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Garmin Columbia 350/400 User's Manual

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2. _ Com PP s P d EE Ba Ee zd oa GARMIN G1 01010 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 2345 Turner Road SE Salem OR 97302 U S A Tel 503 391 3411 Fax 503 364 2138 Garmin Europe Ltd Unit 5 The Quadrangle Abbey Park Industrial Estate Romsey Hampshire 051 ODL U K Tel 44 0870 8501241 Fax 44 0870 8501251 Garmin Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan Tel 886 02 2642 9199 Fax 886 02 2642 9099 Web Site Address www garmin com Except as expressly provided herein no part of this manual may be reproduced copied transmitted disseminated downloaded or stored in any storage medium for any purpose without the express written permission of Garmin Garmin hereby grants permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use pro
3. 6 3 6 5 Pitch Axis Modes ccccsessessesseesseesseessees 6 3 Pitch Hold Mode PIT o an 6 4 Altitude Hold Mode ALT nnn 6 5 Venica DCCC Mode VS Fenin 6 6 Flight Level Change Mode FLC ssssesecesresseesnen 6 7 Go Around Mode GA 6 8 Glideslone GS laonenn T 6 8 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 TABLE OF CONTENTS 6 6 Roll Axis Modes 6 9 ROM HONG Mode ROL ix canina 6 9 Heading Select Mode HDG 6 10 Navigation Mode GPS VOR LOC or BC 6 11 Navigation Mode Armed isasama 6 11 Approach Mode GPS VAPP or LOC 6 12 GATOUNO A as toh Soca ere vcecibaos letter 6 12 6 7 Example Procedures Using AFCG 6 13 DEO E ener emer mene yn tne nT 6 14 Intercepting a VOR Radial 6 15 Pyma GPS Fint PI assisia 6 16 Flight Level Change DeSCent cesssesesseeeaseean 6 17 E a r en er eee ten nee 6 18 Go Around Missed Approach c scsscessessesseesneerees 6 19 SECTION 7 NAVIGATION 7 1 7 4 Navigation Map Pag 0 cccccceseeceen 7 1 Select the MAP Page GIOUD c scessesseseesseeseesesseean 7 1 7 2 Direct to Navigation 0 0 c cscs 7 1 Direct to Navigation trom the MFD 7 1 Enter a Direct to Destination sssini Select a Direct to Destination to a Flight Plan Waypoint or Nearest AIDOFE seese 1 1 Re center the CDI to the Destination Waypoint 7 2 Manually Define the Direct to Course c ccseesesees 7 2 Cancelin
4. Displaying Terrain and Obstacles on the Navigation Map 1 With the Navigation Map displayed select the MAP Softkey 2 Select the TERRAIN Softkey Terrain and obstacle proximity will now be displayed on the map Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 10 9 SECTION 10 HAZARD AVOIDANCE Unlighted Obstacle Lighted Obstacle Unlighted Obstacle Lighted Obstacle Height is less than Height is less than Height is greater than Height is greater than 1000 AGL 1000 AGL 1000 AGL 1000 AGL Figure 10 15 Obstacle Symbols Displaying Terrain on the TAWS Page ELEV FT eatin Mas Fee al tono raphy presently 1 Turn the large FMS Knob to select the Map isplayed on screen Page Group Minimum 2 Turn the small FMS Knob to select the TAWS daa of topograph gt presently Page a ee 3 If desired select the VIEW Softkey to access the ARC and 360 Softkeys When the ARC Softkey is selected a radar like 120 view is displayed Select the 360 Softkey to return to the 360 Aircraft altitude default display 4 Rotate the Joystick clockwise to display a larger Range of of area or rotate counter clockwise to display a topography eleva Ground elevation smaller area tion AS y dis at present aircraft played on screen position eS SS MPTA e DIZUE Figure 10 16 Topography Scale 10 7 TERRAIN AWARENESS amp WARNING SYSTEM TAWS DISPLAY
5. 4 Press the FMS Knob to remove the flashing Cursor 7 14 NEAREST AIRSPACES 136 975 NORTH UP om Ae AIRSPACE Al h i i C FREOUENCIES 536 Figure 7 16 Nearest Airspaces Page Select the Nearest Airspaces 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 Airspace Alerts Box e Ifthe projected course takes the aircraft inside an airspace within the next ten minutes Ahead is displayed e If the aircraft is within two nautical miles of an airspace and the current course takes the aircraft inside Ahead lt 2 nm is displayed Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 1 9 SECTION 7 NAVIGATION e Ifthe aircraft is within two nautical miles of an airspace and the current course will not take the aircraft inside Within 2 nm is displayed e 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 3 Select 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 View and Quickly Load the Frequency for a Control
6. Figure 6 13 Flight Level Change Mode Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 SECTION 6 AUTOMATIC FLIGHT CONTROL Go Around Mode GA 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 Glideslope GS A NOTE Pressing the CWS button while Glideslope Mode is active does not cancel the mode The autopilot guides the aircraft back to the glides lope upon release of the CWS button Glideslope Mode is only available when the flight di rector has been set for approach Glideslope Mode is au tomatically armed under the following conditions Valid localizer frequency is tuned Horizontal Situation Indicator HSI is in LOC mode with valid deviation indication e Valid glideslope deviation APR Key is pressed Autopilot disconnect annunciation Go Around mode is ac flashes yellow for 5 seconds tive in both pitch axis amp roll axis modes Flight Director command bars indicating climb CDI Figure 6 14 Go Around Mode XPOR IDENT TMR REF N 6 8 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 6 6 ROLL AXIS M
7. Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 4 3 SECTION 4 NAV COM amp TRANSPONDER 46 TRANSPONDER Following is a list of important codes e 1200 VFR code in the U S please refer to the Mode Selection ICAO standards for VFR codes in other countries The STBY ON and ALT Softkeys can be accessed by e 7000 VFR code commonly used in Europe please selecting the XPDR Softkey refer to the ICAO standards e 7500 Hijack code Ground Mode Automatic e 7600 Loss of communication code e 7700 Emergency code e 7777 Military interceptor operations code NEVER ENTER THIS CODE eal TE oo e 0000 Code for military use in the U S Figure 4 8 Ground Mode GND is displayed when the aircraft is on the ground Reply Status When the transponder sends replies to interrogations an R indication appears momentarily in the reply status field Figure 4 9 Reply Indication Code Selection 1 Select the XPDR Softkey to display the transponder Mode Selection softkeys 2 Select the CODE Softkey to display the transponder Code Selection softkeys which includes the digit softkeys 3 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 When entering a code select the BKSP Softkey as needed to back up and change code di
8. highlighted press the ENT Key Course 236 from KOC to KIAS ACTIVATEREE CANCEL Figure 8 5 Activate Flight Plan Leg Confirmation STOP NAVIGATING A FLIGHT PLAN Press the FPL Key to display the Active Flight Plan Page Press the MENU Key to display the Page Menu Window Figure 8 6 Delete Flight Plan Turn the large FMS Knob to highlight Delete Flight Plan and press the ENT Key With OK SECTION 8 FLIGHT PLANNING highlighted press the ENT Key to deactivate the flight plan This will not delete the stored flight plan only the active flight plan Figure 8 7 Delete Flight Plan Confirmation INVERT ACTIVE FLIGHT PLAN From the Active Flight Plan Page press the MENU Key to display the Page Menu Turn the large FMS Knob to highlight Invert Flight Plan and press the ENT Key The original flight plan remains intact in its flight plan catalog storage location With OK highlighted press the ENT Key to invert the flight plan Figure 8 9 Invert Flight Plan Confirmation Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 SECTION 8 FLIGHT PLANNING 8 4 Catalog Page The new flight plan is now in the list Create a New Flight Plan Using the PFD 8 7 CREATE A NEW FLIGHT PLAN Create a New Flight Plan Using the MFD 1 Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page NOTE A flight plan cannot be entered usi
9. 3 Select the OPERATE Softkey to begin displaying traffic TIS OPERATIING is displayed in the Traffic Mode field 4 Select the STANDBY Softkey to place the system in the Standby mode TIS STANDBY will be displayed in the Traffic Mode field 5 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area If data is not received fora period longer than 6 seconds the age of the present data will be displayed in the lower left of of the screen along with the annuciation that the system has entered Coast mode The system will maintain the traffic display up to 60 seconds until the next data reception If no data is received after 60 seconds traffic will be removed from the display SECTION 10 HAZARD AVOIDANCE Traffic Advisory aircraft is 400 above amp Traffic out o Traffic Mode descending moving in the direction of the line o j Last data update Proximity Traffic at same Traffic 1600 above amp is older than 6 altitude level flight amp moving climbing moving in the sec resultingin in the direction of the line direction of the line Coast mode Figure 10 11 Traffic Map Page Displaying Traffic on the Navigation Map 1 Ensure TIS is operating With the Navigation Map displayed select the MAP Softkey 2 Select the TRAFFIC Softkey Traffic will now be displayed on the map TIS Audio Alert When a Traffic Advisory TA is displayed an audio
10. Alerts Window 2 Selected Heading Box O Selected Course Box G Inset Map Annunciation Window 4 BRGI Information Window E Vertical Deviation Glideslope Indicator BRG2 Information Window Marker Beacon Annunciation Figure 2 2 Additional PFD Information Desired Track to Distance to Next Waypoint Next Waypoint Next Waypoint Current Track Figure 2 3 PFD Navigation Status Box Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 2 1 AIRSPEED INDICATOR Airspeed oe Trend Vector Ranges Actual Airspeed Vspeed References True Airspeed Box Figure 2 4 Airspeed Indicator Speed Indication The indicated airspeed is displayed inside the black pointer The pointer will become red upon reaching Vne At altitudes above 12 000 feet Vno and Vne will vary with altitude Refer to the Airplane Flight Manual AFM Figure 2 5 Red Pointer at Vne Speed Ranges The color coded speed range strip denotes flaps operating range normal operating range and never exceed speed Vne A red range is also present for low speed awareness At altitudes above 12 000 feet caution and excessive speed range markings will vary with altitude Refer to the Airplane Flight Manual AFM for airspeed limitations and indicator markings Airspeed Trend Vector The end of the trend vector displays approximately what the airspeed will be in 6 seconds if the current rate of acceleration deceleration is maintained SECTIO
11. FPL TRUNC Flight plan has been This occurs when a newly installed aviation database eliminates an obsolete ap truncated proach or arrival used by a stored flight plan The obsolete procedure is removed trom the flight plan Update flight plan with current arrival or approach APPR VPROF Approaching VNAV Aircraft is approaching VNAV profile Prepare to climb or descend to meet VNAV profile profile pili pai e E Aircraft is approaching target altitude Prepare to level aircraft LOCKED FPL Cannot navigate locked This occurs when the pilot attempts to activate a stored flight plan that contains flight plan locked waypoint Remove locked waypoint trom flight plan Update flight plan with current waypoint S Arriving at waypoint xxxx where xxxx is the waypoint name STEEP TURN Steep turn ahead A steep turn is 15 seconds ahead Prepare to turn INSIDE ARSPC Inside airspace The aircraft is inside the airspace Note that depending on the buffer value that is selected and GPS altitude being used for calculation the actual aircraft position in space may differ trom the calculated position This can result in an erroneous alert ARSPC AHEAD Airspace ahead less Special use airspace is ahead of aircraft The aircraft will penetrate the airspace than 10 minutes within 10 minutes Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 17 SECTION 12 ANNUNCIATIONS amp ALERTS Miscella
12. G1000 Altitude Alerter function 18 AP Key Engages disengages the Autopilot and Flight Director Pressing the AP Key activates the Flight Director and engages the Autopilot in the default pitch axis and roll axis modes Pressing the AP Key again disengages the autopilot and deactivates the Flight Director 19 FD Key Activates deactivates the Flight Director only Pressing the FD Key turns on the Flight Director in the detault pitch axis and roll axis modes Pressing the FD Key again deactivates the Flight Director and removes the command bars unless the Autopilot is engaged If the Autopilot is engaged the FD Key is disabled 20 NAV Key Selects deselects the Navigation mode 21 ALT Key Selects deselects the Altitude Hold mode 22 VS Key Selects deselects the Vertical Speed mode 23 FLC Key Selects deselects the Flight Level Change mode 24 HDG Key Selects deselects the Heading Select mode 25 APR Key Selects deselects the Approach mode 26 27 NOSE UP NOSE DN Keys Controls the active pitch reference for the Pitch Hold Vertical Speed and Flight Level Change modes 1 2 GCU 476 CONTROLS The indicators above the PFD MFD NAV and COM keys are lit when the respective control mode key is pressed The unit is in MFD Control Mode by default until the PFD Control Mode selection key is pressed Many of the controls duplicate the controls on the PFD and MFD The discussions later in thi
13. Navigation 7 1 Navigation Mode 6 11 Navigation status window 2 2 NAV Frequency Window 4 1 NCR 10 13 Nearest Airports Page 7 3 7 5 7 7 7 8 7 9 8 1 Nearest ARTCC amp FSS frequencies 7 9 Negative Climb Rate After Takeoff 10 13 NEXRAD 1 6 1 9 10 3 10 6 0 OBS 2 8 Obstacles 10 14 12 11 12 12 12 13 Operation 5 2 overspeed 6 2 Oxygen 3 2 P Page group icon 1 10 PDA 10 12 PFD 1 1 4 1 4 3 PIT 6 3 pitch axis modes 6 3 Pitch hold 1 4 6 1 6 3 6 4 6 8 PLAY key 5 4 Premature Descent Alert 10 12 PROC key 1 3 1 5 Red pointer 2 3 Remove departure arrival or approach 8 5 Replies 4 4 Reversionary mode 11 1 ROC 10 12 10 15 12 6 Roll Axis Modes 6 2 6 9 Roll Hold 6 9 RTC 10 12 RX indicator 4 3 R indication 4 4 S Selected vertical speed 2 5 Severe thunderstorm 10 5 SIGMET 10 5 Slip Skid indicator 2 3 Softkey function MFD 1 6 1 9 Speed ranges 2 3 Split COM 5 2 Squelch 5 4 Store Flight Plan 8 5 Stormscope lightning data 1 6 1 9 10 2 10 3 Strike 10 2 Strike mode 10 2 System annunciations 12 1 12 7 System message advisories 12 9 T TA 10 7 TAF 10 3 TAS 10 8 10 9 12 15 TAWS 10 10 10 11 10 12 10 14 10 15 10 16 12 6 12 7 TAWS B 10 10 TAWS system test 10 12 Terrain 10 9 10 10 10 14 10 16 11 2 12 11 Terrain proximity 10 9 TIT 3 5 Tornado 10 5 Traffic advisory 10 7 10 8 10 9 10 16 Traffic map page 10 7 10 9 10 14 Transpond
14. Use the ALT Knob to set a Selected Altitude to hold The CWS button may be used to set a new pitch attitude As the Selected Altitude is captured Altitude Hold Mode becomes active and the autopilot maintains the Selected Altitude 4 Set the Selected Heading using the HDG Knob and press the HDG Key Use the HDG Knob to guide the aircraft for the remainder of the hold SECTION 6 AUTOMATIC FLIGHT CONTROL 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 A Clovis VORTAC CZQ 74 S 5 We XX Figure 6 25 Go Around Missed Approach Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 SECTION 6 AUTOMATIC FLIGHT CONTROL Blank Page 6 20 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 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 TRAFFIC Turn the large FMS Knob until MAP is highlighted in the Page Group Box in the lower right of the MFD display Turn the small FMS Knob to select the first MAP Page indicated by a solid rectangular icon Select the MAP Softkey to display softkeys for the available information which may be displayed on the map WARNING The map display should o
15. a large red equipment begins to initialize All windows X is typically displayed on windows associated with the should be operational within one minute of power up Should any window continue to remain flagged the G1000 system should be serviced by a Garmin authorized repair facility failed data The following section describes various system annunciations Refer to the AFM for additional information regarding pilot responses to these annunciations System Annunciation Commet Attitude and Heading Reference System is aligning Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 a SECTION 12 ANNUNCIATIONS amp ALERTS System Annunciation Commet Display system is not receiving attitude information trom the AHRS Display system is not receiving airspeed input trom air data computer Display is not receiving altitude input trom the air data computer Display is not receiving vertical speed input trom the air data computer 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 it GPS signals are not present see AFM Display is not receiving valid transponder information S A red X through any other display field such as engine instrumentation Ka US EATEN IAGO fields indicates that the field is not receiving valid data 12 8 Garmin G1000 Cockpit Reference Guide for the Columbia 350
16. second Autopilot disconnect aural alert Manual Disconnect n ROL AP ALT Figure 6 7 Manual Disconnect Annunciation Control Wheel Steering Pressing and holding the CWS button disengages the servos from the flight control surfaces and allows manual manuevering of the aircraft At the same time the flight director is synchronized to the aircraft attitude during the maneuver The AP annunciation is temporarily replaced by CWS in white until the CWS button is released Control Wheel Steering a ROL CHS PIT ALT Figure 6 8 CWS Annunciation SECTION 6 AUTOMATIC FLIGHT CONTROL 6 4 LOSS OF DATA In general a flashing yellow mode annunciation indicates either the loss of sensor data AHRS ADC or GIA or loss of navigation data VOR LOC or GPS required to compute commands When such a loss occurs the system automatically reverts to the default mode for the affected axis wings level ROL for roll axis PIT for pitch axis The flashing annunciation stops when the pilot presses the affected mode button or selects another mode for the axis If no pilot action is taken the flashing annunciation stops after ten seconds OR Te he Figure 6 9 Loss of VOR Signal 6 5 PITCH AXIS MODES Mode annunciations for active pitch axis modes are shown in green during normal operation Note the Go Around button is not located on the MFD FLC FIC Flight Level Change FLC nnn xt Glideslope vertical compo
17. turn the FMS Knobs to enter the identifier of the reference waypoint and the radial and distance to the reference waypoint Press the ENT Key to accept Press the FMS Knob to remove the flashing Cursor VIEWING THE ACTIVE FLIGHT PLAN Press the FPL Key FLIGHT PLAN KIXD KSTL DTK DIS KIXD a KSTL 887 512 1NM 2 Approoch ILS 30R 19 0NH 3 MOODS inf 127 Figure 8 2 Active Flight Plan Window on the PFD Figure 8 3 Active Flight Plan Page on the MFD ACTIVATE A STORED FLIGHT PLAN Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page Figure 8 4 Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan and select the ACTIVE Softkey With OK highlighted press the ENT Key to activate the flight plan To cancel the flight plan activation turn the large FMS Knob to highlight CANCEL and press the ENT Key Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 8 4 3 ACTIVATE A FLIGHT PLAN LEG 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 Select the ACT LEG Softkey using MFD only OR Press the MENU Key select the Activate Leg option trom the page menu and press the ENT Key This step must be used when activating a leg from the PFD With Activate
18. when the Approach mode is selected the mode is automatically armed The armed annunciation appears in white to the left of the active roll axis mode See the Example Procedures Using AFCS section for more information Go Around GA Go Around mode maintains a wings level 7 degree nose up attitude for instances where the pilot wishes to execute a missed approach or go around Figure 6 14 depicts the Go Around mode on the PFD Glideslope is active Figure 6 18 Approach Mode Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 SECTION 6 AUTOMATIC FLIGHT CONTROL 6 7 EXAMPLE PROCEDURES USING AFCS NOTE The diagrams in the following examples This section provides a scenario based set of procedures are for instructional purposes only and may not showing various autopilot modes used during a flight be used for navigation Other modes and uses of the G1000 may be necessary in real world scenarios In this scenario the aircraft departs Reid Hillview Airport KRHV from runway 13L enroute to Fresno Yosemite International Airport KFAT Climb to an altitude of 7 000 feet MSL and fly a heading of 070 degrees to intercept airway V107 Fly airway V107 to Panoche VORTAC PXN using VOR navigation then fly airway V230 using a GPS flight plan Prior to reaching Clovis VORTAC CZQ descend to 3 000 feet and load the ILS approach to R29R at KFAT Fly the ILS approach and execute a mi
