Integrated Flight Deck Cockpit Reference Guide Columbia 350/400
Copyright © 2006 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0530.01 or later for the Columbia 400 and System Software version 0545.00 or later for the Columbia 350. 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.
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 Columbia 350/400 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 190-00567-00 Change Summary Production release. Revision Date of Revision Affected Pages A 3/06 i-Index-4 B 6/06 i-Index-4 Description Production release Added Columbia 350 parameters, TAWS changes, and Stormscope.
RECORD OF REVISIONS Blank Page RR-2 Garmin G1000 Cockpit Reference Guide for the Columbia 350/400
TABLE OF CONTENTS SECTION 1: SYSTEM OVERVIEW.................................... 1-1 1.1 1.2 1.3 1.4 1.5 1.6 1.7 PFD/MFD Controls................................................... 1-2 GCU 476 Controls .................................................... 1-4 PFD Softkeys............................................................ 1-6 MFD Softkeys .......................................................... 1-9 MFD Page Groups ................................................. 1-10 Backlighting ...............
TABLE OF CONTENTS 6.6 Roll Axis Modes....................................................... 6-9 Roll Hold Mode (ROL).................................................. 6-9 Heading Select Mode (HDG) ...................................... 6-10 Navigation Mode (GPS, VOR, LOC, or BC)................... 6-11 Navigation Mode Armed....................................... 6-11 Approach Mode (GPS, VAPP or LOC) .......................... 6-12 Go Around (GA) ........................................................
TABLE OF CONTENTS 8.2 8.3 8.4 8.5 8.6 8.7 8.8 8.9 8.10 8.11 8.12 8.13 8.14 8.15 8.16 8.17 8.18 8.19 8.20 Viewing the Active Flight Plan ............................ 8-2 Activate a Stored Flight Plan............................... 8-2 Activate a Flight Plan Leg .................................... 8-3 Stop Navigating a Flight Plan.............................. 8-3 Invert Active Flight Plan ....................................... 8-3 Create a New Flight Plan ......................................
TABLE OF CONTENTS 11.4 Stormscope operation with loss of Heading Input........................................................ 11-2 11.5 Hazard Displays with Loss of GPS Position .... 11-2 SECTION 12: ANNUNCIATIONS & ALERTS .............. 12-1 12.1 Alert Level Definitions ........................................ 12-2 12.2 Aircraft Alerts ........................................................ 12-3 WARNING Alerts ....................................................... 12-3 CAUTION Alerts ..................
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.
SECTION 1 SYSTEM OVERVIEW 1.
SECTION 1 SYSTEM OVERVIEW PFD and MFD controls function the same with the exception of the dedicated Automatic Flight Control System (AFCS) keys located only on the MFD bezel. (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.
SECTION 1 SYSTEM OVERVIEW (16) ENT Key – Accepts a menu selection or data entry. This key is used to approve an operation or complete data entry. It is also used to confirm selections and information entries. (17) Dual ALT Knob – Sets the selected altitude in the box located above the Altimeter. The large knob selects the thousands, while the small knob selects the hundreds.
SECTION 1 SYSTEM OVERVIEW destination (the destination is either specified by the identifier, chosen from the active route, or taken from the map pointer position). (3) MENU Key – Displays a context-sensitive list of options. This list allows the user to access additional features or make setting changes that relate to particular pages. (4) PROC Key – Gives access to IFR departure procedures (DPs), arrival procedures (STARs) and approach procedures (IAPs) for a flight plan.
SECTION 1 SYSTEM OVERVIEW 1.3 PFD SOFTKEYS Softkey ON INSET PFD OBS TERRAIN – Select to display terrain information on the Inset Map. STRMSCP (optional) – Select to display the Stormscope lightning data on the Inset Map (within a 200 nm radius of the aircraft). NEXRAD (optional) – Select to display NEXRAD precipitation data on the Inset Map. XM LTNG (optional) – Select to display the XM Radio lightning data on the Inset Map. BACK – Select to return to the previous level softkey configuration.
SECTION 1 SYSTEM OVERVIEW 360 HSI – Select to display the 360° compass rose. ARC HSI – Select to display the 140° viewable arc. BRG2 (bearing) – Select 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 – Select to set the barometric pressure to 29.
