying letters/numbers, airport Hot Spots, and airport landmarks including ramps, buildings, control towers, and other prominent features.
ADDITIONAL FEATURES SYSTEM OVERVIEW FLIGHT INSTRUMENTS Taxiway Identification EIS Aircraft Position Airport Hot Spot Outline AUDIO PANEL & CNS Airport Features FLIGHT MANAGEMENT Figure 8-14 SafeTaxi Depiction on the Navigation Map Page DCLTR Softkey Removes Taxiway Markings HAZARD AVOIDANCE The DCLTR Softkey (declutter) label advances to DCLTR-1, DCLTR-2, and DCLTR-3 each time the softkey is pressed for easy recognition of decluttering level.
SYSTEM OVERVIEW ADDITIONAL FEATURES 3) Turn the FMS Knob to select the Aviation Group and press the ENT Key. 4) Turn the large FMS Knob to scroll through the Aviation Group options to SAFETAXI. FLIGHT INSTRUMENTS 5) Turn the small FMS Knob to display the range of distances. 6) Turn either FMS Knob to select the desired distance for maximum SafeTaxi display range. 7) Press the ENT Key to complete the selection. AUDIO PANEL & CNS EIS 8) Press the FMS Knob to return to the Navigation Map Page.
ADDITIONAL FEATURES SYSTEM OVERVIEW SAFETAXI CYCLE NUMBER AND REVISION FLIGHT INSTRUMENTS SafeTaxi database is revised every 56 days. SafeTaxi is always available for use after the expiration date. When turning on the system, the Power-up Page indicates whether the databases are current, out of date, or not available. SafeTaxi Database EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 8-17 Power-up Page, SafeTaxi Database Power-up Page Display HAZARD AVOIDANCE Definition Normal operation.
SYSTEM OVERVIEW ADDITIONAL FEATURES The SafeTaxi Region, Version, Cycle, Effective date and Expires date of the database cycle can also be found on the AUX - System Status page, as seen in Figure 8-18. FLIGHT INSTRUMENTS Select the MFD1 DB Softkey to place the cursor in the DATABASE window. Scroll through the listed information by turning the FMS Knob or pressing the ENT Key until the SafeTaxi database information is shown.
ADDITIONAL FEATURES SYSTEM OVERVIEW Select the PFD1 DB Softkey. The softkey label will change to PFD2 DB. The DATABASE window will now display database information for PFD2. Again, scroll through the listed information by turning the FMS Knob or pressing the ENT Key until the SafeTaxi database information is shown. FLIGHT INSTRUMENTS Refer to Updating Garmin Databases in Appendix B for instructions on revising the SafeTaxi database.
SYSTEM OVERVIEW ADDITIONAL FEATURES 8.3 CHARTVIEW FLIGHT INSTRUMENTS ChartView resembles the paper version of Jeppesen terminal procedures charts. The charts are displayed in full color with high-resolution. The MFD depiction shows the aircraft position on the moving map in the planview of approach charts and on airport diagrams. Airport Hot Spots are outlined in magenta.
ADDITIONAL FEATURES SYSTEM OVERVIEW CHARTVIEW SOFTKEYS FLIGHT INSTRUMENTS ChartView functions are displayed on three levels of softkeys. While on the Navigation Map Page, Nearest Airports Page, or Flight Plan Page, pressing the SHW CHRT Softkey displays the available terminal chart and advances to the chart selection level of softkeys: CHRT OPT, CHRT, INFO-1, DP, STAR, APR, WX, NOTAM, and GO BACK. The chart selection softkeys shown below appear on the Airport Information Page.
SYSTEM OVERVIEW ADDITIONAL FEATURES TERMINAL PROCEDURES CHARTS Selecting Terminal Procedures Charts: FLIGHT INSTRUMENTS While viewing the Navigation Map Page, Nearest Airport Page, or Flight Plan Page, press the SHW CHRT Softkey. Or: 1) Press the MENU Key to display the PAGE MENU. 2) Turn the large FMS Knob to scroll through the OPTIONS Menu to Show Chart. HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS 3) Press the ENT Key to display the chart.
ADDITIONAL FEATURES SYSTEM OVERVIEW When a chart is not available by pressing the SHW CHRT Softkey or selecting a Page Menu Option, charts may be obtained for other airports from the WPT Pages or Flight Plan Pages. FLIGHT INSTRUMENTS If a chart is available for the destination airport, or the airport selected in the active flight plan, the chart appears on the screen.
SYSTEM OVERVIEW ADDITIONAL FEATURES While the APPROACH Box is selected using the FMS Knob, the G1000 softkeys are blank. Once the desired chart is selected, the chart scale can be changed and the chart page can be scrolled using the Joystick. Pressing the Joystick centers the chart on the screen. FLIGHT INSTRUMENTS The aircraft symbol is shown on the chart only if the chart is to scale and the aircraft position is within the boundaries of the chart.
ADDITIONAL FEATURES SYSTEM OVERVIEW Pressing the INFO-1 or INFO-2 Softkey returns to the airport diagram chart when the view is on a terminal procedure chart. If the displayed chart is the airport diagram chart, pressing the INFO-1 or INFO-2 Softkey returns to the Airport Information Page. FLIGHT INSTRUMENTS The aircraft position is shown in magenta on the ChartView diagrams when the location of the aircraft is within the chart boundaries.
SYSTEM OVERVIEW ADDITIONAL FEATURES FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS In the example shown in Figure 8-27, the Class B Chart is selected. Pressing the ENT Key displays the Charlotte Class B Airspace Chart (Figure 8-28). HAZARD AVOIDANCE Figure 8-28 Airport Information Page, Class B Chart Selected from INFO View Pressing the DP Softkey displays the Departure Procedure Chart if available.
ADDITIONAL FEATURES SYSTEM OVERVIEW Pressing the STAR Softkey displays the Standard Terminal Arrival Chart if available. FLIGHT INSTRUMENTS Chart Not To Scale EIS Change Range and Scroll Through the Chart With the Joystick AUDIO PANEL & CNS FLIGHT MANAGEMENT Aircraft Not Shown Icon Figure 8-30 Arrival Information Page HAZARD AVOIDANCE Pressing the APR Softkey displays the approach chart for the airport if available. AFCS ADDITIONAL FEATURES APPENDICES 190-00590-07 Rev.
SYSTEM OVERVIEW ADDITIONAL FEATURES EIS FLIGHT INSTRUMENTS Pressing the WX Softkey shows the airport weather frequency information, and includes weather data such as METAR and TAF from the XM Data Link Receiver, when available. Weather information is available only when an XM Data Link Receiver is installed and the SiriusXM Weather subscription is current.
ADDITIONAL FEATURES SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT NOTAM Softkey Appears for Selected Airports Figure 8-33 NOTAM Softkey Highlighted HAZARD AVOIDANCE Local NOTAM on This Airport AFCS ADDITIONAL FEATURES APPENDICES NOTAM Softkey Selected Figure 8-34 Airport Information Page, Local NOTAMs INDEX Pressing the NOTAM Softkey again removes the NOTAMS information.
SYSTEM OVERVIEW ADDITIONAL FEATURES CHART OPTIONS Pressing the CHRT OPT Softkey displays the next level of softkeys, the chart options level (Figure 8-21). EIS FLIGHT INSTRUMENTS Pressing the ALL Softkey shows the complete approach chart on the screen. HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS Complete Chart Shown INDEX APPENDICES ADDITIONAL FEATURES AFCS Figure 8-35 Approach Information Page, ALL View 476 Garmin G1000 Pilot’s Guide for the Quest KODIAK® 100 190-00590-07 Rev.
ADDITIONAL FEATURES SYSTEM OVERVIEW Pressing the HEADER Softkey shows the header view (approach chart briefing strip) on the screen. FLIGHT INSTRUMENTS EIS Approach Chart Briefing Strip AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 8-36 Approach Information Page, Header View HAZARD AVOIDANCE Pressing the PLAN Softkey shows the approach chart two dimensional plan view.