19. 3 Fuel Calculation cessesseesseessesnees 3 6 SECTION 4 NAV COM AND TRANSPONDER 4 1 4 1 Radio Status Indications 0 ccceeeen 4 3 42 Volume noensinne 4 3 4 3 Automatic Squeleh seen 4 3 4 4 Quickly Activating 121 500 MHZ 4 3 4 5 Frequency Auto tuning 0 0 ccccce een 4 3 Auto tuning on the PFD cassssistsssakesssasnvatsaadanesennatioanceas 4 3 Autotuning on the MFD sessesxescarenunenrenenarvananeees 4 3 4 6 Transponder 4 4 Mode Seletioeesasen n E 4 4 Ground Mode Automatic 4 4 RODIN SIAUUS sianie ecariia Poet ractn trace 4 4 COG OCC nE tet seals 4 4 SECTION 5 AUDIO PANEL 0 000 5 1 5 1 COM Radio Selection 0 cccccssssseseenes 5 2 5 2 Split COM Function 00 sess 5 2 5 3 Marker Beacon Receivel ccccesseeeeees 5 2 5 4 Nav Radio Audio Selection cccccee 5 3 5 5 Intercom System ICS Isolation 5 3 5 6 Intercom Squelch Control 0 cccces 5 4 5 7 Digital Clearance Recorder and Player 5 4 SECTION 6 AUTOMATIC FLIGHT CONTROL 6 1 6 1 Mode Annunciations cccsesseeseeeees 6 1 6 2 Overspeed Protection cesses 6 2 6 3 AP Engagement Disengagement 6 2 Automatic Disengagement csccessssssessesesneeen 6 3 Manual Disengagement scssssessecsessnessneesseen 6 3 Control Wheel tee Ni sson 6 3 6 4 LOSS Of Data
20. 400 SECTION 12 ANNUNCIATIONS amp 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 4A Air Data Computer mar An wW he A ATTITUDES P Loam N a amp GRS 77 AHRS GEA 71 Engine ll P OR Airframe Unit 91 GMU 44 OR FFLOW GPH a Magnetometer GIA 63 Integrated J 48 Avionics Unit OIL PSI INTEG GIA 63 Integrated a cs ae Avionics Units En a j Aves DA F _ bo PORTE A PORE a a ENGINE CDI OBS XPDR IDENT TMREREF NAST ALERTS GDC 74A Air Data GTX 33 Transponder OR me 7 GIA 63 Integrated Figure 12 6 G1000 System Failure Annunciations Avionics Units 12 7 G1000 SYSTEM MESSAGE A NOTE This section provides information ADVISORIES regarding G1000 message advisories that may be displayed by the system Knowledge of the This section describes various G1000 system message aircraft systems flight conditions and other advisories Certain messages are issued due to an LRU existing operational priorities must be considered or an LRU function failure Such messages are normally lel pilot A M B eine accompanied by a corresponding red X annunciation Airplane Flight Manual AFM takes precedence as shown previously in the G1000 System Annunciation over any conflicting guidance found in this section section Garm
21. Annunciation Window Alerts Window The Alerts Window displays alert text messages Up to 64 prioritized alerts can be displayed in the Alerts Window Selecting the ALERTS Softkey displays the Alerts Window Selecting the ALERTS Softkey again removes the Alerts Window from the display When the Alerts Window is displayed the pilot may use the large FMS Knob to scroll through the alert list Higher priority alerts are displayed at the top of the window Lower priority alerts are displayed at the bottom of the window Active alerts are displayed in white text Alerts that have become inactive will change to gray text The ALERTS Softkey will flash if the state of a displayed alert changes or a new alert is displayed The inactive alerts can be removed from the Alerts Window by selecting the flashing ALERTS softkey ALERTS Softkey Annunciation When the Alerting System issues an alert the ALERTS Softkey is used as a flashing annunciation to accompany an alert During the alert the ALERTS Softkey assumes a new label consistent with alert level WARNING CAUTION or ADVISORY Pressing the softkey annunciation acknowledges that the pilot is aware of the alert The softkey then returns to the previous ALERTS label The pilot can then select the ALERTS Softkey again to view alert text messages System Annunciations Typically a large red X appears in a window when a related LRU fails or detects invalid data Garmin G1000 Cockpit Refere
22. Attitude Indicator 0 0 0 ccc 2 3 2 3 Altimeter 3 scicsiesten sess vrccvecererescvereseincavnatenevmnneblenes 2 4 Altitude Select BUG ccssssssssessessssssssssessesssssseaseesees 2 4 Altitude Trend Vector sirsioennorren 2 4 Barometri Setting BOkemeasnaman na 2 4 Altitude Aleni incen 2 4 Barometric Minimum Descent Altitude 2 4 2 4 Vertical Deviation Glideslope Indicator 2 5 2 5 Marker Beacon Annunciations 0 2 5 2 6 Vertical Speed Indicator ccceees 2 5 2 7 Horizontal Situation Indicator HSI 2 6 Ate gs Paceeeteee ene a ene ae oon ence heen eee en 2 Turn Rate Indicator and Heading Trend Vector 0 2 6 Coise POMO atarsan ar 2 7 Course Deviation Indicator CDI 2 7 Bearing Pointers and Information WindoWS 0 2 7 Navigation OUTCE an ronsieincinrouneminere 2 8 SECTION 3 ENGINE INDICATION SYSTEM EIS 3 1 3 1 EIS DES VAY assis stcsen sti tesssasnindbsdiniasbivsaniasysianiassien 3 2 Oxygen System Optional ccsccsseseseseeseeseesean 3 2 TIN EEE sted ct EE EE E eee en eee 3 2 Carbon Monoxide Detection 3 2 3 2 Engine Leaning Assist Display 0 3 3 Engine Leaning for the Columbia 350 cssesesees 3 3 Leaning for B St POWE orccain 3 3 Leaning for Best Economy 3 4 TABLE OF CONTENTS Engine Leaning for the Columbia 400 0 3 5 Leaning for Best POWE orminn 3 5 Leaning for Best ECONOMY 3 5 3
23. Contig service req d memory The G1000 system should be serviced MANIFEST GEA1 software mismatch Communication halted BACKUP PATH EIS using backup The GEA 71 is using a backup communication path The G1000 system should be data path serviced when possible The GEA 71 has incorrect sottware installed The G1000 system should be serviced 12 14 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 SECTION 12 ANNUNCIATIONS amp ALERTS GTX 33 Message Advisories Alerts Window Message Comments S XPDR1 CONFIG XPDR1 contig error The transponder configuration settings do not match those of backup configuration Config service req d memory The G1000 system should be serviced MANIFEST GTX1 software mismatch The transponder has incorrect software installed The G1000 system should be Communication halted serviced BACKUP PATH XPDR1 using backup The 1 transponder is using a backup communications path The G1000 system data path should be serviced when possible GRS 77 Message Advisories Alerts Window Message Comments S AHRS1 TAS AHRS1 not receiving The 1 AHRS is not receiving true airspeed trom the air data computer The AHRS airspeed relies on GPS information to augment the lack of airspeed The G1000 system should be serviced AHRS1 GPS AHRS1 using backup The 1 AHRS is using the backup GPS path Primary GPS path has failed The G1000 GPS source system should be servi
24. FPL OOG Turn the small FMS Knob to display a list possible VNAV profile endpoints When using a flight plan the target reference waypoint itself can be specified from the waypoints contained in the flight plan By default the last waypoint Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 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 protiled descent will be created 11 Press the ENT Key The cursor is now placed in the TARGET VERTICAL SPEED field The default profile utilizes a 400 toot per minute descent rate 12 To change the vertical speed turn the FMS Knobs to enter the desired vertical speed Press the ENT Key when finished With the profile set the vertical speed required VSR is displayed Expect the following to occur when using the vertical navigation feature At one minute prior to reaching the Bottom Of Climb or Top Of Descent point gray arc the message APPR VPROF Approaching VNAV Profile is displayed as a PFD alert The descent or climb angle also locks to prevent changes in speed from altering the profile If selected the vertical speed required VSR readout
25. Selected Altitude the autopilot completes the capture process and levels the aircraft From this point the flight director continues to operate in Altitude Hold Mode 070 ALT Mode 5 Figure 6 20 Departure 6 14 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 SECTION 6 AUTOMATIC FLIGHT CONTROL Intercepting a VOR Radial c Press the NAV Key to arm Navigation Mode The white annunciation VOR appears to the NOTE Changing the HSI mode cancels Navigation left of the active roll mode Mode and causes the flight director to revertto MO Roll Hold Mode ee 2 When the CDI shows less than one dot the During climb out the autopilot continues to fly the flight director changes from Heading Select to aircraft in Heading Select Mode Airway V107 to Panoche Navigation Mode and the green annunciation VORTAC PXN should now be intercepted VOR flashes The autopilot begins turning to 1 Tune the VOR frequency and activate Heading intercept the Selected Course Select Mode VOR JAP ALT TOODET a CDI Soitkey to set the HSI mode to 3 The autopilot continues the turn until the aircraft is established on the Selected Course b Use the CRS Knob to set the Selected Course to 116 Note that at this point the flight director is still in Heading Select Mode and the autopilot continues to fly 070 HDG Mode VOR Armed 4 Panoche Figure 6 21 Intercepting a VOR Garmin G1000 Cockpit Reference Guide
26. alert Traffic is given Traffic Not Available will be heard whenever TIS service becomes unavailable Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 10 7 SECTION 10 HAZARD AVOIDANCE 10 5 RYAN 9900BX TRAFFIC ADVISORY a Taffie Ou of SYSTEM TAS OPTION AL Traffic Mode Altitude oe i climbing Refer to the Ryan 9900BX pilots guide for a detailed discussion and an explanation of the aural alerts 136 975 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 3 Select the ALT MODE Softkey to change the altitude volume Select the desired altitude volume by selecting the the BELOW NORMAL ABOVE or UREST unrestricted Softkey The Non Bearing Traffic system Proximity Traffic selection IS displayed in the Altitude Mode 1S unable to determine bearing 1000 above amp l distance is 8 0 nm 1190 above descendi field and descending E 4 Select the MUTE Softkey to mute aural alerts for currently displayed Traffic Advisories Aural alerts will again be heard when anew _ Displaying Traffic on the Navigation Map Traffic Advisory is issued Selecting the MUTE Figure 10 12 Traffic Map Page Softkey twice will replay the aural alerts for any 1 Ensure the TAS system is operating With the currently displayed Traffi
27. and distance from the reference waypoint Press the FMS Knob to remove the flashing Cursor Modify a User Waypoint With the User Waypoint Information Page displayed press the FMS Knob to activate the cursor Turn the large FMS Knob to move the cursor to the desired field and turn the small FMS Knob to make changes Press the ENT Key to accept the changes Press the FMS Knob to remove the flashing Cursor Delete a User Waypoint 1 Select the User Waypoint Information Page and press MENU to display the User Waypoint Information Page Options or select the DELETE Softkey Turn the large FMS Knob to select Delete User Waypoint and press the ENT Key The message Would you like to delete the user waypoint is displayed With YES highlighted press the ENT Key Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 8 1 SECTION 8 FLIGHT PLANNING Create User Waypoints from the Navigation Map Page 8 2 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 Move the Joystick to place the pointer at the desired position Press the ENT Key The User Waypoint Information Page is now displayed with the captured position Turn the FMS Knobs to select a waypoint name 8 3 Press the ENT Key to accept the selected name The first reference waypoint field is highlighted If desired
28. be the result Altitude Hold mode is active XPOR Selected Heading Bug IDENT TMR REF NRST Figure 6 16 Heading Select Mode Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 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 Turning the CRS Knob moves the Course Pointer and displays the Selected Course Box The Selected Course is displayed in the box The box is displayed while the knob is turning and disappears three seconds after the knob stops turning Backcourse mode is automatically selected when the localizer front course is greater than 105 degrees from the aircraft heading NOTE When making a backcourse approach set Selected Course to the localizer front course Navigation Mode is active using GPS source NAV 113 68 WPT 117 95 Flight Director command bars indicating a left turn to track GPS course and a climb to intercept Selected Altitude CDI Figure 6 17 Navigation Mode SECTION 6 AUTOMATIC FLIGHT CONTROL Navigation Mode Armed If the CDI is not centered deviation gt 1 dot when the Navigation mode is selected the mode
29. denote halt standard and standard turn rates A magenta turn rate trend vector shows the current turn rate The Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 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 Half Standard Turn Rate Tick Mark anaes Standard Tw E Trend Vector Rate Tick Mark rate gt 4 fa cleg sec Turn Rate Trend Vector standard rate Figure 2 15 Standard Rate Turn Indication Course Pointer The Course Pointer is a single line arrow GPS VORI and LOC1 or double line arrow VOR2 and LOC2 which points in the direction of the set course Figure 2 16 Course Pointer SECTION 2 FLIGHT INSTRUMENTS Course Deviation Indicator CDI The CDI scale automatically adjusts to the current phase of flight enroute 5 0 nm terminal area 1 0 nm or approach 0 3 nm Scaling may be selected manually from the MFD System Setup Page See System Setup in the G1000 Pilots Guide for more details Bearing Pointers and Information Windows Selecting the PFD Softkey provides access to the BRG1 and BRG2 Sottkeys The BRGI Pointer is a single line pointer The BRG2 Pointer is a double line pointer Bearing 1 Pointer Bearing 2 Pointer CDI Bearing 1 Bearing 2 Information Information Window Window Figure 2
30. desired NDB The remaining information on the Nearest NDB Page pertains to the selected NDB Press the FMS Knob to remove the flashing Cursor Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 SECTION 7 NAVIGATION 7 11 NEAREST VOR 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 ___ 136 975 _ NORTH UP 117HH ie ee INFORMATION goa PENDLETON PENDLETON OR Figure 7 13 Nearest VOR Page View Information on the Nearest VOR 1 With the Nearest VOR Page displayed select the VOR Softkey to place the cursor in the NEAREST VOR box 2 Turn either FMS Knob to select a VOR 3 Press the FMS Knob to remove the flashing cursor Select and Load a VOR Frequency 1 With the Nearest VOR Page displayed select the FREQ Softkey to highlight the VOR frequency in the FREQUENCY field A 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 2 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 NEAREST USER WAYPOINT T NEAREST USER WPTS 136 975 HORTH UP ees TNFORMAT ION I BOT zen 18 n 43 dit Alb daa i a REFERENCE WAYPOIN
31. error Contig service req d The G1000 system should be serviced MANIFEST GMA1 software The audio panel has incorrect software installed The G1000 system should be mismatch Communication halted serviced GMA1 SERVICE GMA1 needs The audio panel self test has detected a problem in the unit Certain audio functions service Return unit for repair may still be available and the audio panel may still be usable The G1000 system should be serviced when possible BACKUP PATH Audio panel 1 using The 1 audio panel is using a backup communication path The G1000 system backup data path should be serviced when possible GIA 63 Message Advisories Alerts Window Message Comments S GIA1 CONFIG GIA1 configuration error Config service req d The GIA1 and or GIA2 configuration settings do not match backup configuration GIA2 CONFIG GIA2 configuration memory The G1000 system should be serviced 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 GIA2 COOLING GIA2 temperature warm up to operating temperature too low GIA1 COOLING GIA1 over temperature The GIA1 and or GIA2 temperature is too high If problem persists the G1000 GIA2 COOLING GIA2 over system should be serviced temperature Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 SECTION 12 ANNUNCIATIONS amp ALERTS GIA
32. is automatically armed The armed annunciation appears in white to the left of the active roll axis mode See the Example Procedures Using AFCS section for more information NOTE When intercepting a flight plan leg the Flight Director will give commands to capture the active leg at approximately a 45 degree angle to the track between the waypoints defining the active leg The Flight Director will not give commands fly to the starting waypoint of the active leg Flight Level Change mode is active Altitude Hold is armed Selected Course GPS is active navigation receiver on the HSI XPOR IDENT THR REF NRST Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 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 NOTE While using Approach mode the Glideslope mode is automatically armed when LOC mode is selected on the HSI Approach Mode is active Flight Director command bars indicating descent on Localizer Glideslope path LOC2 is the active navigation receiver on the HSI If the CDI is not centered deviation gt 1 dot
33. map pointer when pressed 6 Alphanumeric Keys Allow data entry without using the GDU FMS Knob to select individual characters 7 BKSP Key Moves the cursor back one character space 8 SPC Key Adds a space 9 ENT Key Validates or confirms a menu selection or data entry 10 CLR Key Erases information cancels entries or removes page menus Press and hold to immediately display the Navigation Map Page 11 SEL Key The center of this key activates the selected softkey while the right and left arrows move the softkey selection box light blue box around the softkey label to the right and left respectively 12 Decimal Key Enters a decimal point 13 Plus Minus Key Switches entry between the and characters 14 NAV Key Selects NAV Radio Control Mode The FMS Knob will now control the NAV radios SECTION 1 SYSTEM OVERVIEW 15 COM Key Selects COM Radio Control Mode The FMS Knob will now control the COM radios 16 Frequency Transfer Key Switches between active and standby selected COM or NAV tuning frequencies Pressing and holding this key while in COM radio control mode tunes the COM radio to 121 50 MHz the emergency COM frequency 17 PFD Key Selects PFD Control Mode The FMS Knob will now control PFD functions 18 MFD Key Selects MFD Control Mode The FMS Knob will now control MFD functions 19 Dual FMS NAV COM Knob Multifunction Control Knob With the M
34. of softkeys for additional weather control SFC Selecting the SFC Softkey for Surface Analysis shows current or forecast conditions Forecasts are available for intervals of Current 12 24 36 and 48 hours Select the softkey corresponding to the desired forecast The closest city forecast information is displayed in the legend The display is updated every 12 minutes FRZ LVL Select the FRZ LVL Softkey to display contour lines for freezing levels The display is updated every 12 minutes WIND Select the WIND Softkey to show wind speed and direction at a selected altitude from the ground up to 42 000 feet in 3 000 foot increments After selecting the WIND Softkey select the softkey corresponding to the desired winds aloft altitude The display is updated every 12 minutes COUNTY Selecting the COUNTY Softkey provides specific public awareness and protection weather warnings for Tornado Severe Thunderstorm and Flood conditions provided by the National Weather Service NWS The display is updated 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 Map Panning Information Weather Data Link Page 1 Push in the Joystick to display the panning arrow 2 Move the Joystick to place the panning arrow onAIRMETs TFRs M
35. of the desired airport Press the ENT Key Turn the large FMS Knob to highlight the Arrival field Turn the small FMS Knob to display a list of available arrivals Turn either FMS Knob to select the desired arrival and press the ENT Key Figure 9 3 Select Arrival A second window is displayed listing available transitions for the arrival Turn either FMS Knob Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 SECTION 9 PROCEDURES to highlight the desired transition waypoint and If the GPS receiver cannot be used for primary guidance press the ENT Key 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 Load and or Activate an Approach Procedure 1 With the Navigation Map Page displayed press Figure 9 4 Select Arrival Transition the FPL Key 7 Athird window is displayed listing the available 2 Select the LD APR Softkey If a flight plan is runways Turn either FMS Knob to select the active the destination airport will be displayed desired runway and press the ENT Key as the default A list of available approaches is also displayed 3 If no flight plan is active use the FMS Knobs to enter the identitier of the desired airport Press the ENT Key 4 Turn the large FMS Knob to highlight the App
