G1000 ® Integrated Flight Deck 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 (Europe) Ltd. Liberty House, Bulls Copse Road Houndsdown Business Park Southampton, SO40 9RB, U.K. p:44/0870.8501241 f:44/0870.8501251 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 AT, Inc.
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SYSTEM OVERVIEW FLIGHT INSTRUMENTS ENGINE INDICATION SYSTEM AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AUTOMATIC FLIGHT CONTROL SYSTEM ADDITIONAL FEATURES APPENDICES INDEX
Copyright © 2006-2009 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0552.05 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. Tel: 503/391.
Limited Warranty LIMITED WARRANTY This Garmin product is warranted to be free from defects in materials or workmanship for two years from the date of purchase. Within this period, Garmin will, at its sole option, repair or replace any components that fail in normal use. Such repairs or replacement will be made at no charge to the customer for parts and labor, provided that the customer shall be responsible for any transportation cost.
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: The Garmin G1000, 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. Although unlikely, it may be possible for erroneous operation to occur without a fault indication shown by the G1000.
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.
Revision Information Record of Revision Part Number 190-00590-00 190-00590-00 190-00590-00 190-00590-00 Revision 1 A B C Date 3/13/06 3/21/07 4/3/07 6/22/07 Page Range All All All All 190-00590-01 A 10/13/08 All 190-00590-02 A 7/31/09 All 190-00590-02 Rev. A Description Initial release Production Release Added Print Specification Reference to Cover Sheet Revised AMPS Engine Gauge Added GDU 8.
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.................................... 126 Clearance Recorder and Player................................... 127 Entertainment Inputs................................................. 128 4.6 Audio Panels Preflight Procedure....................... 129 4.7 Abnormal Operation............................................ 131 Stuck Microphone..................................................... 131 COM Tuning Failure...................................................
Table of Contents Section 7 Automatic Flight Control System 7.1 S-TEC Fifty Five X Autopilot (Optional)............. 349 8.1 8.2 8.3 8.4 8.5 8.6 8.7 8.8 8.9 8.10 8.11 viii Section 8 Additional Features Synthetic Vision System (SVS)............................ 352 SVS Operation. ......................................................... 353 SVS Features............................................................. 355 Field of View.............................................................
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 AUDIO PANEL & CNS 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 • GDC 74A (2) – The Air Data Computer (ADC) processes data from the pitot/static system and outside air temperature (OAT) sensor. The ADC provides pressure altitude, airspeed, vertical speed, and OAT information to the G1000 System, and it communicates with the primary IAU, displays, and AHRS using an ARINC 429 digital interface.
SYSTEM OVERVIEW system overview FLIGHT INSTRUMENTS • GMU 44 (2) – The Magnetometer measures local magnetic field and sends data to the AHRS for processing to determine aircraft magnetic heading. This unit receives power directly from the AHRS and communicates with it via an RS-485 digital interface.
system overview PFD #1 GMA 1347 Audio Panel #1 GDU 1040 MFD GMA 1347 Audio Panel #2 SYSTEM OVERVIEW GDU 1040 GDU 1040 PFD #2 FLIGHT INSTRUMENTS EIS GDL 69A Data Link GIA 63W #1 Integrated Avionics Unit GDC 74A #1 GDC 74A #2 Air Data Computer Air Data Computer OAT Airspeed Altitude Vertical Speed OAT Airspeed Altitude ed Vertical Speed GRS 77 #1 AHRS GRS 77 #2 AHRS Attitude Rate of Turn Slip/Skid Attitude Rate of Turn Slip/Skid GMU 44 #1 System Integration Processors I/O Processors V
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 light blue 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
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 unavailable available unavailable available unavailable available unavailable available available AHRS no-GPS Mode AUDIO PANEL & CNS cNS AHRS no- AHRS no-Mag/ Mag Mode no-Air Mode Heading Invalid Air Data le ab ail av un AHRS Normal Operation Magnetometer Data EIS Air Data FLIGHT INSTRUMENTS Magnetometer Data SYSTEM OVERVIEW GPS Data Attitude/Heading Invalid FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 1-12 AHRS Operation GPS Input Failure AFCS Two GPS inputs are prov
SYSTEM OVERVIEW system overview G1000 System Annunciations NOTE: For a detailed description of all annunciations and alerts, refer to Appendix A. Refer to the Aircraft FLIGHT INSTRUMENTS Flight Manual (AFM) for additional information regarding pilot responses to these annunciations. EIS When an LRU or an LRU function fails, a large red ‘X’ is typically displayed over the instrument experiencing failed data (Figure 1-10 displays all possible flags and responsible LRUs).
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.
SYSTEM OVERVIEW system overview 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 AHRS1 AHRS2 PFD EIS FLIGHT INSTRUMENTS SYN VIS PATHWAY SYN TERR Displays rectangular boxes representing the horizontal and vertical flight path of the active flight plan Enables synthetic terrain depiction HRZN HDG Displays compass heading along the Zero-Pitch line APTSIGNS
system overview EIS TMR/REF NRST ALERTS 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 AUDIO PANEL & CNS cNS Select the BACK Softkey to return to the previous level softkeys. Figure 1-19 XPDR Softkeys MFD Softkeys APPENDICES INDEX Garmin G1000 Pilot’s Guide for the Quest Kodiak 100 ADDITIONAL FEATURES 190-00590-02 Rev.
SYSTEM OVERVIEW system overview Selects desired amount of map detail; cycles through declutter levels: DCLTR (No Declutter): All map features visible DCLTR-1: Declutters land data DCLTR-2: Declutters land and SUA data DCLTR-3: Removes everything except for the active flight plan When available, displays airport and terminal procedure charts When available, displays checklists FLIGHT INSTRUMENTS DCLTR (3) SHW CHRT CHKLIST ENGINE DCLTR SHW CHRT CHKLIST EIS MAP AUDIO PANEL & CNS DCLTR-1 DCLTR-2 FLI
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 HAZARD AVOIDANCE GPS Selection Softkeys RAIM Softkey Selected SBAS Softkey Selected Figure 1-22 GPS Status Page (RAIM or SBAS Selected) The GPS Status Page provides the following information: • Satellite constellation diagram AFCS Satellites
system overview SYSTEM OVERVIEW The current calculated GPS position, time, altitude, ground speed, and track for the aircraft are displayed below the satellite signal accuracy measurements. • GPS receiver status 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.
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 Disabling WAAS or MSAS 1) Select the GPS Status Page. 2) If necessary, press the SBAS Softkey. FLIGHT INSTRUMENTS 3) Press the FMS Knob, and turn the large FMS Knob to hightlight ‘MSAS’ or ‘WAAS’. 4) Press the ENT Key to uncheck the box. 5) Press the FMS Knob to remove the cursor. EIS • GPS Satellite Signal Strengths The GPS Status Page can be helpful in troubleshooting weak (or missing) signal levels due to poor satellite coverage or installation problems.
SYSTEM OVERVIEW system overview FLIGHT INSTRUMENTS No Options for NRST Window Options for FPL Window Figure 1-23 Page Menu Examples EIS Data Entry Using the FMS Knob to enter data: AUDIO PANEL & CNS 1) If needed, press the FMS Knob to activate the cursor. 2) Use the large FMS Knob to highlight the desired field. 3) Begin entering data by turning the small FMS Knob to select a character for the first placeholder.
system overview SYSTEM OVERVIEW Page Group MFD Active Page Title FLIGHT INSTRUMENTS Pages in Current Group EIS AUDIO PANEL & CNS cNS Page Groups Figure 1-24 Page Title and Page Groups FLIGHT MANAGEMENT The main page groups are navigated using the FMS Knob; specific pages within each group can vary depending on the configuration of optional equipment.
SYSTEM OVERVIEW system overview • Waypoint Page Group (WPT) Airport/Procedures/Weather Information Pages FLIGHT INSTRUMENTS - Airport Information (INFO-1 Softkey) - Airport Directory Information (INFO-2 Softkey) - Departure Information (DP Softkey) EIS - Arrival Information (STAR Softkey) AUDIO PANEL & CNS - Approach Information (APR Softkey) - Weather Information (optional) (WX Softkey) FLIGHT MANAGEMENT Intersection Information Airport/ Procedures/ Weather Information Pages NDB Information VOR
system overview SYSTEM OVERVIEW • Nearest Page Group (NRST) Nearest Airports Nearest Intersections FLIGHT INSTRUMENTS Nearest NDB Nearest VOR Nearest User Waypoints Nearest Frequencies EIS Nearest Airspaces AUDIO PANEL & CNS cNS Figure 1-28 Nearest Pages FLIGHT MANAGEMENT • Flight Plan Page Group (FPL) Active Flight Plan Flight Plan Catalog HAZARD AVOIDANCE - Stored Flight Plan (NEW Softkey) AFCS ADDITIONAL FEATURES Figure 1-29 Flight Plan Pages APPENDICES There are also several pages (Airpor
SYSTEM OVERVIEW system overview FLIGHT INSTRUMENTS The Procedure Loading pages may be accessed at any time on the MFD by pressing the PROC Key. A menu is initialized, and when a departure, approach, or arrival is selected, the appropriate Procedure Loading page is opened. These pages can also be accessed from the Active and Stored Flight Plan pages using the LD softkeys. Turning the FMS Knob does not scroll through the Procedure Loading pages (note the single page icon in the lower right corner).
system overview SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS cNS FLIGHT MANAGEMENT AFCS ADDITIONAL FEATURES APPENDICES INDEX 33 Garmin G1000 Pilot’s Guide for the Quest Kodiak 100 190-00590-02 Rev.
SYSTEM OVERVIEW system overview Pilot Profiles HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS System settings may be saved under a pilot profile. When the system is powered on, the last selected pilot profile is shown on the MFD Power-up Splash Screen. The G1000 can store up to 25 profiles; the currently active profile, the amount of memory used, and the amount of memory available are shown at the top of the System Setup Page in the box labeled ‘Pilot Profile’.
system overview SYSTEM OVERVIEW 8) With ‘CREATE’ highlighted, press the ENT Key to create the profile Or: Use the large FMS Knob to select ‘CREATE and ACTIVATE’ and press the ENT Key to activate the new profile. FLIGHT INSTRUMENTS 9) To cancel the process, select ‘CANCEL’ with the large FMS Knob and press the ENT Key. Selecting an active profile: 1) Select the AUX - System Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor.
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 Settings Magnetic (North)* True (North) User Fuel and Fuel Flow** Weight** Position All temperatures on PFD Total Air Temperature (Trip Planning Page) Fuel parameters (Trip Planning Page) Engine Indication System (EIS) N/A N/A All positions N/A AFCS ADDITIONAL FEATURES Celsius* Fahrenheit Pounds* Gallons Pounds* Kilograms HDDD°MM.MM’* HDDD°MM’SS.
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 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 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 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.
SYSTEM OVERVIEW system overview The ANN TEST Softkey, when selected, causes an annunciation test tone to be played. FLIGHT INSTRUMENTS Selecting the SYNC DBS Softkey (label background changes to grey indicting the softkey is selected) activates the Automatic Database Synchronization feature. When this feature is active, databases are updated automatically in the MFD and both PFDs from one SD card. For a detailed discussion on database synchronization, see the SD Card Use section in the Appendices.
system overview SYSTEM OVERVIEW Setting the generic timer (PFD): 1) Press the TMR/REF Softkey. 2) Turn the large FMS Knob to select the timer field (hh/mm/ss). FLIGHT INSTRUMENTS 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?’.
AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW system overview Figure 1-38 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. HAZARD AVOIDANCE 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. 2) Press the MENU Key. FLIGHT INSTRUMENTS 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 Scheduler FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS The G1000’s Scheduler feature can be used to enter and display reminder messages (e.g., “Change oil”, “Switch fuel tanks”, “Overhaul”) 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).
system overview SYSTEM OVERVIEW 9) For event-based messages: a) Use the FMS Knob to enter the desired date (DD-MMM-YYY) and press the ENT Key. b) Press the ENT Key again or use the large FMS Knob to move the cursor to the next field. FLIGHT INSTRUMENTS c) Use the FMS Knob to enter the desired time (HH:MM) and press the ENT Key. 10) Press the ENT Key again or use the large FMS Knob to move the cursor to enter the next message. Deleting a scheduler message: 1) Select the AUX - Utility Page.
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.
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 20 19 18 1 17 16 15 2 EIS 14 AUDIO PANEL & CNS 13 3 12 4 11 10 5 FLIGHT MANAGEMENT 9 8 6 ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE 7 1 NAV Frequency Box 11 Turn Rate Indicator 2 Airspeed Indicator 12 Barometric Altimeter Setting 3 True Airspeed 13 Vertical Speed Indicator (VSI) 4 Current Heading 14 Reference Altitude Bug 5 Horizontal Situation Indicator ( HSI) 15 Altimeter 6 Outside Air Temperature (OAT) 16 Ref
Flight Instruments SYSTEM OVERVIEW 14 15 FLIGHT INSTRUMENTS 13 1 12 11 EIS 10 2 9 AUDIO PANEL & CNS 8 3 7 4 6 8 Annunciation Window 2 Selected Heading 9 Selected Course 3 Wind Data Box 10 4 Inset Map Required Vertical Speed Indicator 11 Vertical Deviation Indication 5 Bearing Information Windows 12 Comparator Window 6 Minimum Descent Altitude/ Decision Height Flight Plan Window 13 VNV Target Altitude 14 Terrain Annunciation 15 AFCS Annunciation AFCS Traffic Annunciation
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 numeric labels and major tick marks on the moving tape are marked at intervals of 10 knots.
Flight Instruments SYSTEM OVERVIEW Vspeeds (Vref and Vclimb) can be changed and their flags turned on/off from the Timer/References Window. When active (on), the Vspeeds are displayed to the right of the airspeed scale. All Vspeed values are reset and all flags turned off during power up. FLIGHT INSTRUMENTS Changing Vspeeds and turning flags on/off: 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 (Figure 2-7). Note that the altitude tape does not change scale. Displaying altitude in meters: FLIGHT INSTRUMENTS 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. 3) Turn the large FMS Knob to highlight BARO in the Synchronization box.
SYSTEM OVERVIEW Flight Instruments A Baro Transition Alert is provided to alert the pilot to change the barometric pressure setting when crossing the transition altitude in either direction. This is displayed by the flashing light blue barometric pressure setting when crossing the transition altitude. FLIGHT INSTRUMENTS Setting the Baro Transition Alert: 1) Use the FMS Knob to select the AUX - System Setup Page on the MFD. 2) Press the FMS Knob to activate the cursor.
Flight Instruments SYSTEM OVERVIEW Vertical Speed Indicator (VSI) FLIGHT INSTRUMENTS The Vertical Speed Indicator (VSI; Figure 2-11) displays the aircraft vertical speed on a fixed scale with labels at 1000 and 2000 fpm and minor tick marks every 500 fpm. Digits appear in the pointer when the climb or 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.
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. A digital reading of the current heading appears on top of the HSI, and the current track is represented on the HSI by a magenta diamond.
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 light blue tuning box over the NAV2 standby frequency. 1) Press the CDI Softkey to change from GPS to VOR1 or LOC1. This places the light blue 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 turns yellow on both displays if not synchronized (Figure 2-22). 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 CDI scale varies if VTF is activated 0.3 nm 1.0 nm 2 nm FAF EIS 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 Enabling/disabling OBS Mode while navigating a GPS flight plan: 1) Press the OBS Softkey to select OBS Mode. FLIGHT INSTRUMENTS 2) Turn the CRS Knob to select the desired course to/from the waypoint. Press the CRS Knob to synchronize the Selected Course with the bearing to the next waypoint. 3) Press the OBS Softkey again to return to automatic waypoint sequencing.
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 The Annunciation Window appears to the right of the Vertical Speed Indicator (Figure 2-34) and displays abbreviated annunciation text for aircraft alerts. Warnings appear in red, cautions in yellow, advisory alerts 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.
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. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 2-37 Traffic and Example TAWS Annunciations AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00590-02 Rev.
SYSTEM OVERVIEW Flight Instruments Altitude Alerting FLIGHT INSTRUMENTS Altitude Alerting provides the pilot with a visual alert when approaching the Selected Altitude. Whenever the Selected Altitude is changed, the Altitude Alerter is reset. The Altitude Alerter is independent of the GFC 700 AFCS, but alerting tones are heard only when the GFC 700 is installed. The following occur when approaching the Selected Altitude: • Upon passing through 1000 feet of the Selected Altitude an aural tone is heard.
Flight Instruments SYSTEM OVERVIEW Minimum Descent Altitude/Decision Height Alerting FLIGHT INSTRUMENTS For altitude awareness, a barometric Minimum Descent Altitude (MDA) or Decision Height (DH) can be set in the Timer/References Window and is reset when the power is cycled. When active, the altitude setting is displayed to the bottom left of the Altimeter. Once the altitude is within the range of the tape, a bug appears at the reference altitude on the Altimeter.
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 Unusual Attitudes Nose High FLIGHT INSTRUMENTS When the aircraft enters an unusual pitch attitude, red chevrons pointing toward the horizon warn of extreme pitch. The chevrons are displayed on the Attitude Indicator, starting at 50˚ above and 30˚ below the horizon line.
INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Flight Instruments Blank Page 82 Garmin G1000 Pilot’s Guide for the Quest Kodiak 100 190-00590-02 Rev.
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 readouts, CHRT CHKLIST and slideENGINE bars. Green bandsMAP and readouts indicate normal ranges of operation; yellow DCLTR and redSHW 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 11 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 tr
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 92 Garmin G1000 Pilot’s Guide for the Quest Kodiak 100 190-00590-02 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) 94 Garmin G1000 Pilot’s Guide for the Quest Kodiak 100 190-00590-02 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. 96 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 or the ENT Key. 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 190-00590-02 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 Flight ID Reporting NOTE: If the Flight ID is required but the system is not configured for it, contact a Garmin-authorized service FLIGHT INSTRUMENTS center for configuration. When the Flight ID must be entered before flight operation, the identifier is placed in the Timer/References Window on the PFD. The Flight ID is not to exceed seven characters. No space is needed when entering Flight ID.
Audio Panel and CNS SYSTEM OVERVIEW 4.5 Additional Audio Panel Functions Power-up FLIGHT INSTRUMENTS 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.
SYSTEM OVERVIEW Intercom FLIGHT INSTRUMENTS Audio Panel and CNS 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. EIS 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.
Audio Panel and CNS SYSTEM OVERVIEW 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.
SYSTEM OVERVIEW Audio Panel and CNS 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.
Audio Panel and CNS SYSTEM OVERVIEW Clearance Recorder and Player FLIGHT INSTRUMENTS NOTE: Pressing the play key on the pilot’s Audio Panel plays recorded audio to the pilot. Pressing the play 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.
SYSTEM OVERVIEW Audio Panel and CNS 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.
Audio Panel and CNS SYSTEM OVERVIEW 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 are at maximum volume setting. On single‑pilot flights, verify that all other headsets are not connected to avoid excess noise in the audio system.
SYSTEM OVERVIEW Audio Panel and CNS 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 that the MAN SQ Annunciator is extinguished. 3) Turn the PILOT/PASS Knobs clockwise two full turns.
Audio Panel and CNS SYSTEM OVERVIEW 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.
SYSTEM OVERVIEW Audio Panel and CNS 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.
Audio Panel and CNS SYSTEM OVERVIEW 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.
INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Audio Panel and CNS Blank Page 134 Garmin G1000 Pilot’s Guide for the Quest Kodiak 100 190-00590-02 Rev.
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 part 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 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 Aircraft Icon at Present
Flight Management SYSTEM OVERVIEW Navigation Status Box The Navigation Status Box located at the top of the PFD contains two fields displaying the following information: FLIGHT INSTRUMENTS PFD Navigation Status Box • Active flight plan leg (e.g., ‘D-> KICT’ or ‘KIXD -> KCOS’) or flight plan annunciations (e.g., ‘Turn right to 021˚ in 8 seconds’) EIS • Distance (DIS) and Bearing (BRG) to the next waypoint or flight plan annunciations (e.g.
SYSTEM OVERVIEW Flight Management 4) Turn the small FMS Knob to display and scroll through the data options list. 5) Select the desired data. FLIGHT INSTRUMENTS 6) Press the ENT Key. Pressing the DFLTS Softkey returns any field to its default setting. 5.2 Using Map Displays FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS Map displays are used extensively in the G1000 to provide situational awareness in flight.
Flight Management SYSTEM OVERVIEW • North up (NORTH UP) aligns the top of the map display to north (default setting). • Track up (TRK UP) aligns the top of the map display to the current ground track. • Desired track up (DTK UP) aligns the top of the map display to the desired course. FLIGHT INSTRUMENTS • Heading up (HDG UP) aligns the top of the map display to the current aircraft heading.
SYSTEM OVERVIEW Flight Management Map Group Selection AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Orientation Field Figure 5-5 Map Setup Menu Window - Map Group FLIGHT MANAGEMENT 4) Turn the small FMS Knob to select the desired orientation. 5) Press the ENT Key to select the new orientation. 6) Press the FMS Knob to return to the base page. HAZARD AVOIDANCE Map Range AFCS There are 28 different map ranges available, from 500 feet to 2000 nm.
Flight Management SYSTEM OVERVIEW Auto Zoom FLIGHT INSTRUMENTS Auto zoom allows the G1000 to change the map display range to the smallest range clearly showing the active waypoint. Auto zoom can be overridden by adjusting the range with the Joystick, and remains until the active waypoint changes, a terrain or traffic alert occurs, the aircraft takes off, or the manual override times out (timer set on Map Setup Window).
SYSTEM OVERVIEW Flight Management Auto Zoom: FLIGHT INSTRUMENTS Off, MFD Only, PFD Only, All On AUDIO PANEL & CNS EIS Manual Range Override Expiration Time Maximum Look Forward Time Minimum Look Forward Time Figure 5-7 Map Setup Menu Window - Map Group, Auto Zoom Configuring automatic zoom: FLIGHT MANAGEMENT 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.
Flight Management SYSTEM OVERVIEW Map Panning Map panning allows the pilot to: • View parts of the map outside the displayed range without adjusting the map range FLIGHT INSTRUMENTS • Highlight and select locations on the map • Review information for a selected airport, NAVAID or user waypoint • Designate locations for use in flight planning • View airspace and airway information EIS When the panning function is selected by pressing the Joystick, the Map Pointer flashes on the map display.
SYSTEM OVERVIEW Flight Management FLIGHT INSTRUMENTS When the Map Pointer is placed on an object, the name of the object is highlighted (even if the name was not originally displayed on the map). When any map feature or object is selected on the map display, pertinent information is displayed.