SECTION 1 SYSTEM OVERVIEW OBS – Select to select OBS mode on the CDI when navigating by GPS (only available with active leg). CDI – Select to change navigation mode on the CDI between GPS, VOR1, and VOR2. XPDR – Select to display the transponder mode selection softkeys. STBY – Select to select standby mode. ON – Select to select mode A. ALT – Select to select altitude reporting mode. VFR – Select to automatically squawk 1200 (only in the U.S.A., refer to ICAO standards for VFR codes in other countries).
SECTION 1 SYSTEM OVERVIEW 1.4 MFD SOFTKEYS ENGINE – Selecting this softkey makes available the Engine Display functions. Refer to the Engine Indication System section. MAP – Selecting this softkey enables the following softkeys: TRAFFIC – Selecting this softkey displays/removes Traffic on the Navigation Map. TOPO – Selecting this softkey displays or removes topographic information on the Navigation Map. TERRAIN – Selecting this softkey displays/removes terrain and obstacle data on the Navigation Map.
SECTION 1 SYSTEM OVERVIEW 1.5 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 1-8 Page Group Icon 1.6 Selected Page BACKLIGHTING Manually adjust the backlight for the PFD and MFD: 1-10 1) Press the MENU Key on the PFD to display the PFD Setup Menu Window.
SECTION 1 SYSTEM OVERVIEW 1.7 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.
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 Box 2-2 Garmin G1000 Cockpit Ref
SECTION 2 FLIGHT INSTRUMENTS 2.1 AIRSPEED INDICATOR Speed Ranges Actual Airspeed Airspeed Trend Vector Vspeed References True Airspeed Box Vspeed References Vspeed References are turned on or off in the Timer/References Window. Select the TMR/REF Softkey to display the widow. When active (ON), the Vspeeds are displayed at their respective locations to the right of the airspeed scale.
SECTION 2 FLIGHT INSTRUMENTS 2.3 ALTIMETER Altitude Alerting Selected Altitude Box Altitude Select Bug Within 1000 ft Within 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 Vertical Deviation/Glideslope Indicator Barometric Minimum Box Altitude Reached Figure 2-10 Marker Beacon and Vertical Deviation 2.6 Figure 2-9 Barometric Minimum Descent Altitude Alerting Visual Annunciations 2.
SECTION 2 FLIGHT INSTRUMENTS 2.
SECTION 2 FLIGHT INSTRUMENTS 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 Change navigation sources: 1) Select the CDI Softkey to change from GPS to VOR1/LOC1. 2) Select the CDI Softkey again to change from VOR1/LOC1 to VOR2/LOC2. 3) Select the CDI Softkey a third time to return to GPS.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) SECTION 3: ENGINE INDICATION SYSTEM (EIS) The Engine Instrument Display is displayed on the left side of the MFD.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3.1 Trim EIS DISPLAY Selecting the SYSTEM Softkey on the MFD acesses the Engine Indication System (EIS) Display. For all instruments, green indicates the acceptable operating range; yellow and red indicate caution and warning, respectively. Oxygen System (Optional) Selecting the OXYGEN Softkey on the MFD turns the oxygen system on or off. If no oxygen system is installed, the oxygen gauges will be blank.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3.2 ENGINE LEANING ASSIST DISPLAY 3) Lean the mixture until one of the cylinder’s exhuast temperature peaks. This is indicated by ‘1st’ being displayed below the first cylinder to peak. A bar is also displayed at that point on that cylinder’s bar graph. See Figure 3-3. 4) Richen the mixture until the ∆ PEAK temperature is rich by the amount indicated in the Columbia Airplane Flight Manual (AFM).
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) Leaning for Best Economy 1) Select the SYSTEM Softkey. 2) Select the ASSIST Softkey. 3) Lean the mixture until one of the cylinder’s exhuast temperature peaks. This is indicated by ‘1st’ being displayed below the first cylinder to peak. See Figure 3-3. 4) Continue leaning the mixture until the last of the cylinders peaks. This is indicated by ‘Last’ being displayed below the last peaking cylinder as shown in Figure 3-4.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) Engine Leaning for the Columbia 400 NOTE: The Columbia 400 Airplane Flight Manual (AFM) supersedes information found in this section. Leaning for Best Power 1) Select the SYSTEM Softkey. 2) Select the ASSIST Softkey. 3) Lean the mixture to obtain peak temperature on the TIT displays. See Figure 3-5. Refer to the Columbia Airplane Flight Manual (AFM) for more detailed procedures.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3.3 FUEL CALCULATIONS Fuel Quantity Gauge (Left) Indicates Selected Fuel Tank Fuel Quantity Gauge (Right) Fuel Remaining Fuel Used Calculation Endurance Calculation Range Calculation Figure 3-6 EIS Display - Fuel Calculations Group Fuel used (GAL USED), endurance (ENDUR), and range (RANGE NM) are all calculated based on the last manual adjustment of the fuel remaining (GAL USED). Measured fuel quantity has no effect on fuel calculations.
