Integrated Flight Deck Cockpit Reference Guide Quest Kodiak 100
Copyright © 2007 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0552.00 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.
WARNINGS, CAUTIONS, & NOTES WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain function. The G1000 Terrain Proximity 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 Proximity feature is only to be used as an aid for terrain avoidance and is not certified for use in applications requiring a certified terrain awareness system.
WARNINGS, CAUTIONS, & NOTES WARNING: NEXRAD weather data is to be used for long-range planning purposes only. Due to inherent delays in data transmission and the relative age of the data, NEXRAD weather data should not be used for short-range weather avoidance. WARNING: The Garmin G1000, as installed in the Quest Kodiak 100 aircraft, has a very high degree of functional integrity.
WARNINGS, CAUTIONS, & NOTES CAUTION: The Garmin G1000 does not contain any user-serviceable parts. Repairs should only be made by an authorized Garmin service center. Unauthorized repairs or modifications could void both the warranty and the pilot’s authority to operate this device under FAA/FCC regulations. NOTE: When using Stormscope, there are several atmospheric phenomena in addition to nearby thunderstorms that can cause isolated discharge points in the strike display mode.
RECORD OF REVISIONS Part Number 190-00645-00 Change Summary Initial release. Revision Date of Revision Affected Pages A March, 2007 i through Index-4 190-00645-00 Rev.
RECORD OF REVISIONS Blank Page RR-2 Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100 190-00645-00 Rev.
TABLE OF CONTENTS SECTION 1: SYSTEM OVERVIEW.................................... 1-1 1.1 1.2 1.3 1.4 1.5 1.6 PFD/MFD Controls................................................... 1-2 PFD Softkeys............................................................ 1-4 MFD Softkeys .......................................................... 1-7 MFD Page Groups ................................................... 1-8 Backlighting ............................................................. 1-8 Database Updates .........
TABLE OF CONTENTS 7.12 Nearest User Waypoint.......................................... 7-8 Select the Nearest User Waypoint Page ........................ 7-8 7.13 Nearest Frequencies .............................................. 7-9 Select the Nearest Frequencies Page ............................ 7-9 7.14 Nearest Airspaces ................................................... 7-9 Select the Nearest Airspaces Page................................ 7-9 SECTION 8: FLIGHT PLANNING ................................
TABLE OF CONTENTS SECTION 11: ABNORMAL OPERATION ..................... 11-1 11.1 11.2 11.3 11.4 Reversionary Mode .............................................. 11-1 Abnormal COM Operation .................................. 11-2 Unusual Attitudes ................................................. 11-2 Stormscope Operation with Loss of Heading Input........................................................ 11-2 11.5 Hazard Displays with Loss of GPS Position .... 11-2 SECTION 12: ANNUNCIATIONS & ALERTS .......
TABLE OF CONTENTS Blank Page iv Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100 190-00645-00 Rev.
SECTION 1 SYSTEM OVERVIEW SECTION 1: SYSTEM OVERVIEW The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system more easily. It is not intended to be a comprehensive operating guide. Complete operating procedures for the complete system are found in the G1000 Pilot’s Guide for the Quest Kodiak 100 (19000590-00): 190-00645-00 Rev.
SECTION 1 SYSTEM OVERVIEW 1.1 PFD/MFD CONTROLS 1 17 2 3 5 4 6 7 8 9 Figure 1-1 PFD/MFD Controls 10 14 11 15 12 16 13 1-2 Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100 190-00645-00 Rev.
SECTION 1 SYSTEM OVERVIEW The same controls and keys are found on both PFDs and the MFD. (1) NAV VOL/ID Knob – Controls the NAV audio level. Press to turn the Morse code identifier ON and OFF. Volume level is shown in the field as a percentage. (2) NAV Frequency Transfer Key – Switches the standby and active NAV frequencies. (3) Dual NAV Knob – Tunes the MHz (large knob) and kHz (small knob) standby frequencies for the NAV receiver.
SECTION 1 SYSTEM OVERVIEW 1.2 PFD SOFTKEYS Softkey ON TERRAIN – Press to display terrain information on the Inset Map. STRMSCP (optional) – Press to display the Stormscope lightning data on the Inset Map (within a 200 nm radius of the aircraft). NEXRAD (optional) – Press to display NEXRAD precipitation data on the Inset Map. XM LTNG (optional) – Press to display the XM Radio lightning data on the Inset Map. BACK – Press to return to the previous level softkey configuration.
SECTION 1 SYSTEM OVERVIEW 360 HSI – Press to display the 360° compass rose. ARC HSI – Press to display the 140° viewable arc. BRG2 (bearing) – Press to cycle through the following information: NAV2 – Displays NAV2 waypoint frequency or identifier in the BRG2 Information Window. GPS – Displays GPS waypoint identifier and GPS distance information in the BRG2 Information Window. OFF – Removes the BRG2 Information Window. STD BARO – Press to set the barometric pressure to 29.
SECTION 1 SYSTEM OVERVIEW OBS – Press to select OBS mode on the CDI when navigating by GPS (only available with active leg). CDI – Press to change navigation mode on the CDI between GPS, VOR1, and VOR2. XPDR – Press to display the transponder mode selection softkeys. STBY – Press to select standby mode. ON – Press to select mode A. ALT – Press to select altitude reporting mode. VFR – Press to automatically squawk 1200 (only in the U.S.A., refer to ICAO standards for VFR codes in other countries).