Flight Management SYSTEM OVERVIEW Panning the map: 1) Press the Joystick to display the Map Pointer. 2) Move the Joystick to move the Map Pointer around the map. FLIGHT INSTRUMENTS 3) Press the Joystick to remove the Map Pointer and recenter the map on the aircraft’s current position. Reviewing information for an airport, NAVAID, or user waypoint: 1) Place the Map Pointer on a waypoint. 2) Press the ENT Key to display the Waypoint Information Page for the selected waypoint.
SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS 2) Press the ENT Key to display an options menu. 3) ‘Review Airspace?’ should already be highlighted, if not select it. Press the ENT Key to display the Airspace Information Page for the selected airspace. EIS 4) Press the CLR or ENT Key to exit the Airspace Information Page.
Flight Management SYSTEM OVERVIEW 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.
SYSTEM OVERVIEW Flight Management 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 Management SYSTEM OVERVIEW FLIGHT INSTRUMENTS TOPO DATA Range EIS TOPO DATA On/Off AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT Note: Since the PFD Inset Map is much smaller than the MFD navigation maps, items are removed on the PFD Inset Map two range levels smaller than the range selected in the Map Setup pages (e.g.
SYSTEM OVERVIEW Maximum Displayed Elevation FLIGHT INSTRUMENTS Flight Management Aircraft Altitude (MSL) Minimum Displayed Elevation Range of Displayed Elevations AUDIO PANEL & CNS EIS Ground Elevation at Map Pointer Location (only visible when Map Pointer is displayed) 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.
Flight Management SYSTEM OVERVIEW 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.
SYSTEM OVERVIEW Flight Management Aviation Symbols The following items are configured on the aviation menu: Aviation Symbols FLIGHT INSTRUMENTS (Text label size can be None, Small, Medium (Med), or Large (Lrg) EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES Default Maximum Range (nm) Range (nm) Active Flight Plan Leg (ACTIVE FPL) 2000 2000 Non-active Flight Plan Leg (ACTIVE FPL) 2000 2000 2000 250 150 50 3 Off 15 2000 500 300 100 20 100 30 Non-directional Beaco
Flight Management SYSTEM OVERVIEW Symbol Setup All pages with maps can display land symbols (roads, lakes, borders, etc). Land symbols can be removed totally (turned off). FLIGHT INSTRUMENTS 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.
SYSTEM OVERVIEW Flight Management 7) Press the ENT Key to accept the selected range. FLIGHT INSTRUMENTS 8) Press the FMS Knob to return to the Navigation Map Page.
Flight Management SYSTEM OVERVIEW Map Declutter 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. FLIGHT INSTRUMENTS Declutter Level DCLTR Softkey EIS Navigation Map Page Menu Figure 5-21 Navigation Map - Declutter Level Indications AUDIO PANEL & CNS Decluttering the map: Press the DCLTR Softkey with the Navigation Map Page displayed.
SYSTEM OVERVIEW Flight Management Table 5-3 lists the items displayed at each declutter level. The ‘X’ represents map items displayed for the various levels of declutter.
Flight Management SYSTEM OVERVIEW 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.
SYSTEM OVERVIEW Flight Management Airways may be displayed on the map at the pilot’s discretion using either a combination of AIRWAYS Softkey presses, or menu selections using the MENU Key from the Navigation Map Page. The Airway range can also be programmed to only display Airways on the MFD when the map range is at or below a specific number. FLIGHT INSTRUMENTS Displaying/removing airways: 1) Select the MAP Softkey. 2) Select the AIRWAYS Softkey.
Flight Management SYSTEM OVERVIEW The following range items are configurable on the airways menu: Airway Type Symbol Low Altitude Airway (LOW ALT AIRWAY) 300 High Altitude Airway (HI ALT AIRWAY) FLIGHT INSTRUMENTS Default Maximum Range (nm) Range (nm) 200 500 500 Table 5-4 Airway Range Information EIS Track Vector AUDIO PANEL & CNS The Navigation Map can display a track vector that is useful in minimizing track angle error.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW Flight Management Wind Vector On/Off EIS Nav Range Ring On/Off Track Vector - On/Off - Look Ahead Time AUDIO PANEL & CNS Fuel Range - On/Off - Fuel Reserve Time Figure 5-25 Navigation Map Setup Menu -TRACK VECTOR, WIND VECTOR, NAV RANGE RING, FUEL RANGE RING Setup Wind Vector FLIGHT MANAGEMENT The map displays a wind vector arrow in the upper right-hand portion of the screen.
Flight Management SYSTEM OVERVIEW Nav Range Ring 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).
SYSTEM OVERVIEW Flight Management Fuel Range Ring 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.
Flight Management SYSTEM OVERVIEW 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.
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 5-31 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 following are types of AOPA airport directory information shown (if available) on the Airport Directory Page: • Services Available: Category, Specific Service • Notes: Airport Notes • Pilot Controlled Lighting: High/Med/Low Clicks/Second • FBO: Type, Frequencies, Services, Fees, Fuel, Credit Cards, Phone/Fax Numbers FLIGHT MANAGEMENT • Transportation: Ground Transportation Type Available • Approach: Approach Facility Name, Frequency, Frequency Parameter • Instrumen
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 2) Turn the small FMS Knob to select the desired runway. 3) Press the FMS Knob to remove the flashing cursor. See the Audio Panel and CNS Section for frequency selection and the Procedures section for approaches. FLIGHT INSTRUMENTS The Nearest Airports Box on the System Setup Page defines the minimum runway length and surface type used when determining the 25 nearest airports to display on the MFD Nearest Airports Page.
SYSTEM OVERVIEW Flight Management Intersections FLIGHT INSTRUMENTS Note: The VOR displayed on the Intersection Information Page is the nearest VOR, not necessarily the VOR 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’s 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 or bearing from two existing waypoints.
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 5-45 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 wa
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 5) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’. 6) Press the ENT Key again to activate the direct-to. Cancelling a Direct-to: FLIGHT INSTRUMENTS 1) Press the Direct-to Key to display the Direct-to Window. 2) Press the MENU Key. 3) With ‘Cancel Direct-To NAV’ highlighted, press the ENT Key. If a flight plan is still active, the G1000 resumes navigating the flight plan along the closest leg.
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 5-57 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 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 2) Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page.
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 on the Control Unit 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. Exporting a Flight Plan to an SD Card 1) Insert the SD card into the top card slot on the MFD.
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 5-68 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.TIFTO2.
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 5-71 Arrival Loading Page - Selecting the Transition FLIGHT MANAGEMENT Inserted Arrival Header HAZARD AVOIDANCE - 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 Approaches Available at KCOS Preview of Selected Approach EIS Approach Waypoint Sequence AUDIO PANEL & CNS Figure 5-74 Approach Loading Page - Selecting the Approach FLIGHT MANAGEMENT HAZARD AVOIDANCE Inserted Approach Header - Approach Identifier: [approach airport].
SYSTEM OVERVIEW Flight Management 3) Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight the desired flight plan. 4) The Flight Plan Information is displayed showing departure, destination, total distance, and enroute safe altitude information for the selected Flight Plan. FLIGHT INSTRUMENTS 5) Press the EDIT Softkey to open the Stored Flight Plan Page and view the waypoints in the flight plan. 6) Press the FMS Knob to exit the Stored Flight Plan Page.
Flight Management SYSTEM OVERVIEW 3) Highlight ‘Sort By Comment’ and press the ENT Key. A confirmation window is displayed. 4) With ‘OK’ highlighted, press the ENT Key to change flight plan ordering. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. FLIGHT INSTRUMENTS Activate a Flight Plan Activating a stored flight plan erases the active flight plan and replaces it with the flight plan being activated.
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. 3) Press the DELETE Softkey; press the CLR Key; or press the MENU Key, highlight ‘Delete Flight Plan’, and press the ENT Key.
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. 8) Press the FMS Knob to remove the flashing cursor.
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 5-79 Parallel Track Window Parallel Track Waypoints - TIFTO-p - TOP-p - SLN-p - HYS-p - LAA-p Activating Parallel Track affects the entire active flight segment (e.g.
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).
Flight Management SYSTEM OVERVIEW FLIGHT INSTRUMENTS New Active Flight Plan Leg EIS Confirmation Window AUDIO PANEL & CNS Figure 5-84 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.
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 5-86 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 Q3.FEPOT Airway EIS FLIGHT INSTRUMENTS Collapsed View Expanded View AUDIO PANEL & CNS Figure 5-87 Expanded/Collapsed Airways 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 MANAGEMENT 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 5.7 Vertical Navigation FLIGHT INSTRUMENTS Note: The G1000 supports vertical navigation for all lateral leg types except for CA, CI, FA, FM, HA, HM, PI, 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 Light Blue Text Light Blue 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 An altitude constraint is invalid if: • Meeting the constraint requires the aircraft to climb FLIGHT INSTRUMENTS • Meeting the constraint requires the maximum flight path angle (6° down) or maximum vertical speed (-6000 fpm) to be exceeded • The altitude constraint results in a TOD behind the aircraft present position • The constraint is within a leg type for which altitude constraints are not supported • The altitude constraint is added to the FAF of an approach that
SYSTEM OVERVIEW Flight Management Reverting a manually entered altitude constraint back to the navigation database value: 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 ‘REVERT’ 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 5-91 Departure Selection Loaded Departure ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Selected Departure Procedure Loading Page Selection Softkeys INDEX APPENDICES Figure 5-92 Departure Loading 232 Garmin G1000 Pilot’s Guide for the Quest Kodiak 100 190-00590-02 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.
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 5-94 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 3) Press the ENT 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 INSTRUMENTS Or: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD) 2) Press the FMS Knob, and turn to highlight the arrival header in the active flight plan. 3) Press the CLR Key.
Flight Management SYSTEM OVERVIEW Example on HSI EIS Approach Type - LNAV - LNAV+V - L/VNAV - LPV AUDIO PANEL & CNS FLIGHT MANAGEMENT HSI Annunciation Description LNAV GPS approach using published LNAV minima LNAV+V GPS approach using published LNAV minima.
SYSTEM OVERVIEW Flight Management Destination Airport AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Available Procedure Actions Loaded Procedures Approach Preview Approach Choices FLIGHT MANAGEMENT Figure 5-95 Approach Selection Loaded Approach ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Selected Approach Procedure Loading Page Selection Softkeys APPENDICES Viewing available approaches at an airport: INDEX Figure 5-96 Approach Loading 2) To select another airport, press the FMS Knob to activate
Flight Management SYSTEM OVERVIEW 3) Press the FMS Knob, then turn the large FMS Knob to highlight the Approach. The approach is previewed on the map. FLIGHT INSTRUMENTS 4) Turn the small FMS Knob to view the available approaches. Press the ENT Key to select the approach. The cursor moves to the Runway box. The approach is previewed on the map. 5) Turn the small FMS Knob to view the available runways. Press the ENT Key to select the runway. The cursor moves to the Transition box.
SYSTEM OVERVIEW Flight Management In many cases, it may be easiest to “load” the full approach while still some distance away, enroute to the destination airport. Later, if vectored to final, use the steps above to select ‘Activate Vector-To-Final’ — which makes the inbound course to the FAF waypoint active. FLIGHT INSTRUMENTS Activating a previously loaded approach with vectors to final: 1) Press the PROC Key to display the Procedures Window.