SECTION 4 – NAV/COM & TRANSPONDER SECTION 4: NAV/COM AND TRANSPONDER The NAV/COM controls and frequency boxes are located on the Primary Flight Display and the MultiFunction Display in the same locations. Operations in the following discussions may also be performed with the corresponding controls on the MFD/PFD Control Unit.
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 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. • Press to change tuning box positions.
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 4.6 TRANSPONDER Mode Selection The STBY, ON, and ALT Softkeys can be accessed by selecting the XPDR Softkey. Ground Mode (Automatic) GND is displayed when the aircraft is on the ground. Following is a list of important codes: • 1200 – VFR code in the U.S.
SECTION 5 – AUDIO PANEL SECTION 5: AUDIO PANEL Transmitters (COM3 MIC is unavailable) Transceiver Audio (COM 3 is unavailable) Split COM Telephone (Unavailable) Passenger Address Speaker Marker Beacon/Mute Marker Beacon Signal Sensitivity Aircraft Navigation Radio Audio (DME, ADF, & AUX unavailable) Manual Squelch Aircraft Navigation Radio Audio Recorded COM Audio Playback ICS Isolation VOL/SQ Volume/Squelch VOL Annunciation SQ Annunciation Reversionary Mode Figure 5-1 Audio Panel Controls
SECTION 5 – AUDIO PANEL 5.1 COM RADIO SELECTION 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. Figure 5-2 Transceivers 5.
SECTION 5 – AUDIO PANEL Marker Beacon Signal Sensitivity The HI SENS Key can be pressed for increased marker beacon signal sensitivity. Figure 5-6 Navigation Radios Figure 5-5 Marker Beacon 5.4 5.5 NAV RADIO AUDIO SELECTION Pressing NAV1 or NAV2 selects and deselects the radio source and activates the annunciator. Selected audio can be heard over the headset and the speakers. These two keys can be selected individually or together.
SECTION 5 – AUDIO PANEL 5.6 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. • Pressing MKR/MUTE while playing a memory block stops play. • Pressing the PLAY Key during play begins playing the previously recorded memory block. Each subsequent press of the PLAY Key will begin playing the next previously recorded block.
SECTION 6 – AUTOMATIC FLIGHT CONTROL SECTION 6: AUTOMATIC FLIGHT CONTROL In addition to the AFCS (Automatic Flight Control System) keys on the MFD, as discussed in the System Overview section, the following buttons and switches used by the AFCS are located in the cockpit separately from the PFD and MFD. • AP DISC (Autopilot Disconnect) Button — Located on the pilot’s control stick, pressing this button disengages the autopilot. Pressing it also acknowledges an autopilot disconnect.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Active Mode Autopilot Status Armed Mode Roll Axis Modes Mode Reference Armed Mode Active Mode Pitch Axis Modes AFCS Status Box System Status Field (see Annunciations & Alerts) Selected Altitude Box Aircraft Attitude Symbol Flight Director Command Bars Figure 6-3 PFD AFCS Display 6.2 OVERSPEED PROTECTION An overspeed annunciation (flashing inverse video) is displayed above the airspeed tape.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Automatic Disengagement 6.4 Automatic disengagement typically occurs due to a failure. Automatic disengagement is annunciated by a flashing ‘AP’, alternating red on white and white on red in the Autopilot Status field. Also, the autopilot disconnect aural alert will be heard. Both the annunciation and the aural alert will continue until acknowledged by pressing the AP DISC button or the MET switch.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Pitch Hold Mode (PIT) 1) Press the AP or FD Key. ‘PIT’ will be displayed in green in the Active Mode field of the AFCS Status Box. The system will maintain or give command bar direction for a constant pitch attitude (pitch reference) depending on which key is pressed. selected altitude is reached ‘ALT’ will flash in green for 10 seconds in the Acitve Mode field, after which the annunciation stops flashing.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Altitude Hold Mode (ALT) 1) Press the ALT Key. The flight director is activated (if not already active) and ‘ALT’ is now displayed in green in the Active Mode field with the current altitude displayed in the Altitude Reference field. 2) Pitch commands will be given to manually maintain the current altitude. Press the AP Key to engage the autopilot for maintaining the current altitude.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Vertical Speed Mode (VS) 1) Press the VS Key. The flight director is now activated (if not already active) and ‘VS’ is displayed in green in the Active Mode field and the Vertical Speed Bug will appear on the Vertical Speed Indicator. Pitch commands are given to manually maintain vertical speed. Press the AP Key to engage the autopilot for maintaining the current vertical speed.