SYSTEM OVERVIEW ADDITIONAL FEATURES EIS FLIGHT INSTRUMENTS Pressing the PROFILE Softkey displays the approach chart descent profile strip. FLIGHT MANAGEMENT AUDIO PANEL & CNS Approach Chart Descent Profile Strip Figure 8-38 Approach Information Page, Profile View, Full Screen Width ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Pressing the MINIMUMS Softkey displays the minimum descent altitude/visibility strip at the bottom of the approach chart.
ADDITIONAL FEATURES SYSTEM OVERVIEW If the chart scale has been adjusted to view a small area of the chart, pressing the FIT WIDTH Softkey changes the chart size to fit the available screen width. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES Press FIT WDTH Softkey to Show Full Chart Width Figure 8-40 Airport Information Page, FIT WDTH Softkey Pressed APPENDICES INDEX 190-00590-07 Rev.
SYSTEM OVERVIEW ADDITIONAL FEATURES Pressing the FULL SCN Softkey alternates between removing and replacing the data window to the right. Selecting Additional Information: FLIGHT INSTRUMENTS 1) While viewing the Airport Taxi Diagram, press the FULL SCN Softkey to display the information windows (AIRPORT, INFO). 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the AIRPORT, INFO, RUNWAYS, or FREQUENCIES Box (INFO Box shown).
ADDITIONAL FEATURES SYSTEM OVERVIEW Selecting full screen On or Off: 1) While viewing a terminal chart press the MENU Key to display the Page Menu OPTIONS. 2) Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key. FLIGHT INSTRUMENTS 3) Turn the large FMS Knob to move between the FULL SCREEN and COLOR SCHEME Options. 4) Turn the small FMS Knob to choose between the On and Off Full Screen Options.
SYSTEM OVERVIEW ADDITIONAL FEATURES DAY/NIGHT VIEW FLIGHT INSTRUMENTS ChartView can be displayed on a white or black background for day or night viewing. The Day View offers a better presentation in a bright environment. The Night View gives a better presentation for viewing in a dark environment. When the CHART SETUP Box is selected the G1000 softkeys are blank. Selecting Day, Night, or Automatic View: 1) While viewing a terminal chart press the MENU Key to display the Page Menu OPTIONS.
ADDITIONAL FEATURES SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 8-44 Arrival Information Page, Day View HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Figure 8-45 Arrival Information Page, Night View INDEX 190-00590-07 Rev.
SYSTEM OVERVIEW ADDITIONAL FEATURES CHARTVIEW CYCLE NUMBER AND EXPIRATION DATE AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS ChartView database is revised every 14 days. Charts are still viewable during a period that extends from the cycle expiration date to the disables date. ChartView is disabled 70 days after the expiration date and is no longer available for viewing. When turning on the system, the Power-up Page displays the current status of the ChartView database.
ADDITIONAL FEATURES SYSTEM OVERVIEW FLIGHT INSTRUMENTS The ChartView time critical information can also be found on the AUX - System Status page. The database CYCLE number, EXPIRES, and DISABLES dates of the ChartView subscription appear in either blue or yellow text. When the ChartView EXPIRES date is reached, ChartView becomes inoperative 70 days later. This is shown as the DISABLES date. When the DISABLES date is reached, charts are no longer available for viewing.
SYSTEM OVERVIEW ADDITIONAL FEATURES The ChartView database is obtained directly from Jeppesen. Refer to Updating Jeppesen Databases in Appendix B for instructions on revising the ChartView database. FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Other possible AUX - System Status page conditions are shown in Figure 8-48. The EXPIRES date, in yellow, is the revision date for the next database cycle. The DISABLES date, in yellow, is the date that this database cycle is no longer viewable.
ADDITIONAL FEATURES SYSTEM OVERVIEW 8.4 FLITECHARTS FLIGHT INSTRUMENTS FliteCharts® resemble the paper version of AeroNav Services terminal procedures charts. The charts are displayed with high-resolution and in color for applicable charts. The MFD depiction shows the aircraft position on the moving map in the planview of approach charts. The geo-referenced aircraft position is indicated by an aircraft symbol displayed on the chart when the current position is within the boundaries of the chart.
SYSTEM OVERVIEW ADDITIONAL FEATURES NOTE: Do not maneuver the aircraft based solely upon the geo-referenced aircraft symbol. FLIGHT INSTRUMENTS FLITECHARTS SOFTKEYS FliteCharts functions are displayed on three levels of softkeys. While on the Navigation Map Page, Nearest Airports Page, or Flight Plan Page, pressing the SHW CHRT Softkey displays the available terminal chart and advances to the chart selection level of softkeys: CHRT OPT, CHRT, INFO, DP, STAR, APR, WX, and GO BACK.
ADDITIONAL FEATURES SYSTEM OVERVIEW TERMINAL PROCEDURES CHARTS Selecting Terminal Procedures Charts: FLIGHT INSTRUMENTS While viewing the Navigation Map Page, Nearest Airport Page, or Flight Plan Page, press the SHW CHRT Softkey. Or: 1) Press the MENU Key to display the PAGE MENU. 2) Turn the large FMS Knob to scroll through the OPTIONS Menu to Show Chart. EIS 3) Press the ENT Key to display the chart.
SYSTEM OVERVIEW ADDITIONAL FEATURES When a chart is not available by pressing the SHW CHRT Softkey or selecting a Page Menu Option, charts may be obtained for other airports from the WPT Pages or Flight Plan Pages. FLIGHT INSTRUMENTS If a chart is available for the destination airport, or the airport selected in the active flight plan, the chart appears on the screen.
ADDITIONAL FEATURES SYSTEM OVERVIEW While the APPROACH Box is selected using the FMS Knob, the G1000 softkeys are blank. Once the desired chart is selected, the chart scale can be changed and the chart can be panned using the Joystick. Pressing the Joystick centers the chart on the screen. FLIGHT INSTRUMENTS The aircraft symbol is not shown on FliteCharts. The Chart Scale Box displays a banner NOT TO SCALE, and the Aircraft Not Shown Icon is displayed in the lower right corner of the screen.
SYSTEM OVERVIEW ADDITIONAL FEATURES Pressing the INFO-1 or INFO-2 Softkey returns to the airport diagram chart when the view is on a terminal procedure chart. If the displayed chart is the airport diagram chart, pressing the INFO-1 or INFO-2 Softkey returns to the Airport Information Page. AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Another source for additional airport information is from the INFO Box above the chart (Figure 8-55) or to the right of the chart (Figure 8-56) for certain airports.
ADDITIONAL FEATURES SYSTEM OVERVIEW In the example shown in Figure 8-56, TAKE OFF MINIMUMS is selected. Pressing the ENT Key displays the Take-off Minimums and Departure Procedures Chart (Figure 8-57). FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 8-57 Airport Information Page, TAKE OFF MINIMUMS Selected from INFO View HAZARD AVOIDANCE Pressing the DP Softkey displays the Departure Procedure Chart if available.
SYSTEM OVERVIEW ADDITIONAL FEATURES FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Pressing the STAR Softkey displays the Standard Terminal Arrival Chart if available. Figure 8-59 Arrival Information Page APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Pressing the APR Softkey displays the approach chart for the airport if available. INDEX Figure 8-60 Approach Information Page 494 Garmin G1000 Pilot’s Guide for the Quest KODIAK® 100 190-00590-07 Rev.
ADDITIONAL FEATURES SYSTEM OVERVIEW Pressing the WX Softkey shows the airport weather frequency information, when available, and includes weather data such as METAR and TAF from the XM Data Link Receiver. Weather information is available only when an XM Data Link Receiver is installed and the SiriusXM Weather subscription is current. FLIGHT INSTRUMENTS Selecting Additional Information: 1) While viewing the Airport Taxi Diagram, press the WX Softkey to display the information windows (AIRPORT, INFO).