SECTION 1 SYSTEM OVERVIEW 1.3 MFD SOFTKEYS STRMSCP (optional) – Pressing this softkey displays/ removes Stormscope lightning data on the Navigation Map. NEXRAD (optional) – Pressing this softkey displays/ removes precipitation data on the Navigation Map. XM LTNG (optional) – Pressing this softkey displays/ removes XM Radio lightning data on the Navigation Map. BACK – Pressing this softkey displays the ENGINE and MAP top level softkeys.
SECTION 1 SYSTEM OVERVIEW 1.4 MFD PAGE GROUPS 1) Turn the large FMS Knob until the desired page group is selected. 2) Turn the small FMS Knob to select pages within the group. See Figure 1-8. Nearest Group Auxiliary Page Group Number of Pages in Current Group Waypoint Page Group Map Page Group Figure 1-7 Page Group Icon 1.5 Selected Page BACKLIGHTING To manually adjust the backlight for the PFD and MFD: 1-8 1) Press the MENU Key on the PFD to display the PFD Setup Menu Window.
SECTION 1 SYSTEM OVERVIEW 1.6 DATABASE UPDATES Aviation Database Update 7) Terrain and Obstacle Database Updates NOTE: The display downloads the aviation database and stores it internally. The aviation database SD card is not required to remain in the display after the update. 1) 2) 3) NOTE: The data contained in the terrain and obstacle databases comes from government agencies.
SECTION 1 SYSTEM OVERVIEW 3) Acknowledge the Power-up Page agreement by pressing the ENT Key or the right most softkey. 4) At the MAP – NAVIGATION MAP page, select the MAP Softkey and check to make sure that the TOPO and TERRAIN softkeys are functional (not grayed out). 5) Power down the G1000. Figure 1-11 Power-Up Splash Screen Window 1-10 Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100 190-00645-00 Rev.
SECTION 2 FLIGHT INSTRUMENTS SECTION 2: FLIGHT INSTRUMENTS The following discussions pertain to the Primary Flight Display, unless otherwise indicated.
SECTION 2 FLIGHT INSTRUMENTS 10 1 9 8 2 7 3 6 4 5 1 Traffic Annunciation 6 Alerts Window 2 Selected Heading Box 7 Selected Course Box 3 Inset Map 8 Annunciation Window 4 BRG1 Information Window 9 Vertical Deviation/Glideslope Indicator 5 BRG2 Information Window 10 Marker Beacon Annunciation Figure 2-2 Additional PFD Information Distance to Next Waypoint Next Waypoint Desired Track to Next Waypoint Current Track Figure 2-3 PFD Navigation Status Window 2-2 Garmin G1000 Cockpit
SECTION 2 FLIGHT INSTRUMENTS 2.1 AIRSPEED INDICATOR Max Speed for Approach Flap Setting Actual Airspeed True Airspeed Box Airspeed Trend Vector Speed Ranges Vspeed References Figure 2-4 Airspeed Indicator Speed Indication The indicated airspeed is displayed inside the black pointer. The pointer will become red upon reaching Vne. Vspeed References Vspeed References are turned on or off in the Timer/References Window. Press the TMR/REF Softkey to display the widow.
SECTION 2 FLIGHT INSTRUMENTS 2.3 ALTIMETER Altitude Alerting Selected Altitude Box Altitude Select Bug Within 200 ft Deviation of ±200 ft Figure 2-8 Altitude Alerting Visual Annunciations Altitude Trend Vector Current Altitude Visual annunciations appear in the Selected Altitude Box. Whenever the Selected Altitude is changed, the Altitude Alerter is reset. The Altitude Alerter is independent of the Automatic Flight Control System.
SECTION 2 FLIGHT INSTRUMENTS Within 2500 ft Within 100 ft 2.5 MARKER BEACON ANNUNCIATIONS Marker Beacon Annunciation Barometric Minimum Bug Barometric Minimum Box Vertical Deviation/Glideslope Indicator Altitude Reached Figure 2-10 Marker Beacon and Vertical Deviation 2.6 VERTICAL SPEED INDICATOR Figure 2-9 Barometric Minimum Descent Altitude Alerting Visual Annunciations 2.
SECTION 2 FLIGHT INSTRUMENTS 2.
SECTION 2 FLIGHT INSTRUMENTS turn rate trend vector shows the current turn rate. The end of the trend vector gives the heading predicted in six seconds, based on the present turn rate. At rates greater than 4 deg/sec, an arrowhead appears at the end of the magenta trend vector and the prediction is no longer valid.
SECTION 2 FLIGHT INSTRUMENTS Distance to Bearing Source Waypoint Identifier Bearing Pointer Source Icon Figure 2-19 BRG2 Information Window Navigation Source To change between navigation sources: 1) Press the CDI Softkey to change from GPS to VOR1/LOC1. 2) Press the CDI Softkey again to change from VOR1/LOC1 to VOR2/LOC2. 3) Press the CDI Softkey a third time to return to GPS.
SECTION 3 – EICAS SECTION 3: ENGINE INDICATION Engine Display In all cases green indicates normal operation, yellow indicates caution, and red indicates warning. Engine System Display Pressing the SYSTEM Softkey displays the System Display. This display presents a numerical indication of oil, fuel, and electrical parameters. Pressing the ENGINE Softkey makes available the SYSTEM and FUEL softkeys which in turn provide access to the System Display and the Fuel Display, respectively.
SECTION 3 – EICAS Engine Fuel Display NOTE: Fuel calculations do not use the aircraft fuel quantity indicators, and are calculated from the last time the fuel was reset using fuel flow. Pressing the FUEL Softkey displays the System Display. The following softkeys allow for adjustment of the remaining fuel quantity.