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Flight Level Change Mode (FLC) 1) 2) 3) Select the desired altitude by turning the ALT Knob to set the altitude in the Altitude Select Box. This altitude must be selected first because Flight Level Change mode will only fly toward a selected altitude. Press the FLC Key. The flight director is activated (if not already active) and ‘FLC’ is now displayed in green in the Active Mode field and the Airspeed Bug will appear on the Airspeed Indicator.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Go-Around Mode (GA) Glideslope (GS) Pressing the GO AROUND button (not located on the MFD) engages the flight director in a wings level, 7 degree pitch up attitude. Go-Around mode disengages the autopilot, and arms Altitude Hold Mode automatically. Subsequent autopilot engagement is also allowed. If the pitch attitude is changed manually (e.g with the CWS button or the NOSE UP/NOSE DN Keys), Pitch and Roll Hold modes will automatically be selected.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 6.6 ROLL AXIS MODES only the flight director is active, command bars indicate the proper roll attitude. Mode annunciations for active roll axis modes are shown in green during normal operation.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Heading Select Mode (HDG) 1) 2) 3) Turn the HDG Knob to move the heading bug on the HSI to the desired heading. When the knob is turned, the Selected Heading Box will appear and remain for three seconds after the knob stops moving. The selected heading will be displayed in the Selected Heading Box. With the autopilot and/or flight director engaged, press the HDG Key. ‘HDG’ is now displayed in green in the Active Mode field.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Navigation Mode (GPS, VOR, LOC, or BC) Pressing the NAV Key activates the Navigation Mode. The Navigation mode acquires and tracks the selected navigation receiver on the HSI (e.g. GPS, VOR or LOC). GPS roll steering commands are followed when the HSI is in GPS mode, and creates roll steering commands from the Selected Course and deviation when the HSI is in VOR, LOC, or BC (backcourse) modes.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Approach Mode (GPS, VAPP or LOC) The Approach mode acquires and tracks the selected navigation receiver on the HSI (GPS, VOR or LOC). This mode uses the selected navigation receiver deviation and desired course inputs to fly the approach. The Approach mode provides greater sensitivity for VOR tracking than Navigation mode, and allows the autopilot to fly an ILS approach with a glideslope.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 6.7 EXAMPLE PROCEDURES USING AFCS NOTE: The diagrams in the following examples are for instructional purposes only and may not be used for navigation. This section provides a scenario-based set of procedures showing various autopilot modes used during a flight. Other modes and uses of the G1000 may be necessary in real-world scenarios.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Departure 3) Activate Heading Select Mode while the autopilot is engaged in the climb. Climb to the selected altitude and fly an assigned heading: a) Use the HDG Knob to set the Selected Heading to 070°. 1) Upon takeoff, set the Selected Altitude to 7000 feet using the ALT Knob. b) Press the HDG Key. The autopilot follows the Heading Bug on the HSI and turns the aircraft to the desired heading.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Intercepting a VOR Radial NOTE: Changing the HSI mode cancels Navigation Mode and causes the flight director to revert to Roll Hold Mode. During climb-out, the autopilot continues to fly the aircraft in Heading Select Mode. Airway V107 to Panoche VORTAC (PXN) should now be intercepted. 1) Tune the VOR frequency and activate Heading Select Mode. a) Use the CDI Softkey to set the HSI mode to VOR. b) Use the CRS Knob to set the Selected Course to 116°.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Flying a GPS Flight Plan 1) Enter Panoche VORTAC (PXN) and Clovis VORTAC (CZQ) into the GPS flight plan, in preparation to intercept this leg. 2) Transition from VOR to GPS Navigation Mode. a) Use the CDI Softkey to put the HSI in GPS mode. This cancels VOR mode on the HSI and the flight director loses the VOR signal. As a result, the VOR annunciation flashes yellow.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Flight Level Change (Descent) While flying the GPS leg from Panoche VORTAC to Clovis VORTAC, the aircraft is cleared to make a descent to 3000 feet in preparation for the approach to KFAT. 1) Enter Flight Level Change Mode. a) Using the ALT Knob, set the Selected Altitude to 3000 feet. b) Press the FLC Key to activate Flight Level Change Mode. The annunciation ‘FLC’ appears next to the Airspeed Reference, which defaults to the current aircraft airspeed, 142 knots.