SYSTEM OVERVIEW ADDITIONAL FEATURES CHART OPTIONS Pressing the CHRT OPT Softkey displays the next level of softkeys, the chart options level (Figure 8-50). EIS FLIGHT INSTRUMENTS Pressing the ALL Softkey shows the complete chart on the screen. HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS Complete Chart Shown INDEX APPENDICES ADDITIONAL FEATURES AFCS Figure 8-62 Airport Information Page, ALL View Selected 496 Garmin G1000 Pilot’s Guide for the Quest KODIAK® 100 190-00590-07 Rev.
ADDITIONAL FEATURES SYSTEM OVERVIEW Pressing the FIT WIDTH Softkey fits the width of the chart in the display viewing area. In the example shown, the chart at close range is replaced with the full width chart. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES Press FIT WDTH Softkey to Show Full Chart Width Figure 8-63 Approach Information Page, FIT WDTH Softkey Selected APPENDICES INDEX 190-00590-07 Rev.
SYSTEM OVERVIEW ADDITIONAL FEATURES FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Pressing the FULL SCN Softkey alternates between removing and replacing the data window to the right.
ADDITIONAL FEATURES SYSTEM OVERVIEW The full screen view can also be selected by using the page menu option. Selecting full screen On or Off: FLIGHT INSTRUMENTS 1) While viewing a terminal chart press the MENU Key to display the Page Menu OPTIONS. 2) Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key. 3) Turn the large FMS Knob to move between the FULL SCREEN and COLOR SCHEME Options. 4) Turn the small FMS Knob to choose between the On and Off Full Screen Options.
SYSTEM OVERVIEW ADDITIONAL FEATURES DAY/NIGHT VIEW FLIGHT INSTRUMENTS FliteCharts can be displayed on a white or black background for day or night viewing. The Day View offers a better presentation in a bright environment. The Night View gives a better presentation for viewing in a dark environment. When the CHART SETUP Box is selected the G1000 softkeys are blank. Selecting Day, Night, or Automatic View: 1) While viewing a terminal chart press the MENU Key to display the Page Menu OPTIONS.
ADDITIONAL FEATURES SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 8-67 Approach Information Page, Day View HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Figure 8-68 Approach Information Page, Night View INDEX 190-00590-07 Rev.
SYSTEM OVERVIEW ADDITIONAL FEATURES FLITECHARTS CYCLE NUMBER AND EXPIRATION DATE AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS FliteCharts data is revised every 28 days. Charts are still viewable during a period that extends from the cycle expiration date to the disables date. FliteCharts is disabled 180 days after the expiration date and are no longer available for viewing upon reaching the disables date.
ADDITIONAL FEATURES SYSTEM OVERVIEW FliteCharts time critical information can also be found on the AUX - System Status page. The FliteCharts database REGION, CYCLE number, EFFECTIVE, EXPIRES, and DISABLES dates of the subscription appear in either blue or yellow text. Dates shown in blue are current data. Dates shown in yellow indicate the data is not within the current subscription period.
SYSTEM OVERVIEW ADDITIONAL FEATURES The FliteCharts database is provided from Garmin. Refer to Updating Garmin Databases in Appendix B for instructions on revising the FliteCharts database. FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS The other four possible AUX - System Status page conditions are shown here. The EFFECTIVE date, in yellow, indicates the current date preceeds the date the FliteCharts database becomes effective.
ADDITIONAL FEATURES SYSTEM OVERVIEW 8.5 AIRPORT DIRECTORY FLIGHT INSTRUMENTS The Aircraft Owners and Pilots Association (AOPA) and optional AC-U-KWIK Airport Directory databases offer detailed information regarding services, hours of operation, lodging options, and more. This information is viewed on the Airport Information Page by pressing the INFO Softkey until INFO-2 is displayed as shown in Figure 8-72. Both Airport Directories are available for downloading at flygarmin.com.
SYSTEM OVERVIEW ADDITIONAL FEATURES AIRPORT DIRECTORY DATABASE CYCLE NUMBER AND REVISION AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS The Airport Directory databases are revised every 56 days and offered on a subscription basis. Check fly. garmin.com for the current database. The Airport Directory is always available for use after the expiration date. When turning on the system, the Power-up Page indicates whether the databases are current, out of date, or not available.
ADDITIONAL FEATURES SYSTEM OVERVIEW The Airport Directory database cycle number shown in the figure, 13D1, is deciphered as follows: 13 – Indicates the year 2013 D – Indicates the data is for Airport Directory FLIGHT INSTRUMENTS 1 – Indicates the first issue of the Airport Directory database for the year The Airport Directory EFFECTIVE date 11–JAN–13 is the beginning date for the current database cycle. The Airport Directory EXPIRES date 10–MAR–13 is the revision date for the next database cycle.
SYSTEM OVERVIEW ADDITIONAL FEATURES 8.6 SIRIUSXM SATELLITE RADIO (OPTIONAL) FLIGHT INSTRUMENTS NOTE: Refer to the Hazard Avoidance Section for information about SiriusXM Weather products. The optional SiriusXM Satellite Radio entertainment feature of the GDL 69A Data Link Receiver is available for the pilot’s and passengers’ enjoyment. The GDL 69A can receive SiriusXM Satellite Radio entertainment services at any altitude throughout the Continental U.S.
ADDITIONAL FEATURES SYSTEM OVERVIEW Activating the SiriusXM Satellite Radio services: 1) Contact SiriusXM Satellite Radio. Follow the instructions provided by SiriusXM Satellite Radio services. 2) Select the Auxiliary Page Group. FLIGHT INSTRUMENTS 3) Select the next to last page in the AUX Page Group. 4) Press the INFO Softkey to display the XM Information Page. 5) Verify that the desired services are activated. 6) Press the LOCK Softkey. EIS 7) Turn the large FMS Knob to highlight YES.
SYSTEM OVERVIEW ADDITIONAL FEATURES USING SIRIUSXM SATELLITE RADIO FLIGHT INSTRUMENTS The XM Radio Page provides information and control of the audio entertainment features of the SiriusXM Satellite Radio. Selecting the XM Radio Page: 1) Turn the large FMS Knob to select the Auxiliary Page Group. 2) Turn the small FMS Knob to select the displayed AUX - XM Information Page. EIS 3) Press the RADIO Softkey to show the XM Radio Page where audio entertainment is controlled.
ADDITIONAL FEATURES SYSTEM OVERVIEW 1) Press the FMS Knob to highlight the channel list and turn the large FMS Knob to scroll through the channels. 2) Press the ENT Key to activate the selected channel. Selecting a channel directly: FLIGHT INSTRUMENTS 1) While on the XM Radio Page, press the CHNL Softkey. 2) Press the DIR CH Softkey. The channel number in the Active Channel Box is highlighted.
SYSTEM OVERVIEW Setting a preset channel number: FLIGHT INSTRUMENTS ADDITIONAL FEATURES 2) Press the MORE Softkey to access the next five channels (PS6 – PS10), and again to access the last five channels (PS11 – PS15). Pressing the MORE Softkey repeatedly cycles through the preset channels. 1) On the XM Radio Page, while listening to an Active Channel that is wanted for a preset, press the PRESETS Softkey to access the first five preset channels (PS1 - PS5).
ADDITIONAL FEATURES SYSTEM OVERVIEW 8.7 MAINTENANCE LOGS FLIGHT INSTRUMENTS The system provides recording of CAS, CMC, exceedances, and other critical aircraft data that occur while the aircraft is on the ground or in flight. This may include, but not limited to, engine trend, exceedance and/ or aircraft position data. The recorded data is assembled into folders and can be copied to an SD Card.
SYSTEM OVERVIEW ADDITIONAL FEATURES Selecting the desired log folder: FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS 1) While viewing the Maintenance Logs Page, press the small FMS Knob to activate the cursor in the Folders Window, as shown in Figure 8-81. Figure 8-81 Activate Folder Cursor INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE 2) Turn the small FMS Knob to display the list of available folders as seen in Figure 8-82.