SECTION 4 – NAV/COM & TRANSPONDER SECTION 4: NAV/COM AND TRANSPONDER 4.1 NAV/COM DESCRIPTION The Nav/Com controls and frequency boxes are located on the Primary Flight Display and the Multi-Function Display in the same locations. NAV Controls NAV Frequency Box COM Frequency Box COM Controls Figure 4-1 G1000 NAV/COM Control Location (PFD) 190-00645-00 Rev.
SECTION 4 – NAV/COM & TRANSPONDER Standby NAV Frequency Field Tuning Box Selected COM Frequency Selected NAV Frequency Figure 4-2 Frequency Fields Active NAV Frequency Field Frequency Transfer Arrow Active COM Frequency Field Standby COM Frequency Field Tuning Box Tuning Box Figure 4-3 Frequency Transfer Arrow and Tuning Box NAV Controls COM Controls VOL/PUSH ID Knob VOL/PUSH SQ Knob Frequency Transfer Key Dual NAV Knob Dual COM Knob • Turn to tune in desired frequencies.
SECTION 4 – NAV/COM & TRANSPONDER 4.1 RADIO STATUS INDICATIONS 4.4 QUICKLY ACTIVATING 121.500 MHZ • RX – When a COM signal is received, a white ‘RX’ appears by the active COM frequency during signal reception. Pressing and holding the COM Frequency Transfer Key for approximately two (2) seconds automatically tunes the selected COM radio to the emergency frequency. • TX – When a COM radio is transmitting, a white ‘TX’ indication appears to the right of the corresponding COM frequency. 4.
SECTION 4 – NAV/COM & TRANSPONDER 4.5 TRANSPONDER OPERATION Mode Selection The STBY, ON, ALT, VFR, CODE, and IDENT Softkeys can be accessed by pressing the XPDR Softkey. 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. All transponder replies requesting altitude information are provided with pressure altitude information.
SECTION 4 – NAV/COM & TRANSPONDER 2) 3) Press the CODE Softkey to display the transponder Code Selection softkeys, which includes the digit softkeys. Press the appropriate digit softkeys to enter the code in the four-digit code field of the Transponder Status Box. Five seconds after the fourth digit has been entered, the transponder code becomes activated. Flight ID Reporting If so configured, the Flight ID may be entered in the Timer/Reference Window.
SECTION 4 – NAV/COM & TRANSPONDER Blank Page 4-6 Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100 190-00645-00 Rev.
SECTION 5 – AUDIO PANEL SECTION 5: AUDIO PANEL Transceiver Audio Transmitters Disabled on Quest Kodiak 100 Disabled on Quest Kodiak 100 Speaker Passenger Address Marker Beacon Signal Sensitivity Marker Beacon/Mute Navigation Radio Audio Disabled on Quest Kodiak 100 Manual Squelch Digital Recording Playback ICS Isolation ICS Volume and Squelch Control Master Volume Control SQ Annunciation VOL Annunciation Reversionary Mode for PFD1 and MFD Reversionary Mode for PFD2 and MFD Pilot Side Copi
SECTION 5 – AUDIO PANEL 5.1 COM RADIO SELECTION Outer Marker Annunciator Middle Marker Annunciator Pressing the COM1 MIC or COM2 MIC Key selects the active transmitter (i.e., microphone). The associated receiver audio (COM1 or COM2) also becomes selected when the COM MIC Key is pressed. To prevent deselecting the desired received audio when pressing another COM MIC Key, press the already selected COM1 or COM2 Key before pressing the other COM MIC Key.
SECTION 5 – AUDIO PANEL 5.4 INTERCOM SYSTEM (ICS) ISOLATION Press the PILOT and/or COPLT Key to select who is isolated from hearing the Nav/Com radios and music. Selection scenarios are addressed in Table 5-1. 5.5 INTERCOM SQUELCH CONTROL Select manual squelch for intercom audio by pressing the MAN SQ Key to light the annunciator. Pressing the small VOL/SQ Knob now switches between volume and squelch adjustment by lighting VOL or SQ respectively.
SECTION 5 – AUDIO PANEL 5.6 DIGITAL CLEARANCE RECORDER AND PLAYER Each reception of primary active COM audio is automatically recorded in a memory block. When the next transmission is received, it is recorded in the next memory block, and so on. Once the 2.5 minutes of recording time has been reached, the recorder begins recording over the stored memory blocks, starting from the oldest block. Powering off the unit automatically clears all recorded blocks. Figure 5-8 Clearance Recorder Play Key 5.
SECTION 6 – AUTOMATIC FLIGHT CONTROL SECTION 6: AUTOMATIC FLIGHT CONTROL Refer to the pilot’s guide for the installed autopilot system. 190-00645-00 Rev.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Blank Page 6-2 Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100 190-00645-00 Rev.
SECTION 7 – NAVIGATION SECTION 7: NAVIGATION The following discussions pertain to the Multi Function Display, unless otherwise indicated. 7.1 NAVIGATION MAP PAGE Select the MAP Page Group 1) Turn the large FMS Knob until ‘MAP’ is highlighted in the page group window in the lower right of the MFD display. 2) Turn the small FMS Knob to select the first MAP page (indicated by a solid rectangular icon).