SECTION 6 – AUTOMATIC FLIGHT CONTROL ILS Approach 3) In preparation for approach, tune the localizer frequency and select LOC mode on the HSI. 1) Transition from GPS Navigation Mode to Heading Select Mode. 4) Press the APR Key when cleared for approach to arm the Approach Mode. ‘LOC’ and ‘GS’ appear in the armed roll and pitch mode fields, respectively. The autopilot and flight director determine when to begin the turn to intercept the final approach course.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Go-Around / Missed Approach NOTE: As a result of the calculations being performed by the system while flying the holding pattern, the display may resize automatically and the aircraft may not precisely track the holding pattern. 1) Push the Go Around button at the Decision Height to execute a missed approach.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Blank Page 6-20 Garmin G1000 Cockpit Reference Guide for the Columbia 350/400
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 Box 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. 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 NOTE: The numeric keypad is functional in the frequency field, but is not intended to be used to change the frequency value. Highlighting the frequency field is only intended for NAV tuning. 5) 7.7 Press the FMS Knob to remove the flashing cursor. USER WAYPOINT INFORMATION PAGE See the Flight Planning section for a discussion on creating and modifying user defined waypoints. 7.
SECTION 7 – NAVIGATION Access Information on a Specific Airport 1) With the Nearest Airports Page displayed, select the APT Softkey to place the cursor in the ‘NEAREST AIRPORTS’ field. The first airport in the nearest airports list is highlighted. 2) Press the FMS Knob, then turn the large FMS Knob to highlight the desired airport. 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 NOTE: The numeric keypad is functional in the frequency field, but is not intended to be used to change the frequency value. Highlighting the frequency field is only intended for NAV tuning. 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. 2) 3) Press the ENT Key. The selected VOR frequency is placed in the NAV standby frequency field.
SECTION 7 – NAVIGATION 2) 3) within 200 nm, these will be displayed with the closest listed first. 2) Turn the FMS Knobs to select the desired facility or frequency. Turn either FMS Knob to select the desired waypoint. The remaining information on the Nearest User Waypoint Page pertains to the selected Nearest User Waypoint. 3) Press the ENT Key to load the frequency into the COM frequency standby field. 4) Press the FMS Knob to remove the flashing cursor.
SECTION 7 – NAVIGATION • If the aircraft is within two nautical miles of an airspace and the current course will not take the aircraft inside, ‘Within 2 nm’ is displayed. • If the aircraft has entered an airspace, ‘Inside’ is displayed. 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.
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 map 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) Select the ACT LEG Softkey (using MFD only). highlighted, press the ENT Key to deactivate the flight plan. This will not delete the stored flight plan, only the active flight plan.
SECTION 8 – FLIGHT PLANNING 8.7 CREATE A NEW FLIGHT PLAN Create a New Flight Plan Using the MFD 1) 2) Catalog Page. The new flight plan is now in the list. Create a New Flight Plan Using the PFD Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page. NOTE: A flight plan cannot be entered using the PFD if another flight plan is active. Select the NEW Softkey to display a blank flight plan window for the first empty storage location.
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) Select 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, select the AUTO or MANUAL Softkey. Starting WPT to enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint. OR, 6) Ending WPT For flight plan leg planning, select 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 11) The flashing cursor moves to the calibrated airspeed field. Turn the FMS Knobs to enter a calibrated airspeed. Press the ENT Key when finished. 4) 8.20 VERTICAL NAVIGATION (VNAV) PAGE 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 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. If the selected altitude is below the current aircraft altitude, a profiled descent will be created. 11) Press the ENT Key. The cursor is now placed in the ‘TARGET VERTICAL SPEED’ field.
SECTION 8 – FLIGHT PLANNING Blank Page 8-10 Garmin G1000 Cockpit Reference Guide for the Columbia 350/400
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) Select 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 to highlight the desired transition waypoint and press the ENT Key. If the GPS receiver cannot be used for primary guidance, the appropriate navigation receiver must be used for the selected approach (e.g., VOR or ILS). The final course segment of ILS approaches, for example, must be flown by tuning the Nav receiver to the proper frequency and selecting that Nav receiver on the CDI.