ADDITIONAL FEATURES SYSTEM OVERVIEW 4) Press the ENT Key. The log files for the selected folder are displayed as seen in Figure 8-83. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 8-83 Select Desired Folder Name 5) Press the small FMS Knob to remove the cursor. Copy a log file to an SD Card: HAZARD AVOIDANCE 1) Place an SD Card in the top card slot of the MFD. 2) While viewing the Maintenance Logs Page, press the FMS Knob to activate the cursor.
SYSTEM OVERVIEW ADDITIONAL FEATURES Delete all logs from a select folder: 1) While viewing the Maintenance Logs Page, press the FMS Knob to activate the cursor. FLIGHT INSTRUMENTS 2) Turn the large FMS Knob to display the list of available folders. 3) Turn either FMS Knob to select the desired folder. 4) Press the ENT Key. AUDIO PANEL & CNS EIS 5) Press the MENU Key to display the Page Menu as in Figure 8-85.
ADDITIONAL FEATURES SYSTEM OVERVIEW Delete all logs from internal memory: 1) While viewing the Maintenance Logs Page, press the MENU Key to display the Page Menu as in Figure 8-87. FLIGHT INSTRUMENTS EIS Figure 8-87 Delete All Logs in Internal Memory AUDIO PANEL & CNS 2) Turn either FMS Knob to highlight ‘Delete All Logs’. 3) Press the ENT Key. The Confirmation Window is displayed as shown in Figure 8-88.
SYSTEM OVERVIEW ADDITIONAL FEATURES 8.8 SCHEDULER FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS The Scheduler feature can be used to enter and display reminder messages (e.g., change oil, switch fuel tanks, or altimeter-transponder check) in the Alerts Window on the PFD. Messages can be set to display based on a specific date and time (event), once the message timer reaches zero (one-time; default setting), or recurrently whenever the message timer reaches zero (periodic).
ADDITIONAL FEATURES SYSTEM OVERVIEW Deleting a scheduler message: 1) Select the AUX - Utility Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. FLIGHT INSTRUMENTS 3) Turn the large FMS Knob to highlight the name field of the scheduler message to be deleted. 4) Press the CLR Key to clear the message text. If the CLR Key is pressed again, the message is restored. 5) Press the ENT Key while the message line is cleared to clear the message text.
SYSTEM OVERVIEW ADDITIONAL FEATURES 8.9 ELECTRONIC CHECKLISTS FLIGHT INSTRUMENTS NOTE: The checklists presented in this section are for example only and may not reflect checklists actually available for the KODIAK 100. The information described in this section is not intended to replace the checklist information described in the AFM or the Pilot Safety and Warning Supplements document. NOTE: Garmin is not responsible for the content of checklists.
ADDITIONAL FEATURES SYSTEM OVERVIEW 8) Press the ENT Key. ‘GO TO NEXT CHECKLIST?’ will be highlighted by the cursor. 9) Press the ENT Key to advance to the next checklist. 10) Press the EXIT Softkey to exit the Checklist Page and return to the page last viewed.
SYSTEM OVERVIEW ADDITIONAL FEATURES 6) Press the ENT Key. ‘GO TO NEXT CHECKLIST?’ will be highlighted by the cursor. 7) Press the ENT Key to advance to the next checklist. FLIGHT INSTRUMENTS 8) Press the RETURN Softkey to return to the previous checklist. AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS 9) Press the EXIT Softkey to exit the Checklist Page and return to the page last viewed.
ADDITIONAL FEATURES SYSTEM OVERVIEW 8.10 FLIGHT DATA LOGGING NOTE: Some aircraft installations may not provide all aircraft/engine data capable of being logged by the FLIGHT INSTRUMENTS system. The Flight Data Logging feature will automatically store critical flight and engine data on an SD data card (up to 16GB) inserted into the top card slot of the MFD. Approximately 1,000 flight hours can be recorded for each 1GB of available space on the card.
SYSTEM OVERVIEW ADDITIONAL FEATURES FLIGHT INSTRUMENTS The file containing the recorded data will appear in the format shown in Figure 8-94. This file can be imported into most computer spreadsheet applications. Local Date YYMMDD Local 24hr Time HHMMSS Nearest Airport (A blank will be inserted if no airport is found) EIS log_110210_104506_KIXD.
ADDITIONAL FEATURES SYSTEM OVERVIEW 8.11 AUXILIARY VIDEO The G1000 system provides a control and display interface to an auxiliary video system. The system can display video for up to two inputs. FLIGHT INSTRUMENTS There are four modes of operation of the auxiliary video display: Full-Screen, Full-Screen with Digital Zoom, Split-Screen with Map, and Split-Screen with Map and Digital Zoom. Displaying auxiliary video: 1) Turn the large FMS Knob to select the AUX page group.
SYSTEM OVERVIEW ADDITIONAL FEATURES VIDEO SETUP FLIGHT INSTRUMENTS Video brightness, contrast, and saturation may be adjusted be selecting the setup function. While viewing the setup function softkeys, after 45 seconds of softkey inactivity, the system reverts to the AUX - VIDEO Page softkeys. Adjusting the video settings: 1) With the AUX-VIDEO Page displayed, press the SETUP Softkey. EIS 2) Press the BRIGHT - or BRIGHT +, to adjust display brightness in five percent increments from 0 to 100%.
ADDITIONAL FEATURES SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 8-98 Full Screen Video Display INPUT SELECTION HAZARD AVOIDANCE While on the AUX - VIDEO Page, press the INPUT Softkey to select Input 1 or Input 2. The selected input is displayed in the upper left of the video display. AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00590-07 Rev.
SYSTEM OVERVIEW ZOOM/RANGE FLIGHT INSTRUMENTS ADDITIONAL FEATURES The Joystick can be used to increase or decrease the range setting on the map display or zoom in and out on the video display. While in the Split-Screen mode, pressing the MAP ACTV or VID ACTV Softkey determines which display the Joystick adjusts. Pressing the softkey to display MAP ACTV allows the Joystick to control the range setting of the map display.
ADDITIONAL FEATURES SYSTEM OVERVIEW 8.12 ELECTRONIC STABILITY & PROTECTION (ESP™) FLIGHT INSTRUMENTS Electronic Stability and Protection (ESP™) is an optional feature that is intended to discourage the exceedance of attitude and established airspeed parameters. This feature will only function when the aircraft is above 200 feet AGL and the autopilot is not engaged. ESP engages when the aircraft exceeds one or more conditions (pitch, roll, low airspeed, and Vmo) beyond the normal flight parameters.
SYSTEM OVERVIEW ADDITIONAL FEATURES ROLL ENGAGEMENT FLIGHT INSTRUMENTS Roll Limit Indicators are displayed on the roll scale at 45° right and left, indicating where ESP will engage (see Figure 8-100). As roll attitude exceeds 45°, ESP will engage and the on-side Roll Limit Indicator will move to 30°, as shown in Figure 8-101. The Roll Limit Indicator is now showing where ESP will disengage as roll attitude decreases.
ADDITIONAL FEATURES SYSTEM OVERVIEW Once engaged, ESP force will be applied between 30° and 75°, as illustrated in Figure 8-101. The force increases as roll attitude increases and decreases as roll attitude decreases. The applied force is intended to encourage pilot input that returns the airplane to a more normal roll attitude. As roll attitude decreases, ESP will disengage at 30°.
SYSTEM OVERVIEW ADDITIONAL FEATURES PITCH ENGAGEMENT FLIGHT INSTRUMENTS ESP engages at 21° nose-up and 21° nose-down. Once ESP is engaged, it will apply opposing force between 19° and 50° nose-up and between 19° and 50° nose-down, as indicated in Figure 8-104. Maximum opposing force is applied between 25° and 50° nose-up and between 25° and 50° nose-down. The opposing force increases or decreases depending on the pitch angle and the direction of pitch travel.