Flight Management SYSTEM OVERVIEW Course To Altitude FLIGHT INSTRUMENTS In this missed approach procedure, the altitude immediately following the MAP (in this case ‘6368ft’) is not part of the published procedure. It is simply a Course to Altitude (CA) leg which guides the aircraft along the runway centerline until the altitude required to safely make the first turn toward the MAHP is exceeded.
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 6) Turn the FMS Knobs to enter an arrival date and press the ENT Key. 7) Press the ENT Key with ‘COMPUTE RAIM?’ highlighted to begin the computation. FLIGHT INSTRUMENTS 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. 3) Press the MENU Key, highlight ‘Set WPT to Present Position’, and press the ENT Key.
Flight Management SYSTEM OVERVIEW Enabling/Disabling SBAS: 1) Select the AUX-GPS Status Page. 2) Press the FMS Knob, and turn the large FMS Knob to highlight ‘MSAS’ or ‘WAAS’. FLIGHT INSTRUMENTS 3) 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 WAAS 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 5-106. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 5-106 Assigned Heading of 290º 4) Enter V4 into the flight plan. a) Press the FMS Knob to activate the cursor. AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00590-02 Rev.
SYSTEM OVERVIEW Flight Management 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 5-107. 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 5-109. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-109 TOP Inserted into the Flight Plan e) With SLN still highlighted as in Figure 5-109, 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 5-110.
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 5-111. FLIGHT MANAGEMENT Figure 5-111 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 5-111. 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 5-113. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-113 V4 is Loaded in the Flight Plan 5) Making V4 the active leg of the flight plan. a) Press the FMS Knob to activate the cursor. HAZARD AVOIDANCE b) Turn the large FMS Knob to highlight SLN. The TO waypoint of the leg is selected in order to activate the leg. c) Press the ACT LEG Softkey.
SYSTEM OVERVIEW Flight Management HAZARD AVOIDANCE 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 5-115, 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 5-116. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-116 Turn on to Active Leg HAZARD AVOIDANCE 8) At SLN, Victor Airway 244 (V244) is intercepted. Turn prompts are displayed in the PFD Navigation Status Box as seen in Figure 5-117. AFCS ADDITIONAL FEATURES APPENDICES Figure 5-117 Turn to Intercept V244 INDEX 190-00590-02 Rev.
SYSTEM OVERVIEW Flight Management FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS 9) As seen in Figure 5-118, V244 is now the active flight plan leg. INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Figure 5-118 V244 Now Active Leg 260 Garmin G1000 Pilot’s Guide for the Quest Kodiak 100 190-00590-02 Rev.
Flight Management SYSTEM OVERVIEW 10) At Lamar VOR (LAA) V263 is intercepted. See Figure 5-119. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-119 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 5-121. FLIGHT MANAGEMENT Figure 5-121 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 5-122.
Flight Management SYSTEM OVERVIEW FLIGHT INSTRUMENTS h) Press the ENT Key twice to activate the direct-to. Note, in Figure 5-123, the magenta arrow indicating the directto 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 5-124. FLIGHT MANAGEMENT Figure 5-124 Procedures Window ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE c) Press the ENT Key. A list of available approaches for the destination airport is displayed as in Figure 5-125. APPENDICES Figure 5-125 List of Available Approaches INDEX d) Turn either FMS Knob to select the LPV approach for 35R as shown in Figure 5-125.
Flight Management SYSTEM OVERVIEW e) Press the ENT Key. A list of available transitions for the selected approach is displayed as in Figure 5-126. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-126 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 5-127 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 5-128. INDEX Figure 5-128 Loaded Approach 266 Garmin G1000 Pilot’s Guide for the Quest Kodiak 100 190-00590-02 Rev.
Flight Management SYSTEM OVERVIEW 13) Note the altitude constraints associated with each of the approach waypoints as seen in Figure 5-129. These altitudes are loaded from the database and are displayed as light blue text, indicating these values are “designated” for use in computing vertical deviation guidance. a) Press the FMS Knob to activate the cursor. b) Turn the small FMS Knob to highlight the desired altitude. c) Press the CLR Key. d) Press the FMS Knob to deactivate 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 5-130.
Flight Management SYSTEM OVERVIEW 15) As seen in Figure 5-131, 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 5-132. When the aircraft is within one minute of the TOD, it is annunciated as shown in Figure 5-132, 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 which places the VSI pointer in line with the RVSI as shown in Figure 5-133.
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 5-135. 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 5-136. The magenta arrow in the flight plan list now indicates the OPSHN to FSHER leg of the arrival procedure is now active. Figure 5-136 Tracking the OPSHN to FSHER Leg HAZARD AVOIDANCE 20) The flight continues through the arrival procedure to PYNON (see Figure 5-137).
Flight Management SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Figure 5-137 Approaching PYNON INDEX 190-00590-02 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 5-138).
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 5-140 Descending Turn to the Initial Approach Fix (IAF) HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00590-02 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 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 5-142. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-142 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 5-143. 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 5-144. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-144 Establishing the Holding Pattern 27) The aircraft maintains 10,000 feet while following the magenta line through the hold as in Figure 5-145.
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 & Bearing FLIGHT INSTRUMENTS Dead Reckoning Annunciaion Wind Data Current Track Indicator EIS GPS Navigation Lost Message AUDIO PANEL & CNS Bearing Pointer/ Distance Navigation Data Bar Wind Data FLIGHT MANAGEMENT All data except Active Leg, TAS, and DTK are in yellow Dead Reckoning Annunciation HAZARD AVOIDANCE Subdued Aircraft Symbol AFCS Figure 5-146 Dead Reckoning Mode - GPS Derived Data Shown in Yellow ADDITIONAL FEATURES Note: The Inset Map
INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Flight Management Blank Page 282 Garmin G1000 Pilot’s Guide for the Quest Kodiak 100 190-00590-02 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 Activating Services FLIGHT INSTRUMENTS Before XM Satellite Weather can be used, the service must be activated. Service is activated by providing XM Satellite Radio with coded IDs unique to the installed GDL 69A. XM Satellite Radio and XM Satellite Weather services each have coded IDs. The Data and Audio Radio IDs must be provided to XM Satellite Radio to activate the weather service and entertainment subscriptions, respectively.
Hazard Avoidance SYSTEM OVERVIEW Using XM Satellite Weather Products The primary map for viewing XM Weather data is the Weather Data Link Page in the Map Page Group. This is the only G1000 map display capable of showing information for all available XM weather products. FLIGHT INSTRUMENTS Viewing the Weather Data Link Page: 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Weather Data Link Page.
SYSTEM OVERVIEW Hazard Avoidance Expiration Time (Minutes) 30 Refresh Rate (Minutes) 5 Cloud Top (CLD TOP) 60 15 Echo Top (ECHO TOP) 30 7.5 XM Lightning (LTNG) 30 5 Cell Movement (CELL MOV) 30 1.
Hazard Avoidance SYSTEM OVERVIEW Cloud Top (CLD TOP) + Echo Top (ECHO TOP) + Nearest Page Group Flight Plan Pages + AUX - Trip Planning Page Weather Data Link Page + Weather Information Page Navigation Map Page + + + + + + + + + + Cell Movement (CELL MOV) + + + + + + + + + + City Forecast (CITY) + Surface Analysis (SFC) + Freezing Levels (FRZ LVL) + Winds Aloft (WIND) + County Warnings (COUNTY) + Cyclone Warnings (CYCLONE) + Icing Potential (ICNG) + PIREPs +
SYSTEM OVERVIEW Hazard Avoidance FLIGHT INSTRUMENTS 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 Page). When a weather product is selected for display, the corresponding softkey label changes to gray to indicate the product is enabled. Unavailable weather products have subdued softkey labels (softkeys are disabled from selection).
Hazard Avoidance SYSTEM OVERVIEW Setting up and customizing the Weather Data Link Page: 1) Select the Weather Data Link Page. 2) Press the MENU Key. FLIGHT INSTRUMENTS 3) With ‘Weather Setup’ highlighted, press the ENT Key (Figure 6-4). 4) Turn the small FMS Knob to select ‘XM Product Group 1’ or ‘XM 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.
SYSTEM OVERVIEW Hazard Avoidance Weather displayed on Pages other than the Weather Data Link Page use settings based on those selected for the Navigation Map Page. FLIGHT INSTRUMENTS Setting up and customizing weather data for 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 6-6). 4) Turn the small FMS Knob to select the ‘Weather’ Group and press the ENT Key (Figure 6-7).
Hazard Avoidance SYSTEM OVERVIEW Each active weather product has an associated legend which can be displayed on the Weather Data Link Page. Viewing legends for displayed weather products FLIGHT INSTRUMENTS 1) Select the Weather Data Link Page. 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. EIS 3) Turn the FMS Knob to scroll through the legends.
SYSTEM OVERVIEW NEXRAD FLIGHT INSTRUMENTS Hazard Avoidance WSR-88D, or NEXRAD (NEXt-generation RADar), is a network of 158 high-resolution Doppler radar systems that are operated by the National Weather Service (NWS). NEXRAD data provides centralized meteorological information for the continental United States and selected overseas locations. The maximum range of a single NEXRAD radar site is 250 nm.
Hazard Avoidance SYSTEM OVERVIEW Displaying NEXRAD weather information: 1) Press the MAP Softkey (for the PFD Inset Map, press the INSET Softkey). This step is not necessary on the Weather Data Link Page. FLIGHT INSTRUMENTS 2) Press the NEXRAD Softkey. 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. The display of the information is color-coded to indicate the weather severity level.
SYSTEM OVERVIEW Hazard Avoidance 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.
Hazard Avoidance SYSTEM OVERVIEW NEXRAD Limitations (Canada) • Radar coverage extends to 55ºN. FLIGHT INSTRUMENTS • Any precipitation displayed between 52ºN and 55ºN is displayed as mixed because it is unknown. No Coverage Above 55ºN EIS AUDIO PANEL & CNS Precipitation Above 52ºN Displays As Mixed FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 6-13 NEXRAD Data - Canada AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00590-02 Rev.
SYSTEM OVERVIEW Echo Tops FLIGHT INSTRUMENTS Hazard Avoidance Echo Tops data (Figure 6-14) shows the location, elevation, and direction 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 precipitation is detected. Information is derived from NEXRAD data. HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS Note: Display of Echo Tops is mutually exclusive with Cloud Tops and NEXRAD.
Hazard Avoidance SYSTEM OVERVIEW 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 grayish-purple. Radar capability exists in these areas, but it is not active or is off-line. FLIGHT INSTRUMENTS Cloud Tops Note: Cloud Tops and Echo Tops cannot be displayed at the same time.
SYSTEM OVERVIEW XM Lightning FLIGHT INSTRUMENTS Hazard Avoidance Lightning data (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. AUDIO PANEL & CNS EIS Note: XM Lightning and optional L-3 STORMSCOPE® WX-500 Lightning are mutually exclusive.
Hazard Avoidance SYSTEM OVERVIEW Cell Movement FLIGHT INSTRUMENTS Cell Movement data (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. EIS AUDIO PANEL & CNS Storm Cells FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 6-20 Cell Movement Data On most applicable maps, Cell Movement data is selected for display along with NEXRAD.
SYSTEM OVERVIEW Hazard Avoidance SIGMETS and AIRMETS EIS 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.
Hazard Avoidance SYSTEM OVERVIEW 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 aviation database service area.
SYSTEM OVERVIEW Hazard Avoidance 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 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.