SECTION 9 – PROCEDURES 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. (The “Vectors” option assumes vectors will be received to the final course segment of the approach and will provide navigation guidance relative to the final approach course.) Figure 9-7 Selecting an Approach Transition 7) Turn the large FMS Knob to highlight ‘Activate?’ and press the ENT Key to activate the approach.
SECTION 9 – PROCEDURES Blank Page 9-4 Garmin G1000 Cockpit Reference Guide for the Columbia 350/400
SECTION 10 – HAZARD AVOIDANCE SECTION 10: HAZARD AVOIDANCE 10.2 STORMSCOPE® (OPTIONAL, 350 ONLY) WARNING: The Stormscope system is not intended to be used for hazardous thunderstorm penetration. Weather information on the G1000 MFD is approved for weather avoidance only. 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.
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. Stormscope Page 1) Turn the large FMS Knob until the Map Page group is selected. 2) Turn the small FMS Knob until the Stormscope Page is selected.
SECTION 10 – HAZARD AVOIDANCE Change the viewing mode between 360˚ and 120˚: 1) Select the Stormscope Page. 2) Select the VIEW Softkey. The 360 and ARC Softkeys are displayed. Select the 360 Softkey to display a 360˚ viewing area or select the ARC Softkey to display a 120˚ viewing area. Select the CLEAR Softkey to remove all Stormscope lightning data from the display. 10.3 XM® WEATHER (OPTIONAL) WARNING: XM Weather is not intended to be used for hazardous weather penetration.
SECTION 10 – HAZARD AVOIDANCE Displaying Weather on 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) Select the available softkeys to select the desired XM weather product. 4) Select the LEGEND Softkey to view the legends for the selected products. If necessary, turn either FMS Knob to scroll through the list. Press the small FMS Knob or the ENT Softkey to return to the map.
SECTION 10 – HAZARD AVOIDANCE every 5 minutes. CYCLONE – Selecting the CYCLONE Softkey shows the current location of cyclones (hurricanes and tropical storms) and their projected track at various time intervals. The update rate is every 12 minutes. CELL MOV – Selecting 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 – Selecting the SIG/AIR Softkey shows SIGMET and AIRMET information.
SECTION 10 – HAZARD AVOIDANCE Echo Top (Cloud Top and Echo Top Mutually Exclusive) Figure 10-10 Weather Product Symbols • • • • • • City Forecast Surface Analysis Freezing Levels Winds Aloft County Warnings Cyclone Warnings Weather Product 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 RYAN® 9900BX TRAFFIC ADVISORY SYSTEM (TAS) (OPTIONAL) Traffic Advisory, aircraft is 400’ below Traffic Mode Altitude Mode & climbing Traffic, Out of Range Refer to the Ryan 9900BX pilot’s guide for a detailed discussion and an explanation of the aural alerts. 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. ‘TAS OPERATING’ is displayed in the Traffic Mode field.
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 Maximum elevation of topography presently displayed on-screen Minimum elevation of topography presently displayed on-screen Displaying Terrain on the TAWS Page 1) Turn the large FMS Knob to select the Map Page Group.
SECTION 10 – HAZARD AVOIDANCE Enable/Disable Aviation Data 1) While the TAWS Page is displayed, press the MENU Key. 2) Turn the small FMS Knob to select “Show (or Hide) Aviation Data”. 3) Press the ENT Key. Figure 10-18 TAWS Page (ARC View) Figure 10-19 TAWS Page Menu Color Red Terrain/Obstacle Location Suggested Pilot Response Terrain/Obstacle at or within 100’ below or above aircraft altitude. Initiate climb and/or turn away from terrain/obstacle.
SECTION 10 – HAZARD AVOIDANCE TAWS Inhibit Flying VFR into an area where unique terrain exists could cause the system to annunciate a nuisance alert. When TAWS is inhibited, only FLTA and PDA alerts are disabled. Inhibit TAWS: 1) While the TAWS Page is displayed, press the MENU Key. 2) Turn the small FMS Knob to select‘Inhibit TAWS’. 3) Press the ENT Key. Enable TAWS: 1) While the TAWS Page is displayed, press the MENU Key. 2) Turn the small FMS Knob to select ‘Enable TAWS’. 3) Press the ENT Key.