SECTION 7 – NAVIGATION 3) Turn the small FMS Knob to display a list of waypoints or airports. 4) Continue turning the small FMS Knob to scroll through the list and highlight the desired waypoint or airport. 5) Press the ENT Key to confirm the selection. Press ENT again to activate a Direct-to. To Re-center the CDI to the Destination Waypoint Press the Direct-to ( ) Key, followed by pressing the ENT Key twice. If a missed approach point (MAP) is the current destination, the approach will be canceled.
SECTION 7 – NAVIGATION 7.3 AIRPORT INFORMATION a list is displayed from which to choose the desired location. 6) To remove the flashing cursor, press the FMS Knob. Access Runway Information 1) With the Airport Information Page displayed, press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to place the cursor on the ‘RUNWAYS’ identifier field. 3) Turn the small FMS Knob to display the next runway for the selected airport.
SECTION 7 – NAVIGATION 7.4 INTERSECTION INFORMATION 7.5 NDB INFORMATION Select the Intersection Information Page 1) Turn the large FMS Knob to select the ‘WPT’ page group. 2) Turn the small FMS Knob to select the second rectangular page icon. Figure 7-7 NDB Information Page Select the NDB Information Page 1) Turn the large FMS Knob to select the ‘WPT’ page group.
SECTION 7 – NAVIGATION 7.6 VOR INFORMATION 7.7 USER WAYPOINT INFORMATION PAGE See the Flight Planning section for a discussion on creating and modifying user defined waypoints. 7.8 NEAREST AIRPORTS Figure 7-8 VOR Information Page Select the VOR Information Page 1) Turn the large FMS Knob to select the ‘WPT’ page group. 2) Turn the small FMS Knob to select the fourth rectangular page icon.
SECTION 7 – NAVIGATION 3) Press the FMS Knob to remove the flashing cursor. Access Runway Information for the Selected Airport 1) With the Nearest Airports Page displayed, press the RNWY Softkey to place the cursor in the ‘RUNWAYS’ field. 2) Turn the small FMS Knob to select the desired runway. 3) Press the FMS Knob to remove the flashing cursor.
SECTION 7 – NAVIGATION 7.9 NEAREST INTERSECTIONS 7.10 NEAREST NDB Figure 7-11 Nearest Intersections Page Select the Nearest Intersections Page 1) 2) Turn the large FMS Knob to select the ‘NRST’ page group. Turn the small FMS Knob to select the second rectangular page icon. Figure 7-12 Nearest NDB Page Select the Nearest NDB Page 1) Turn the large FMS Knob to select the ‘NRST’ page group. 2) Turn the small FMS Knob to select the third rectangular page icon.
SECTION 7 – NAVIGATION 7.11 NEAREST VOR 2) Select the Nearest VOR Page 1) Turn the large FMS Knob to select the ‘NRST’ page group. 2) Turn the small FMS Knob to select the fourth rectangular page icon. 3) Press the ENT Key. The selected VOR frequency is placed in the NAV standby frequency field. Press the FMS Knob to remove the flashing cursor. 7.
SECTION 7 – NAVIGATION 3) Press the FMS Knob to remove the flashing cursor. 7.14 NEAREST AIRSPACES 7.13 NEAREST FREQUENCIES Figure 7-16 Nearest Airspaces Page Select the Nearest Airspaces Page Figure 7-15 Nearest Frequencies Page 1) Turn the large FMS Knob to select the ‘NRST’ page group. 2) Turn the small FMS Knob to select the seventh rectangular page icon. Select the Nearest Frequencies Page 1) Turn the large FMS Knob to select the ‘NRST’ page group.
SECTION 7 – NAVIGATION View Additional Details for a Listed Airspace 1) With the Nearest Airspace Page displayed, press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to scroll through the list, highlighting the desired airspace. 3) Press the ALERTS Softkey to place the cursor in the ‘AIRSPACE ALERTS’ field. 4) Turn either FMS Knob to select the desired airspace. 5) Press the FMS Knob to remove the flashing cursor.
SECTION 8 – FLIGHT PLANNING SECTION 8: FLIGHT PLANNING 4) Repeat steps 2 and 3 until the desired name is entered. The following discussions pertain to the Multi Function Display, unless otherwise indicated. 5) Press the ENT Key. 6) Press the ENT Key a again to accept the new waypoint identifier. 7) The cursor is now in the ‘REFERENCE WAYPOINTS’ field. If desired, the waypoint can be defined by a reference waypoint.
SECTION 8 – FLIGHT PLANNING Create User Waypoints from the Navigation Map Page 1) With the Navigation Map Page displayed, push the Joystick to activate the panning function. The target pointer is displayed at the present aircraft position. 2) Move the Joystick to place the pointer at the desired position 3) Press the ENT Key. The User Waypoint Information Page is now displayed with the captured position. 4) Turn the FMS Knobs to select a waypoint name.
SECTION 8 – FLIGHT PLANNING 8.4 ACTIVATE A FLIGHT PLAN LEG 1) From the Active Flight Plan Page, press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the desired destination waypoint. 2) Press the ACT LEG Softkey (using MFD only). OR 3) 4) Press the MENU Key, select the ‘Activate Leg’ option from the page menu and press the ENT Key. This step must be used when activating a leg from the PFD. the flight plan.
SECTION 8 – FLIGHT PLANNING 8.7 CREATE A NEW FLIGHT PLAN Create a New Flight Plan Using the MFD 1) 2) NOTE: A flight plan cannot be entered using the PFD if another flight plan is active. Press the NEW Softkey to display a blank flight plan page for the first empty storage location. 3) Turn the small FMS Knob to display the Waypoint Information Window. 4) Turn the small FMS Knob to enter the first character of the identifier of the departure waypoint.