Hazard Avoidance SYSTEM OVERVIEW Surface Analysis and City Forecast Note: Surface Analysis and City Forecast data are displayed only within the installed Aviation Database FLIGHT INSTRUMENTS service area. Surface Analysis and City Forecast information is available for current and forecast weather conditions. Forecasts are available for intervals of 12, 24, 36, and 48 hours.
SYSTEM OVERVIEW Hazard Avoidance Freezing Levels HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Freezing Level data shows the color-coded contour lines for the altitude and location at which the first isotherm is found (Figure 6-30). When no data is displayed for a given altitude, the data for that altitude has not been received, or is out of date and has been removed from the display. New data appears at the next update.
Hazard Avoidance SYSTEM OVERVIEW Winds Aloft Winds Aloft data (Figure 6-32) shows the forecasted wind speed and direction at the surface and at selected altitudes. Altitude can be displayed in 3,000-foot increments up to 42,000 feet MSL. FLIGHT INSTRUMENTS Displaying Winds Aloft data: 1) Select the Weather Data Link Page. 2) Press the MORE WX Softkey. 3) Press the WIND Softkey. EIS 4) Select the desired altitude level: SFC (surface) up to 42,000 feet.
SYSTEM OVERVIEW Hazard Avoidance County Warnings FLIGHT INSTRUMENTS County data (Figure 6-34) provides specific public awareness and protection weather warnings from the National Weather Service (NWS). This can include information on fires, tornadoes, severe thunderstorms, flood conditions, and other natural disasters.
Hazard Avoidance SYSTEM OVERVIEW Cyclone FLIGHT INSTRUMENTS The Cyclone weather product (Figure 6-36) shows the current location of cyclones (hurricanes), tropical storms, and depressions using the symbol shown below (Figure 6-37). Storm tracks include date and time of arrival inside orange boxes. EIS Cyclone AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 6-36 Cyclone Data Selected for Display HAZARD AVOIDANCE Displaying cyclone (hurricane) track information: 1) Select the Weather Data Link Page.
SYSTEM OVERVIEW Hazard Avoidance Icing (CIP & SLD) FLIGHT INSTRUMENTS Current Icing Product (CIP) data (Figure 6-38) 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.
Hazard Avoidance SYSTEM OVERVIEW Turbulence FLIGHT INSTRUMENTS Turbulence data (Figure 6-40) 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.Turbulence data is intended to supplement AIRMETs and SIGMETs. Displaying Turbulence data: 1) Select the Weather Data Link Page. 2) Press the MORE WX Softkey. 3) Press the TURB Softkey.
SYSTEM OVERVIEW Hazard Avoidance PIREPs and AIREPs FLIGHT INSTRUMENTS Pilot Weather Reports (PIREPs) (Figure 6-42) provide timely weather information for a particular route of flight. When significant weather conditions are reported or forecast, Air Traffic Control (ATC) facilities are required to solicit PIREPs. A PIREP may contain unforecast adverse weather conditions, such as low in-flight visibility, icing conditions, wind shear, and turbulence.
Hazard Avoidance SYSTEM OVERVIEW FLIGHT INSTRUMENTS Decoded PIREP Text EIS AUDIO PANEL & CNS Raw PIREP Text FLIGHT MANAGEMENT Figure 6-43 PIREP Text on the Weather Data Link Page HAZARD AVOIDANCE To display the PIREP or AIREP legend (Figure 6-44), press the LEGEND Softkey when PIREPs or AIREPs are selected for display. The PIREP color is determined by the type (routine or urgent). AFCS Figure 6-44 AIREPs & PIREPs Legend ADDITIONAL FEATURES APPENDICES INDEX 190-00590-02 Rev.
SYSTEM OVERVIEW Hazard Avoidance 6.2 WX-500 Stormscope FLIGHT INSTRUMENTS NOTE: The Stormscope system is not intended for hazardous thunderstorm penetration. Weather information on the G1000 MFD is approved for weather avoidance only. Refer to the WX-500 User’s Guide for a detailed description of Stormscope operation. Note: L-3 STORMSCOPE® WX-500 Lightning and GDL 69/69A XM® Satellite Weather Lightning are EIS mutually exclusive.
Hazard Avoidance SYSTEM OVERVIEW The following options are available (Figure 6-46): • 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 6-47). 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 6-41). 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 The maximum zoom range can also be set on the Navigation Map. Note that Stormscope data above the selected maximum zoom range is decluttered. Selecting a Stormscope range on the Navigation Map: FLIGHT INSTRUMENTS 1) Press the MENU Key. 2) Select ‘MAP SETUP’. 3) Select the ‘Weather’ group. 4) Press the ENT Key. EIS 5) Turn the large FMS Knob to select ‘STRMSCP SMBL’. 6) Turn the small FMS Knob to select the maximum display range. 7) Press the ENT Key.
Hazard Avoidance SYSTEM OVERVIEW 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. 3) To change the map range, turn the RANGE Knob clockwise to zoom out or counter-clockwise to zoom in.
SYSTEM OVERVIEW Hazard Avoidance 6.3 Terrain Awareness & Warning System 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 EIS processes and cross-validates the data but cannot guarantee the accuracy and completeness of the data.
Hazard Avoidance SYSTEM OVERVIEW Displaying TAWS Data FLIGHT INSTRUMENTS TAWS 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. The colors and symbols in Figure 6-44 and Table 6-4 are used to represent terrain, obstacles, and potential impact points.
SYSTEM OVERVIEW Hazard Avoidance 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). FLIGHT INSTRUMENTS 2) Press the TERRAIN Softkey to display terrain and obstacle data. AUDIO PANEL & CNS EIS When TAWS is selected on maps other than the TAWS-B Page, an icon is shown to indicate that the feature is enabled for display.
Hazard Avoidance SYSTEM OVERVIEW Customizing terrain and obstacle display on 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 6-53). 4) Turn the small FMS Knob to select the ‘Map’ Group and press the ENT Key (Figure 6-54). 5) Turn the large FMS Knob or press the ENT Key to scroll through product selections (Figure 6-55).
SYSTEM OVERVIEW Hazard Avoidance 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.
Hazard Avoidance SYSTEM OVERVIEW Yellow Terrain (Caution Terrain Between 100’ and 1000’ Below the Aircraft Altitude) FLIGHT INSTRUMENTS Red Terrain (Warning - Terrain Above or Within 100’ Below the Aircraft Altitude) EIS Black Terrain (Terrain More than 1000’ Below the Aircraft Altitude) Map Range Rings AUDIO PANEL & CNS Terrain Legend Annunciation Window FLIGHT MANAGEMENT Figure 6-56 TAWS-B Page HAZARD AVOIDANCE Yellow Terrain (Caution Terrain Between 100’ and 1000’ Below the Aircraft Altitude)
SYSTEM OVERVIEW Hazard Avoidance TAWS Alerts FLIGHT INSTRUMENTS Alerts are issued when flight conditions meet parameters that are set within TAWS software algorithms. TAWS alerts typically employ a CAUTION or a WARNING alert severity level, or both. When an alert is issued, visual annunciations are displayed and aural alerts are simultaneously issued. Table 6-11 shows TAWS alert types with corresponding annunciations and aural messages. When an alert is issued, annunciations appear on the PFD and MFD.
Hazard Avoidance MFD Pop-Up Alert Aural Message Excessive Descent Rate Warning (EDR) “Pull Up” or * or Imminent Obstacle Impact Warning (IOI) or * “Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up”* or “Obstacle, Obstacle; Pull Up, Pull Up” * “Terrain Ahead; Terrain Ahead”* or “Caution, Terrain; Caution, Terrain” * “Obstacle Ahead; Obstacle Ahead”* or “Caution, Obstacle; Caution, Obstacle” * “Obstacle Ahead; Obstacle Ahead”* or “Caution, Obstacle; Caution, Obstacle” or Imminent Terrain Impac
SYSTEM OVERVIEW Hazard Avoidance 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 6-60 shows the parameters for the alert as defined by TSO-C151b.
Hazard Avoidance SYSTEM OVERVIEW Forward Looking Terrain Avoidance FLIGHT INSTRUMENTS 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 the minimum clearance values in Figure 6-61. When an RTC alert is issued, a potential impact point is displayed on the TAWS-B Page.
SYSTEM OVERVIEW Hazard Avoidance 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 6-62). 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.
Hazard Avoidance SYSTEM OVERVIEW Five-Hundred Aural Alert FLIGHT INSTRUMENTS The purpose of the aural alert message “Five-hundred” is to provide an advisory alert that the aircraft is 500 feet above terrain. When the aircraft descends within 500 feet of terrain, the aural message “Five-hundred” is generated. There are no display annunciations or pop-up alerts that accompany the aural message.
SYSTEM OVERVIEW Hazard Avoidance 1000 FLIGHT INSTRUMENTS Height Above Terrain (Feet) 900 800 700 600 “DON’T SINK” or “TOO LOW, TERRAIN” 500 400 300 EIS 200 100 0 500 1000 AUDIO PANEL & CNS 0 1500 2000 2500 3000 3500 4000 4500 5000 5500 6000 6500 7000 Sink Rate (FPM) Figure 6-65 Negative Climb Rate (NCR) Sink Rate FLIGHT MANAGEMENT System Status HAZARD AVOIDANCE During G1000 power-up, TAWS conducts a self-test of its aural and visual annunciations.
Hazard Avoidance SYSTEM OVERVIEW Manually testing the TAWS System: 1) Select the TAWS-B Page. 2) Press the MENU Key (Figure 6-66). FLIGHT INSTRUMENTS 3) Select ‘Test TAWS’ and press the ENT Key to confirm the selection. EIS AUDIO PANEL & CNS Figure 6-66 TAWS-B Page Menu FLIGHT MANAGEMENT TAWS continually monitors several system-critical items such as database validity, hardware status, and GPS status.
SYSTEM OVERVIEW Hazard Avoidance 6.4 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.
Hazard Avoidance SYSTEM OVERVIEW Displaying TRAFFIC Data Traffic information can be displayed on the following maps (when TIS is operating): • Trip Planning Page • Navigation Map Page • Nearest Pages • Traffic Map Page • Active Flight Plan Page FLIGHT INSTRUMENTS • PFD Inset Map Traffic information is also displayed on the PFD when the Synthetic Vision System (SVS) option is installed and enabled. See the Additional Features Section for details.
SYSTEM OVERVIEW Hazard Avoidance 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.
Hazard Avoidance SYSTEM OVERVIEW 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. The traffic mode is annunciated in the upper left corner of the Traffic Map Page.
SYSTEM OVERVIEW Hazard Avoidance TIS Alerts When the number of TAs on the Traffic Map Page increases from one scan to the next, the following occur: FLIGHT INSTRUMENTS • A single “Traffic” voice alert is generated. • 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.
Hazard Avoidance SYSTEM OVERVIEW Muting the “TIS Not Available” voice alert: 1) Select the Traffic Map Page. 2) Press the TNA MUTE Softkey. The status is displayed in the upper left corner of the Traffic Map Page. FLIGHT INSTRUMENTS Or: a) Press the MENU Key. b) Select ‘‘’Not Available” Mute On’ (shown if TNA muting is currently off) and press the ENT Key. System Status EIS The G1000 performs an automatic test of TIS during power-up.
SYSTEM OVERVIEW Hazard Avoidance AUDIO PANEL & CNS EIS 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. If traffic is selected for display on another map while Standby Mode is selected, the traffic display enabled icon is crossed out (also the case whenever TIS has failed). Once the aircraft is airborne, TIS switches to Operating Mode and traffic information is displayed.