ADDITIONAL FEATURES SYSTEM OVERVIEW 8.13 ABNORMAL OPERATION SVT TROUBLESHOOTING FLIGHT INSTRUMENTS SVT is intended to be used with traditional attitude, heading, obstacle, terrain, and traffic inputs. SVT is disabled when valid attitude or heading data is not available for the display. In case of invalid SVT data, the PFD display reverts to the standard blue-over-brown attitude display.
SYSTEM OVERVIEW ADDITIONAL FEATURES UNUSUAL ATTITUDES FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Unusual attitudes are displayed with red chevrons overlaid on the display indicating the direction to fly to correct the unusual attitude condition. The display shows either a brown or blue colored bar at the top or bottom of the screen to represent earth or sky. This is intended to prevent losing sight of the horizon during extreme pitch attitudes.
ADDITIONAL FEATURES SYSTEM OVERVIEW GDL 69/69A DATA LINK RECEIVER TROUBLESHOOTING Some quick troubleshooting steps listed below can be performed to find the possible cause of a failure.
SYSTEM OVERVIEW ADDITIONAL FEATURES If a failure still exists, the following messages may provide insight as to the possible problem: FLIGHT INSTRUMENTS Message CHECK ANTENNA UPDATING NO SIGNAL LOADING OFF AIR --- Message Location XM Radio Page - active channel field XM Radio Page - active channel field XM Radio Page - active channel field Weather Datalink Page - center of page XM Radio Page - active channel field XM Radio Page - active channel field XM Radio Page - active channel field Description Dat
APPENDIX A SYSTEM OVERVIEW ANNUNCIATIONS AND ALERTS NOTE: The KODIAK 100 aircraft Pilot’s Operating Handbook (POH) supersedes information found in this document. FLIGHT INSTRUMENTS The G1000 Alerting System conveys alerts to the pilot using a combination of the following items: EIS • Annunciation Window: The Annunciation Window displays abbreviated annunciation text. Text color is based on alert levels described later in the Alert Levels Definitions section.
SYSTEM OVERVIEW APPENDIX A • System Annunciations: Typically, a large red ‘X’ appears in windows when a failure is detected in the LRU providing the information to the window. See the G1000 System Annunciations section for more information. FLIGHT INSTRUMENTS • Audio Alerting System: The G1000 System issues audio alert tones when specific system conditions are met. See the Alert Level Definitions Section for more information. The annunciation tone may be tested from the AUX - System Status Page.
APPENDIX A SYSTEM OVERVIEW Figure A-4 CAUTION Softkey Annunciation Figure A-5 ADVISORY Softkey Annunciation EIS Figure A-3 WARNING Softkey Annunciation FLIGHT INSTRUMENTS • MESSAGE ADVISORY: This level of alert provides general information to the pilot. A message advisory alert does not issue annunciations in the Annunciation Window. Instead, message advisory alerts only issue a flashing ADVISORY Softkey annunciation, as shown in Figure A-5.
SYSTEM OVERVIEW APPENDIX A AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Annunciation Window Text FLAP FAIL FLAP TRIM FAIL FUEL LOW L FUEL LOW R FUEL LOW L-R FUEL PRESS LOW GEN FAIL HI ICE SPEED INLET NOT NRM INLET SW FAULT LO ICE SPEED PITOT FL L PITOT FL R PITOT FL L-R PITOT OFF L PITOT OFF R PITOT OFF L-R PTCH INHIB FAIL STALL HT FL TKS BACKUP TKS LOW QTY TKS HI FLOW TKS HI PRESS VOLTAGE LOW Alerts Window Message Flaps system is inoperative. Flap Trim failure.
APPENDIX A SYSTEM OVERVIEW MESSAGE ADVISORY ALERTS Audio Alert None None FLIGHT INSTRUMENTS Alerts Window Message AVN FAN 1 FAIL – Avionics cooling fan #1 is inoperative. AVN FAN 2 FAIL – Avionics cooling fan #2 is inoperative. AURAL ALERTS Aural Alert “Minimums, minimums” EIS Description The aircraft has descended below the preset minimum descent altitude or decision altitude. “Vertical track” The aircraft is one minute from Top of Descent. Issued only when vertical navigation is enabled.
SYSTEM OVERVIEW APPENDIX A COMPARATOR ANNUNCIATIONS FLIGHT INSTRUMENTS The Comparator monitors critical values generated by redundant sensors. If differences in the sensors exceed a specified amount, this discrepency is annunciated in the Comparator Window as a ‘MISCOMP’ (miscompare) as seen in Figure A-6. If one or both of the sensed values are unavailable, it is annunciated as a ‘NO COMP’ (no compare).
APPENDIX A SYSTEM OVERVIEW REVERSIONARY SENSOR ANNUNCIATIONS Condition Both PFDs are displaying data from the number one Air Data Computer. Both PFDs are displaying data from the number two Air Data Computer. Both PFDs are displaying data from the number one Attitude & Heading Reference System. Both PFDs are displaying data from the number two Attitude & Heading Reference System. Both PFDs are displaying data from the number one GPS receiver. Both PFDs are displaying data from the number two GPS receiver.
SYSTEM OVERVIEW APPENDIX A G1000 SYSTEM ANNUNCIATIONS FLIGHT INSTRUMENTS When a new alert is issued, the ALERTS Softkey will flash to alert the pilot of a new message. It will continue to flash until acknowledged by pressing the softkey. Active alerts are displayed in white text. Alerts that have become inactive will change to gray text. The ALERTS Softkey will flash if the state of a displayed alert changes or a new alert is displayed.
APPENDIX A SYSTEM OVERVIEW System Annunciation Comment Display system is not receiving attitude information from the AHRS. System is not receiving valid heading input from GMU, but is receiving GPS-derived track information. FLIGHT MANAGEMENT System is not receiving valid heading input from GMU and is not receiving GPS-derived track information. CDI is not receiving valid data from the corresponding GIA. Does not apply when the CDI is set to GPS.
SYSTEM OVERVIEW APPENDIX A G1000 SYSTEM MESSAGE ADVISORIES FLIGHT INSTRUMENTS This section describes various G1000 system message advisories. Certain messages are issued due to an LRU or an LRU function failure. Such messages are normally accompanied by a corresponding red ‘X’ annunciation as shown previously in the G1000 System Annunciation section. NOTE: This Section provides information regarding G1000 message advisories that may be displayed by the EIS system.
APPENDIX A SYSTEM OVERVIEW Comments The PFD and/or MFD is overheating and is reducing power consumption by dimming the display. If problem persists, the G1000 system should be serviced. FLIGHT INSTRUMENTS A key is stuck on the PFD and/or MFD bezel. Attempt to free the stuck key by pressing it several times. The G1000 system should be serviced if the problem persists. EIS AUDIO PANEL & CNS The PFD1 configuration module backup memory has failed. The G1000 system should be serviced.
SYSTEM OVERVIEW APPENDIX A Comments The MFD and/or PFD detected a failure in the terrain database. Ensure that the terrain card is properly inserted in display. Replace terrain card. If problem persists, the G1000 system should be serviced. The terrain database is present on another LRU, but is missing on the specified LRU. Ensure that the terrain card is properly inserted in the specified display. Replace terrain card. If problem persists, the G1000 system should be serviced.
APPENDIX A SYSTEM OVERVIEW Comments The MFD and/or PFD detected a failure in the Safe Taxi database. Ensure that the data card is properly inserted. Replace data card. If problem persists, the G1000 system should be serviced. FLIGHT INSTRUMENTS Alerts Window Message MFD1 DB ERR – MFD1 Safe Taxi database error exists. PFD1 DB ERR – PFD1 Safe Taxi database error exists. PFD2 DB ERR – PFD2 Safe Taxi database error exists. MFD1 DB ERR – MFD1 Chartview database error exists.
SYSTEM OVERVIEW APPENDIX A GMA 1347 MESSAGE ADVISORIES FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Alerts Window Message GMA1 FAIL – GMA1 is inoperative. GMA2 FAIL – GMA2 is inoperative. GMA XTALK – GMA crosstalk error has occurred. GMA1 CONFIG – GMA1 config error. Config service req’d. GMA2 CONFIG – GMA2 config error. Config service req’d. GMA1 MANIFEST – GMA1 software mismatch. Communication halted. GMA2 MANIFEST – GMA2 software mismatch. Communication halted.