SECTION 10 – HAZARD AVOIDANCE for alerting based on speed, distance, and other parameters. Negative Climb Rate After Takeoff Alert (NCR) The purpose of the Negative Climb Rate After Takeoff alert is to provide suitable alerts to the pilot when the system determines that the aircraft is losing altitude (closing upon terrain) after takeoff. The aural message “Don’t Sink” is given for NCR alerts, accompanied by an annunciation and a pop-up terrain alert on the display.
SECTION 10 – HAZARD AVOIDANCE Displaying Terrain and Obstacles on the Navigation Map 1) 2) With the Navigation Map displayed, select the MAP Softkey. Select 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 • 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. Figure 12-2 WARNING Softkey Annunciation 12.1 ALERT LEVEL DEFINITIONS The G1000 Alerting System, as installed in Columbia 350/400 aircraft, uses three alert levels. • WARNING: This level of alert requires immediate pilot attention.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.2 AIRCRAFT ALERTS See the Airplane Flight Manual for information regarding pilot responses.
SECTION 12 – ANNUNCIATIONS & ALERTS Annunciation Advisory Annunciation Window Text OXYGEN ON SPEED BRAKES Alerts Window Message Reminder: Turn off oxygen Speed brakes are active Audio Alert None None Message Advisory Alerts Alerts Window Message PFD FAN FAIL – The cooling fan for the PFD is inoperative. MFD FAN FAIL – The cooling fan for the MFD is inoperative. AVIONICS FAN – The cooling fan for remote avionics is inoperative. TIMER ZERO – Timer has counted down to zero.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.4 AFCS ALERTS System Status Annunciation System Status Annunciation The following alert annunciations appear in the AFCS System Status Annunciation on the PFD. Figure 12-5 AFCS System Status Annunciation Condition Pitch Failure Annunciation Description Pitch axis control failure. AP is inoperative. Roll Failure Roll axis control failure. AP is inoperative.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.5 TAWS ALERTS Annunciations appear on the PFD and MFD. Pop-up alerts appear only on the MFD.
SECTION 12 – ANNUNCIATIONS & ALERTS TAWS System Status Annunciations 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. System Test in progress None None None “TAWS System Test OK” Alert Type None System Test pass 12.
SECTION 12 – ANNUNCIATIONS & ALERTS System Annunciation Comment Display system is not receiving attitude information from the AHRS. Display system is not receiving airspeed input from air data computer. Display is not receiving altitude input from the air data computer. 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.
SECTION 12 – ANNUNCIATIONS & ALERTS A red ‘X’ may be the result of an LRU or an LRU function failure. The Figure 12-6 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 12-6 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. MFD1 SERVICE – MFD1 needs service. Return unit for repair. PFD1 CONFIG – PFD1 configuration error. Config service req’d. MFD1 CONFIG – MFD1 configuration error. Config service req’d. SW MISMATCH – GDU software mismatch. Xtalk is off.
SECTION 12 – ANNUNCIATIONS & ALERTS Database Message Advisories Alerts Window Message Comments MFD1 DB ERR – MFD1 aviation database error exists. The MFD and/or PFD detected a failure in the aviation database. Attempt to reload the aviation database. If problem persists, the G1000 system should be serviced. PFD1 DB ERR – PFD1 aviation database error exists. MFD1 DB ERR – MFD1 basemap database error exists. The MFD and/or PFD detected a failure in the basemap database.
SECTION 12 – ANNUNCIATIONS & ALERTS Database Message Advisories (Cont.) Alerts Window Message DB MISMATCH – Airport Terrain database mismatch. Xtalk is off Comments The PFD and MFD have different airport terrrain databases installed. Crossfill is off. Install correct airport terrain database in both displays. GMA 1347 Message Advisories Alerts Window Message GMA1 FAIL – GMA1 is inoperative. Comments The audio panel self-test has detected a failure. The audio panel is unavailable.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63 Message Advisories (Cont.) Alerts Window Message Comments GIA1 SERVICE – GIA1 needs service. Return the unit for repair. The GIA1 and/or GIA2 self-test has detected a problem in the unit. The G1000 system should be serviced. GIA2 SERVICE – GIA2 needs service. Return the unit for repair. There is a hardware mismatch between GIA1 and GIA2. The G1000 system should HW MISMATCH – GIA hardware be serviced. mismatch. Communication halted.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63 Message Advisories (Cont.) Alerts Window Message Comments DGRD GPS ACC – GPS position GPS position accuracy has been degraded and RAIM is not available. accuracy degraded & RAIM unavailable. GPS1 FAIL – GPS1 is inoperative. A failure has been detected in the GPS1 and/or GPS2 receiver. The receiver is unavailable. The G1000 system should be serviced. GPS2 FAIL – GPS2 is inoperative. GPS1 SERVICE – GPS1 needs service. Return unit for repair.