Hazard Avoidance SYSTEM OVERVIEW 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). Traffic Status Banner Annunciation TA X.
SYSTEM OVERVIEW Hazard Avoidance 6.5 Traffic Advisory System (TAS) FLIGHT INSTRUMENTS NOTE: Refer to the SKY497 Pilot’s Guide for a detailed discussion of the TAS. TAS Symbology EIS The optional Traffic Advisory System (TAS) is designed to help in detection and avoidance of other aircraft. TAS uses an on-board interrogator-processor and an altitude reporting transponder for the air-to-air traffic data link. Traffic is displayed according to TCAS symbology using four different symbols.
Hazard Avoidance SYSTEM OVERVIEW Operation 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. FLIGHT INSTRUMENTS 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.
SYSTEM OVERVIEW Hazard Avoidance Operating Mode Traffic Display Range FLIGHT INSTRUMENTS Altitude Mode Traffic Advisory, Aircraft is 400’ Below, Climbing AUDIO PANEL & CNS EIS “Non-Bearing” Traffic (Bearing Undetermined), Distance 8.
Hazard Avoidance SYSTEM OVERVIEW Traffic Advisory FLIGHT INSTRUMENTS Proximity Traffic EIS Non-Threat Traffic AUDIO PANEL & CNS TA Off Scale Banner FLIGHT MANAGEMENT Non-Bearing Traffic Advisories Figure 6-75 TAS Traffic on Navigation Map Displaying traffic information (PFD Inset Map): HAZARD AVOIDANCE 1) Press the INSET Softkey. 2) Press the TRAFFIC Softkey to display traffic data on the inset map (TRFC-1). 3) Press the softkey again to display the traffic-only inset (TRFC-2).
SYSTEM OVERVIEW Hazard Avoidance Altitude Display Changing the altitude display mode: FLIGHT INSTRUMENTS 1) On the Traffic Page, press the ALT MODE Softkey. EIS 2) Press one of the following Softkeys: • BELOW • NORMAL • ABOVE • UNREST (unrestricted) 3) To return to the Traffic Page, press the BACK Softkey. AUDIO PANEL & CNS Or: 1) Press the MENU Key.
Hazard Avoidance SYSTEM OVERVIEW Customizing the traffic display on 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 6-76). 4) Turn the small FMS Knob to select the Traffic Group and press the ENT Key (Figure 6-77). 5) Turn the large FMS Knob or press the ENT Key to scroll through the selections (Figure 6-78).
SYSTEM OVERVIEW Hazard Avoidance TAS Alerts FLIGHT INSTRUMENTS NOTE: Refer to the TAS documentation for information on alerts generated by the TAS equipment. 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.
Hazard Avoidance SYSTEM OVERVIEW If the unit fails, an annunciation as to the cause of the failure is shown in the center of the Traffic Map Page.
INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Hazard Avoidance Blank Page 348 Garmin G1000 Pilot’s Guide for the Quest Kodiak 100 190-00590-02 Rev.
Automatic Flight Control System SYSTEM OVERVIEW Section 7 Automatic Flight Control System FLIGHT INSTRUMENTS Note: Refer to the Aircraft Flight Manual (AFM) for the installed autopilot. 7.1 S-TEC Fifty Five X Autopilot (Optional) Note: This section covers only the additional ‘AP’, ‘YD’, and ‘FD’ status annunciations that may appear in the EIS G1000 AFCS Status Box. These status annunciations are not analogous to both the G1000 and the S-TEC Fifty Five X.
INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Automatic Flight Control System Blank Page 350 Garmin G1000 Pilot’s Guide for the Quest Kodiak 100 190-00590-02 Rev.
Additional Features SYSTEM OVERVIEW Section 8 Additional Features FLIGHT INSTRUMENTS NOTE: With the availability of SafeTaxi, ChartView, or FliteCharts in electronic form, it is still advisable to carry another source of charts on board the aircraft.
SYSTEM OVERVIEW Additional Features 8.1 Synthetic Vision System (SVS) FLIGHT INSTRUMENTS WARNING: Use appropriate primary systems for navigation, and for terrain, obstacle, and traffic avoidance. SVS 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 SVS Operation HAZARD AVOIDANCE SVS 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 SVS is enabled, the pitch scale increments are reduced to 10 degrees up and 7.5 degrees down. AFCS SVS 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 SVS Softkeys Activating and deactivating SVS: FLIGHT MANAGEMENT 1) Press the PFD Softkey. 2) Press the SYN VIS Softkey. 3) Press the SYN TERR Softkey. The SVS display will cycle on or off with the SYN TERR Softkey.
Additional Features SYSTEM OVERVIEW SVS Features Pathways Color Matches CDI Indicating NAV Source Flight Path Marker Airplane Symbol EIS Zero Pitch Line (ZPL) with Compass Heading Marks FLIGHT INSTRUMENTS Selected Altitude Airport Runway AUDIO PANEL & CNS Synthetic Terrain FLIGHT MANAGEMENT HAZARD AVOIDANCE SVS Softkeys Figure 8-3 SVS on the Primary Flight Display NOTE: Pathways and terrain features are not a substitute for standard course and altitude deviation information provided by the CDI
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, 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 SVS 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. EIS Runway data provides improved awareness of runway location with respect to the surrounding terrain. All runway thresholds are depicted at their respective elevations as defined in the database.
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. EIS 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.
EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Additional Features AUDIO PANEL & CNS Field of View FLIGHT MANAGEMENT Navigation Map Page OPTIONS Menu Map Setup Menu, Map Group, Field of View Option Figure 8-12 Option Menus 3) Turn the FMS Knob to select the Map Group and press the ENT Key. HAZARD AVOIDANCE 4) Turn the large FMS Knob to scroll through the Map Group options to FIELD OF VIEW. 5) Turn the small FMS Knob to select On or Off. 6) Press the FMS Knob to return to the Navigation Map Page.
Additional Features SYSTEM OVERVIEW 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.
SYSTEM OVERVIEW Additional Features EIS FLIGHT INSTRUMENTS During ground operations the aircraft’s position is displayed in reference to taxiways, runways, and airport features. In the example shown, the aircraft is on taxiway Bravo inside the High Alert Intersection boundary on KSFO airport. Airport Hot Spots are outlined in magenta. When panning over the airport, features such as runway holding lines and taxiways are shown at the cursor.
Additional Features SYSTEM OVERVIEW FLIGHT INSTRUMENTS Figure 8-15 Navigation Map PAGE MENU, Map Setup Option EIS 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. AUDIO PANEL & CNS 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.
SYSTEM OVERVIEW Additional Features 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. FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS SafeTaxi Database Figure 8-17 Power-up Page, SafeTaxi Database HAZARD AVOIDANCE Power-up Page Display Definition Normal operation.
Additional Features SYSTEM OVERVIEW The SafeTaxi database cycle number shown in the figure, 09S3, is deciphered as follows: 09 – Indicates the year 2009 S – Indicates the data is for SafeTaxi FLIGHT INSTRUMENTS 3 – Indicates the third issue of the SafeTaxi database for the year The SafeTaxi EFFECTIVE date 07–MAY–09 is the beginning date for the current database cycle. SafeTaxi EXPIRES date 02–JUL–09 is the revision date for the next database cycle.
SYSTEM OVERVIEW Additional Features FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Figure 8-19 illustrates possible SafeTaxi database conditions that may appear on the AUX - System Status Page. The EFFECTIVE date is the beginning date for this database cycle. If the present date is before the effective date, the EFFECTIVE date appears in yellow and the EXPIRES date appears in blue. The EXPIRES date is the revision date for the next database cycle.
Additional Features SYSTEM OVERVIEW 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 plan view of approach charts and on airport diagrams. Airport Hot Spots are outlined in magenta. The ChartView database subscription is available from Jeppesen, Inc.
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 8-26, the Class B Chart is selected. Pressing the ENT Key displays the Charlotte Class B Airspace Chart (Figure 8-27). HAZARD AVOIDANCE Figure 8-27 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 8-29 Arrival Information Page HAZARD AVOIDANCE Pressing the APR Softkey displays the approach chart for the airport if available. AFCS ADDITIONAL FEATURES APPENDICES 190-00590-02 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 XM Weather subscription is current.
Additional Features SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT NOTAM Softkey Appears for Selected Airports Figure 8-32 NOTAM Softkey Highlighted HAZARD AVOIDANCE Local NOTAM on This Airport AFCS ADDITIONAL FEATURES APPENDICES NOTAM Softkey Selected Figure 8-33 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 8-20). 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 8-34 Approach Information Page, ALL View 380 Garmin G1000 Pilot’s Guide for the Quest Kodiak 100 190-00590-02 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 8-35 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 8-37 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 8-39 Airport Information Page, FIT WDTH Softkey Pressed APPENDICES INDEX 190-00590-02 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 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 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 8-43 Arrival Information Page, Day View HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Figure 8-44 Arrival Information Page, Night View INDEX 190-00590-02 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 AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Other possible AUX - System Status page conditions are shown in Figure 8-47. 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. CYCLE NOT AVAILABLE in blue, indicates no ChartView data is available on the database card or no database card is inserted.
Additional Features SYSTEM OVERVIEW 8.4 FliteCharts • Departure Procedures (DP) FLIGHT INSTRUMENTS FliteCharts resemble the paper version of National Aeronautical Charting Office (NACO) terminal procedures charts. The charts are displayed with high-resolution and in color for applicable charts. FliteCharts database subscription is available from Garmin.
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 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.
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 Another source for additional airport information is from the INFO Box above the chart (Figure 8-53) or to the right of the chart (Figure 8-54) for certain airports.
SYSTEM OVERVIEW Additional Features FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS In the example shown in Figure 8-54, TAKE OFF MINIMUMS is selected. Pressing the ENT Key displays the Take-off Minimums and Departure Procedures Chart (Figure 8-55). HAZARD AVOIDANCE Figure 8-55 Airport Information Page, TAKE OFF MINIMUMS Selected from INFO View INDEX APPENDICES ADDITIONAL FEATURES AFCS 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 EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 8-57 Arrival Information Page Pressing the APR Softkey displays the approach chart for the airport if available. HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES 190-00590-02 Rev.
SYSTEM OVERVIEW Additional Features 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 XM 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).
Additional Features SYSTEM OVERVIEW Chart Options Pressing the CHRT OPT Softkey displays the next level of softkeys, the chart options level (Figure 8-48). Pressing the ALL Softkey shows the complete chart on the screen. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS Complete Chart Shown FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 8-60 Airport Information Page, ALL View Selected AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00590-02 Rev.
SYSTEM OVERVIEW Additional Features ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS 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.
Additional Features SYSTEM OVERVIEW Pressing the FULL SCN Softkey alternates between removing and replacing the data window to the right. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE Press FULL SCN Softkey to Switch Between Chart on Full Screen and Chart with Info Window AFCS Figure 8-62 Airport Information Page, Full Screen and Info Window ADDITIONAL FEATURES Pressing the BACK Softkey, or waiting for 45 seconds reverts to the chart selection softkeys.
SYSTEM OVERVIEW Additional Features 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.
Additional Features SYSTEM OVERVIEW 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.
FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Additional Features APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Figure 8-65 Approach Information Page, Day View INDEX Figure 8-66 Approach Information Page, Night View 404 Garmin G1000 Pilot’s Guide for the Quest Kodiak 100 190-00590-02 Rev.