APPENDIX A Comments A failure has been detected in glideslope receiver 1 and/or receiver 2. The receiver may still be available. The system should be serviced when possible. FLIGHT INSTRUMENTS A GIA mismatch has been detected, where only one is SBAS capable. The G1000 system should be serviced. EIS The GIA1 and/or GIA 2 has incorrect software installed. The G1000 system should be serviced. AUDIO PANEL & CNS Incorrect servo software is installed, or gain settings are incorrect.
SYSTEM OVERVIEW APPENDIX A Comments The COM1 and/or COM2 transfer switch is stuck in the enabled (or “pressed”) position. Press the transfer switch again to cycle its operation. If the problem persists, the G1000 system should be serviced. GPS integrity is insufficient for the current phase of flight. Loss of GPS navigation due to insufficient satellites. Loss of GPS navigation due to position error. Loss of GPS navigation due to GPS failure. Abort approach due to loss of GPS navigation.
APPENDIX A SYSTEM OVERVIEW GEA 71 MESSAGE ADVISORIES Comments The GEA1 configuration settings do not match those of backup configuration memory. The G1000 system should be serviced. The GEA2 configuration settings do not match those of backup configuration memory. The G1000 system should be serviced. The #1 GEA 71 has incorrect software installed. The G1000 system should be serviced. The #2 GEA 71 has incorrect software installed. The G1000 system should be serviced.
SYSTEM OVERVIEW APPENDIX A INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Alerts Window Message AHRS2 GPS – AHRS2 using backup GPS source. AHRS1 GPS – AHRS1 not receiving any GPS information. AHRS2 GPS – AHRS2 not receiving any GPS information. AHRS1 GPS – AHRS1 not receiving backup GPS information. AHRS2 GPS – AHRS2 not receiving backup GPS information. AHRS1 GPS – AHRS1 operating exclusively in no-GPS mode.
APPENDIX A SYSTEM OVERVIEW GMU 44 MESSAGE ADVISORIES Comments A fault has occurred in the #1 GMU 44. Heading is flagged as invalid. The AHRS uses GPS for backup mode operation. The G1000 system should be serviced. A fault has occurred in the #2 GMU 44. Heading is flagged as invalid. The AHRS uses GPS for backup mode operation. The G1000 system should be serviced. FLIGHT INSTRUMENTS The GMU 44 has incorrect software installed. The G1000 system should be serviced.
SYSTEM OVERVIEW APPENDIX A GWX 68 MESSAGE ADVISORIES FLIGHT INSTRUMENTS Alerts Window Message GWX CONFIG – GWX config error. Config service req’d. GWX FAIL – GWX is inoperative. EIS GWX SERVICE – Needs service. Return unit for repair. WX ALERT – Possible severe weather ahead. GWX MANIFEST – GWX software mismatch, communication halted. Comments GWX 68 configuration settings do not match those of the GDU configuration. The G1000 system should be serviced.
APPENDIX A SYSTEM OVERVIEW MISCELLANEOUS MESSAGE ADVISORIES AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Garmin G1000 Pilot’s Guide for the Quest KODIAK® 100 EIS 190-00590-07 Rev. A FLIGHT INSTRUMENTS Alerts Window Message Comments FPL WPT LOCK – Flight plan waypoint Upon power-up, the G1000 system detects that a stored flight plan waypoint is is locked. locked. This occurs when an navigation database update eliminates an obsolete waypoint.
SYSTEM OVERVIEW APPENDIX A FLIGHT INSTRUMENTS Alerts Window Message PTK FAIL – Parallel track unavailable: invalid leg type. PTK FAIL – Parallel track unavailable: past IAF. UNABLE V WPT – Can’t reach current vertical waypoint. EIS VNV – Unavailable. Unsupported leg type in flight plan. FLIGHT MANAGEMENT AUDIO PANEL & CNS VNV – Unavailable. Excessive crosstrack error. VNV – Unavailable. Excessive track angle error. VNV – Unavailable. Parallel course selected.
APPENDIX A Comments The SD card in the top card slot of the specified PFD or MFD contains invalid data. FLIGHT INSTRUMENTS The SD card in the bottom card slot of the specified PFD or MFD contains invalid data. The audio source for terrain awareness is offline. Check GIA1 or GIA 2. Terrain audio alerts are not configured properly. The system should be serviced TAWS is disabled because a terrain database of sufficient resolution (9 arc-second or better) is not currently installed.
SYSTEM OVERVIEW APPENDIX A AFCS ALERTS FLIGHT INSTRUMENTS System Status Field Figure A-6 AFCS System Status Field The following alert annunciations appear in the AFCS System Status field on the PFD.
APPENDIX A SYSTEM OVERVIEW TAWS-B ALERTS Annunciations appear on the PFD and the MFD. Pop-up alerts appear only on the MFD.
SYSTEM OVERVIEW APPENDIX A TAWS-B SYSTEM STATUS ANNUNCIATIONS PFD/MFD* Alert Annunciation TAWS-B Page Center Banner Annunciation Voice Message TAWS TEST TAWS TEST None None None “TAWS System Test OK” TAWS-B FLTA Alerting Inhibited TAWS INH None None No GPS position TAWS N/A NO GPS POSITION “TAWS Not Available”† TAWS N/A None “TAWS Not Available”† TAWS FAIL TAWS FAIL “TAWS System Failure” None TERRAIN DATABASE FAILURE None FLIGHT INSTRUMENTS Alert Type System Test in progress EI
APPENDIX A SYSTEM OVERVIEW FLIGHT PLAN IMPORT/EXPORT MESSAGES In some circumstances, some messages may appear in conjunction with others. ‘User waypoint database full. Not all loaded.’ AFCS ‘Flight plan successfully exported.’ ‘Flight plan export failed.’ HAZARD AVOIDANCE ‘One or more user waypoints renamed.’ FLIGHT MANAGEMENT ‘Some waypoints not loaded. Waypoints locked.’ AUDIO PANEL & CNS ‘Too many points. Flight plan truncated.’ EIS ‘File contained user waypoints only.
SYSTEM OVERVIEW APPENDIX A PILOT PROFILE IMPORT/EXPORT MESSAGES Description Displayed if the SD card does not have one or more valid pilot profile filenames. Displayed if the profile name matches the name of existing profile. Displayed if the profile name is invalid. Displayed if the maximum number for pilot profiles has been reached. Displayed if the importing operation fails for any other reason. Displayed if the importing operation succeeds.
APPENDIX B SYSTEM OVERVIEW DATABASE MANAGEMENT CAUTION: Never disconnect power to the system when loading a database. Power interuption during the FLIGHT INSTRUMENTS database loading process could result in maintenance being required to reboot the system. The system uses Secure Digital (SD) cards to load and store various types of data. For basic flight operations, SD cards are required for database storage as well as navigation and ChartView database updates.
SYSTEM OVERVIEW APPENDIX B NOTE: Garmin requests the flight crew report any observed discrepancies related to database information. FLIGHT INSTRUMENTS These discrepancies could come in the form of an incorrect procedure; incorrectly identified terrain, obstacles and fixes; or any other displayed item used for navigation or communication in the air or on the ground. Go to FlyGarmin.com and select ‘Report An Aviation Data Error Report.
APPENDIX B SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS Figure B-2 Database Update Confirmation AUDIO PANEL & CNS 5) After the update completes, the display starts in normal mode. Do not remove power while the display is starting. 6) Turn the system OFF and remove the SD card from the top card slot. FLIGHT MANAGEMENT 7) Repeat steps 1 through 6 for the other displays (PFD1, PFD2 or MFD). Remove the SD card when finished. 8) Apply power to the system and press the ENT Key to acknowledge the startup screen.