36. on the default NAV and map pages shows the desired vertical speed to maintain the proper descent or climb angle At 500 feet above or below for a climb the target altitude white arc an APPR TRG ALT Approaching Target Altitude message is provided The VSR readout on the Navigation Map Page is blanked out at this point SECTION 8 FLIGHT PLANNING ALERTS APPR VPROF Eaa aaae man ek prof ile Figure 8 17 Approaching VNAV Profile Message PFD ALERTS APPR TRG ALTE ge target altitude Figure 8 18 Approaching Target Altitude Message PFD To display map data on the Vertical Navigation Map Page select the MAP Softkey Select the TOPO TERRAIN or LING Softkey Select the same softkey to remove the displayed data from the Vertical Navigation Page VNAV Page Menu Options The VNAV messages are not enabled until the VNAV Messages On option is enabled from the VNAV Page Menu Options To display the page menu press the MENU Key with the VNAV Page displayed The VNAV Page Options Menu also allows the pilot to restore VNAV page defaults Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 8 9 SECTION 8 FLIGHT PLANNING Blank Page 8 10 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 9 1 SECTION 9 PROCEDURES ARRIVALS AND DEPARTURES Load and Activate a Departure Procedure 1 2 With the Navigation Map Page displayed press the FPL Key Select
37. pop up alerts that accompany the aural message Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 10 13 SECTION 10 HAZARD AVOIDANCE Displaying Terrain and Obstacles on the Navigation Map 1 With the Navigation Map displayed select the MAP Softkey 2 Select the TERRAIN Softkey Terrain and obstacle proximity will now be displayed on the map Unlighted Obstacle Lighted Obstacle Unlighted Obstacle Lighted Obstacle Potential Impact Points Height is less than Height is less than Height is greater than Height is greater than 1000 AGL 1000 AGL 1000 AGL 1000 AGL Figure 10 22 TAWS Symbols Pop up Alerts When the Navigation Map Page is displayed and a terrain or obstacle alert is issued a pop up window is displayed with the appropriate alert 118 000 ia Figure 10 23 Alert Pop Up Press the ENT Key to display the TAWS Page or press the CLR Key to remain on the Navigation Map Page 10 14 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 SECTION 10 HAZARD AVOIDANCE TAWS Alerts Summary The following table shows the possible TAWS alert types with corresponding annunciations and aural messages PFD MFD TAWS MFD Alert Type Page Annunciation Pop Up Alert Excessive Descent Rate Warning EDR PULL UF ame Pull Up Reduced Required Terrain Clearance Warn PULL UP Terrain Terrain Pull Up Pull Up ing RTC or or Terrain Ahead Pull
38. signals the altitude capture is complete and the selected altitude will be maintained Altitude Hold mode is armed 118 708 con 123 8808 DOM2 Figure 6 10 Pitch Hold Mode If only the flight director is engaged pitch commands are given to manually maintain the selected altitude 6 4 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 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 SECTION 6 AUTOMATIC FLIGHT CONTROL NOTE If the Selected Altitude is captured during CWS maneuvering the Flight Director altitude reference is not changed To adjust the altitude reference in this case the pilot must again press the CWS button after the Selected Altitude is Reference field captured 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 Altitude Hold mode is active Altitude Reference newt 113 88 118 98 ITXD wer 118 788 com DIS DTK TR 118 98 ITxD 123 808 ponz Flight Director command bars hold pitch attitude to maintain the altitude reference Figure 6 11 Altitude Hold Mode 3 To change aircraft altitude press and hold the CWS button and manually maneuver to the desired altitude Upon reaching the desired altitude r
39. the G1000 and tive the CO Guardian 12 4 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 SECTION 12 ANNUNCIATIONS amp ALERTS 12 4 AFCS ALERTS System Status Annunciation ws 113 00 110 90 IDD vir pis ore Th 1118 700 coms Nerv 118 98 95 325 lt 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 Annunciation Description o Pitch Failure PTCH Pitch axis control failure AP is inoperative Roll Failure ROLL Roll axis control failure AP is inoperative MET Switch Stuck or PTRM If annunciated when AP is engaged take control of the aircraft and disengage the Pitch Trim Axis Control autopilot If annunciated when AP is not engaged move each halt of the MET switch Failure separately to check if a stuck switch is causing the annunciation System Failure AFCS AP and MET are unavailable FD may still be available Elevator Mistrim Up TEI F A condition has developed causing the pitch servo to provide a sustained force Be prepared to apply nose up control wheel force upon autopilot disconnect IFI F A condition has developed causing the pitch servo to provide a sustained force Be Down i prepared to apply nose down control wheel force upon autopilot disconnect ATI A condition has developed causing the roll servo to provide a sustained lett force En sure the slip skid
40. the Navigation Map XM LING optional Selecting this softkey displays removes XM Radio lightning data on the Navigation Map BACK Selecting this softkey displays the ENGINE and MAP top level softkeys DCLTR declutter Selecting this softkey removes map information in three levels Press to return to the top softkey level m pr Figure 1 7 MFD Softkeys Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 SECTION 1 SYSTEM OVERVIEW 1 10 1 6 MFD PAGE GROUPS Turn the large FMS Knob until the desired page group is selected Turn the small FMS Knob to select pages within the group See Figure 1 8 Nearest Group Auxiliary Page Group Waypoint Page Group Map Page Group Number of Pages in Current Figure 1 8 Page Group Icon Selected Page BACKLIGHTING Manually adjust the backlight for the PFD and MFD Press the MENU Key on the PFD to display the PFD Setup Menu Window Press the small FMS Knob to activate the cursor PFD DSPL gt AUTO is now highlighted Turn the small FMS Knob to display the selection window Turn the FMS Knob to select MANUAL then press the ENT Key With the intensity value now highlighted turn the small FMS Knob to select the desired backlighting Turn the large FMS Knob to highlight MFD DSPL gt AUTO and repeat steps 3 through 5 PFD SETUP MENU Jie AUTO 23 444 MFD DSPL AUTA uue f Figure 1 9 PFD Setup Menu Win
41. to activate the cursor Turn the large FMS Knob to highlight the desired flight plan and press the ENT Key Turn the large FMS Knob to place the cursor in the desired locations for entering changes Turn the FMS Knobs to make the desired changes then press the ENT Key Press the FMS Knob to return to the Flight Plan Catalog Page DELETE A WAYPOINT FROM THE FLIGHT PLAN With either the Active or Stored Flight Plan displayed press the FMS Knob to activate the cursor Turn the large FMS Knob to select the waypoint to be deleted Press the CLR Key to display a REMOVE Wpt Name confirmation window Remove KCRQ OK or CANCEL Figure 8 14 Remove Waypoint Confirmation With OK highlighted press the ENT Key to remove the waypoint To cancel the delete request turn the large FMS Knob to highlight CANCEL and press the ENT Key Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 8 5 SECTION 8 FLIGHT PLANNING Ul 8 15 8 6 Once all changes have been made press the FMS Knob to remove the cursor INVERT AND ACTIVATE A STORED FLIGHT PLAN From the Flight Plan Catalog Page press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan Select the INVERT Softkey Invert and activate stored flight plan will be displayed With OK highlighted press the ENT Key The selected flight plan is now inverted and activated T
42. to the desired new heading Release the CWS button and the aircraft will maintain wings level at approximately the new heading but will not hold the heading The same practice applies to holding roll attitude Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 6 9 SECTION 6 AUTOMATIC FLIGHT CONTROL Heading Select Mode HDG 1 6 10 elected Heading ox 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 If the autopilot is engaged the aircraft will begin to turn toward the selected heading When the selected heading is reached the aircraft will maintain this heading If only the flight director is engaged manually maneuver the aircraft to the command bars to aquire the selected heading Heading Select mode NAVI 113 68 now2 108 00 117 95 Flight Director command bars tracking Selected Heading PFD 06S CDI The heading may be adjusted by turning the HDG Knob and moving the heading bug to a new heading The aircraft will turn in the same direction the heading bug is moved However if the heading bug is moved more than 340 degrees at a time a turn reversal will
43. 00 11508 Ie A Pin 123 4 SB 36 SECTION 3 ENGINE INDICATION SYSTEM EIS A Richen the mixture to obtain the desired delta A values as specitied in the AFM Leaning for Best Economy 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 4 Continue leaning the mixture until the desired delta A values are obtained as specitied in the AFM Selecting the ASSIST Softkey returns the MFD to the EIS Display Selecting the SYSTEM Softkey exits the Assist Display and returns the MFD to default operation HT F 347 329 334 son 358 365 320 400 300 200 F 51 12645 6 LEAN Indicates Lean or Rich From Peak Figure 3 5 Engine Leaning Assist Display Columbia 400 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 J3 SECTION 3 ENGINE INDICATION SYSTEM EIS 3 3 FUEL CALCULATIONS Fuel Quantit Indicates Selected Fuel Quantity Fuel Fuel Used Gauge Left Fuel Tank Gauge Right Remaining Calculation FUEL CALCE A 4 Endurance Calculation GAL USED RANGE NM Range L FUEL QTY GAL R FUEL QTY GAL 0 4 o 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 remaini
44. 1 2 NM 9 NM 15 NM Figure 10 20 PDA Alerting Excessive Descent Rate Alert EDR 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 21 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 5000 4500 4000 3500 3000 2500 2000 1500 1000 PULL UP 500 Height Above Terrain Feet 0 4000 6000 8000 10000 12000 Descent Rate FPM Figure 10 21 Excessive Descent Rate SECTION 10 HAZARD AVOIDANCE 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 Five Hundred Aural Alert The purpose of the aural alert message Five hundred is to provide an advisory alert to the aircrew that the aircraft is five hundred feet above terrain When the aircraft descends within 500 feet of terrain the aural message Five hundred is heard There are no display annunciations or
45. 17 HSI with Bearing Information Distance to Bearing Source Waypoint Identifier Pointer Source Icon Figure 2 18 BRG1 Information Window Bearing Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 SECTION 2 FLIGHT INSTRUMENTS Distance to Bearing Source E A NY 3 3 h Waypoint K E Vu eq Identifier al gt _NAY2 Pointer Bearing Icon Source Figure 2 19 BRG2 Information Window Navigation Source Change navigation sources 1 Select the CDI Softkey to change trom GPS to VOR1 LOC1 2 Select the CDI Softkey again to change trom VOR1 LOC1 to VOR2 LOC2 3 Select the CDI Softkey a third time to return to GPS When using GPS as the navigation source the following may appear Figure 2 19 GPS INTEG GPS SUSP LOC1 and VOR2 INTEG GPS information is either not present or Enable disable OBS mode while navigating is invalid for navigation use with GPS e WARN GPS detects a position error 1 Select the OBS Softkey to select OBS Mode SUSP Displayed when in OBS Mode indicating 2 Turn the CRS Knob to select the desired course GPS waypoint sequencing is suspended TO FROM the waypoint 3 Select the OBS Softkey again to return to normal operation A NOTE The OBS Softkey is only displayed when navigating an active leg using GPS 2 8 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 INDICATION SYSTEM EIS SECTION 3 ENGINE INDICATION SYSTEM EIS The Engine Instrument Disp
46. 2 The transmitter will operate at reduced power If the problem persists the G1000 system should be serviced The COM1 and or COM2 transfer switch is stuck in the enabled or pressed posi COM RMT XER COND tion Press the transter switch again to cycle its operation If the problem persists aaa puu the G1000 system should be serviced transfer key is stuck RAIM UNAVAIL RAIM is not GPS satellite coverage is insufficient to perform Receiver Autonomous Integrity available trom FAF to MAP waypoints Monitoring RAIM from the FAF to the MAP waypoints RAIM UNAVAIL RAIM is not GPS satellite coverage is insufficient to perform Receiver Autonomous Integrity available Monitoring RAIM for the current phase of flight POSN ERROR RAIM has determined When a RAIM position error is detected GPS is flagged and the system no longer GPS position is in error provides GPS based guidance Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 12 13 SECTION 12 ANNUNCIATIONS amp ALERTS GIA 63 Message Advisories Cont Alerts Window Message DGRD GPS ACC GPS position z accuracy degraded amp RAIM unavailable GPS position accuracy has been degraded and RAIM is not available GPS1 FAIL GPS1 is inoperative A failure has been detected in the GPS1 and or GPS2 receiver The receiver is GPS2 FAIL GPS2 is inoperative unavailable The G1000 system should be serviced GPS1 SERVICE GPS1 needs s
47. 2 Approaches 00 0 0 ccc 9 2 Load and or Activate an Approach Procedure 9 2 Activate An Approach in the Active Flight Plan 9 3 SECTION 10 HAZARD AVOIDANCE 000 10 1 10 1 Customizing the Hazard Displays on the Navigation Map 0 ccccccsssseeseeseesen 10 1 10 2 STORMSCOPE Optional 350 only 10 1 Displaying Stormscope Lightning Data on the Navigation Map Pagi cictseiecarasavea tastnwsurasevutiteasanucucadas 10 1 SOMS ODE ACs aana 10 2 10 3 XM Weather Optional 0 0 0 10 3 Displaying METAR and TAF information on the Airport Information Page c scsscessessessesseesseeseessen 10 3 TABLE OF CONTENTS Displaying Weather on the Weather Data Link Page 10 4 NEARAD EHTNGTIONS rainira 10 4 Map Panning Information Weather Data Link Page 10 5 Weather Products and Symbols sssseseeseesseesseen 10 5 Weather Product ACE cd aa 10 6 10 4 Traffic Information Service TIS 10 7 Displaying Traffic on the Traffic Map Page 10 7 Displaying Traffic on the Navigation Map 10 7 AUS UGTA Ee TO 10 7 10 5 Ryan 9900BX Traffic Advisory System TAS Optional sssscetoy rect atone Meco ications date 10 8 Displaying Traffic on the Traffic Map Page 10 8 Displaying Traffic on the Navigation Map 10 8 10 6 Terrain And Obstacle Proximity 0 10 9 Displaying Terrain and Obstacles on the Terrain PrO PAGE nnana 10
48. 5 SECTION 2 FLIGHT INSTRUMENTS 2 6 2 7 HORIZONTAL SITUATION INDICATOR HSI C1 Turn Rate Indicator Lateral Deviation Scale G Navigation Source 4 Aircraft Symbol Course Deviation Indicator Rotating Compass Rose OBS Mode TO FROM Indicator Heading Bug Course Pointer Flight Phase Turn Rate and Heading Trend Vector Heading 14 Lubber Line QOOOOOQOOOOO Figure 2 12 Horizontal Situation Indicator 360 Arc HSI A NOTE When the Arc HSI is displayed the BRG1 and BRG2 Information Windows and pointers are disabled A NOTE If the pilot makes a heading change greater than 105 with respect to the course the CDI switches to the opposite side of the deviation scale and displays reverse sensing The Arc HSI is a 140 expanded section of the compass rose The Arc contains a Course Pointer arrow the TO FROM indicator a sliding deviation indicator the TO FROM and sliding deviation indicators are one and the same and a deviation scale Upon station passage the TO FROM indicator flips and points to the tail of the aircraft just like the conventional TO FROM flag Depending on the navigation source the CDI on the Arc HSI can appear in two different ways e GPS OBS VOR Arrowhead e Localizer Diamond Lateral Course Deviation and Deviation TO FROM Indicator Scale Figure 2 13 Arc HSI Turn Rate Indicator and Heading Trend Vector Tick marks to the left and right of the lubber line
49. 63 Message Advisories Cont Alerts Window Message Comments S 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 GIA2 SERVICE GIA2 needs service system should be serviced Return the unit for repair HW MISMATCH GIA hardware There is a hardware mismatch between GIA1 and GIA2 The G1000 system should mismatch Communication halted be serviced MANIFEST GIA1 software mismatch Communication halted The GIA1 and or GIA 2 has incorrect software installed The G1000 system should MANIFEST GIA2 software mismatch be serviced Communication halted COM1 TEMP COM1 over temp Reducing transmitter power COM2 TEMP COM2 over temp Reducing transmitter power COM1 SERVICE COM1 needs service Return unit for repair The system has detected a failure in COM1 and or COM2 COM1 and or COM2 may COM2 SERVICE COM 2 needs still be usable The G1000 system should be serviced when possible service Return unit for repair COM1 PTT COM1 push to talk ke a i j The COM1 and or COM2 external push to talk switch is stuck in the enable or COM2 PTT COM oushttotalk k pressed position Press the PTT switch again to cycle its operation If the problem persists the G1000 system should be serviced COM1 RMT XFR COM1 remote transfer key is stuck The system has detected an over temperature condition in COM1 and or COM
50. 9 Displaying Terrain and Obstacles on the Navigaton Macarie a 10 9 10 7 Terrain Awareness amp Warning System TAWS Display Optional 0 00 000 000 10 10 Displaying Terrain on the TAWS Page c scseeeeses 10 10 Enable Disable Aviation Data c ccseseeseseeesen 10 11 TANS ANON teschestaatnistcatansnce tina tanmatonan tebe 10 12 Manual System TESTS ccascasesanasesceansescadarsscnemeriaues 10 12 Forward Looking Terrain Avoidance FLTA 10 12 Reduced Required Terrain Clearance RTC and Reduced Required Obstacle Clearance ROC 10 12 Imminent Terrain Impact ITI and Imminent OSTA ACD O rasta tne na 10 12 Premature Descent Alert PDA 10 12 Excessive Descent Rate Alert EDR ou cece 10 13 Negative Climb Rate After TakeotfAlert NCR 10 13 Five Hundred Aural Alert 10 13 Displaying Terrain and Obstacles on the DGG MOM MoDa ea NAN 10 14 POUD FIRMS erion REON 10 14 TAWS Alerts SUMM aN rannen 10 15 AVE PUAN MUNCISTION anasan 10 16 SECTION 11 ABNORMAL OPERATION 11 1 11 1 Reversionary Mode 0 0 cccccce ese ceaees 11 1 11 2 Abnormal COM Operation 0 0 0 000 11 2 11 3 Unusual Attitudes cscs 11 2 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 TABLE OF CONTENTS 11 4 Stormscope operation with loss of Heading Input cece cesses 11 2 11 5 Hazard Displays with Loss of GPS Position 11 2 SECTION 12 ANNUNCIATIONS am
51. Ahead Terrain Ahead CAUTION TERRAIN TERRAIN AHEAD Imminent Terrain Impact Caution ITI TERRAIN AHEAD Terrain Ahead Terrain Ahead or or CAUTION TERRAIN humi Caution Terrain Caution Terrain Reduced Required Obstacle Clearance TERRAIN Caution Obstacle Caution Obstacle Caution ROC 0 or OBSTACLE AHEAD Obstacle Ahead Obstacle Ahead Imminent Obstacle Impact Caution IOI TERRAIN OBSTACLE AHEAD Obstacle Ahead Obstacle Ahead 0 or CAUTION OBSTACLE Caution Obstacle Caution Obstacle Premature Descent Alert Caution PDA Atude Callout 500 Fe Hundred Excessive Descent Rate Caution EDR Sink Rate Negative Climb Rate Caution NCR DONT SINK Don t Sink or or TOOLOW TERRAIN Too Low Terrain 12 6 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 SECTION 12 ANNUNCIATIONS amp ALERTS TAWS System Status Annunciations PFD MFD TAWS MFD Alert Type Page Annunciation Pop Up Alert TAWS System Test Fail TAWS FAIL TAWS System Failure Aural Message No GPS position or excessively degraded TAWS N A None TAWS Not Available GPS signal TAWS Availble will be heard when sufficient GPS signal is re established System Test pass TAWS System Test OK 12 6 G1000 SYSTEM ANNUNCIATIONS A NOTE Upon power up of the G1000 system certain windows remain invalid as G1000 When an LRU or an LRU function fails
52. C 2 Selected radios Selected radios Passengers pilot copilot pilot copilot MUSIC 2 Table 5 1 ICS Isolation Modes Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 5 3 SECTION 5 AUDIO PANEL 5 4 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 fe RELAY w CREW wv PILOT COPLT ICS_ISOLATION PILOT O PASS VOL Figure 5 8 Volume Squelch Control 5 7 DIGITAL CLEARANCE RECORDER AND PLAYER Fach reception of primary active COM audio is automatically recorded ina 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 v v MAN SQ PLAY Figure 5 9 Playback e Pressing PLAY once plays the latest recorded memory block then returns to normal operation Pressing MKR MUTE while playing a memory block stops play e 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 If a COM input signal is detected
53. CWS button is released the current vertical speed will be maintained A desired altitude may be entered in the Selected Altitude Box by turning the ALT Knob With Altitude Hold mode armed as the selected altitude is reached ALT will flash in green for 10 seconds in the Active Mode field after which the annunciation stops flashing This signals the altitude capture is complete and the selected altitude will be maintained If only the flight director is engaged pitch commands are given to manually maintain the selected altitude Vertical Speed Reference Vertical Speed mode is active Nay 118 98 ITXD wer 110 90 ITXD Altitude Hold is Armed 123 8000 135 325 con Selected Altitude Selected Vertical Speed Vertical Speed Reference Bug Figure 6 12 Vertical Speed Hold Mode Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 Flight Level Change Mode FLC 1 Airspeed Reference Bu 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 SECTION 6 AUTOMATIC FLIGHT CONTROL Airspeed Box above the Airspeed Indicator and in the Airspeed Reference field in the AFCS Status Box Airspeed may also be changed by pressing and holding the CWS button to manua