SECTION 8 – FLIGHT PLANNING 8.8 LOAD A DEPARTURE See the Procedures section for a discussion on loading and activating departure procedures. 8.9 LOAD AN ARRIVAL Figure 8-13 Store Flight Plan Confirmation 8.13 EDIT A STORED FLIGHT PLAN See the Procedures section for a discussion on loading and activating arrival procedures. 1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page. 8.10 LOAD AN APPROACH 2) Press the FMS Knob to activate the cursor.
SECTION 8 – FLIGHT PLANNING 5) Once all changes have been made, press the FMS Knob to remove the cursor. 3) Press the DELETE Softkey. 4) A ‘Delete flight plan #?’ confirmation window is displayed. With ‘OK’ highlighted, press the ENT Key to delete the flight plan. To cancel, turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key. 8.15 INVERT AND ACTIVATE A STORED FLIGHT PLAN 1) From the Flight Plan Catalog Page, press the FMS Knob to activate the cursor.
SECTION 8 – FLIGHT PLANNING 3) The current page mode is displayed at the top of the page: ‘AUTOMATIC’ or ‘MANUAL’. To change the page mode, press the AUTO or MANUAL Softkey. Starting WPT 6) Ending WPT For flight plan leg planning, press the FPL Softkey (at the bottom of the display) and turn the small FMS Knob to select the desired flight plan (already stored in memory), by number.
SECTION 8 – FLIGHT PLANNING airspeed field. Turn the FMS Knobs to enter a calibrated airspeed. Press the ENT Key when finished. 3) Press the FMS Knob to activate the cursor. 4) With the ‘TARGET POSITION’ distance field highlighted, turn the FMS Knobs to select the desired distance for Top Of Climb or Bottom Of Descent from the VNAV profile endpoint. The default distance is 4 nm. 5) Press the ENT Key. The cursor is now positioned over the ‘Before’ and ‘After’ field.
SECTION 8 – FLIGHT PLANNING can be specified from the waypoints contained in the flight plan. By default, the last waypoint in the flight plan is selected. Highlight the desired waypoint. 9) Press the ENT Key. 10) With the ‘TARGET ALTITUDE’ field highlighted, turn the small and large FMS Knobs to select the target altitude. If the selected altitude is above the current aircraft altitude, a profiled climb is created.
SECTION 8 – FLIGHT PLANNING Blank Page 8-10 Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100 190-00645-00 Rev.
SECTION 9 – PROCEDURES SECTION 9: PROCEDURES 9.1 ARRIVALS AND DEPARTURES Load and Activate a Departure Procedure 1) With the Navigation Map Page displayed, press the FPL Key. 2) Press the LD DP Softkey. If a flight plan is active, the departure airport will be displayed as the default. A list of available departures is also displayed. 3) If no flight plan is active, use the FMS Knobs to enter the identifier of the desired airport. Press the ENT Key.
SECTION 9 – PROCEDURES 9.2 Figure 9-3 Select Arrival 6) A second window is displayed listing available transitions for the arrival. Turn either FMS Knob to highlight the desired transition waypoint and press the ENT Key. APPROACHES Not all approaches in the database are approved for GPS use. When selecting an approach, a “GPS” designation to the right of the procedure name indicates the procedure can be flown using the GPS receiver.
SECTION 9 – PROCEDURES Selecting ‘Load?’ will add the procedure to the flight plan without immediately using it for navigation guidance. Activate An Approach in the Active Flight Plan Figure 9-6 Selecting an Approach Procedure 5) Turn either FMS Knob to highlight the desired approach. Press the ENT Key. 6) The cursor will move to the TRANSITIONS field. Turn the large FMS Knob to highlight the desired transition waypoint and press the ENT Key.
SECTION 9 – PROCEDURES Blank Page 9-4 Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100 190-00645-00 Rev.
SECTION 10 – HAZARD AVOIDANCE SECTION 10: HAZARD AVOIDANCE 10.2 STORMSCOPE® (OPTIONAL) WARNING: Weather information on the G1000 MFD is approved for weather avoidance only, not weather penetration. Refer to the WX-500 Pilot’s Guide for detailed operation. 10.1 CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1) 2) 3) With the Navigation Map Page displayed, press the MENU Key to display the Navigation Map Page Menu. The cursor flashes on the ‘Map Setup’ option. Press the ENT Key.
SECTION 10 – HAZARD AVOIDANCE At a map range of less than 25 nm, Stormscope lightning data is not displayed, but can still be present. The presence of Stormscope lightning data is indicated by the annunciation ‘LTNG < 25 nm’ in the upper right corner. 2) Turn the small FMS Knob until the Stormscope Page is selected. Figure 10-5 Lightning Display Range Annunciation To select ‘cell’ or ‘strike’ as the Stormscope lightning mode: 1) With the Weather Group selected, press the ENT Key.
SECTION 10 – HAZARD AVOIDANCE Softkeys are displayed. Press the 360 Softkey to display a 360˚ viewing are or press the ARC Softkey to display a 120˚ viewing area. Press the CLEAR Softkey to remove all Stormscope lightning data from the display. 10.3 XM WEATHER (OPTIONAL) WARNING: Use of XM weather for hazardous weather penetration is not recommended. Weather information provided by XM Radio Service is approved only for weather avoidance, not penetration. 1) Press the MAP Softkey.
SECTION 10 – HAZARD AVOIDANCE Displaying Weather on the Weather Data Link Page To select 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. 3) Press the available softkeys to select the desired XM weather product. 4) Press the LEGEND Softkey to view the legends for the selected products. If necessary, turn either FMS Knob to scroll through the list.