SYSTEM OVERVIEW Loading a standby navigation database: FLIGHT INSTRUMENTS APPENDIX B 2) Verify that an SD card is inserted in the bottom slot of each PFD and the MFD. 1) With the system OFF, insert the SD card containing the new navigation database version into the top card slot of the MFD. AUDIO PANEL & CNS EIS 3) Turn the system ON. A prompt similar to the following is displayed. Figure B-3 Standby Navigation Database Prompt FLIGHT MANAGEMENT 4) Press the YES Softkey.
APPENDIX B SYSTEM OVERVIEW FLIGHT INSTRUMENTS Figure B-6 Active Navigation Database Prompt EIS 8) Press the NO Softkey. The display now starts in normal mode. Since the database effective date is not yet valid, it should not be loaded as the active database. The display now starts in normal mode. Do not remove power while the display is starting. AUDIO PANEL & CNS 9) Press the ENT Key to acknowledge the startup screen. 10) Turn the large FMS Knob to select the AUX Page group on the MFD.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW APPENDIX B MFD PFD2 AUDIO PANEL & CNS EIS PFD1 Figure B-7 Correct Database Locations Since these databases are not stored internally in the displays, a Supplemental Data Card containing identical database versions must be kept in each display unit. FLIGHT MANAGEMENT The basemap database contains data for the topography and land features, such as rivers, lakes, and towns. It is updated only periodically, with no set schedule. There is no expiration date.
APPENDIX B SYSTEM OVERVIEW AUTOMATIC DATABASE SYNCHRONIZATION FEATURE FLIGHT INSTRUMENTS The automatic database synchronization feature automatically transfers the database from a single SD database card to the SD cards on each PFD and the MFD to ensure that all databases are synchronized throughout the system. After power-up, the system compares all copies of each applicable database.
SYSTEM OVERVIEW APPENDIX B repeatedly, the softkey will cycle through PFD1, PFD2, and MFD. Database status information in the Database Window will reflect the database of the selected PFD or MFD. After a successful sync and restart, verify that the proper databases are now in use on the AUX–System Status Page (Figure B-8).
APPENDIX B SYSTEM OVERVIEW UPDATING BASEMAP, SAFETAXI, AIRPORT TERRAIN, OBSTACLE, AND AIRPORT DIRECTORY DATABASES FLIGHT INSTRUMENTS These databases may be copied to one Supplemental Data Card, then automatically synchronized to other card in the system: 1) With system power OFF, remove the MFD database card from the bottom card slot of the MFD. 2) Update the basemap, SafeTaxi, airport terrain, obstacle and/or airport directory databases on the MFD card.
SYSTEM OVERVIEW APPENDIX B UPDATING TERRAIN, FLITECHARTS, AND CHARTVIEW DATABASES 1) With system power OFF, remove the Supplemental Data Card from the bottom card slot of the MFD and PFDs. FLIGHT INSTRUMENTS 2) Copy the updated terrain database to each of the Supplemental Data Cards. Copy the updated FliteCharts or ChartView database to one Supplemental Data Card. 3) Insert the updated Supplemental Data Cards into the bottom card slot of the MFD and PFDs.
APPENDIX B SYSTEM OVERVIEW Loading the magnetic field variation database update: 1) With ‘OK’ highlighted, as seen in Figure B-12, press the ENT Key on the MFD. A progress monitor is displayed as shown in Figure B-13. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS Figure B-13 Uploading Database to GRS1 2) When the upload is complete, the prompt for the next GRS upload is displayed, as seen in Figure B-14.
INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW APPENDIX B Blank Page 576 Garmin G1000 Pilot’s Guide for the Quest KODIAK® 100 190-00590-07 Rev.
APPENDIX C SYSTEM OVERVIEW GARMIN AVIATION GLOSSARY INDEX Garmin G1000 Pilot’s Guide for the Quest KODIAK® 100 APPENDICES Degrees Celsius Center Runway Course to Altitude Leg Calibrated Calculator Indicated airspeed corrected for installation and instrument errors.
SYSTEM OVERVIEW APPENDIX C FLIGHT INSTRUMENTS CI CLD CLR CM CN CNS AUDIO PANEL & CNS EIS CO COM CONFIG COOL COPLT Course FLIGHT MANAGEMENT Course to Steer APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE CPDLC CPL CR CRG CRNT Crosstrack Error CRS CRSR CSC CTA CTR CTRL Cumulative, CUM CVR CVRG CWS CYL INDEX D ALT DB, DBASE 578 Course to Intercept Leg Cloud Clear Centimeter Canada Communication, Navigation, & Surveillance Carbon Monoxide Communication Radio Configuration Coolant Copilot T
APPENDIX C Elevation, Elevator Emergency FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS Glideslope Go-Around Gallon(s) Gearbox Ground Clutter Suppression Garmin Air Data Computer Garmin Display Unit Garmin Engine/Airframe Unit Geographic Garmin Flight Control Garmin Integrated Avionics Unit Garmin Audio Panel System Garmin Mode Controller APPENDICES INDEX Garmin G1000 Pilot’s Guide for the Quest KODIAK® 100 ADDITIONAL FEATURES G/S GA GAL, GL GBOX GCS GDC GDU GEA GEO GFC GIA GMA GMC AUDIO PANEL & CNS 190-00
SYSTEM OVERVIEW APPENDIX C AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS GMT GMU GND GPH GPN GPS GPWS Grid MORA Groundspeed HAZARD AVOIDANCE FLIGHT MANAGEMENT Ground Track GRS GS GSA GSL GTS GTX GWX AFCS HA HDG HDOP Heading ADDITIONAL FEATURES HF INDEX APPENDICES HFOM Hg HI HI SENS HM Horizontal Figure of Merit hPa 580 Greenwich Mean Time Garmin Magnetometer Unit Ground Gallons per Hour Garmin Part Number Global Positioning System Ground Proximity Warning System Grid Minimum Off-Route Altitude;
APPENDIX C ADDITIONAL FEATURES APPENDICES INDEX Garmin G1000 Pilot’s Guide for the Quest KODIAK® 100 AFCS North Navigation Navigation Aid HAZARD AVOIDANCE 190-00590-07 Rev. A N NAV NAVAID FLIGHT MANAGEMENT M Meter, Middle Marker MMO (VMO) Maximum Speed Mach Number Mach number is the ratio of the true airspeed to the speed of sound.
SYSTEM OVERVIEW APPENDIX C INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS NDB NEXRAD NM NoPT 582 NOTAM NRST Non-Directional Beacon Next Generation Radar Nautical Mile(s) No Procedure Turn Required (procedure shall not be executed without ATC clearance) Notice To Airman Nearest O OAT OBS OFST OXY Outer Marker Outside Air Temperature Omni Bearing Selector Offset Oxygen P ALT PA PASS PC PFD PI PIREP PIT, PTCH POH POHS POS,
APPENDIX C APPENDICES INDEX Garmin G1000 Pilot’s Guide for the Quest KODIAK® 100 ADDITIONAL FEATURES Velocity (airspeed) Maximum landing gear extended speed AFCS V, Vspeed VLE HAZARD AVOIDANCE Unavailable United States User Coordinated Universal Time Universal Transverse Mercator/ Universal Polar Stereographic Grid FLIGHT MANAGEMENT 190-00590-07 Rev.
SYSTEM OVERVIEW APPENDIX C HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS VLO VMC VMO (MMO) VNE VR VX VY VYSE V V DEV VA VAC VAPP VAR VD VDC VERT Vertical Figure of Merit Vertical Speed Required ADDITIONAL FEATURES AFCS VFOM VFR VHF VI VLOC VM APPENDICES VMC VNAV, VNV VOL VOR VORTAC INDEX VPATH, VPTH VPL VPROF VR 584 Maximum landing gear operating speed Minimum Control Speed Maximum Speed Never-Exceed Speed Rotate Speed Best Angle of Climb Speed Best Rate of Clim
APPENDIX D SYSTEM OVERVIEW FREQUENTLY ASKED QUESTIONS FLIGHT INSTRUMENTS If a particular aspect of G1000 operational capability is not addressed by these commonly asked questions or in the index, contact Garmin (see the copyright page or back cover for contact information) or a Garmin-authorized dealer. Garmin is dedicated to supporting its products and customers. What is SBAS? EIS The Satellite Based Augmentation System (SBAS) uses a system of ground stations to correct any GPS signal errors.