54. E EA EA E S 8 2 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 8 2 Viewing the Active Flight Plan 8 2 8 3 Activate a Stored Flight Plan 8 2 8 4 Activate a Flight Plan Leg 0 cc 8 3 8 5 Stop Navigating a Flight Plan 8 3 8 6 Invert Active Flight Plan ees 8 3 8 7 Create a New Flight Plan 0 0 8 4 Create a New Flight Plan Using the MFD uu 8 4 Create a New Flight Plan Using the PFD uu 8 4 8 8 Load a Departure occas 8 5 8 9 Load an Arrival css 8 5 8 10 Load an Approach ou css 8 5 8 11 Remove a Departure Arrival or Approach from a Flight Plan cece 8 5 8 12 Store a Newly Created Flight Plan 8 5 8 13 Edit a Stored Flight Plan 8 5 8 14 Delete a Waypoint from the Flight Plan 8 5 8 15 Invert and activate a Stored Flight Plan 8 6 8 16 Copy a Flight Plan ou cesses 8 6 8 17 Delete a Flight Plan ou sees 8 6 8 18 Graphical Flight Plan Creation 0 008 8 6 8 19 Trip PlANMINg c cccc esses 8 6 8 20 Vertical Navigation VNAV Page 8 8 Create a Vertical Navigation Profile 8 8 VNAV Page Menu Options 8 9 SECTION 9 PROCEDURES s 9 1 9 1 Arrivals and Departures 551555111111111111 9 1 Load and Activate a Departure Procedure uu 9 1 Load and Activate An Arrival Procedure 9 1 9
55. ENT An overspeed annunciation flashing inverse video is When the AP Key is pressed the system engages the displayed above the airspeed tape autopilot If the flight director is not already active it is also engaged when the AP Key is pressed Autopilot engagement is displayed in the Autopilot Status field of the AFCS Status Box Autopilot engagement is indicated by a green AP Figure 6 4 Overspeed Annunciation When an overspeed caution occurs reduce engine Autopilot Engaged power and or adjust the pitch reference to slow the aircraft ROLJAP AL T Figure 6 5 Autopilot Engaged Annunciation 6 2 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 Automatic Disengagement 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 Automatic Disconnect ROL A ALT Figure 6 6 Automatic Disconnect Annunciation Manual Disengagement The autopilot may also be manually disengaged by pressing the AP DISC button the GO AROUND button or by pressing the AP Key on the MFD Manual disengagement is annunciated by a five second flashing yellow AP in the Autopilot Status field and by a two
56. ETARs or SIGMETs Press the ENT Key to display pertinent information for the selected product Note that pressing the ENT Key when panning over an AIRMET or a SIGMET displays an information box that displays the text of the report Panning over an airport with METAR information does not display more information but allows the user to press the ENT Key and select that Airport s Information Page to display the text of the report Pressing the ENT Key when panning over a TFR displays TFR specific information Weather Products and Symbols Figure 10 10 depicts the symbol for each weather product read from left to right When a weather product is active the product symbol is displayed in the lower right of the screen e NEXRAD e Cloud Top Echo Top e XM Lightning e Cell Movement SIGMETs AIRMETs e METARs Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 SECTION 10 HAZARD AVOIDANCE m Echo Top Cloud Top and Echo Top Mutually Exclusive m EA att q er Np tt OT oe a EAS Figure 10 10 Weather Product Saab e City Forecast Surface Analysis Weather Product Expires After e Freezing Levels E e Winds Aloft SIGMETS AIRMETS County Warnings a e Cyclone Warnings County Warnings BO The XM Information Page in the AUX Page Group will _Liclone Warnings o O display the weather products available for the current Echo Tops subscription A green box by the weather product means Freezing Levels o o that it is avail
57. FD indicator illuminated the FMS NAV COM Knob performs the same functions as a the FMS NAV and COM Knobs on the MFD With the PFD indicator illuminated the FMS NAV COM Knob performs the same functions as a the FMS NAV and COM Knobs on the PFD Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 SECTION 1 SYSTEM OVERVIEW PFD SOFTKEYS TERRAIN 1 3 Softkey ON Softkey OFF Nnoonnnnnd oO Figure 1 3 PFD Top Level Softkeys INSET Select to display the Inset Map in the lower left corner of the PFD OFF Select to remove the Inset Map DCLTR 3 Select momentarily to select the desired amount of map detail The declutter level appears adjacent to the DCLTR Softkey e No declutter All map features are visible Declutter 1 Removes land data Declutter 2 Removes land and SUA data Declutter 3 Removes everything except the active flight plan TRAFFIC Select to display traffic on the inset map TOPO Select to display topographical data Q e coastlines terrain rivers lakes and elevation scale on the Inset Map 350 only 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 LING optional Select to display the XM
58. Frequency Frequency Frequency Field nav1 189 98 gt 110 60 Cv TSI 188 Figure 4 2 Frequency Fields Tuning Box Active NAV Active COM Tuning Box Frequency Field Frequency Field 135 100 1 858 cont 3 600 gt 121 900 conz Frequency Transfer Arrow Tuning Box Figure 4 3 Frequency Transfer Arrow and Tuning Box NAV Controls COM Controls VOL PUSH VOL PUSH ID Knob SQ Knob Frequency Transfer Key Dual NAV Dual COM Knob Knob Turn to tune in desired frequencies e Press to change tuning box positions Figure 4 4 NAV COM Controls 4 2 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 4 1 RADIO STATUS INDICATIONS RX When a COM signal is received a white RX appears by the active COM frequency during signal reception e TX When a COM radio is transmitting a white TX indication appears to the right of the corresponding COM frequency ID When the Morse code identifier is ON fora NAV radio a white ID indication appears to the lett of the corresponding active NAV frequency The Morse code identifier can be heard if the corresponding NAV radio is selected on the audio panel 118 6804 com TX COM2 121 900 Figure 4 5 Radio Status Indications 4 2 VOLUME VOLUME is displayed in place of the associated radio name i e COMI or NAV2 for two seconds after the volume level is last changed The percentage of maximum volume is displayed in place of the standby f
59. Key E Turn the large FMS Knob to place the cursor in the desired selection field Turn the small FMS Knob to begin selecting the desired identifier location etc Press the ENT Key The cursor is now flashing on ACTIVATE Press the ENT Key again to activate Cancelling Direct to Navigation Press the Direct to GE Key Press the MENU Key to display the Options Window The cursor will be flashing on Cancel Direct to NAV Press the ENT Key to cancel the direct to Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 136 975 Figure 7 5 Airport Information Page Select the Airport Information Page 1 2 Turn the large FMS Knob to select the WPT page group Turn the small FMS Knob to select the first rectangular page icon Enter a Waypoint Facility Name or City Location With the Airport Information Page displayed press the FMS Knob to activate the cursor Turn the large FMS Knob to select the facility name or location city field Turn the small FMS Knob to select the desired first character Turn the large FMS Knob to select the next character field Repeat steps 3 and 4 until the facility name or location is selected then press the ENT Key If there are duplicate names in the database 6 SECTION 7 NAVIGATION a list is displayed from which to choose the desired location To remove the flashing cursor press the FMS Knob Access Runway Informatio
60. Map 1 From the Navigation Map Page press the MENU Key Select Map Setup and press the ENT Key 2 Turn the small FMS Knob to select Weather and press the ENT Key 3 Turn the large FMS Knob to select STRMSCP MODE 4 Turn either FMS Knob to display the Cell Strike ee TAGE Window Change the Stormscope lightning mode 5 Turn either FMS Knob to select Cell or Strike between cell and strike Press the ENT Key 1 Select the Stormscope Page 6 beak me FMS Knob to return to the Navigation 2 Select the MODE Softkey The CELL and STRIKE ae Softkeys are displayed Select the CELL Softkey Clear Stormscope lightning data from the to display CELL data or select the STRIKE Navigation Map Page Softkey to display STRIKE data CELL or 1 Press the MENU Key with the Navigation Map STRIKE is displayed in the mode box located in Page displayed the upper left corner of the Stormscope Page NOTE Cell mode uses a clustering program to identify clusters of electrical activity that indicate cells 2 Turn either FMS Knob to highlight the Clear A Lightning Data field and press the ENT Key 10 2 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 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 S
61. N 2 FLIGHT INSTRUMENTS 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 To activate the Vspeed References display the Timer Reference Window and turn the large FMS Knob to place the cursor in the ON OFF field Turn the small FMS Knob to select ON or OFF 2 2 ATTITUDE INDICATOR The Slip Skid Indicator is located under the Roll Pointer and moves laterally away from the pointer to indicate lateral acceleration One Slip Skid indicator displacement is equal to one ball displacement when compared to a traditional slip skid indicator C1 Roll Pointer Roll Scale G Horizon Line 4 Aircraft Symbol Land Representation Roll Scale Zero 6 Aircraft Wing Tips E Pitch Scale Slip Skid Indicator 0 Sky Representation Figure 2 6 Attitude Indicator Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 2 gt SECTION 2 FLIGHT INSTRUMENTS 2 4 2 3 ALTIMETER Selected Altitude Altitude Select Bug Box Altitude Trend Vector Current Altitude Barometric Setting Box Figure 2 7 Altimeter Altitude Select Bug The Altitude Select Bug is displayed at the selected altitude or if the selected altitude is beyond the altitudes currently displayed the bug is displayed at the top or bottom of the display wh
62. NNING to enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint OR 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 Turn the large FMS Knob to highlight the LEG field and turn the small FMS Knob to select the desired leg of the flight plan or select CUM to apply trip planning calculations to the entire flight plan Selecting FPL 00 will display an active flight plan If an active flight plan is selected REM will be an available option to display planning data for the remainder of the flight plan NOTE The Page Mode must be set to MANUAL to perform the following steps Turn the large FMS Knob to highlight the departure time DEP TIME field Turn the FMS Knobs to enter the departure time Press the ENT Key when finished Departure time may be entered in local or UTC time depending upon system settings Turn the FMS Knobs to enter the fuel flow Press the ENT Key when finished Note that in automatic page mode fuel flow is provided by the system The flashing cursor moves to the fuel on board field Turn the FMS Knobs to modify the fuel on board Press the ENT Key when finished In AUTOMATIC mode fuel onboard is provided by the entry made in GAL REM on the EIS System Page Garmin G1000 Cockpit Reference Guide for the Col
63. ODES Mode annunciations for active roll axis modes are shown in green during normal operation Key FD AP only Roll Hold Default Heading Select HDG VOR Enroute Arm Capture Track us nay GPS Arm Capture Track BC Arm Capture Track BC LOC Arm Capture Track No Glideslope Eo GO GPS Arm Capture Track VOR Approach Arm Capture Track ILS Approach Arm Capture Track Glideslope pitch mode automatically armed AROUND Go Around Wings Level The default roll axis mode is Roll Hold ROL When no other roll axis modes are selected this is the active roll axis mode when the autopilot and or flight director is engaged Roll Hold Mode ROL 1 Press the FD or AP Key If the aircraft bank angle is gt 6 degrees when the key is pressed Roll Hold mode is selected by default Roll attitude at the time of activation is maintained by the autopilot up to 22 If SECTION 6 AUTOMATIC FLIGHT CONTROL only the flight director is active command bars indicate the proper roll attitude If the aircraft bank angle is lt 6 degrees when the key is pressed the aircraft will be maintained at wings level If only the flight director is active command bars give guidance to maintain wings level Roll Hold mode is annunciated by ROL a ROL ALT Figure 6 15 Roll Hold Mode A new heading can be established by pressing and holding the CWS button and manually turning the aircraft
64. 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 Displaying Stormscope Lightning Data on the Navigation Map Page 1 Select the MAP Softkey 2 Select the STRMSCP Softkey Select the STRMSCP Softkey again to remove Stormscope Lightning Data trom the Navigation Map Page U CARENE i D Figure 10 4 In Flight Navigation Map Page Displaying Stormscope Lightning Data Lightning Age symbol Strike is less than 6 seconds old Strike is between 6 and 60 seconds old Strike is between 1 and 2 minutes old Strike is between 2 and 3 minutes old Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 10 1 SECTION 10 HAZARD AVOIDANCE At a map range of less than 25 nm Stormscope Stormscope Page lightning data is not displayed but can still be present The presence of Stormscope lightning data is indicated by the annunciation LTNG lt 25 nm in the upper right corner 2 Turn the small FMS Knob until the Stormscope NORTH UP Page is selected 1 Turn the large FMS Knob until the Map Page group is selected NODE CELL 136 975 COM STRIKE RATE i HOG UF 7 oe a j Tam Figure 10 5 Lightning Display Range Annunciation Select cell or strike as the Stormscope lightning mode on the Navigation
65. OPTIONAL NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south A NOTE TAWS operation is only available when the G1000 is configured for a TAWS B installation Figure 10 17 TAWS Page 360 View 10 10 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 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 PAGE MENU OPTIONS Inhibit TAWS View Arc Show Aviation Data TERRAIN 1700F iT 1000r i l a Press the FMS CRSR knob to Figure 10 18 TAWS Page ARC View return to base puge Figure 10 19 TAWS Page Menu Terrain Obstacle Location Suggested Pilot Response Terrain Obstacle at or within 100 Initiate climb and or turn away trom below or above aircraft altitude terrain obstacle ane Terrain Obstacle between 100 and Be aware of surroundings 1000 below current aircraft altitude Be prepared to take action Terrain Obstacle is more than 1000 No action required Black below aircraft altitude Potential Impact Point Projected Flight Path Unlighted Obstacle Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 10 11 SECTION 10 HAZARD AVOIDANCE TAWS Inhibit Flying VFR into an area where unique terrain exists could cause the system t
66. PFD1 terrain database error exists MFD1 DB ERR MFD1 obstacle database error exists PFD1 DB ERR PFD1 obstacle database error exists MFD1 DB ERR MFD1 airport terrain database error exists PFD1 DB ERR PFD1 airport terrain database error exists DB MISMATCH Aviation database The PFD and MFD have different aviation database versions installed Crossfill is off version mismatch Xtalk is off Install correct aviation database version in both displays DB MISMATCH Aviation database The PFD and MFD have different aviation database types installed Americas Euro type mismatch Xtalk is off pean etc Crosstill is off Install correct aviation database type in both displays DB MISMATCH Basemap database The PFD and MFD have different basemap database versions installed Crosstill is version mismatch Xtalk is off off Install correct basemap database version in both displays DB MISMATCH Terrain database The PFD and MFD have different terrain database versions installed Crosstill is off version mismatch Xtalk is off Install correct terrain database version in both displays The MFD and or PFD detected a failure in the basemap database The MFD and or PFD detected a failure in the terrain database Ensure that the ter rain card is properly inserted in display Replace terrain card If problem persists The G1000 system should be serviced The MFD and or PFD detected a failure in the obstacle database En
67. Radio lightning data on the Inset Map BACK Select to return to the previous level softkey configuration ALERTS Select to display the Alerts Window optional optional Press the BACK or OFF Softkey to return to the top level softkeys Figure 1 4 PFD Softkey Flow Chart 1 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 SECTION 1 SYSTEM OVERVIEW PFD Select to display the additional softkeys for 360 HSI Select to display the 360 compass additional configuration of the PFD rose METRIC Select to display the current and reference ARC HSI Select to display the 140 viewable arc altitudes in meters in addition to feet Selecting BRG2 bearing Select to cycle through the the metric softkey also changes the barometric setting to hectopascals DFLTS Select to reset default settings on the PFD BRGI bearing Select to cycle through the following information NAVI Displays NAV1 waypoint frequency or identifier in the BRG1 Information Window GPS Displays GPS waypoint identifier and GPS 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 distance information in the BRG1 Information STD BARO Select to set the barometric pressure to Window OFF Removes the BRG1 Informatio
68. STORMSCOPE OPERATION WITH LOSS OF HEADING INPUT If heading is lost strikes and or cells must be cleared manually after the execution of each turn This is to ensure that the strike and or cell positions are depicted accurately in relation to the nose of the aircratt Ve Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 SECTION 12 ANNUNCIATIONS amp ALERTS NOTE The Airplane Flight Manual supersedes information found in this document System Annunciation Red X Annunciation Window remote avionics is inoperative Alerts Window TRAFFIC FAIL Traffic device has failed GMA1 FAIL Owes EAEN 1s Mae Met ALERTS Softkey Annunciation Figure 12 1 G1000 Alerting System The G1000 Alerting System conveys alerts to the pilot using a combination of the following items e Annunciation Window The Annunciation Window displays abbreviated annunciation text The Annunciation Window is located to the right of the Altitude and Vertical Speed Windows on the PFD display or the MFD if system is in reversionary mode Up to 12 annunciations can be displayed simultaneously A white horizontal line separates annunciations that are acknowledged SECTION 12 ANNUNCIATIONS amp ALERTS from annunciations that are not yet acknowledged Acknowledged annunciations are always above the line Annunciations are displayed in order of priority from top to bottom The highest priority annunciation is displayed at the top of the
69. TS feu Hin RiT Figure 7 14 Nearest User Waypoints Page Select the Nearest User Waypoint Page 1 Turn the large FMS Knob to select the NRST page group 2 Turn the small FMS Knob to select the fifth rectangular page icon Select a Nearest User Waypoint 1 With the Nearest User Waypoint Page displayed press the FMS Knob to activate the cursor It any previously entered User Waypoints are 7 8 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 within 200 nm these will be displayed with the closest listed first 2 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 FMS Knob to remove the flashing Cursor 7 13 NEAREST FREQUENCIES 17 955 7 Sh 136 975 in NORTH UP A TN gt NEAREST ARTCC Figure 7 15 Nearest Frequencies Page Select the Nearest Frequencies Page 1 Turn the large FMS Knob to select the NRST page group 2 Turn the small FMS Knob to select the sixth rectangular page icon Select and Load the Nearest ARTCC FSS or Weather Frequency 1 With the Nearest Frequencies Page displayed select the ARTCC FSS or Wx Softkey to place the cursor in the appropriate field SECTION 7 NAVIGATION 2 Turn the FMS Knobs to select the desired facility or frequency 3 Press the ENT Key to load the frequency into the COM frequency standby field
70. Up Terrain Ahead Pull Up Imminent Terrain Impact Warning ITI PULL UP Terrain Ahead Pull Up Terrain Ahead Pull Up or or TERRAIN PULL UP Terrain Terrain Pull Up Pull Up Reduced Required Obstacle Clearance PULL UP Obstacle Obstacle Pull Up Pull Up Warning ROC or or Obstacle Ahead Pull Up Obstacle Ahead Pull Up Imminent Obstacle Impact Warning 101 PULL UP Obstacle Ahead Pull Up Obstacle Ahead Pull Up OF or Obstacle Obstacle Pull Up Pull Up Reduced Required Terrain Clearance Caution Caution Terrain Caution Terrain Aural Message RTC or ERRAIN A Terrain Ahead Terrain Ahead Imminent Terrain Impact Caution ITI Terrain Ahead Terrain Ahead or Caution Terrain Caution Terrain Reduced Required Obstacle Clearance UTIOI ACL Caution Obstacle Caution Obstacle Caution ROC or Obstacle Ahead Obstacle Ahead Imminent Obstacle Impact Caution IOI Obstacle Ahead Obstacle Ahead or Caution Obstacle Caution Obstacle Premature Descent Alert Caution PDA Altitude Callout 500 None Five Hundred Excessive Descent Rate Caution EDR TERRAIN see o Sink Rate Negative Climb Rate Caution NCR TERRAIN DONTSINK Don t Sink or or TOOLOW TERRAIN Too Low Terrain Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 10 15 SECTION 10 HAZARD AVOIDANCE The following system stat