Additional Features SYSTEM OVERVIEW FliteCharts Cycle Number and Expiration Date 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. When turning on the system, the Power-up Page displays the current status of the FliteCharts database.
SYSTEM OVERVIEW Additional Features When the 180 day grace period has expired, ‘Chart data is disabled.’ in yellow indicates that the FliteCharts database has expired and is no longer viewable. ‘Chart Data: N/A’ appears in white if no FliteCharts data is available on the database card or no database card is inserted. FLIGHT INSTRUMENTS FliteCharts time critical information can also be found on the AUX - System Status page.
Additional Features SYSTEM OVERVIEW The FliteCharts database is provided from Garmin. Refer to Updating Garmin Databases in Appendix B for instructions on revising the FliteCharts database. FLIGHT INSTRUMENTS The other three possible AUX - System Status page conditions are shown here. 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.
SYSTEM OVERVIEW Additional Features 8.5 AOPA Airport Directory HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS The Aircraft Owners and Pilots Association (AOPA) Airport Directory database offers detailed information regarding services, hours of operation, lodging options, and more. This information is viewed on the Airport Information Page by selecting the INFO Softkey until INFO-2 is displayed as shown in Figure 8-70.
Additional Features SYSTEM OVERVIEW AOPA Database Cycle Number and Revision FLIGHT INSTRUMENTS The AOPA Airport Directory database is revised four times per year. 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.
SYSTEM OVERVIEW Additional Features The Airport Directory database cycle number shown in the figure, 09D2, is deciphered as follows: 09 – Indicates the year 2009 FLIGHT INSTRUMENTS D – Indicates the data is for Airport Directory 2 – Indicates the second issue of the Airport Directory database for the year AUDIO PANEL & CNS EIS The Airport Directory EFFECTIVE date 15–APR–09 is the beginning date for the current database cycle.
Additional Features SYSTEM OVERVIEW 8.6 XM Radio Entertainment (Optional) FLIGHT INSTRUMENTS Note: Refer to the Hazard Avoidance Section for information about XM Weather products. The optional XM Radio entertainment feature of the GDL 69A Data Link Receiver is available for the pilot’s and passengers’ enjoyment. The GDL 69A can receive XM Satellite Radio® entertainment services at any altitude throughout the Continental U.S.
SYSTEM OVERVIEW Additional Features 5) Verify that the desired services are activated. 6) Press the LOCK Softkey. FLIGHT INSTRUMENTS 7) Turn the large FMS Knob to highlight YES. 8) To complete activation, press the ENT Key.
Additional Features SYSTEM OVERVIEW Active Channel FLIGHT INSTRUMENTS EIS Channel List AUDIO PANEL & CNS Volume Field Categories Field FLIGHT MANAGEMENT Figure 8-74 XM Radio Page Active Channel and Channel List HAZARD AVOIDANCE The Active Channel Box on the XM Radio Page displays the currently selected channel that the XM Radio is using. The Channels List Box of the XM Radio Page shows a list of the available channels for the selected category.
SYSTEM OVERVIEW Additional Features Category FLIGHT INSTRUMENTS The Category Box of the XM Radio Page displays the currently selected category of audio. Categories of channels such as jazz, rock, or news can be selected to list the available channels for a type of music or other contents. One of the optional categories is PRESETS to view channels that have been programmed. Selecting a category: 1) Press the CATGRY Softkey on the XM Radio Page.
Additional Features SYSTEM OVERVIEW 3) Press any one of the (PS1 - PS15) softkeys to assign a number to the active channel. 4) Press the SET Softkey on the desired channel number to save the channel as a preset.
SYSTEM OVERVIEW Additional Features 8.7 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 9) For event-based messages: a) Use the FMS Knob to enter the desired date (DD-MM-YY) and press the ENT Key. b) Press the ENT Key again or use the large FMS Knob to move the cursor to the next field. FLIGHT INSTRUMENTS c) Use the FMS Knob to enter the desired time (HH:MM) and press the ENT Key. 10) Press the ENT Key again or use the large FMS Knob to move the cursor to enter the next message. Deleting a scheduler message: 1) Select the AUX - Utility Page.
SYSTEM OVERVIEW Additional Features 8.8 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 • Yellow - Caution notes • Red - Warning notes FLIGHT INSTRUMENTS The following colors are used for checklist items: • Blue - Items not selected • White - Item is selected • Green - Item has been checked SYSTEM OVERVIEW 7) When all checklist items have been checked, ‘*Checklist Finished*’ is displayed in green text at the bottom left of the checklist window.
SYSTEM OVERVIEW Additional Features 4) Press the ENT Key or press the CHECK Softkey to check the selected emergency checklist item. The line item turns green and a checkmark is placed in the box next to it. The next line item is automatically highlighted for checking. FLIGHT INSTRUMENTS Either FMS Knob can be used to scroll through the checklist and select the desired checklist item. Press the CLR Key or press the UNCHECK Softkey to remove a check mark from an item.
Additional Features SYSTEM OVERVIEW 8.9 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 8-80. 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_090210_104506_KIXD.
Additional Features SYSTEM OVERVIEW 8.10 Auxiliary Video FLIGHT INSTRUMENTS The G1000 system provides a control and display interface to an auxiliary video system. The system can display video for up to two inputs. 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 Selecting video menu options: 1) While viewing the AUX - VIDEO Page press the MENU Key to display the Page Menu OPTIONS. FLIGHT INSTRUMENTS 2) Turn the large FMS Knob to highlight the desired video adjustment option and press the ENT Key. Once the ENT key is pressed on any option, the page menu closes and returns to the AUX - VIDEO Page. Video Setup EIS Video brightness, contrast, and saturation may be adjusted be selecting the setup function.
Additional Features SYSTEM OVERVIEW Input 1 Displayed FLIGHT INSTRUMENTS Video Display EIS AUDIO PANEL & CNS Map View FLIGHT MANAGEMENT Figure 8-86 AUX - Video Split-Screen HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Figure 8-87 Full Screen Video Display INDEX 190-00590-02 Rev.
SYSTEM OVERVIEW Input Selection FLIGHT INSTRUMENTS Additional Features Zoom/Range 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. EIS When zooming in on the video display, a Zoom Window will appear in the upper right of the display. A box within this window indicates the portion of the display currently being viewed.
Additional Features SYSTEM OVERVIEW 8.11 Abnormal Operation SVS Troubleshooting FLIGHT INSTRUMENTS SVS is intended to be used with traditional attitude, heading, obstacle, terrain, and traffic inputs. SVS is disabled when valid attitude or heading data is not available for the display. In case of invalid SVS 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 FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Annunciation Window Text CARGO DOOR EMER PWR LVR FLAP FAIL FUEL LOW L FUEL LOW R FUEL LOW L-R FUEL PRESS LOW GEN FAIL HI ICE SPEED LO ICE SPEED PITOT FL L PITOT FL R PITOT FL L-R PITOT OFF L PITOT OFF R PITOT OFF L-R STALL HT FL VOLTAGE LOW Alerts Window Message Cargo door is not closed and locked (on ground). Emergency power lever is active. Flaps system is inoperative. Left fuel tank quantity is low.
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 Description “Minimums, minimums” The aircraft has descended below the preset barometric minimum descent altitude. The aircraft is one minute from Top of Descent. Issued only when vertical navigation is enabled.
SYSTEM OVERVIEW APPENDIX A Reversionary Sensor Annunciations FLIGHT INSTRUMENTS Reversionary sensor selection is annunciated in the Reversionary Sensor Window, as shown in Figure A-7. These annunciations reflect reversionary sensors selected on one or both PFDs. Pressing the SENSOR Softkey gives access to ADC1, ADC2, AHRS1, and AHRS2 Softkeys. These softkeys allow manual switching of sensors. In the case of certain types of sensor failures, the G1000 may make some sensor selections automatically.
aPPENDIX a SYSTEM OVERVIEW G1000 System Annunciations FLIGHT INSTRUMENTS When a new alert is issued, the ALERT 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 ALERT Softkey will flash if the state of a displayed alert changes or a new alert is displayed.
SYSTEM OVERVIEW APPENDIX A System Annunciation Comment FLIGHT INSTRUMENTS Attitude and Heading Reference System is aligning. AUDIO PANEL & CNS EIS Display system is not receiving attitude information from the AHRS. FLIGHT MANAGEMENT Display system is not receiving airspeed input from air data computer. HAZARD AVOIDANCE Display is not receiving altitude input from the air data computer. AFCS Display is not receiving vertical speed input from the air data computer.
aPPENDIX a SYSTEM OVERVIEW TIS Voice Alerts The following voice alerts can be configured for ‘Male’ or ‘Female’ gender by using the Aux System Setup Page on the MFD. Alert Trigger Played when a Traffic Advisory (TA) is issued. “Traffic Not Available” Played when the traffic system fails or cannot communicate. FLIGHT INSTRUMENTS Voice Alert “Traffic” EIS Note: Voice alerts are provided to the G1000 by GIA 63/W #1. Should this unit fail, audio and voice alerts will no longer be available.
SYSTEM OVERVIEW APPENDIX A MFD & PFD Message Advisories INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Alerts Window Message DATA LOST – Pilot stored data was lost. Recheck settings. XTALK ERROR – A flight display crosstalk error has occurred. PFD1 SERVICE – PFD1 needs service. Return unit for repair. PFD2 SERVICE – PFD2 needs service. Return unit for repair. MFD1 SERVICE – MFD1 needs service. Return unit for repair.
aPPENDIX a SYSTEM OVERVIEW Comments The PFD2 voltage is low. The G1000 system should be serviced. The MFD voltage is low. The G1000 system should be serviced. FLIGHT INSTRUMENTS Alerts Window Message PFD2 VOLTAGE – PFD2 has low voltage. Reducing power usage MFD1 VOLTAGE – MFD1 has low voltage. Reducing power usage Database Message Advisories The MFD and/or PFD detected a failure in the navigation database. Attempt to reload the navigation database.
SYSTEM OVERVIEW APPENDIX A HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Alerts Window Message MFD1 DB ERR – MFD1 airport terrain database error exists. PFD1 DB ERR – PFD1 airport terrain database error exists. PFD2 DB ERR – PFD2 airport terrain database error exists. MFD1 DB ERR – MFD1 airport terrain database missing. PFD1 DB ERR – PFD1 airport terrain database missing. PFD2 DB ERR – PFD2 airport terrain database missing.
aPPENDIX a SYSTEM OVERVIEW GMA 1347 Message Advisories Comments The audio panel self-test has detected a failure. The audio panel is unavailable. The G1000 system should be serviced. FLIGHT INSTRUMENTS An error has occurred in transferring data between the two GMAs. The G1000 system should be serviced. The audio panel configuration settings do not match backup configuration memory. The G1000 system should be serviced. EIS The audio panel has incorrect software installed.
SYSTEM OVERVIEW APPENDIX A INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Alerts Window Message HW MISMATCH – GIA hardware mismatch. GIA1 communication halted. HW MISMATCH – GIA hardware mismatch. GIA2 communication halted. MANIFEST – GIA1 software mismatch, communication halted. MANIFEST – GIA2 software mismatch, communication halted. COM1 TEMP – COM1 over temp. Reducing transmitter power. COM2 TEMP – COM2 over temp.
aPPENDIX a SYSTEM OVERVIEW Comments A failure has been detected in the NAV1 and/or NAV2 receiver. The receiver may still be available. The G1000 system should be serviced. FLIGHT INSTRUMENTS The remote NAV1 and/or NAV2 transfer switch is stuck in the enabled (or “pressed”) state. Press the transfer switch again to cycle its operation. If the problem persists, the G1000 system should be serviced. A failure has been detected in glideslope receiver 1 and/or receiver 2. The G1000 system should be serviced.