SECTION 10 – HAZARD AVOIDANCE CELL MOV – pressing the CELL MOV Softkey shows storm cell movement by displaying an arrow. pointing in the direction of predicted movement. The display is updated every 12 minutes. SIG/AIR – pressing the SIG/AIR Softkey shows SIGMET and AIRMET information. The display is updated every 12 minutes. METAR – press the METAR Softkey to graphically display METARs. METARS are shown as colored flags at airports providing METAR reports. The display is updated every 12 minutes.
SECTION 10 – HAZARD AVOIDANCE • • • • • Surface Analysis Freezing Levels Winds Aloft County Warnings Cyclone Warnings Echo Top (Cloud Top and Echo Top Mutually Exclusive) Figure 10-10 Weather Product Symbols The XM Information Page in the AUX Page Group will display the weather products available for the current subscription. A green box by the weather product means that it is available.
SECTION 10 – HAZARD AVOIDANCE 10.4 TRAFFIC INFORMATION SERVICE (TIS) Traffic Advisory, aircraft is 400’ above & Traffic out of Traffic Mode descending, moving in the direction of the line range NOTE: If the G1000 is configured to use the optional Ryan 9900BX Traffic Advisory System, TIS will not be available for use. NOTE: Traffic Information Service (TIS) is only available when the aircraft is within the service volume of a TIS capable terminal radar site.
SECTION 10 – HAZARD AVOIDANCE 10.5 SKYWATCH TRAFFIC ADVISORY SYSTEM (TAS)(OPTIONAL) Traffic Advisory, aircraft is 400’ below Traffic Mode Altitude Mode & climbing Traffic, Out of Range Refer to the SkyWatch pilot’s guide for a detailed discussion of the SkyWatch system. Displaying Traffic on the Traffic Map Page 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Traffic Map Page. 3) Press the OPERATE Softkey to begin displaying traffic.
SECTION 10 – HAZARD AVOIDANCE 4) Traffic Advisory Non-Bearing Traffic Off Scale Traffic Advisories Banner Rotate the Joystick clockwise to display a larger area or rotate counter-clockwise to display a smaller area. Non-Threat Traffic Figure 10-13 TAS Traffic on Navigation Map 10.6 TERRAIN AND OBSTACLE PROXIMITY NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south.
SECTION 10 – HAZARD AVOIDANCE Unlighted Obstacle (Height is less than 1000’ AGL) Lighted Obstacle (Height is less than 1000’ AGL) Unlighted Obstacle (Height is greater than 1000’ AGL) Lighted Obstacle (Height is greater than 1000’ AGL) Figure 10-15 Obstacle Symbols 10.7 TERRAIN AWARENESS & WARNING SYSTEM (TAWS) DISPLAY (OPTIONAL) NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south.
SECTION 10 – HAZARD AVOIDANCE Color Terrain/Obstacle Location Red Terrain/Obstacle above or within 100’ below or above aircraft altitude. Yellow Terrain/Obstacle between 100’ and 1000’ below current aircraft altitude. Black Terrain/Obstacle is more than 1000’ below aircraft altitude. Potential Impact Point Projected Flight Path 100' Threshold Unlighted Obstacle 1000' Enable/Disable Aviation Data 1) While the TAWS Page is displayed, press the MENU Key.
SECTION 10 – HAZARD AVOIDANCE 1) 2) 3) While the TAWS Page is displayed, press the MENU Key. Turn the small FMS Knob to select ‘Test TAWS’. Press the ENT Key. During the test ‘TAWS TEST’ is displayed in the center of the TAWS Page. When all is in working order, “TAWS System Test, OK” will be heard.
The purpose of the Excessive Descent Rate alert is to provide suitable alerts when the aircraft is determined to be closing (descending) upon terrain at an excessive speed. Figure 10-20 displays the correlation between height above terrain and descent rate, resulting in the two EDR alerts. EDR alerts have two levels of severity, caution (sink rate) and warning (pull-up).
SECTION 10 – HAZARD AVOIDANCE Alert Annunciations Figure 10-22 Alert Pop-Up Press the ENT Key to display the TAWS Page, or press the CLR Key to remain on the Navigation Map Page. Alert Annunciation Figure 10-24 Alert Annunciation on the TAWS Page Alert Annunciation Displaying Terrain and Obstacles on the Navigation Map 1) 2) With the Navigation Map displayed, press the MAP Softkey. Press the TERRAIN Softkey. Terrain and obstacle proximity will now be displayed on the map.
SECTION 10 – HAZARD AVOIDANCE TAWS Alerts Summary The following table shows the possible TAWS alert types with corresponding annunciations and aural messages.
SECTION 10 – HAZARD AVOIDANCE The following system status annunciations may also be issued. PFD/MFD TAWS Page Annunciation MFD Pop-Up Alert Aural Message TAWS System Test Fail None “TAWS System Failure” TAWS Alerting is disabled None None No GPS position or excessively degraded GPS signal None “TAWS Not Available” “TAWS Availble” will be heard when sufficient GPS signal is re-established.
SECTION 11 – ABNORMAL OPERATION SECTION 11: ABNORMAL OPERATION 11.1 REVERSIONARY MODE Should a system detected failure occur in either display, the G1000 automatically enters reversionary mode. In reversionary mode, critical flight instrumentation is combined with engine instrumentation on the remaining display. Minimal navigation capability is available on the reversionary mode display.