71. able METARs a A NOTE The DONE Softkey on the AUX XM_ Lightning INFORMATION Page is used to save the GDL NEXRAD 69 A activation data when the XM services Radar Coverage are initially set up It is not used during normal operation of the GDL 69 A and it should have Cell Movement no adverse effects if inadvertently selected during Surface Analysis o flight Refer to the GDL 69 69A XM Satellite wmo T oo Radio Activation Instructions 190 00355 04 Rev E or later for further information Winds Aloft o a Clouds Tops Oo o Weather Product Age The age for each of the enabled products is displayed on the right side of the display Times are based on Zulu time when the data was assembled on the ground not the time the data was received by the XM receiver When the age of a weather product has exceeded half of the expiration time the product time will change from light blue to amber in color 10 6 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 10 4 TRAFFIC INFORMATION SERVICE TIS A NOTE If the G1000 is configured to use the optional Ryan 9900BX Traffic Advisory System TIS will not be available for use A NOTE Traffic Information Service TIS is only available when the aircraft is within the service volume of a TIS capable terminal radar site 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
72. always takes precedence over the information found in this section Normal MFD Display MFD in Reversionary Mode Figure 11 1 G1000 Reversionary Mode Failed PFD Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 11 1 SECTION 11 ABNORMAL OPERATION 11 2 ABNORMAL COM OPERATION 11 5 HAZARD DISPLAYS WITH LOSS OF When a COM tuning failure is detected by the system GPS POSITION the emergency frequency 121 500 MHz is automatically If GPS position is lost or becomes invalid selected loaded into the active frequency field of the COM radio hazards being displayed on the Navigation Map Page lor which the tuning failure was detected In the event of will be removed until GPS position is again established a dual display failure the emergency frequency 121 500 The icons in the lower right of the screen indicating the MHz automatically becomes the active frequency to the selected functions for display will show an X as shown pilot through the pilot headset in Figure 11 3 11 3 UNUSUAL ATTITUDES The PFD will declutter when the aircraft enters an unusual attitude Only the basic primary functions will be displayed in these situations Figure 11 3 Loss of Hazard Functions with Loss of GPS Position BUUUOU Red extreme pitch warning chevrons pointing toward the horizon are displayed starting at 50 degrees above and 30 degrees below the horizon line Figure 11 2 Extreme Pitch Indication 11 4
73. ated 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 3 Dual NAV Knob Tunes the MHz large knob and kHz small knob standby frequencies for the NAV receiver Press to move the tuning cursor light blue box between the NAV1 and NAV2 fields 4 Heading Knob Turn to manually select a heading on the HSI When pressed it synchronizes the heading bug with the compass lubber line Selected Heading provides the heading reference to the Flight Director while operating in Heading Select mode 5 Joystick Changes the map range distance top to bottom of map display when rotated Activates the map pointer when pressed 6 CRS BARO Knob The large knob sets the altimeter barometric pressure and the small knob adjusts the course The course is only adjustable when the HSI is in VORI VOR2 or OBS SUSP mode Pressing this knob centers the CDI on the currently selected VOR Selected Course provides course reference to the Flight Director when operating in Navigation and Approach modes 7 Dual COM Knob Tunes the MHz large knob and kHz small knob standby frequencies for the COM transceiver Pressing this knob moves the tuning cursor light blue box between the COM and COM2 fields 8 COM Frequency Transfer Key Sw
74. ather 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 ICELL MOV SIG AIR METAR LEGEND HORE WX Figure 10 9 Weather Data Link Page NEXRAD Select the NEXRAD Softkey to show NEXRAD weather and radar coverage information Areas where radar coverage is not available will be shown in grayish purple The display is updated every five minutes NEXRAD Limitations 10 4 Certain limitations exist regarding the NEXRAD radar displays Some but not all are listed here NEXRAD base reflectivity does not provide sufficient information to determine cloud layers or precipitation characteristics hail vs rain etc An individual NEXRAD site cannot depict high altitude storms at close ranges and has no information about storms directly over the site The resolution of displayed NEXRAD data is 4 square kilometers Therefore when zoomed in on the display each square block is 2 kilometers on each side The intensity level reflected by the square will be the highest level sampled within the square area ECHO TOP Select the ECHO TOP Softkey to sh
75. ating and is reducing power consumption by dimming MFD1 COOLING MFD1 has poor the display If problem persists the G1000 system should be serviced cooling Reducing power usage PFD1 KEY KEYSTK Key is stuck A key is stuck on the PFD and or MFD bezel Attempt to free the stuck key by press MFD1 KEY KEYSTK Key is stuck ing it several times The G1000 system should be serviced if the problem persists CNFG MODULE PFD1 configuration The PFD configuration module backup memory has failed The G1000 system should module is inoperative be serviced PFD1 VOLTAGE PFD1 has low volt age Reducing power usage MFD1 VOLTAGE MFD1 has low volt age Reducing power usage The PFD1 voltage is low The G1000 system should be serviced The MFD1 voltage is low The G1000 system should be serviced 12 10 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 SECTION 12 ANNUNCIATIONS amp ALERTS Database Message Advisories Alerts Window Message Comments o MFD1 DB ERR MFD1 aviation database error exists The MFD and or PFD detected a failure in the aviation database Attempt to reload PFD1 DB ERR PFD aviation the aviation database It problem persists the G1000 system should be serviced database error exists MFD1 DB ERR MFD1 basemap database error exists PFD1 DB ERR PFD1 basemap database error exists MFD1 DB ERR MFD1 terrain database error exists PFD1 DB ERR
76. c Advisories Navigation Map displayed select the MAP 5 Rotate the Joystick clockwise to display a larger pone E area or rotate counter clockwise to display a 2 Select the TRAFFIC Softkey Traffic will now be smaller area displayed on the map 10 8 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 Traffic Advisory iP NAVIGATION HAP ol AMA Non Bearing Traffic Off Scale Non Threat Traffic Advisories ieee Traffic Figure 10 13 TAS Traffic on Navigation Map 10 6 TERRAIN AND OBSTACLE PROXIMITY A NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south Displaying Terrain and Obstacles on the Terrain Proximity Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the last rectangular page icon 3 If desired select the VIEW Softkey to access the ARC and 360 Softkeys When the ARC Softkey is selected a radar like 120 view is displayed Select the 360 Softkey to return to the 360 default display SECTION 10 HAZARD AVOIDANCE 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area 136 975 K 10D per RED WARNING Terrain Obstacle at or within 100 below or above aircraft altitude YELLOW CAUTION Terrain Obstacle between 100 and 1000 below current aircraft altitude Aircraft Altitude 100 Threshold
77. ced when possible AHRS1 GPS AHRS1 not receiving The 1 AHRS is not receiving any or any useful GPS information Check AFMS limita any GPS information tions The G1000 system should be serviced AHRS1 GPS AHRS1 not receiving The 1 AHRS is not receiving backup GPS information The G1000 system should be backup GPS information serviced AHRS1 GPS AHRS1 operating The 1 AHRS is operating exclusively in no GPS mode The G1000 system should be exclusively in no GPS mode serviced MANIFEST GRS1 software mismatch Communication halted BACKUP PATH AHRS1 using backup The 1 AHRS is using a backup communications data path The G1000 system data path should be serviced when possible AHRS1 SRVC AHRS1 Magnetic tield The 1 AHRS earth magnetic field model is out of date Update magnetic field model model needs update when practical GEO LIMITS AHRS1 too far North The aircraft is outside geographical limits for approved AHRS operation Heading is South no magnetic compass flagged as invalid The AHRS has incorrect software installed The G1000 system should be serviced Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 1245 SECTION 12 ANNUNCIATIONS amp ALERTS GMU 44 Message Advisories Alerts Window Message Comments HDG FAULT AHRS1 magnetometer A fault has occurred in the GMU 44 Heading is flagged as invalid The AHRS uses fault has occurred GPS for backup mode operation Th
78. des without engaging the autopilot Pressing the AP Key activates the flight director and engages the autopilot When only the flight director is engaged pressing the FD Key disengages the flight director Upon activation of the autopilot and or flight director command bars are displayed on the PFD If the attitude information being sent to the flight director becomes invalid or unavailable the command bars are removed from the display O Figure 6 2 Command Bars 6 1 MODE ANNUNCIATIONS Mode annunciations are displayed on the PFD Figure 6 3 shows the AFCS Status Box fields Modes associated with aircraft movement about the roll axis are displayed on the left side Modes associated with aircraft movement about the pitch axis are displayed on the right Armed modes are displayed in white and active modes are displayed in green Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 6 1 SECTION 6 AUTOMATIC FLIGHT CONTROL Active Mode Mode Reference Armed Mode Autopilot Status Active Mode Armed Mode GPS ROL AP ALT Roll Axis Modes Pitch Axis Modes AFCS Status Box newt 113 88 118 909TE xD wer DIS DTK TRX 133 118 700 com id MA2 118 98 11x0 P 135 325 DONZ System Status Fie v see Annunciations amp Alerts A Altitude Aircraft Attitude Symbol Flight Director Command Bars PFD OBS CDI XPOR TOENI EF Tea Acns Figure 6 3 PFD AFCS Display 6 2 OVERSPEED PROTECTION 6 3 AP ENGAGEMENT DISENGAGEM
79. dow Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 1 7 DATABASE UPDATES Aviation Database Update 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 With the G1000 System OFF insert the aviation database update SD card into the top card slot of the PFD Label of SD card facing left 2 Turn the G1000 System ON This prompt is displayed on the upper left corner of the PFD DO YOU WANT TO UPDATE THE AVIATION DATABASE PRESS CLR FOR NO AND ENT FOR YES YOU HAVE 3 SECONDS BEFORE NO IS RETURNED Figure 1 10 Database Update Prompt 3 Press the ENT Key to confirm the database updated This prompt is displayed DO YOU WANT TQ UPDATE THE AVIATION DATABASE PRESS CLR FOR NO AND ENT FOR YES YOU HAVE 3 SECONDS BEFORE NO IS RETURNED UPDATING AVIATION DATABASE UPDATED HE TRESS SOULE Se ULL Ys Figure 1 11 Database Update Confirmation 4 After the update completes the PFD starts in normal mode Remove the aviation database update SD card trom the PFD 5 Turn the G1000 System OFF 6 Repeat steps 1 through 4 for the MFD The MFD and PFD aviation databases are now updated SECTION 1 SYSTEM OVERVIEW 7 Verity that the correct update cycle is loaded during startup of the MFD Terrain and Obstacle Database Updates NOTE The data contained in the terrain and obstacle databases comes f
80. e inserted ABOVE the cursor After placing the cursor at the desired point in the list of waypoints select the LD WPT Softkey To change the user waypoint name follow the procedure for modifying a user waypoint TRIP PLANNING Turn the large FMS Knob to select the AUX page group Turn the small FMS Knob to select the first rectangular page icon Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 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 Ending WPT JONH FUEL CHEARD FUEL STATS EFFICIENCY TOTAL ENDUR REH FUEL REH ENDUR FUEL REG TOTAL RANGE Figure 8 15 Trip Planning Page For Direct to planning select the WPTS Softkey and verity that the starting waypoint field indicates P POS present position If necessary press the MENU Key and select Set WPT to Present Position to display P POS Press the ENT Key and the flashing cursor moves to the ending waypoint field Turn the FMS Knobs to enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint OR For point to point planning turn the FMS Knobs to enter the identitier of the starting waypoint Once the waypoints identifier is entered press the ENT Key to accept the waypoint The flashing cursor moves to the ending waypoint Again turn the FMS Knobs SECTION 8 FLIGHT PLA
81. e G1000 system should be serviced MANIFEST GMU1 software mismatch Communication halted GDL 69 Message Advisories Alerts Window Message Comments S O GDL69 CONFIG GDL 69 configura GDL 69 configuration settings do not match those of backup configuration memory tion error Contig service req d The G1000 system should be serviced GDL69 FAIL GDL 69 has failed A failure has been detected in the GDL 69 The receiver is unavailable The G1000 system should be serviced The GMU 44 has incorrect sottware installed The G1000 system should be serviced GDC 74A Message Advisories Alerts Window Message Comments S O GDC1 CONFIG GDC1 configuration GDC 74A configuration settings do not match those of backup configuration error Contig service req d memory The G1000 system should be serviced MANIFEST GDC1 software The GDC 74A has incorrect software installed The G1000 system should be mismatch Communication halted serviced BACKUP PATH ADC1 using backup The GDC 74A is using a backup communications data path The G1000 system data path should be serviced when possible GCU 476 Message Advisories Alerts Window Message Comments o GCU CNFG GCU Contig error Con GCU 476 configuration settings do not match those of backup configuration memory fig service req d The G1000 system should be serviced GCU FAIL GCU is inoperative The GCU 476 has failed The G1000 system should be serviced when p
82. e altitudes MSAs are only advisory in nature and should not be relied upon as the sole source of obstacle and terrain avoidance information Always refer to current aeronautical charts for appropriate minimum clearance altitudes WARNING The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and could vary significantly from the altitude displayed by pressure altimeters such as the GDC 74A Air Data Computer or other altimeters in aircraft GPS altitude should never be used for vertical navigation Always use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft WARNING The Jeppesen database used in the G1000 system must be updated regularly in order to ensure that its information remains current Updates are released every 28 days A database information packet is included in the G1000 package Pilots using an outdated database do so entirely at their own risk WARNING The basemap land and water data must not be used for navigation but rather only for non navigational situational awareness Any basemap indication should be compared with other navigation Sources WARNING Traffic information shown on the G1000 Multi Function Display is provided as an aid in visually acquiring traffic Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic WARNING Use of the Stormscope is not intended for hazardous weath
83. ears on the tape in light blue once in range e When the aircraft passes through 100 feet of the MDA the bug and text turn white e Once the aircraft descends past the MDA the bug and text turn yellow and the aural alert Minimums Minimums is generated Alerting is inhibited while the aircraft is on the ground If the aircraft climbs after having reached the MDA once it reaches 50 feet above the MDA alerting is disabled Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 Within 100 ft Barometric Minimum Bug Barometric E Minimum Box Eam BARO MIN 30 04IN Figure 2 9 Barometric Minimum Descent Altitude Alerting Visual Annunciations 2 4 VERTICAL DEVIATION GLIDESLOPE INDICATOR The Vertical Deviation Glideslope Indicator appears when an ILS is tuned in the active NAV field Selected Vertical Speed SECTION 2 FLIGHT INSTRUMENTS 2 5 MARKER BEACON ANNUNCIATIONS Marker Beacon Annunciation Vertical Deviation Glideslope Indicator Figure 2 10 Marker Beacon and Vertical Deviation 2 6 VERTICAL SPEED INDICATOR Vertical Speed Bug Vertical Speed Pointer Figure 2 11 Vertical Speed Indicator The actual vertical speed is displayed inside the pointer When the Flight Director is placed in Vertical Speed Mode by pressing the VS Key the Vertical Speed Bug is displayed Press the NOSE UP or NOSE DN Key to adjust Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 2
84. ed roll and pitch mode fields respectively The autopilot and flight director determine when to begin the turn to intercept the final approach course 5 The autopilot flies the ILS Approach At the Decision Height there are two options push the AP DISC switch and land the aircraft or use the Go Around button to execute a missed approach reter to the following procedure Figure 6 24 ILS Approach to KFAT Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 Go Around Missed Approach 1 Push the Go Around button at the Decision Height to execute a missed approach Note that when the Go Around button is pushed the autopilot disconnects and the AP annunciation flashes yellow for five seconds The flight director Command Bars establish a 7 degree nose up climb to follow 2 Add power and retract flaps per the go around procedures in the Columbia AFM Start the climb to the prescribed altitude in the published Missed Approach Procedure a Press the AP Key to re engage the autopilot b Press the FLC Key and adjust for Vx or Vy c After reaching 400 AGL set the HSI to HDG or GPS mode In this example GPS mode is selected d Select the SUSP Softkey to resume sequencing approach legs to the Missed Approach Hold Point MAHP e Press the NAV Key to have the autopilot fly to the MAHP In this example the autopilot flies direct to Clovis VORTAC according to the loaded approach see Figure 6 25 3
85. elease the CWS button This new altitude is now displayed in the Altitude Reference field The autopilot will now hold the aircraft at this altitude Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 6 5 SECTION 6 AUTOMATIC FLIGHT CONTROL Vertical Speed Mode VS 1 6 6 Flight Director command bars indicating a climb at the prescribed vertical speed to the Selected Altitude 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 Altitude Hold mode is automatically armed with ALT displayed white in the Armed Mode field to the right of the VS annunciation The Vertical Soeed Bug can be adjusted in 100 fom increments by pressing the NOSE UP NOSE DN Keys to set the desired vertical speed The vertical speed setting will be displayed in the Selected Vertical Soeed Box and in the Vertical Speed Reference field in the AFCS Status Box The Vertical Speed Box is located above the VSI when the aircraft is climbing and below the VSI when descending Vertical speed may also be changed by pressing and holding the CWS button to manually establish the desired vertical speed using the control stick When the
86. er 4 4 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 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 Soeed 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 Weather warnings 10 5 Wind direction 10 5 Wind speed 10 5 X XM weather 10 4 XPDR softkey 4 4 INDEX Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 Index 3 INDEX Blank Page Index 4 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 ul Garmin International Inc 1200 East 151st Street Olathe KS 66062 U S A p 913 397 8200 f 913 397 a E mn Garmin AT Inc 2345 Turner Road S Salem OR 97302 US y p 503 391 3411 f 503 364 2138 Garmin Europe Ltd Unit 5 The Quadrangle Abbey Park Industrial Estate Romsey 051 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 or its subsidiaries