SYSTEM OVERVIEW APPENDIX D For RAIM to work correctly, the GPS receiver must track at least five satellites. A minimum of six satellites is required to allow RAIM to eliminate a single corrupt satellite from the navigation solution. FLIGHT INSTRUMENTS RAIM ensures that satellite geometry allows for a navigation solution calculation within a specified protection limit (2.0 nm for oceanic and en route, 1.0 nm for terminal, and 0.3 nm for non-precision approaches).
APPENDIX D SYSTEM OVERVIEW the G1000 automatically activates the next waypoint in the flight plan once the aircraft has crossed the present active waypoint.
SYSTEM OVERVIEW APPENDIX D When does the CDI scale change? FLIGHT INSTRUMENTS Once a departure is activated, the G1000 Course Deviation Indicator (CDI) full scale deflection is set to 0.3 nm. The CDI scale changes to 1.0 nm (terminal mode) then ramps up to 2.0 nm (enroute mode) at 30 nm from the departure airport. When 31 nm from the destination, the CDI scale smoothly transition from 2.0 nm back to 1.0 nm (terminal mode). At 2.
APPENDIX E SYSTEM OVERVIEW GENERAL TIS INFORMATION INTRODUCTION FLIGHT INSTRUMENTS NOTE: Aircraft without an operating transponder are invisible to TIS. EIS The Traffic Information Service (TIS) provides traffic advisory information to non-TAS/TCAS-equipped aircraft. TIS is a ground-based service providing the relative locations of all ATCRBS Mode-A and Mode-C transponder equipped aircraft within a specified service volume.
SYSTEM OVERVIEW APPENDIX E WARNING: Garmin is not responsible for Mode S geographical coverage. Operation of the ground stations FLIGHT INSTRUMENTS is the responsibility of the FAA. Refer to the AIM for a Terminal Mode S radar site map. NOTE: TIS is unavailable at low altitudes in many areas of the United States. This is often the case in mountainous regions. AUDIO PANEL & CNS EIS TIS information is collected during a single radar sweep.
APPENDIX F SYSTEM OVERVIEW MAP SYMBOLS AIRPORT BASEMAP Symbol Item Symbol Item Symbol FLIGHT INSTRUMENTS Item Interstate Highway Unknown Airport State Highway Non-towered, Non-serviced Airport EIS US Highway Towered, Non-serviced Airport National Highway AUDIO PANEL & CNS Non-towered, Serviced Airport Small City or Town Medium City Restricted (Private) Airport Large City FLIGHT MANAGEMENT Towered, Serviced Airport Heliport TRAFFIC Item Symbol Intersection HAZARD AVOIDANCE NAVAIDS
SYSTEM OVERVIEW APPENDIX F LINE SYMBOLS Item Symbol FLIGHT INSTRUMENTS ICAO Control Area Class B Airspace Mode C Tower Area FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS Warning Area Alert Area Caution Area Danger Area Prohibited Area Restricted Area Training Area Unknown Area Class C Terminal Radar Service Area Mode C Area Military Operations Area (MOA) HAZARD AVOIDANCE State or Province Border International Border Road AFCS Railroad INDEX APPENDICES ADDITIONAL FEATURES Lattitude/Longitude 592
APPENDIX F SYSTEM OVERVIEW OBSTACLE SYMBOLS Obstacle Color Obstacle Location Red (WARNING) Obstacle within 100 ft or above aircraft altitude Yellow (CAUTION) Obstacle within 1000 ft of aircraft altitude FLIGHT INSTRUMENTS Obstacle Symbol Unlighted Obstacle Lighted Obstacle < 1000 ft AGL > 1000 ft AGL < 1000 ft AGL > 1000 ft AGL EIS Gray Obstacle more than 1000 (NO DANGER) ft below aircraft altitude Table F-1 Obstacle Symbols and Colors AUDIO PANEL & CNS TAWS COLOR CHART FLIGHT MANAGEMENT Pote
SYSTEM OVERVIEW APPENDIX F MISCELLANEOUS HAZARD AVOIDANCE FEATURES Item Symbol FLIGHT INSTRUMENTS ARTCC Frequency or FSS Frequency Feature Symbol Terrain Proximity/TAWS display enabled Traffic display enabled Default Map Pointer Data Link Weather display enabled Elevation Pointer EIS Cloud Top display enabled AUDIO PANEL & CNS Wind Vector Echo Top display enabled Lightning display enabled Measuring Pointer Cell Movement display enabled Overzoom Indicator FLIGHT MANAGEMENT SIGMETs/AIRMET
INDEX EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE B Backlighting-------------------------------------------------- 49 Barometric altimeter setting---------------------------52, 58 Basic Empty Weight----------------------------------------254 Basic Operating Weight------------------------------------254 Bearing/distance, measuring------------------------------148 Bearing information-------------------------------------53, 66 Bearing line------------------------------------------- 335, 339 Bear
SYSTEM OVERVIEW INDEX FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS ChartView plan view---------------------------------------477 ChartView profile View-------------------------------------478 Checklist---------------------------------------------- 520–521 Checklist softkeys-------------------------------------------520 Clearance recorder and player----------------------------130 Closest Point-------------------------------------------------226 CNS system----------------------------------
INDEX J Gain-----------------------------------------------------------338 GDL 69/69A-------------------------------------------------292 Generator speed------------------------------------ 91, 93, 95 Geodetic sea level------------------------------------------351 Glidepath-----------------------------------------------------284 Glidepath indicator------------------------------------------ 61 Glidepath Mode-------------------------------------- 414, 422 Glidepath Mode (GP)---------------------------------
SYSTEM OVERVIEW INDEX N FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS National Weather Service----------------------------------317 NAV1 audio--------------------------------------------------112 NAV2 audio--------------------------------------------------112 Navigation database-------------------------------- 233, 234 Navigation Map---------------------------------------------192 Navigation Mode----------------------- 420–421, 431–432 Navigation mode selection----------------------------
INDEX AUDIO PANEL & CNS FLIGHT MANAGEMENT U Unable to display chart----------------------------- 468, 489 Updating Garmin databases------------------------------465 Updating Jeppesen databases----------------------------485 User-Defined Holding Pattern-----------------------------228 HAZARD AVOIDANCE V Vertical deviation-------------------------------------------412 Vertical deviation guidance-------------------------------234 Vertical Deviation Indicator (VDI)------------------ 277, 278 Vertical naviga
SYSTEM OVERVIEW INDEX FLIGHT INSTRUMENTS VNV indications---------------------------------------------- 77 Voice alerts--------------------------------------------------539 Voice alerts, TIS Traffic---------------------------80, 373, 395 Voltmeter--------------------------------------------------91, 93 Volume-------------------------------------------------------512 VOR Nearest--------------------------------------------- 186–187 VOR selection------------------------------------------------111 Vspeed refe
G1000 ® Integrated Avionics System Pilot’s Guide ® G1000 Pilot’s Guide Garmin International, Inc. 1200 East 151st Street Olathe, KS 66062, U.S.A. p:913.397.8200 f:913.397.8282 Garmin AT, Inc. 2345 Turner Road SE Salem, OR 97302, U.S.A. p:503.391.3411 f:503.364.2138 Garmin Corporation No. 68, Jangshu 2nd Road Shijr, Taipei County, Taiwan p:886/02.2642.9199 f:886/02.2642.9099 www.garmin.com Quest KODIAK® 100 Garmin (Europe) Ltd. Liberty House, Hounsdown Business Park Southampton, Hampshire SO40 9LR U.