SECTION 11 – ABNORMAL OPERATION 11.2 ABNORMAL COM OPERATION When a COM tuning failure is detected by the system, the emergency frequency (121.500 MHz) is automatically loaded into the active frequency field of the COM radio for which the tuning failure was detected. In the event of a dual display failure, the emergency frequency (121.500 MHz) automatically becomes the active frequency to the pilot through the pilot headset. 11.
SECTION 12 – ANNUNCIATIONS & ALERTS SECTION 12: ANNUNCIATIONS & ALERTS NOTE: The Airplane Flight Manual supersedes information found in this document. System Annunciation Red ‘X’ Annunciation Window Alerts Window Figure 12-1 G1000 Alerting System ALERTS Softkey Annunciation The G1000 Alerting System conveys alerts to the pilot using a combination of the following items: • Annunciation Window: The Annunciation Window displays abbreviated annunciation text.
SECTION 12 – ANNUNCIATIONS & ALERTS detects invalid data. • Audio Alerting System: The G1000 system issues audio alert tones when specific system conditions are met. See the Alert Levels Definitions section for more information. 12.1 ALERT LEVEL DEFINITIONS of the message advisory alert and displays the alert text message in the Alerts Window. Figure 12-2 WARNING Softkey Annunciation The G1000 Alerting System, as installed in Quest Kodiak 100 aircraft, uses three alert levels.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.2 AIRCRAFT ALERTS See the Airplane Flight Manual for information regarding pilot responses. WARNING Alerts Annunciation Window Text BETA OIL PRES LO FUEL OFF RESERVE FUEL CO LVL HIGH OIL PRES LOW Alerts Window Message Beta operation is active while airborne. Oil pressure is below 40 psi. Fuel cutoff switch is active. Reserve fuel is in use. Carbon Monoxide level is too high. Low oil pressure.
SECTION 12 – ANNUNCIATIONS & ALERTS Annunciation Advisory Annunciation Window Text AUX PUMP ON BETA DE-ICE PR HI FOD DOOR BP IGNITION ON PITO FL L PITO FL R PITO FL L-R STARTER ON Alerts Window Message Auxiliary fuel pump is on. Beta operation is active. De-icing fluid pressure is greater than TBD psi. FOD door is in bypass position Engine ignition is active. Left pitot heat is inoperative. Right pitot heat is inoperative. Left and right pitot heat are inoperative. Engine starter is active.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.4 G1000 SYSTEM ANNUNCIATIONS When an LRU or an LRU function fails, a large red ‘X’ is typically displayed on windows associated with the failed data. The following section describes various system annunciations. Refer to the POH for additional information regarding pilot responses to these annunciations. System Annunciation NOTE: Upon power-up of the G1000 system, certain windows remain invalid as G1000 equipment begins to initialize.
SECTION 12 – ANNUNCIATIONS & ALERTS System Annunciation Comment Display is not receiving vertical speed input from the air data computer. Display is not receiving valid heading input from AHRS. GPS information is either not present or is invalid for navigation use. Note that AHRS utilizes GPS inputs during normal operation. AHRS operation may be degraded if GPS signals are not present (see POH). Display is not receiving valid transponder information.
SECTION 12 – ANNUNCIATIONS & ALERTS A red ‘X’ may be the result of an LRU or an LRU function failure. The Figure 12-5 illustrates all possible flags and the responsible LRUs. GIA 63 Integrated Avionics Units GIA 63 Integrated Avionics Units GDC 74A Air Data Computer GRS 77 AHRS OR GMU 44 Magnetometer GEA 71 Engine Airframe Unit OR GIA 63 Integrated Avionics Unit GIA 63 Integrated Avionics Units GDC 74A Air Data Computer Figure 12-5 G1000 System Failure Annunciations 12.
SECTION 12 – ANNUNCIATIONS & ALERTS MFD & PFD Message Advisories 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. PFD1 CONFIG – PFD1 configuration error. Config service req’d. PFD2 CONFIG – PFD2 configuration error. Config service req’d.
SECTION 12 – ANNUNCIATIONS & ALERTS MFD & PFD Message Advisories (Cont.) Message Comments PFD1 VOLTAGE – PFD1 has low voltThe PFD1 voltage is low. The G1000 system should be serviced. age. Reducing power usage. PFD2 VOLTAGE – PFD2 has low voltThe PFD2 voltage is low. The G1000 system should be serviced. age. Reducing power usage. MFD1 VOLTAGE – MFD1 has low voltThe MFD1 voltage is low. The G1000 system should be serviced. age. Reducing power usage.
SECTION 12 – ANNUNCIATIONS & ALERTS Database Message Advisories (Cont.) Alerts Window Message DB MISMATCH – Basemap database version mismatch. Xtalk is off. DB MISMATCH – Terrain database version mismatch. Xtalk is off. DB MISMATCH – Terrain database type mismatch. Xtalk is off. DB MISMATCH – Obstacle database version mismatch. Xtalk is off DB MISMATCH – Airport Terrain database mismatch. Xtalk is off Comments The PFD and MFD have different basemap database versions installed. Crossfill is off.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63 Message Advisories Alerts Window Message Comments GIA1 CONFIG – GIA1 configuration error. Config service req’d. The GIA1 and/or GIA2 configuration settings do not match backup configuration memory. The G1000 system should be serviced. GIA2 CONFIG – GIA2 configuration error. Config service req’d. GIA1 COOLING – GIA1 temperature too low. The GIA1 and/or GIA2 temperature is too low to operate correctly. Allow units to warm up to operating temperature.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63 Message Advisories (Cont.) Alerts Window Message Comments COM1 PTT – COM1 push-to-talk key The COM1 and/or COM2 external push-to-talk switch is stuck in the enable (or is stuck. “pressed”) position. Press the PTT switch again to cycle its operation. COM2 PTT – COM2 push-to-talk key If the problem persists, the G1000 system should be serviced. is stuck.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63 Message Advisories (Cont.) Alerts Window Message NAV1 RMT XFR – NAV1 remote transfer key is stuck. NAV2 RMT XFR – NAV2 remote transfer key is stuck. G/S1 FAIL – G/S1 is inoperative. G/S2 FAIL – G/S2 is inoperative. G/S1 SERVICE – G/S1 needs service. Return unit for repair. G/S2 SERVICE – G/S2 needs service. Return unit for repair. Comments The remote NAV1 and/or NAV2 transfer switch is stuck in the enabled (or “pressed”) state.