87. er penetration thunderstorm penetration Stormscope information as displayed on the G1000 MFD is to be used only for weather avoidance not penetration WARNING GDL 69 Weather should not be used for hazardous weather penetration Weather information provided by the GDL 69 is approved only for weather avoidance not penetration Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 WARNINGS CAUTIONS amp 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 However the pilot must recognize that providing monitoring and or self test capability for all conceivable system failures is not practical Although unlikely it may be possible for erroneous operation to occur without a fault indication shown by the G1000 It is thus the responsibility of the pilot to detect such an occurrence by means of cross checking with all redundant or correlated information available in the cockpit WARNING For safety reasons G1000 operational procedures must be learned on the ground WARNING The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance The GPS system
88. ersection Information Page Access Information on an Intersection 1 1 4 With the Intersection Information Page displayed press the FMS Knob to activate the cursor Turn the FMS Knobs to enter a name for the identifier and press the ENT Key Press the FMS Knob to remove the flashing Cursor Figure 7 7 NDB Information Page Select the NDB Information Page 1 2 Turn the large FMS Knob to select the WPT page group Turn the small FMS Knob to select the third rectangular page icon View Information on a Specific NDB 1 2 With the NDB Information Page displayed press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired selection field identifier name or closest city Turn the FMS Knobs to enter an identifier name or city and press the ENT Key Press the FMS Knob to remove the flashing cursor Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 Figure 7 8 VOR Information Page Select the VOR Information Page 1 2 Turn the large FMS Knob to select the WPT page group Turn the small FMS Knob to select the fourth rectangular page icon Access Information on a VOR 1 2 With the VOR Information Page displayed press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired selection field identifier name or closest city Turn the FMS Knobs to enter an identifier name or city and p
89. ervice Return unit for repair A failure has been detected in the GPS1 and or GPS2 receiver The receiver may still GPS2 SERVICE GPS needs service be available The G1000 system should be serviced Return unit for repair NAV1 SERVICE NAV1 needs service Return unit for repair A failure has been detected in the NAV1 and or NAV2 receiver The receiver may still NAV2 SERVICE NAV2 needs service be available The G1000 system should be serviced Return unit for repair NAV1 RMT XFR NAV1 remote os transfer key is stuck The remote NAV1 and or NAV2 transfer switch is stuck in the enabled or pressed NAV2 RMT XER NAV state Press the transter switch again to cycle its operation If the problem persists en eno the G1000 system should be serviced transter Key is stuck G S1 FAIL G S1 is inoperative A failure has been detected in glideslope receiver 1 and or receiver 2 The G1000 G S2 FAIL G S2 is inoperative system should be serviced G S1 SERVICE G S1 needs service Return unit for repair A failure has been detected in glideslope receiver 1 and or receiver 2 The receiver G S2 SERVICE G S2 needs service may still be available The G1000 system should be serviced when possible Return unit for repair GEA 71 Message Advisories Alerts Window Message Comments S O GEA1 CONFIG GEA1 configuration The GEA 71 configuration settings do not match those of backup configuration error
90. for the Columbia 350 400 6 15 SECTION 6 AUTOMATIC FLIGHT CONTROL Flying a GPS Flight Plan If the NAV Key is not pressed within 10 seconds of the HSI mode change the flight 1 Enter Panoche VORTAC PXN and Clovis VORTAC director will roll the wings level and enter Roll CZQ into the GPS flight plan in preparation to Hold Mode his leg eet 9 eg Ea 3 Once the flight plan leg is intercepted the 2 Transition from VOR to GPS Navigation Mode autopilot continues to track GPS guidance to the a Use the CDI Softkey to put the HSI in GPS end of the flight plan mode This cancels VOR mode on the HSI and the flight director loses the VOR signal As a result the VOR annunciation flashes yellow Flashes for ten seconds then transitions to ROL b Press the NAV Key to activate GPS Navigation Mode to cause the autopilot to steer the aircraft toward the active flight plan leg 33 0 Clovis VORTAC CZQ Panoche VORTAC PXN Figure 6 22 Transition to GPS Flight Plan 6 16 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 SECTION 6 AUTOMATIC FLIGHT CONTROL Flight Level Change Descent 2 Reduce power to allow descent in Flight Level While flying the GPS leg from Panoche VORTAC to The autopilot maintains the Clovis VORTAC the aircraft is cleared to make a descent BOP ae to 3000 feet in preparation for the approach to KFAT 3 Upon capturing the Selected Altitude the fligh
91. formation for the Selected Airport 1 With the Nearest Airports Page displayed select 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 Quickly Tune the COM Transceiver to a Nearby Airport Frequency 1 With the Nearest Airports Page displayed select the FREQ Softkey to place the cursor in the FREQUENCIES field 2 Turn either FMS Knob to select the desired frequency 3 Press the ENT Key The selected frequency is placed in the COM standby frequency field 4 Press the Frequency Transfer Key to place the frequency in the active field 5 Press the FMS Knob to remove the flashing Cursor Nearest Airports Information on the PFD Bearing TO Dienne Airport Symbol Identifier U56 M ers 9 3NM VFR MULTICOM 122 900 RNWY 35 FT Runway Length KIDA r 9 5NM ILS TOWER 118 500 RNWY 9 1FT KRXE 352 26 1NM VOR UNICOM 122 800 RNWY 42 FT Primary COM Frequency Figure 7 10 Nearest Airports Window Select the NRST Softkey to display the PFD Nearest Airports Window View Information on a Specific Airport in the List 1 With the Nearest Airports Window displayed turn either FMS Knob to place the cursor on the desired airport identifier 2 Press the ENT Key to display airport information 3 Press the ENT Key again cursor is on BACK to return to the list Load an A
92. g Direct to Navigation cesseessesseseeseerees l 2 Direct to Navigation from the PFD s s s 7 2 Cancelling Direct to Navigation c ccseesceesseseeseesees 7 2 7 3 Airport Information 0 0 cece 7 3 Select the Airport Information Page 7 3 Enter a Waypoint Facility Name or City Location 7 3 Access RUNWAY Information 1 3 Access Frequency Information 1 3 7 4 Intersection Information 0 0 0 cc ee 7 4 Select the Intersection Information Page sseseeee 7 4 Access Information on an Intersection 1 4 7 5 NDB Information 0 0 cccccscc sess l Select the NDB Information Page 7 4 View Information on a Specific NDB seescsseesveeseeee 7 4 7 6 VOR Information 0 0 0 cesses 7 5 Select the VOR Information Page c sseseseesesresseeen 7 5 Access Information on a VOR 7 5 7 7 User Waypoint Information Page 7 5 7 8 Nearest Airports 0 0 cc ccs 7 5 Nearest Airport Information on the MFD uu 7 5 Select the Nearest Airports Page essessessessesseeen 7 5 Access Information on a Specific Airport 1 6 Access Runway Information for the Selected ANDON oei ETE 1 6 Quickly Tune the COM Transceiver to a Nearby Airport Requena aa 1 6 Nearest Airports Information on the PFD 7 6 View Information on a Specific Airport in the List 7 6 Load an Airport COM Frequency into the AVEC OM aiaeei OETA 1 6 7 9 Neare
93. ght level change 1 4 6 3 6 7 6 11 6 16 Flight Plan Catalog 9 1 9 2 FLTA 10 12 Forward Looking Terrain Avoidance 10 12 FPL key 1 3 1 5 Freezing level 10 5 Frequency toggle key 1 3 4 3 Fuel remaining 3 6 Fuel used 3 6 G GA 6 1 6 3 6 8 6 9 6 12 Glideslope 2 2 2 5 6 3 6 8 6 9 6 12 GMA 1347 1 1 Go Around 6 1 6 3 6 8 6 9 6 12 6 19 HDG key 6 10 Heading hold 6 9 Heading indication 2 7 Heading Select 1 3 1 4 6 9 6 10 Heading Select Mode 6 10 Headset s 5 3 Hijack code 4 4 Horizontal situation indicator 2 6 Hurricanes 10 5 Index 1 INDEX 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 Manual Electric Trim 6 1 MAP 7 1 Map panning 10 5 Marker beacon 2 5 messages 12 1 Message advisories 12 2 12 10 12 18 MET 6 1 6 3 12 5 METAR 10 3 10 5 MFD 1 1 4 3 Military interceptor operations code 4 4 Missed Approach 6 19 Mistrim 12 5 Mixture 3 3 3 4 3 5 MKR MUTE 5 2 5 3 5 4 Mode selection softkeys 4 4 Morse code identifier 4 3 Nav Com controls 4 1 NAV1 5 3 NAV2 5 3
94. gits 4 4 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 SECTION 5 AUDIO PANEL SECTION 5 AUDIO PANEL oo ail E COMI com ii ie Transmitters ras Transceiver Audio MIC COM 3 is unavailable COM3 MIC is unavailable Split COM Telephone Unavailable Passenger Address Speaker Marker Beacon Mute Marker Beacon Signal Sensitivity DS Aircraft Navigation Radio Audio Aircraft Navigation Radio Audio DME ADF amp AUX unavailable Manual Squelch Na Recorded COM Audio Playback CREW w PILOT sn ICS Isolation ES ISOLATION PILOT O PASS VOL SO Volume Squelch VOL Annunciation S sa SQ Annunciation Reversionary Mode DISPLAY BACKUP Figure 5 1 Audio Panel Controls Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 5 1 SECTION 5 AUDIO PANEL Jz 5 1 COM RADIO SELECTION Pressing the COMI MIC or COM2 MIC Key selects the active transmitter i e microphone The associated receiver audio COMI 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 COMI or COM2 Key before pressing the other COM MIC key wv wv COM1 MIC COM1 gt a COM2 ile COM2 Figure 5 2 Transceivers 5 2 SPLIT COM FUNCTION NOTE Split COM performance is affected by
95. he marker beacon audio is turned off Outer Marker Annunciator Middle Marker Annunciator Inner Marker Annunciator Figure 5 4 Marker Beacon Annunciators on the PFD Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 Marker Beacon Signal Sensitivity The HI SENS Key can be pressed for increased marker beacon signal sensitivity al al MKR HI MUTE SENS Figure 5 5 Marker Beacon 5 4 NAV RADIO AUDIO SELECTION Pressing NAVI 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 Figure 5 6 Navigation Radios 5 5 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 CREW w PILOT COPLT ICS ISOLATION Figure 5 7 ICS Isolation PILOT KEY COPLT KEY Pilot Hears Conilot Hears Passenger ANNUNCIATOR ANNUNCIATOR p Hears COPILOT FF FF ON ON Selected radios Selected radios Selected radios pilot copilot pilot copilot pilot copilot passengers passengers passengers MUSIC 1 MUSIC 1 MUSIC 2 En Selected radios 0 pilot Copilot Copilot passengers passengers MUSIC 1 MUSIC 2 Selected radios Selected radios pilot passengers Copilot pilot passengers MUSIC 1 MUSI
96. he original flight plan remains intact in its flight plan catalog storage location COPY A FLIGHT PLAN From the Flight Plan Catalog press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the flight plan to be copied Select the COPY Softkey A Copy to flight plan confirmation window is displayed With OK highlighted press the ENT Key to copy the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key DELETE A FLIGHT PLAN From the Flight Plan Catalog Page press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the flight plan to be deleted Select the DELETE Softkey 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 GRAPHICAL FLIGHT PLAN CREATION Press the FPL Key to display the Active Flight Plan Page Press the Joystick to activate the map pointer Use the Joystick to move the pointer to the desired point on the map to be inserted as a waypoint in the flight plan Select the LD WPT Softkey The selected waypoint will be inserted at the end of the flight plan The default user waypoint naming is USROOO USROO1 USROO2 and so on If the selected waypoint is to be placed elsewhere in the flight plan press the FMS Knob to activate the cursor Waypoints ar
97. hout immediately using it for navigation guidance Activate An Approach in the Active Flight Plan With the Navigation Map Page displayed press the PROC Key Turn the large FMS Knob to highlight ACTIVATE APPROACH Press the ENT Key The approach procedure is now active SECTION 9 PROCEDURES Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 9 3 SECTION 9 PROCEDURES Blank Page 9 4 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 SECTION 10 HAZARD AVOIDANCE 10 1 CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 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 The Map Setup Menu is displayed Turn the small FMS Knob to select the Weather or Traffic group to customize the display of weather features Select Traffic to customize the display of traffic Press the small FMS Knob to return to the Navigation Map Page PAGE HENL OPTIONS Measure Beoring Distonce Clear Stormscope Lightning Press the FMS CRSR knob to Figure 10 1 Page Menu HAP SETUP STRHSCP LTNG n STRHSCP HODE Cal STRHSCP SHEL SGN NEXRAD DATA OFF 2Q 0NH WH LTNG OFF 2000NH CELL HOVEHENT 4 On Figure 10 2 Map Setup Menu MAP SETUP 1SQNH Figure 10 3 Map Setup Group List SECTION 10 HAZARD 10 2 STORMSCOPE OPTIONAL 350
98. ichever is closest to the selected altitude Set the Selected Altitude Bug Turn the ALT Knobs to set the Altitude Select Bug The small ALT Knob sets the hundreds and the large ALT Knob sets the thousands This altitude also appears in the Selected Altitude Box above the Altimeter Altitude Trend Vector The end of the trend vector displays approximately what the altitude will be in 6 seconds if the current rate of vertical speed is maintained Barometric Setting Box To set barometric pressure turn the BARO Knob to select the desired setting Altitude Alerting Within 1000 ft K 4000 Within 200 ft Deviation of 200 ft Figure 2 8 Altitude Alerting Visual Annunciations 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 An aural tone is heard when the aircraft is within 200 feet of acquiring the selected altitude or when deviating beyond 200 feet of the acquired selected altitude Barometric Minimum Descent Altitude The desired barometric minimum descent altitude MDA or Decision Height DH can be set in the Timer References Window Visual annunciations alert the pilot when approaching the MDA e When the aircraft altitude descends to within 2500 feet of the MDA setting the Barometric Minimum Box appears with the altitude in light blue text The bug app
99. ight the desired waypoint or airport 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 E Key followed by pressing the ENT Key twice If a missed approach point MAP is the current destination the approach will be canceled Manually Define the Direct to Course 1 Press the Direct to Key and enter a waypoint as discussed in previous steps or to edit the active direct to Turn the large FMS Knob to highlight the COURSE field Turn the FMS Knobs to select the desired course and press the ENT Key Press the ENT Key again to begin navigation using the selected destination and course Canceling Direct to Navigation 1 2 3 1 2 Press the Direct to G39 Key Press the MENU Key to display the Direct to options menu With Cancel Direct To NAV highlighted press the ENT Key If a flight plan is still active the G1000 resumes navigating the flight plan along the closest leg PAGE MENU OPT TONS Cancel Direct To NAV Press the FMS CRSR knob to return to bose page Figure 7 3 Canceling Direct to Navigation Direct to Navigation from the PFD WPT Symbol Identifier WPT Location Facility Name Flight Plan WPT Nearest WPT Bearing to WPT N 43 36 44 Lat Lon Distance from WPT wees Course to Selected WPT ACTIVATE Figure 7 4 PFD Direct to Window Press the Direct to
100. in G1000 Cockpit Reference Guide for the Columbia 350 400 12 9 SECTION 12 ANNUNCIATIONS amp ALERTS MFD amp PFD Message Advisories Message Comments S O DATA LOST Pilot stored data was The pilot profile data was lost System reverts to default pilot profile and settings lost Recheck settings The pilot may reconfigure the MFD amp PFD with preferred settings if desired XTALK ERROR A flight display The MFD and PFD are not communicating with each other The G1000 system should crosstalk error has occurred be serviced PFD1 SERVICE PFD1 needs service Return unit for repair The PFD and or MFD self test has detected a problem The G1000 system should be MFD1 SERVICE MFD1 needs serviced service Return unit for repair PFD1 CONFIG PFD1 configuration error Contig service req d The PFD and or MFD configuration settings do not match backup configuration MFD1 CONFIG MFD1 configuration memory The G1000 system should be serviced error Contig service req d SW MISMATCH GDU software The MFD and PFD have different software versions installed The G1000 system mismatch Xtalk is off should be serviced MANIFEST PFD1 software mismatch Communication halted The PFD and or MFD has incorrect software installed The G1000 system should be MANIFEST MFD1 software serviced mismatch Communication halted PFD1 COOLING PFD1 has poor cooling Reducing power usage The PFD and or MFD is overhe
101. indicator is centered and observe any maximum fuel imbalance limits ATI A condition has developed causing the roll servo to provide a sustained right force En o sure the slip skid indicator is centered and observe any maximum fuel imbalance limits Preflight Test Performing preflight system test Upon completion of the test the aural alert will be Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 P2 SECTION 12 ANNUNCIATIONS amp ALERTS 12 5 TAWS ALERTS Annunciations appear on the PFD and MFD Pop up alerts appear only on the MFD PFD MFD TAWS Alert Type Page Mua age bie Pop Up Alert Annunciation Excessive Descent Rate Warning EDR PULL UP Pull Up Reduced Required Terrain Clearance Warn PULL UP Terrain Terrain Pull Up Pull Up ing RTC or or Terrain Ahead Pull Up Terrain Ahead Pull Up Imminent Terrain Impact Warning ITI PULL UP Terrain Ahead Pull Up Terrain Ahead Pull Up or or TERRAIN PULL UP Terrain Terrain Pull Up Pull Up Reduced Required Obstacle Clearance PULL UP Obstacle Obstacle Pull Up Pull Up Warning ROC or or Obstacle Ahead Pull Up Obstacle Ahead Pull Up Imminent Obstacle Impact Warning IOI PULL UP Obstacle Ahead Pull Up Obstacle Ahead Pull Up or or Obstacle Obstacle Pull Up Pull Up Aural Message Reduced Required Terrain Clearance Caution RTC Caution Terrain Caution Terrain or Terrain
102. irport COM Frequency into the Active COM 1 With the Nearest Airports Window displayed turn either FMS Knob to place the cursor on the desired airport trequency shown in the window 2 Press the ENT Key and the selected frequency will be placed in the COM standby frequency field 3 Press the Frequency Transfer Key to make the frequency the active frequency Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 7 9 17 95 NEAREST INTERSECTIONS 136 975 NEAREST INT oo A NORTH UP os E E 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 View Information on the Nearest Intersection With the Nearest Intersections Page displayed press the FMS Knob to activate the cursor Turn either FMS Knob to select the desired intersection Press the FMS Knob to remove the flashing Cursor 17 95 SECTION 7 NAVIGATION 7 10 NEAREST NDB 136 975 ecT NAO NEAREST NDE Figure 7 12 Nearest NDB Page Select the Nearest NDB Page 1 2 Turn the large FMS Knob to select the NRST page group Turn the small FMS Knob to select the third rectangular page icon Access Information on a Specific NDB 1 2 With the Nearest NDB Page displayed press the FMS Knob to activate the cursor Turn either FMS Knob to select the
103. is subject to changes which could affect the accuracy and performance of all GPS equipment Portions of the Garmin G1000 utilize GPS as a precision electronic NAVigation AID NAVAID Therefore as with all NAVAIDs information presented by the G1000 can be misused or misinterpreted and therefore become unsafe WARNING To reduce the risk of unsafe operation carefully review and understand all aspects of the G1000 Pilot s Guide documentation and the Columbia 350 400 Pilot s Operating Handbook Thoroughly practice basic operation prior to actual use During flight operations carefully compare indications from the G1000 to all available navigation sources including the information from other NAVAIDs visual sightings charts etc For safety purposes always resolve any discrepancies before continuing navigation WARNING The illustrations in this guide are only examples Never use the G1000 to attempt to penetrate a thunderstorm Both the FAA Advisory Circular Subject Thunderstorms and the Airman s Information Manual AIM recommend avoiding by at least 20 miles any thunderstorm identified as severe or giving an intense radar echo CAUTION The GDU 1040 PFD and GDU 1042 MFD displays use a lens coated with a special anti reflective coating that is very sensitive to skin oils waxes and abrasive cleaners CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI REFLECTIVE COATING It is very important to clean the lens using a clean lint free c
104. isplay the Alerts Window IDENT Select to provide special aircraft position identification to Air Traffic Control ATC TMR REF Select to display the Timer References Window NRST Select to display the Nearest Airports Window ALERTS Select to display the Alerts Window s Ca Caro Caer mer ee CER A Press the BACK Softkey to return to the top level softkeys Co e Oe ee Ge Ged Ges Press the BACK A Softkey to return to the top level softkeys CO e Ee eo Ge nnonwg D Figure 1 6 PFD Softkey Flow Chart 3 1 8 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 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 Press the ENGINE Softkey to return to the default page level MAP A optional 350 only optional optional SECTION 1 SYSTEM OVERVIEW STRMSCP optional Selecting this softkey displays removes Stormscope lightning data on the Navigation Map NEXRAD optional Selecting this softkey displays removes precipitation data on