SYSTEM OVERVIEW APPENDIX A GRS 77 Message Advisories FLIGHT INSTRUMENTS Alerts Window Message AHRS1 TAS – AHRS1 not receiving valid airspeed. AHRS2 TAS – AHRS2 not receiving valid airspeed. The #1 AHRS and #2 AHRS magnetic model database versions do not match. The #1 AHRS earth magnetic field model is out of date. Update magnetic field model when practical. The #2 AHRS earth magnetic field model is out of date. Update magnetic field model when practical.
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 Miscellaneous Message Advisories INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS 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 locked. is locked. This occurs when a navigation database update eliminates an obsolete waypoint. The flight plan cannot find the specified waypoint and flags this message.
aPPENDIX a Bad parallel track geometry. Invalid leg type for parallel offset. IAF waypoint for parallel offset has been passed. The current vertical waypoint can not be reached within the maximum flight path angle and vertical speed constraints. The system automatically transitions to the next vertical waypoint. The lateral flight plan contains a procedure turn, vector, or other unsupported leg type prior to the active vertical waypoint. This prevents vertical guidance to the active vertical waypoint.
SYSTEM OVERVIEW APPENDIX A TAWS ALERTS Annunciations appear on the PFD and MFD. Pop-up alerts appear only on the MFD.
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.
INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW APPENDIX A Blank Page 452 Garmin G1000 Pilot’s Guide for the Quest Kodiak 100 190-00590-02 Rev.
aPPENDIX b SYSTEM OVERVIEW SD Card Use 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 Jeppesen navigation and ChartView database updates. FLIGHT INSTRUMENTS CAUTION: Do not load Jeppesen navigation data (except ChartView) onto Garmin Supplemental Data Cards.
SYSTEM OVERVIEW APPENDIX b AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS 4) A prompt similar to the following is displayed, press the YES Softkey to update the active navigation database. Figure B-2 Database Update Confirmation 5) After the update completes, the display starts in normal mode. FLIGHT MANAGEMENT 6) Turn the system OFF and remove the SD card. 7) Repeat steps 1 through 4 for the other PFD and the MFD. The MFD and PFD databases are now updated. Remove the SD card when finished.
aPPENDIX b SYSTEM OVERVIEW 3) Turn the system ON. A prompt similar to the following is displayed. FLIGHT INSTRUMENTS EIS Figure B-3 Standby Navigation Database Prompt 4) Press the YES Softkey, to start the update. AUDIO PANEL & CNS 5) After the navigation database files are copied to the bottom SD card. A prompt similar to the following is displayed.
SYSTEM OVERVIEW APPENDIX b EIS FLIGHT INSTRUMENTS After subscribing to the desired database product, these database products will be downloaded to three Supplemental Data Cards (with the exception of FliteCharts, which is loaded on only one card). Insert each Supplemental Data Card into the correct location shown in Figure B-5. These cards must not be removed except to update the databases stored on each card.
aPPENDIX b SYSTEM OVERVIEW Updating Garmin Databases FLIGHT INSTRUMENTS The Garmin database updates can be obtained by following the instructions detailed in the ‘Aviation Databases’ section of the Garmin website (fly.garmin.com). Once the updated files have been downloaded from the website, a PC equipped with an appropriate SD card reader is used to unpack and program the new databases onto the existing Supplemental Data Cards.
SYSTEM OVERVIEW APPENDIX b Unselected MFD1 DB Selected PFD1 DB Selected FLIGHT INSTRUMENTS Figure B-7 Display Database Softkey 6) Press the Display Database Softkey (Figure B-7) to place the cursor in the ‘Database’ box. 7) Turn either FMS Knob to scroll through the database list and check that all databases are current and there are no errors. 8) Press the Display Database Softkey to view the Database info pertaining to the desired PFD or MFD.
aPPENDIX b SYSTEM OVERVIEW An indication of ‘Complete’ still requires a power cycle before the synchronized databases will be used by the system. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure B-8 AUX-System Status Page, Database Window AFCS The Display Database Softkey (Figure B-7) is used to place the cursor in the Database Window.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW APPENDIX b Database Synchronization Error Message EIS Figure B-9 Synchronization Error Message AUDIO PANEL & CNS Error Message Canceled Card Full Err Timeout Description An active synchronization has been canceled using the SYNC DBS Softkey SD card does not contain sufficient memory Displayed for all other errors that may cause the synchronization process to be halted System timed-out prior to the database transfer completing FLIGHT MANAGEMENT Table B-1 HAZARD AV
aPPENDIX b SYSTEM OVERVIEW 9) Monitor the Sync Status in the Database Window, wait for all databases to complete synching. 10) Remove and reapply power to the system, select the AUX-System Status Page, and verify that all databases have been synchronized. FLIGHT INSTRUMENTS Canceling an automatic database synchronization: 1) Turn the large FMS Knob to select the AUX Page group on the MFD. 2) Turn the small FMS Knob to select the System Status Page.
INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW APPENDIX b Blank Page 462 Garmin G1000 Pilot’s Guide for the Quest Kodiak 100 190-00590-02 Rev.
aPPENDIX c SYSTEM OVERVIEW Glossary BFO BKSP BRG AFCS ADDITIONAL FEATURES APPENDICES CO COM CONFIG COOL COPLT Course HAZARD AVOIDANCE CD CDI CDU CF CHT CHKLIST CHNL CI CLD CLR cm CNS center runway celsius Course to Altitude calculator Indicated airspeed corrected for installation and instrument errors.
SYSTEM OVERVIEW APPENDIX c FLIGHT INSTRUMENTS Course to Steer EIS CR CRG CRNT Crosstrack Error FLIGHT MANAGEMENT AUDIO PANEL & CNS CRS CRS CRSR CTRL Cumulative CVR CVRG CWS CYL density altitude database decibels ‘Z’ (Radar Return) declutter decrease fuel degree de-icing departure The desired course between the active “from” and “to” waypoints.
aPPENDIX c Hold Terminating at Altitude heading Garmin G1000 Pilot’s Guide for the Quest Kodiak 100 INDEX HA HDG APPENDICES 190-00590-02 Rev.
SYSTEM OVERVIEW APPENDIX c Heading FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS HF HFOM Hg HI HI SENS HM Horizontal Figure of Merit hPa HPL hr HSDB HSI HT HUL Hz AFCS HAZARD AVOIDANCE I IAF IAT IAU ICAO ICS ID APPENDICES ADDITIONAL FEATURES IDENT, IDNT IF IFR IG ILS IMC INDEX in INACTV INC FUEL IND 466 The direction an aircraft is pointed, based upon indications from a magnetic compass or a properly set directional gyro.
aPPENDIX c POSN PPM P.
SYSTEM OVERVIEW APPENDIX c FLIGHT INSTRUMENTS RAM REF REM REQ RES FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS REV RF RMI RMT RNG RNWY ROL ROM rpm RST FUEL RSV HAZARD AVOIDANCE RT RVRSNRY RX AFCS S SA SAT SCIT ADDITIONAL FEATURES SD sec SEL, SLCT SFC SIAP APPENDICES SID SIGMET INDEX Sim SLP/SKD SMBL SPD 468 random access memory reference remaining (fuel remaining above Reserve) required reserve (fuel reserve entered by pilot) reverse, revision, revise Constant Radius Turn to Fix Radio Magnetic
aPPENDIX c Track Angle Error Zero Pitch Line INDEX Garmin G1000 Pilot’s Guide for the Quest Kodiak 100 APPENDICES 190-00590-02 Rev. A ZPL ADDITIONAL FEATURES VMC VNAV, VNV transfer transponder cross-talk cross-track AFCS VFOM VFR VHF VI VLOC VM XFER, XFR XPDR XTALK XTK HAZARD AVOIDANCE velocity (airspeed) Heading Vector to Altitude VOR approach variation Heading Vector to DME Distance volts, direct current vertical A measure of the uncertainty in the aircraft’s vertical position.
INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW APPENDIX c Blank Page 470 Garmin G1000 Pilot’s Guide for the Quest Kodiak 100 190-00590-02 Rev.
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 WAAS? EIS The Wide Area Augmentation System (WAAS) 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 When OBS mode is active, the G1000 allows the pilot to set a desired course to/from a waypoint using the CRS/BARO Knob and HSI (much like a VOR). FLIGHT INSTRUMENTS The most common application for using the OBS Softkey is the missed approach. The G1000 suspends automatic waypoint sequencing (indicated by a ‘SUSP’ annunciation placed on the HSI) when the missed approach point (MAP) is crossed.
SYSTEM OVERVIEW APPENDIX d Why does the HSI not respond like a VOR when OBS mode is active? FLIGHT INSTRUMENTS Unlike a VOR, the CDI scale used on GPS equipment is based on the crosstrack distance to the desired course, not on the angular relationship to the destination. Therefore, the CDI deflection on the GPS is constant regardless of the distance to the destination and does not become less sensitive when further away from the destination.
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 Item Symbol Intersection HAZARD AVOIDANCE Traffic NAVAID
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 478 G
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 NEXRAD display enabled Elevation Pointer EIS Cloud Top display enabled AUDIO PANEL & CNS Wind Vector Echo Top display enabled XM Lightning display enabled Measuring Pointer Cell Movement display enabled Overzoom Indicator FLIGHT MANAGEMENT SIGMETs/AIRMETs displa
Index B Backlighting-------------------------------------------------- 46 Barometric altimeter setting---------------------------48, 54 Basic Empty Weight----------------------------------------246 Basic Operating Weight------------------------------------246 Bearing/distance, measuring------------------------------147 Bearing information-------------------------------------49, 62 Bearing pointer----------------------------------------------- 61 Bearing source-----------------------------------------------
INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Index I-2 D F Database(s)------------------------------------------ 11, 12, 39 Databases----------------------------------------------------453 Database synchronization--------- 40, 455, 458, 460, 461 Data entry------------------------------------------------ 28–29 Data Link Receiver--------------------------------------------- 4 Data Link Receiver troubleshooti
Index N M P Page groups--------------------------------------------- 29–32 Page menus--------------------------------------------------- 28 Parallel Track------------------------------------------ 217, 218 Passenger address (PA) system---------------------------126 Passengers-------------------------------------------- 246, 247 PA system----------------------------------------------------126 PFD failure---------------------------------------------------132 Pilot and Stores Weight--------------------------
SYSTEM OVERVIEW Index Q Quick tuning 121.
Index Unable to display chart----------------------------- 372, 392 Updating Garmin databases------------------------------369 Updating Jeppesen databases----------------------------389 Z EIS Zoom Auto--------------------------------------------------------141 AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE VDI----------------------------------------------------- 269, 270 Vertical deviation guidance-------------------------------228 Vertical Deviation Indicator-------------------------------269 Ve
INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Index Blank Page I-6 Garmin G1000 Pilot’s Guide for the Quest Kodiak 100 190-00590-02 Rev.
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G1000 ® Integrated Flight Deck 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 (Europe) Ltd. Liberty House, Bulls Copse Road Houndsdown Business Park Southampton, SO40 9RB, U.K. p:44/0870.8501241 f:44/0870.8501251 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 AT, Inc.