SECTION 12 – ANNUNCIATIONS & ALERTS GRS 77 Message Advisories Alerts Window Message AHRS1 TAS – AHRS1 not receiving airspeed. AHRS1 GPS – AHRS1 using backup GPS source. AHRS1 GPS – AHRS1 not receiving any GPS information. AHRS1 GPS – AHRS1 not receiving backup GPS information. AHRS1 GPS – AHRS1 operating exclusively in no-GPS mode. MANIFEST – GRS1 software mismatch. Communication halted. BACKUP PATH – AHRS1 using backup data path. AHRS1 SRVC – AHRS1 Magnetic-field model needs update.
SECTION 12 – ANNUNCIATIONS & ALERTS GDL 69 Message Advisories Alerts Window Message GDL69 CONFIG – GDL 69 configuration error. Config service req’d. GDL69 FAIL – GDL 69 has failed. Comments GDL 69 configuration settings do not match those of backup configuration memory. The G1000 system should be serviced. A failure has been detected in the GDL 69. The receiver is unavailable. The G1000 system should be serviced GDC 74A Message Advisories Alerts Window Message GDC1 CONFIG – GDC1 configuration error.
SECTION 12 – ANNUNCIATIONS & ALERTS Miscellaneous Message Advisories (Cont.) FPL TRUNC – Flight plan has been truncated. APPR VPROF – Approaching VNAV profile. APPR TRG ALT – Approaching target altitude. LOCKED FPL – Cannot navigate locked flight plan. WPT ARRIVAL – Arriving at waypoint -[xxxx] STEEP TURN – Steep turn ahead. INSIDE ARSPC – Inside airspace. ARSPC AHEAD – Airspace ahead less than 10 minutes. ARSPC NEAR – Airspace near and ahead. ARSPC NEAR – Airspace near – less than 2 nm.
SECTION 12 – ANNUNCIATIONS & ALERTS Miscellaneous Message Advisories (Cont.) Alerts Window Message TRAFFIC FAIL – Traffic device has failed. STRMSCP FAIL – Stormscope has failed. BACKUP PATH – Stormscope using backup path. 190-00645-00 Rev. A Comments The G1000 is no longer receiving data from the traffic system. The traffic device should be serviced. Stormscope has failed. The G1000 system should be serviced. Stormscope is using the backup communication path.
SECTION 12 – ANNUNCIATIONS & ALERTS Blank Page 12-18 Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100 190-00645-00 Rev.
INDEX A Abnormal COM operation 11-2 Activate a flight plan 8-3 Active flight plan 8-2 ADVISORY 12-1 Advisory alerts 12-4 Age 10-6 AHRS 12-14 Aircraft alerts 12-3 AIRMET 10-5 Airport frequency 7-6 Airport information 7-3 Airspace alerts 7-9 Airspeed indicator 2-3 Airspeed trend vector 2-3 Alerting System 12-1 Alerts 12-1 Alert levels 12-2 Alert Pop-Up 10-14 Altitude alerting 2-4 Altitude trend vector 2-4 ALT knob 1-3 Annunciations 12-1 Approaches 9-2 Approach activation 4-3 Approach markers Signal augmentation
INDEX Load departure 8-5 Load the frequency for a controlling agency 7-10 Load the nearest ARTCC frequency 7-9 Loss of communication code 4-5 M MAP 7-1 Map panning 10-5 Marker beacon 2-5 messages 12-1 Message advisories 12-2, 12-8 – 1210, 12-12 – 12-17 METAR 10-3, 10-5 MFD 1-1, 4-3 Military interceptor operations code 4-5 MKR/MUTE 5-2, 5-4 Mode selection softkeys 4-4 Morse code identifier 4-3 N Nav/Com controls 4-1 NAV1 5-2 NAV2 5-2 Navigation 7-1 Navigation status window 2-2 NAV frequency window 4-1 NCR 1
Garmin International, Inc. 1200 East 151st Street Olathe, KS 66062, U.S.A. p: 913.397.8200 f: 913.397.8282 Garmin AT, Inc. 2345 Turner Road SE Salem, OR 97302, U.S.A. p: 503.391.3411 f: 503.364.2138 Garmin (Europe) Ltd. Unit 5, The Quadrangle Abbey Park Industrial Estate Romsey, SO51 9DL, U.K. p: 44/0870.851241 f: 44/0870.8501251 Garmin Corporation No. 68, Jangshu 2nd Road Shijr, Taipei County, Taiwan p: 886/2.2642.9199 f: 886/2.2642.9099 www.garmin.com 190-00645-00 Rev. A © 2007 Garmin Ltd.