105. itches the standby and active COM frequencies Pressing and holding this key for two seconds automatically tunes the emergency frequency 121 5 MHz in the active frequency field 9 COM VOL SQ Knob Controls COM audio level Pressing this knob turns the COM automatic squelch ON and OFF Audio volume level is shown in the field as a percentage SECTION 1 SYSTEM OVERVIEW 10 Direct to Key Allows the user to enter a destination waypoint and establish a direct course to the selected destination specified by the identifier chosen from the active route or taken from the map pointer position 11 FPL Key Displays the active Flight Plan Page for creating and editing the active flight plan or for accessing stored flight plans 12 CLR Key DFLT MAP Erases information cancels an entry or removes page menus To display the Navigation Map Page immediately press and hold CLR MFD only 13 Dual FMS Knob Used to select the page to be viewed only on the MFD The large knob selects a page group MAP WPT AUX NRST while the small knob selects a specific page within the page group Pressing the small knob turns the selection cursor ON and OFF When the cursor is ON data may be entered in the different windows using the small and large knobs The large knob is used to move the cursor on the page while the small knob is used to select individual characters for the highlighted cursor location When the G1000 displays a lis
106. lay is displayed on the lett side of the MFD Manifold p Pressure Gauge s Tachometer Indicates Selected Fuel Tank a Indicates i Selected Fuel A Tank a r Fuel Quantity A 10 20 30 40 49 Indicator A 10 270 30 40 49 FFLOW GPH 15 8 FFLOW GPH 17 0 Y e A S q Fuel Flow a 3A Indicator 45 OIL PSI 51 OIL PSI 51 Oil Pressure Indicator l ELEV Oil Tempera OIL F TRIM o ELEY ture Indicator TRIM OIL F Bis Elevator Trim __ ide B TIT F Slide Bar eee 1429 Exhaust Gas Turbine Inlet Temperature Temperature Cylinder Head 378 Indicator Temperature f 7 I m A AILERON TRIM Aileron Trim h A Slide Bar AILERON TRIM bd Columbia 350 Columbia 400 Figure 3 1 Engine Instrument Display Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 a SECTION 3 ENGINE INDICATION SYSTEM EIS 3 2 3 1 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 Oxygen Quantity OXY QTY PSI Amount of remaining oxygen in terms of pressure Oxygen Outlet P
107. lert provides general information to the pilot A message advisory alert does not issue annunciations in the Annunciation Window Instead message advisory alerts only issue a flashing ADVISORY Softkey annunciation as shown in Figure 12 4 Selecting the ADVISORY Softkey acknowledges the presence of the message advisory alert and displays the alert text message in the Alerts Window 12 2 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 SECTION 12 ANNUNCIATIONS amp ALERTS 12 2 AIRCRAFT ALERTS See the Airplane Flight Manual for information regarding pilot responses WARNING Alerts Annunciation Window Text Alerts Window Message Audio Alert Voice Message Repeating Chime Door Open Fuel tank is not correctly selected Chime Fuel Valve or in OFF position CAUTION Alerts Columbia 350 only Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 ee SECTION 12 ANNUNCIATIONS amp ALERTS Annunciation Advisory Annunciation Window Text Alerts Window Message Audio Alert OXYGEN ON Reminder Turn off oxygen SPEED BRAKES Speed brakes are active Message Advisory Alerts Columbia 400 only 12 3 CO GUARDIAN MESSAGES Alerts Window Message Comments CO DET SRVC The carbon There is a problem within monoxide detector needs the CO Guardian that service requires services CO DET FAIL The carbon Loss of communication monoxide detector is inopera between
108. ling Agency 1 With the Nearest Airspace Page displayed select the FREQ Softkey to place the cursor in FREQUENCIES field 2 Turn either FMS Knob to select the desired frequency 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 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 SECTION 8 FLIGHT PLANNING The following discussions pertain to the Multi Function Display unless otherwise indicated 8 1 USER DEFINED WAYPOINTS Figure 8 1 User WPT Information Page Select the User WPT Information Page 1 2 Turn the large FMS Knob to select the WPT page group Turn the small FMS Knob to select the fifth rectangular page icon Create a New User Waypoint 1 With the User Waypoint Information Page displayed select the NEW Softkey A waypoint is created at the current aircraft position Turn the small FMS Knob to enter first character of the waypoint name Turn the large FMS Knob to move the cursor to the next character field 8 SECTION 8 FLIGHT PLANNING Repeat steps 2 and 3 until the desired name is entered Press the ENT Key Press the ENT Key a again to accept the new waypoint identifier The cursor is now in the REFERENCE WAYPOINTS field If desired the waypoint can be defined by a reference waypoint Turn the FMS Knobs to enter the position coordinates or the radial
109. lly establish the desired airspeed using the control wheel When the CWS button is released the current airspeed will be maintained now displayed in green in the Active Mode 5 Adjust engine power to allow the autopilot field and the Airspeed Bug will appear on the to fly the aircraft at a pitch attitude which Airspeed Indicator Pitch commands are given corresponds to the selected airspeed and the to manually maintain airspeed Press the AP desired flight profile descent or climb Key to engage the autopilot for maintaining 6 With Altitude Hold mode armed as the selected the current airspeed altitude is reached ALT will flash in green Altitude Hold mode is automatically armed with for 10 seconds in the Acitve Mode field after ALT displayed white in the Armed Mode field which the annunciation stops flashing This to the right of the FLC annunciation signals the altitude capture is complete and The Airspeed Bug can be adjusted in 1 knot the selected altitude will be maintained at the increments by pressing the NOSE UP NOSE DN selected airspeed i oniy Mie gnt ueo Keys to set the desired airspeed The airspeed engaged pitch commands ae i setting will be displayed in the Selected manually maintain the selected altitude Airspeed Reference Flight Level Change mode is active 113 68 ww2 108 00 117 95 Selected Airspeed PFD Altitude Hold mode is armed 123 800 135 325 corz Selected Altitude 199A
110. loth and an eyeglass lens cleaner that is specified as safe for anti reflective coatings Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 WARNINGS CAUTIONS amp 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 However clusters of two or more discharge points in the strike display mode do indicate thunderstorm activity if these points reappear after the screen has been cleared NOTE All visual depictions contained within this document including screen images of the G1000 panel and displays are subject to change and may not reflect the most current G1000 system Depictions of equipment may differ slightly from the actual equipment NOTE This device complies with part 15 of the FCC Rules Operation is subject to the following two conditions 1 this device may not cause harmful interference and 2 this device must accept any interference received including interference that may cause undesired operation NOTE This product its packaging and its components contain chemicals known to the S
111. n 29 92 inches of mercury 1013 hPa by selecting the METRIC Softkey Window BACK Select to return to the previous level softkeys ALERTS Select to display the Alerts Window A Press the DFLTS Softkey to change the PFD Press the STD BARO or BACK Softkeys metric values to standard to return to the top level softkeys Figure 1 5 PFD Softkey Flow Chart 2 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 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 VORI 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 CODE Select to display transponder code selection softkeys 0 7 0 through 7 Select numbers to enter code IDENT Select to provide special aircraft position identification to Air Traffic Control ATC BKSP Select to remove numbers entered one at a time BACK Select to return to the previous level softkeys IDENT Select to provide special aircraft position identification to Air Traffic Control ATC BACK Select to return to the previous level softkeys ALERTS Select to d
112. n With the Airport Information Page displayed press the FMS Knob to activate the cursor Turn the large FMS Knob to place the cursor on the RUNWAYS identifier field Turn the small FMS Knob to display the next runway for the selected airport Continue turning the small FMS Knob to select the desired runway To remove the flashing cursor press the FMS Knob Access Frequency Information 1 2 3 5 With the Airport Information Page displayed press the FMS Knob to activate the cursor Turn the large FMS Knob to move the cursor to the Frequencies box Turn either FMS Knob to scroll through the list placing the cursor on the desired frequency It a listed frequency has sector or altitude restric tions the frequency is preceded by an info i designation Press the ENT Key to view the information The following may be displayed with the frequency TX transmit only RX receive only PT part time frequency Press the ENT Key to place the selected fre quency in the standby field of the COM or NAV To remove the cursor press the FMS Knob Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 1 3 SECTION 7 NAVIGATION 7 4 INTERSECTION INFORMATION Select the Intersection Information Page Turn the large FMS Knob to select the WPT page group Turn the small FMS Knob to select the second rectangular page icon 136 975 Figure 7 6 Int
113. nce Guide for the Columbia 350 400 SECTION 12 ANNUNCIATIONS amp ALERTS e Audio Alerting System The G1000 system issues audio alert tones when specific system conditions WARNI NG 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 A warning alert is accompanied by an annunciation in the Annunciation Window Warning text appearing in the Annunciation Window is RED A warning alert is also accompanied by a flashing WARNING Soitkey annunciation as shown in Figure 12 2 Selecting the WARNING Softkey acknowledges the presence of the warning alert and stops the aural tone if applicable DYI SORY e CAUTION This level of alert indicates the Figure 12 4 ADVISORY Softkey existence of abnormal conditions on the aircraft Annunciation that may require pilot intervention A caution alert is accompanied by an annunciation in the Annunciation Window Caution text appearing in the Annunciation Window is YELLOW A caution alert is also accompanied by a flashing CAUTION Softkey annunciation as shown in Figure 12 3 Selecting the CAUTION Softkey acknowledges the presence of the caution alert Figure 12 3 CAUTION Softkey Annunciation e MESSAGE ADVISORY This level of a
114. nent of Approach ial AROUND The default pitch axis mode is Pitch Hold PIT When no other pitch axis modes are selected this is the active pitch axis mode when the autopilot and or flight director is engaged Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 6 3 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 reterence depending on which key is pressed Pitch Hold mode is active nev1 113 88 118 98 ITXD wer NAW 118 98 ITxD Flight Director command bars maintain desired pitch reference 2 Altitude Hold mode is automatically armed with ALT displayed white in the Armed Mode field to the right of the PIT annunciation 3 Pitch attitude can be adjusted in 0 5 degree increments by pressing the NOSE UP NOSE DN Keys 4 Aircraft pitch may also be changed by pressing and holding the CWS button to manually establish the desired pitch using the control stick When the CWS button is released the current pitch angle will be maintained 5 If desired enter an altitude in the Selected Altitude Box by turning the ALT Knob As the selected altitude is reached ALT will flash in green for 10 seconds in the Acitve Mode field after which the annunciation stops flashing This
115. neous Message Advisories Cont Alerts Window Message Comments S Special use airspace is near and ahead of the aircraft position than 2 nm not be smooth Prepare for steep turns ahead and expect noticeable course deviations active proach when required sequence mode deactivate the OBS mode frequency for approach receiver Select the correct frequency for the approach approach to the correct NAV receiver TRAFFIC FAIL Traffic device has The G1000 is no longer receiving data trom the traffic system The traffic device failed should be serviced Ta Pel a Stormscope has failed The Stormscope system should be serviced BACKUP PATH Stormscope using Stormscope is using the backup communication path The G1000 system should be backup path serviced when possible NO WGS84 WPT Non WGS 84 The selected waypoint xxxx does not use the WGS 84 datum Cross check position waypoint for navigation xxxx with alternate navigation sources 12 18 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 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 Po
116. ng GAL USED Measured fuel quantity has no effect on fuel calculations Fuel calculations are based on sensed fuel flow and the last manual adjustment of the fuel remaining NOTE When full the Columbia 350 400 has 98 gallons of usable fuel The following softkeys allow for adjustment of the remaining fuel quantity DEC FUEL Allows the pilot to decrease the gallons of fuel remaining GAL REM in 1 gallon increments INC FUEL Allows the pilot to increase the gallons of fuel remaining in l gallon increments RST FUEL Resets the fuel remaining to 98 gallons 3 6 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 SECTION 4 NAV COM amp TRANSPONDER SECTION 4 NAV COM AND TRANSPONDER The NAV COM controls and frequency boxes are located on the Primary Flight Display and the Multi Function Display in the same locations Operations in the following discussions may also be performed with the corresponding controls on the MFD PFD Control Unit NAV COM Controls NAV Frequency Box COM Frequency Box Controls navi 108 08 117 95 wT KSUS Ag RK e03 118 000 con 18 00 117 95 fF oo GIS JU conz 3 CRS4 BARO PUSH CAS CTA RANGE a 4 b War POE cL 02 112 i Figure 4 1 G1000 VHF NAV COM Controls PFD Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 4 1 SECTION 4 NAV COM amp TRANSPONDER Standby NAV Selected NAV Selected COM Standby COM Frequency Field
117. ng the PFD if another flight plan is active 2 Select the NEW Softkey to display a blank flight plan window for the first empty storage a location A NOTE After the first leg is entered using the PFD only it is immediately activated 1 Press the FPL Key then press the FMS Knob to activate the cursor 2 Turn the small FMS Knob to enter the first letter Figure 8 10 Create FPL on MFD of the destination waypoint identifier Turn the n T O ah large FMS Knob to the right to move the cursor 3 Turn E FMS Kno ce Giepicy Wie to the next character position Waypoint Information Window l 3 Repeat step 2 to spell out the rest of the 4 Turn the small FMS Knob to enter the first P E a ypoint identifier character of the identifier of the departure l waypoint 4 Press the ENT Key and the cursor is now ready for entering of the next flight plan waypoint 5 Turn the large FMS Knob to move the cursor to iain the next character field Repeat steps 4 and 5 5 Repeat steps 2 through 4 to enter the identifier until the desired identifier has been entered for each additional flight plan waypoint 6 Once all waypoints have been entered press foe FACILITY ETY the FMS Knob remove the cursor The new flight plan is now active a Figure 8 11 Waypoint Info Window 6 Press the ENT Key Figure 8 12 Creating Flight Plan on the PFD 7 Repeat steps 3 through 5 to enter the identifier for each additional flight plan waypoint 8 When all waypoints ha
118. nly be used for situational awareness Any map display indication should be compared with approved navigation sources Figure 7 1 Navigation Map Page SECTION 7 NAVIGATION 7 2 DIRECT TO NAVIGATION Direct to Navigation from the MFD DIRECT TH Identifier aA r Symbol Facility Name MIAMI INTL City MIAMI FL Flight Plan Field Erer Nearest Airport Map Orientation Map of the Selected Waypoint Map Range Bearing Region Distance Latitude Longitude o Activate Field ourse Figure 7 2 MFD Direct to Window Enter a Direct to Destination 1 Press the Direct to G39 Key 2 Turn the small FMS Knob to enter the first letter of the destination waypoint identifier Turn the large FMS Knob to the right to move the cursor to the next character position 3 Repeat step 2 to spell out the rest of the waypoint identifier 4 Press the ENT Key to confirm the identifier The Activate field is highlighted 5 Press the ENT Key to activate Select a Direct to Destination to a Flight Plan Waypoint or Nearest Airport 1 While navigating an active flight plan press the Direct to GE Key 2 Turn the large FMS Knob to highlight the FPL NRST WAYPOINT field Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 7 1 SECTION 7 NAVIGATION 3 4 5 Turn the small FMS Knob to display a list of waypoints or airports Continue turning the small FMS Knob to scroll through the list and highl
119. o 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 Reduced Required Terrain Clearance RTC and Reduced Required Obstacle Clearance ROC This provides alerts when the aircraft flight path is above terrain and or obstacles yet is projected to come within minimum clearance values outlined in the following table When an RTC or ROC alert is issued a potential impact point is displayed on the TAWS Page as a yellow or red X Imminent Terrain Impact ITI and Imminent Obstacle Impact 101 This provides alerts when the aircraft is below the elevation of terrain in the aircrafts projected path ITI and IOI alerts are accompanied by a potential impact point displayed on the TAWS Page as a yellow or red X The alert is given when the projected vertical flight path is calculated to come within minimum clearance altitudes in the following table Manual System Test A system test is automatically performed at power up After sucessful completion of the test TAWS System Test OR will be heard The system test may also be initiated manually but only when the aircraft is on the gr
120. oftkey to display a 120 viewing area Select the CLEAR Softkey to remove all Stormscope lightning data trom the display XM WEATHER OPTIONAL WARNING XM Weather is not intended to be used for hazardous weather penetration Weather information provided by XM Radio Service is approved only for weather avoidance not penetration 1 Select the MAP Softkey 2 Select the NEXRAD or XM LTNG Softkey to display the desired weather Select the applicable softkey again to remove weather data from the Navigation Map Page __ 136 975 roe MINNEAPOLIS WORTH LP Figure 10 7 Navigation Map Page Displaying NEXRAD Weather SECTION 10 HAZARD AVOIDANCE Displaying METAR and TAF information on the Airport Information Page Display METAR and TAF text on the Airport Information Page 1 Turn the large FMS Knob to select the WPT Page Group 2 Turn the small FMS Knob to select the Airport Information Page 3 Select the WX Softkey to display METAR and TAF text METAR and TAF information is updated every 12 minutes NORTH UP __arRPOR pL pe PUBLIC WU KMSP MINNEAPOLIS ST PAUL INTL MINNEAPOLIS MN DEW POINT 14 E ALTIMETER 29 721N CCTASh BENTSE FMB460 296Q5KT P6 amp SM WX Softkey Figure 10 8 METAR and TAF Text Displayed on the Airport Weather Information Page Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 10 3 SECTION 10 HAZARD AVOIDANCE Displaying We
121. ossible GCU PATH A GCU path has failed The GCU 476 is using a backup communications data path The G1000 system should be serviced when possible 12 16 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 SECTION 12 ANNUNCIATIONS amp ALERTS Miscellaneous Message Advisories Alerts Window Message Comments S 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 way point 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 Remove the waypoint from the flight plan if it no longer exists in any database OR update the waypoint name identitier to reflect the new information FPL WPT MOVE Flight plan The system has detected that a waypoint coordinate has changed due to a new waypoint moved aviation database update Verity that stored flight plans contain correct waypoint locations TIMER EXPIRD Timer has expired The system notifies the pilot that the timer has expired DB CHANGE Database changed This occurs when a stored flight plan contains procedures that have been manually Verify user modified procedures edited This alert is issued only after an aviation database update Verity that the user moditied procedures in stored flight plans are correct and up to date