SECTION 12 – ANNUNCIATIONS & ALERTS GTX 33 Message Advisories Alerts Window Message XPDR1 CONFIG – XPDR1 config error. Config service req’d. MANIFEST – GTX1 software mismatch. Communication halted. BACKUP PATH – XPDR1 using backup data path. Comments The transponder configuration settings do not match those of backup configuration memory. The G1000 system should be serviced. The transponder has incorrect software installed. The G1000 system should be serviced.
SECTION 12 – ANNUNCIATIONS & ALERTS GMU 44 Message Advisories Alerts Window Message HDG FAULT – AHRS1 magnetometer fault has occurred. MANIFEST – GMU1 software mismatch. Communication halted. Comments A fault has occurred in the GMU 44. Heading is flagged as invalid. The AHRS uses GPS for backup mode operation. The G1000 system should be serviced. The GMU 44 has incorrect software installed. The G1000 system should be serviced.
SECTION 12 – ANNUNCIATIONS & ALERTS Miscellaneous Message Advisories Alerts Window Message Comments FPL WPT LOCK – Flight plan waypoint Upon power-up, the G1000 system detects that a stored flight plan waypoint is is locked. locked. This occurs when an aviation database update eliminates an obsolete waypoint. The flight plan cannot find the specified waypoint and flags this message. This can also occur with user waypoints in a flight plan that is deleted.
SECTION 12 – ANNUNCIATIONS & ALERTS Miscellaneous Message Advisories (Cont.) Alerts Window Message Comments ARSPC NEAR – Airspace near and Special use airspace is near and ahead of the aircraft position. ahead. ARSPC NEAR – Airspace near – less Special use airspace is within 2 nm of the aircraft position. than 2 nm. LEG UNSMOOTH – Flight plan leg will The approaching flight plan waypoints are too close to allow for smooth turns. not be smooth.
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 AFCS 1-3, 6-1, 6-2, 6-4, 6-6, 6-7, 6-9, 6-11, 6-12, 6-13, 12-5 Age 10-6 AHRS 12-15, 12-16 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 Hold 1-4 Altitude hold 1-4, 6-3 – 6-8, 6-10 Altitude t
INDEX I ICAO 4-4 ID 4-3 Imminent Terrain Impact 10-12 Impact point 10-12 Inhibit 10-12 Inhibit TAWS 10-12 INTEG 2-8 Interrogations 4-4 IOI 10-12, 10-15, 12-6 ITI 10-12 K Key(s) 1-4, 1-5 L Lighted obstacle 10-14 Lightning 1-6, 1-9, 10-2, 10-3, 10-4 Load approach 8-5 Load a VOR frequency 7-8 Load departure 8-5 Load the frequency for a controlling agency 7-10 Load the nearest ARTCC frequency 7-9 Loss of communication code 4-4 Index-2 MKR/MUTE 5-2, 5-3, 5-4 Mode selection softkeys 4-4 Morse code identifier 4
INDEX Transponder Status bar 4-4 Trim 3-2, 6-1 Tropical storms 10-5 TX 4-3 U Unlighted obstacle 10-14 Usable fuel 3-6 V Vertical Deviation/Glideslope indicator 2-5 Vertical navigation profile 8-8 Vertical speed 1-4, 2-1, 2-5, 6-3, 6-6, 12-1 Vertical Speed Bug 2-5 Vertical Speed Mode 6-6 VFR code 4-4 VHF 4-1 VOL/PUSH ID 4-2 VOL/PUSH SQ 4-2, 4-3 Volume/squelch 5-4 VS 1-4, 6-3, 6-6 Vspeeds 2-3 W WARN 2-8 Warning 12-1, 12-2 Weather data link page 10-4 Weather product symbol 10-5 Weather product symbols 10-6 W
INDEX Blank Page Index-4 Garmin G1000 Cockpit Reference Guide for the Columbia 350/400
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: 44/0870.8501241 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 190-00567-00 Rev. B © 2006 Garmin Ltd.