122. ound To manually verity proper operation of the aural and visual annunciations of the system perform the following steps 1 While the TAWS Page is displayed press the During the final approach phase of flight RTC ROC ITIIOI alerts are automatically inhibited when the aircraft is below 200 feet AGL while within 0 5 nm of the approach runway or is below 125 feet AGL while within 1 nm of the runway a Premature Descent Alert PDA 2 Turn the small FMS Knob to select Test EN eer aoe TAWS A Premature Descent Alert is issued when the system 3 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 Forward Looking Terrain Avoidance FLTA The Forward Looking Terrain Avoidance alert is composed of two sub functions detects that the aircraft is significantly below the normal approach path to a runway The PDA alert mode functions only during descent to land PDA alerting begins when the aircraft is within 15 nm of the destination airport and ends when the aircraft is either 0 5 nm from the runway threshold OR is at an alti tude of 125 feet AGL while within 1 nm of the threshold During the final descent algorithms will set a threshold Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 for alerting based on speed distance and other param eters 700 Runway Threshold PDA Alerting Area
123. ow the location elevation and direction the highest radar echo This may not indicate the top of a storm or clouds only the highest radar return echo ECHO TOPS cannot be displayed along with NEXRAD and CLOUD TOPS When ECHO TOPS is activated NEXRAD and CLOUD TOPS are removed Refer to the Legend for a description of the ECHO TOPS coding The display is updated every 7 5 minutes CLD TOP Select the CLD TOP Softkey to show the cloud top altitude determined from satellite imagery The display is updated every 15 minutes LING Selecting the LING Softkey shows the location of cloud to ground lightning strikes The display is updated every five minutes NOTE Strikes depicted represent cloud to ground strikes within a 2 kilometer radius of the actual strike location Therefore the exact location of the strike is not displayed Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 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 The display is updated every 12 minutes METAR Select 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 MORE WX Select the MORE WX Softkey to display the following group
124. p ALERTS 12 1 12 1 Alert Level Definitions 0 00 0 ee 12 2 12 2 Aircraft Alerts 0 0 cccccseseseeseeeaean 12 3 WARNING AICS ossunsararisaananaa 12 3 CAUTION ACRES sscassitisaessanaxcssharerimnanciinarewaerns 12 3 Annunciation ACVISOLY scesscessessseestesstesstesssesneeseeseen 12 4 Message Advisory Alerts sssssscsesssssssessessessneeen 12 4 12 3 CO Guardian Messages cccceeeeen 12 4 12 4 APCS ALOIS 5 sscesiciczlercicecaserannnaienraneuneass 12 5 System Status ANMUNCIATION cccsssssesssesesseseeeen 125 12 5 TAWS ALERIS 00aeieeerren 12 6 TAWS System Status Annunciations s es 12 7 12 6 G1000 System Annunciations 0 0008 12 7 12 7 G1000 System Message Advisories 12 9 MFD amp PFD Message AdVISOTICS ccscesseeseseeseesen 12 10 Database Message AdVISOFES c sscsseseeseseeseeseen 12 11 GMA 1347 Message Advisories ccsscescecseesteeseeseen 12 12 GIA 63 Message Advisories cssscessesssesseeseesesseean 12 12 GEA 71 Message Advisories scesccsceseeseeseeseeseen 12 14 GTX 33 Message Advisories 12 15 GRS 77 Message Advisories 12 15 GMU 44 Message Advisories scesseeseseeseesesseeen 12 16 GDL 69 Message Advisories 12 16 GDC 74A Message Advisories 12 16 GCU 476 Message Advisories 12 16 Miscellaneous Message AdVISOFES c sseeseees 12 17 INDE K aune T Index 1 iV Garmin G1000 Cockpit Reference G
125. p Up 10 14 Altitude alerting 2 4 Altitude Hold 1 4 Altitude hold 1 4 6 3 6 8 6 10 Altitude trend vector 2 4 ALT knob 1 4 Annunciations 12 1 AP 1 4 1 5 6 1 6 7 6 9 12 5 Approaches 9 2 Approach activation 4 3 Approach markers Signal augmentation 5 3 Approach Mode 6 12 AP disconnect 6 1 Arc HSI 2 6 Arrivals 9 1 Attitude indicator 2 3 Audio alerting system 12 2 Audio panel 4 3 5 1 Audio panel controls COM 1 2 5 2 Auto tuning 4 3 Automatic squelch 4 3 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 Autopilot 6 1 6 2 6 3 6 5 6 10 6 12 6 13 12 5 Aviation database 1 11 Backcourse 6 11 Barometric setting 2 4 Base reflectivity 10 4 BKSP softkey 4 4 BRG1 2 7 BRG2 2 7 C Carbon monoxide 3 2 Caution 12 1 12 2 CDI 2 8 12 18 Cell 10 2 Cell mode 10 2 Cell movement 10 5 Cloud tops 10 4 CLR key 1 3 1 5 Coast mode 10 7 Codes important 4 4 Code selection 4 4 CODE softkey 4 4 COM Frequency Window 4 1 COM knob 4 3 Controls 1 2 4 1 Control Wheel Steering 6 1 6 3 Create a new flight plan 8 4 Create a new user waypoint 8 1 CWS 6 1 6 3 6 9 Cyclones 10 5 D Departures 9 1 Direct to 7 1 Dual CDU failure 11 2 E ECHO TOPS 10 4 Edit a flight plan 8 5 INDEX EDR 10 13 Emergency code 4 4 Endurance 3 6 Excessive Descent Rate 10 13 F FD 1 4 1 5 12 5 Five Hundred Aural Alert 10 13 FLC 1 4 6 3 6 7 Flight director 6 1 6 4 6 6 6 10 Fli
126. requency selected by the tuning box COM1 135 675 35 VOLUME Figure 4 6 COM Volume Level 4 3 AUTOMATIC SQUELCH Automatic squelch can be disabled for a COM radio by pressing the COM Knob to place the tuning box on the desired COMS standby frequency then by pressing the VOL PUSH SQ Knob SECTION 4 NAV COM amp TRANSPONDER 4 4 QUICKLY ACTIVATING 121 500 MHZ Pressing and holding the COM Frequency Transfer Key for approximately two 2 seconds automatically tunes the selected COM radio to the emergency frequency 4 5 FREQUENCY AUTO TUNING Auto tuning on the PFD NEAREST AIRPORTS 124 6 8NM VFR 122 700 RNWY 244 FT 270 1 2NM ILS 123 000 RNWY 57 FT 150 11 4NM ILS 133 000 RNWY 7339FT Figure 4 7 Nearest Airports Window PFD 1 Select the NRST Softkey to display the Nearest Airports Window 2 Turn either FMS Knob to highlight the desired frequency 3 Press the ENT Key to place the frequency in the standby field of the active COM 4 Press the Frequency Transfer Key to place the frequency in the active field NAV frequencies are entered automatically in the active NAV frequency field upon approach loading or approach activation Auto tuning on the MFD Auto tuning on the MFD is done in much the same way as on the PFD Use the FMS Knobs to select the desired frequency on any of the information pages Pressing the ENT Key then loads the selected frequency in the tuning box as a standby frequency
127. ress the ENT Key The FREQUENCY field is now highlighted If desired press the ENT Key to place the frequency in the NAV receiver standby field SECTION 7 NAVIGATION 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 Press the FMS Knob to remove the flashing Cursor 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 17 95 136 975 NORTH UP Fa lt NEAREST AIRPORTS ee 221 f pi j W o3 INFORMATION y RNWY FREQ APR Figure 7 9 Nearest Airports Page Nearest Airport Information on the MFD Select the Nearest Airports Page 1 Turn the large FMS Knob to select the NRST page group 2 Turn the small FMS Knob to select the first rectangular page icon Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 l3 SECTION 7 NAVIGATION 1 6 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 Access Runway In
128. ressure OXY OUTLET PSI Oxygen outlet pressure in pounds per square inch psi Oil Tempera Oil Pres Manifold ture sure Pressure Gauge Gauge Gauge AS 203 49 9 Trim Correct takeoff aileron and elevator trim positions are indicated by the green boxes Carbon Monoxide Detection If carbon monoxide in the cabin becomes too high above 50 ppm a flashing annunciation will be displayed in the lower left of the EIS System Display as shown in Figure 3 2 The current amount of CO is displayed in parts per million A warning annunciation will also be displayed on the PFD in the Annunciations Window and an aural warning will be generated Oxygen Quantity Gauge Tachometer Oxy v 1600 MAN IN HG 21 3 15 20 10 250 a 5 Eaa fal S E ENDUR T Oxygen Outlet j o Gauge BEANT es Lat ype A as Pressure Gauge F 17 f 8 8 GAL USED RANGE NM p Cal r L FUEL QTY GAL R FUEL QTY GAL 0 4 0 eand a TEMPERATURE ELECTRICAL Group EGT F HT F 1710 16901612 1437 an 1437 362 378 360 ALT AMPS BATT AMPS BUS VOLTS sean 1052 1748 1630 son 304 372 370 37 199 1750 BETTEN A m Trim Group Engin Tem one po aa roup 1450 1300 1300 1158 1158 my 1900 1606 A eS Zs 43 AILERON TRIM CO LVL HIGH PPM 32 0 Figure 3 2 EIS Display Columbia 400 shown Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 SECTION 3 ENGINE INDICATION SYSTEM EIS 3 2 ENGINE LEANING ASSIST DISPLAY 3 Lean
129. roach field Turn the small FMS Knob to display a list of available approaches Figure 9 5 Select Arrival Runway 8 With LOAD highlighted press the ENT Key If a flight plan is active the selected arrival procedure is inserted after the destination airport and becomes part of the active flight plan If no flight plan is active when the arrival is loaded the arrival procedure will become the active flight plan 9 2 APPROACHES Not all approaches in the database are approved for GPS Figure 9 6 Selecting an Approach Procedure as a ee aoe ae cen 5 Turn either FMS Knob to highlight the desired the right of the procedure name indicates the procedure can be flown using the GPS receiver Some procedures apical cee Key will not have this designation meaning the GPS receiver can be used for supplemental navigation guidance only 9 2 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 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 Turn the large FMS Knob to highlight Activate and press the ENT Key to activate the approach Selecting Load will add the procedure to the flight plan wit
130. rom government agencies Garmin accurately processes and cross validates the data but cannot guarantee the accuracy and completeness of the data NOTE Obstacles 200 and higher are included in the obstacle database It is very important to note that not all obstacles are necessarily charted and therefore may not be contained in the obstacle database These databases are not stored internally in the MFD or PFD Supplemental Data Cards containing identical database versions must be kept in both displays to retain terrain and obstacle data A Supplemental Data Card should be inserted into the bottom card slot of the PFD and MFD NOTE If the Supplemental Data Card is removed from the display the TOPO and TER RAIN softkeys are not functional and are grayed out on the MFD Map Page 1 Insert one card in the bottom card slot of the MFD and one in the bottom card slot of the PFD 2 Apply power to the G1000 System View the MFD power up splash screen Check that the Terrain and Obstacle databases are initialized and displayed on the scrolling window of the splash screen Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 SECTION 1 SYSTEM OVERVIEW 1 12 3 4 5 Acknowledge the Power up Page agreement by pressing the ENT Key or the right most softkey 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 Po
131. s manual are centered around using the controls on the PFD and or MFD When reading these discussions keep in mind that many of the operations may also be performed on the GCU 476 OO OC RANGE De MENU iJ FMS g NAV COM 1 q PROC yo _ PUSH 1 2 CRSA_ ee ae 5 MFD EMERG Figure 1 2 MFD PFD Control Unit GCU 476 1 FPL Key Displays the active Flight Plan Page for creating and editing the active flight plan 2 Direct to Key Allows the userto enter a destination waypoint and establish a direct course to the selected Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 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 Ifa flight plan is used available procedures for the departure and or arrival airport are automatically suggested and can be loaded into the active flight plan Ifa flight plan is not used both the desired airport and the desired procedure may be selected 5 Joystick Changes the map range distance top to bottom of map display when rotated activates the
132. ssed approach KRHV se 070 33 0 X 2 Clovis VORTAC o CZQ Panoche gt VORTAC 8 GV PXN Figure 6 19 Flight Plan Overview Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 6 13 SECTION 6 AUTOMATIC FLIGHT CONTROL Departure Climb to the selected altitude and fly an assigned heading 1 Upon takeoff set the Selected Altitude to 7000 feet using the ALT Knob To have the autopilot capture this altitude use Pitch Hold Vertical Speed or Flight Level Change Mode In this example Vertical Soeed Mode is used 2 Upon reaching the desired vertical speed of 1000 fom enable the flight director in Vertical Speed Mode a Press the VS Key Altitude Hold Mode is armed automatically PS ROL i ALT b Press the AP Key to engage the autopilot in Roll Hold and Vertical Soeed modes a ROL AP ALT e HDG Mode Selected Altitude of 7 000 MSL 3 Activate Heading Select Mode while the autopilot is engaged in the climb a Use the HDG Knob to set the Selected Heading to 070 b Press the HDG Key The autopilot follows the Heading Bug on the HSI and turns the aircraft to the desired heading _ HDG JAP ALT 4 As the aircraft climbs to the Selected Altitude the flight director changes from Vertical Speed to Altitude Hold Mode This active mode change is indicated by the green ALT annunciation flashing for ten seconds 5 Upon reaching the
133. st Intersections ccc l 1 Select the Nearest Intersections Page 7 7 View Information on the Nearest Intersection 1 1 7 10 Nearest NDB 000 cscs l 1 Select the Nearest NDB Page scssessesseseeressesseean 1 1 Access Information on a Specific NDB l 1 7 11 Nearest VOR 1 8 Select the Nearest VOR Page c ssessessessseseesessessean 1 8 View Information on the Nearest VOR 1 8 Select and Load a VOR FreQUENCY tessesseesseesseesseeen 1 8 7 12 Nearest User Waypoint 0 0 0 cccceeeeen 1 8 Select the Nearest User Waypoint Page 1 8 Select a Nearest User Waypoint tesseessesesesreeen 1 8 7 13 Nearest Frequencies 0 c ccc 1 9 Select the Nearest Frequencies PaQe cssessesresseeen 7 9 Select and Load the Nearest ARTCC FSS or AT T a 1 9 7 14 Nearest Airspace 7 9 Select the Nearest Airspaces Page 7 9 Airspace Alerts BOK ccs ecassseoacesostmasscuseromessaxanenls 7 9 View Additional Details for a Listed Airspace 7 10 View and Quickly Load the Frequency for a CONTOS AGEN Diaea 7 10 SECTION 8 FLIGHT PLANNING 000000000 8 1 8 1 User Defined Waypoints 0 0 c cece 8 1 Select the User WPT Information Page scseseseen 8 1 Create a New User Waypoint 8 1 Modify a User Waypoint cescescssessesesseeseeressen 8 1 Delete a User Waypoint sssssssssssssssssssssssssrrrrnreeenn 8 1 Create User Waypoints from the Navigation aD Pade EELE
134. sure that the data card is properly inserted Replace data card If problem persists The G1000 system should be serviced The MFD and or PFD detected a failure in the airport terrain database Ensure that the data card is properly inserted Replace data card If problem persists The G1000 system should be serviced DB MISMATCH Terrain database The PFD and MFD have different terrain database types installed Crossfill is off type mismatch Xtalk is off Install correct terrain database type in both displays DB MISMATCH Obstacle database The PFD and MFD have different obstacle database versions installed Crossfill is off version mismatch Xtalk is off Install correct obstacle database version in both displays Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 12 11 SECTION 12 ANNUNCIATIONS amp ALERTS Database Message Advisories Cont Alerts Window Message Comments S O DB MISMATCH Airport Terrain The PFD and MFD have different airport terrrain databases installed Crosstill is off database mismatch Xtalk is off Install correct airport terrain database in both displays GMA 1347 Message Advisories Alerts Window Message Comments S GMA1 FAIL GMAT is inoperative The audio panel self test has detected a failure The audio panel is unavailable The G1000 system should be serviced GMA1 CONFIG GMA1 configuration The audio panel configuration settings do not match backup configuration memory
135. t 1 Enter Flight Level Change Mode director changes trom Flight Level Change to Altitude Hold Mode The annunciation ALT a Using the ALT Knob set the Selected Altitude flashes in green to indicate the altitude capture to 3000 feet After the capture is complete the autopilot holds b Press the FLC Key to activate Flight Level the aircraft level at the Selected Altitude Change Mode The annunciation FLC appears next to the Airspeed Reference ARLES CTSA RECT e which defaults to the current aircraft airspeed 142 knots Altitude Hold Mode is armed automatically J GPS AP TALT Cruise Altitude of 7 000 MSL 3 Selected Altitude of 3 000 MSL ALT Hold Mode Figure 6 23 FLC Descent Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 6 17 SECTION 6 AUTOMATIC FLIGHT CONTROL ILS Approach 1 Transition trom GPS Navigation Mode to Heading Select Mode a Load the Runway 29R ILS approach for KFAT into the Flight Plan b Select Vectors to Final for the transition c Set the Selected Heading after getting vectors from ATC and press the HDG Key The autopilot turns the aircraft to the desired heading 2 Use Heading Select Mode to comply with ATC vectors as requested 3 In preparation for approach tune the localizer frequency and select LOC mode on the HSI 4 Press the APR Key when cleared for approach to arm the Approach Mode LOC and GS appear in the arm
136. t that is too long for the display screen a scroll bar appears along the right side of the display indicating the availability of additional items within the selected category Press the small FMS Knob to activate the cursor and turn the large FMS Knob to scroll through the list 14 MENU Key Displays a context sensitive list of options This list allows the user to access additional features or to make setting changes that relate to certain pages 15 PROC Key Selects approaches departures and arrivals from the flight plan If a flight plan is used available procedures for the departure and or arrival airport are automatically suggested If a flight plan is not used the desired airport and the desired procedure may be selected This key selects IFR departure procedures DPs arrival procedures STARs and approaches IAPs from the database and loads them into the active flight plan Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 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 Itis 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 Altitude Select is used by the Automatic Flight Control System in certain modes in addition to the standard
137. tate of California to cause cancer birth defects or reproductive harm This notice is being provided in accordance with California s Proposition 65 If you have any questions or would like additional information please refer to our web site at www garmin com prop65 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 RECORD OF REVISIONS Part Number Change Summary 190 00567 00 Production release Revision Date of Revision fected Pages A 3 06 i Index 4 Production release B 6 06 i Index 4 Added Columbia 350 parameters TAWS changes and Stormscope Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 RR RECORD OF REVISIONS Blank Page RR Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 SECTION 1 SYSTEM OVERVIEW 000000 00000 1 1 1 1 PFD MFD Conttols 0 ccccccceseseseeseenees 1 2 1 2 GCU 476 Controls ccs 1 4 1 3 PED SOTMKGYS 2 6 ccssencecensenantionparenienxss 1 6 1 4 MFD Softkeys occas 1 9 1 5 MFD Page Groups cscs 1 10 1 6 Backlighting 0 0 cc ccc cesses teas 1 10 1 7 Database Updates sees 1 11 Aviation Database Update sccseseseseseereeren 1 11 Terrain and Obstacle Database Updates 1 11 SECTION 2 FLIGHT INSTRUMENTS 00000 2 1 2 1 Airspeed IndicatOl 0 cccccccs sess 2 3 speed Indications 2 3 Speed RaNOE Sisuke A 2 3 Airspeed Trend VeCtor snoren aano 2 3 Vspeed RETEreNCeS sopita 2 3 2 2
138. the distance between the antennas and the separa tion of the tuned frequencies Figure 5 3 Split COM Function Pressing the COM 1 2 Key selects and deselects the split COM function During split COM operation the COMI COMI MIC COM2 and COM2 MIC Keys are active When the COM 1 2 Key is selected COM1 is used by the pilot for transmission and COM2 is used by the copilot The COMI MIC annunciator blinks when the pilot s Push to talk is pressed and the COM2 MIC annunciator blinks when the copilot s Push to talk is presssed In this mode both the pilot and the copilot can transmit simultaneously over separate radios The pilot can still monitor NAV1 NAV2 and MKR audio as selected but the copilot is only able to monitor COM2 5 3 MARKER BEACON RECEIVER The marker beacon receiver is always on Only the marker beacon audio can be turned off Figure 5 4 shows the marker beacon annunciators on the PFD When the MKR MUTE Key is pressed the key annunciator is lit and the audio tone can be heard over the speaker or headsets during marker beacon reception When the tone is active pressing the MKR MUTE Key once mutes the audio but does not affect the marker annunciator The audio returns when the next marker signal is received To turn off the marker beacon audio press the MKR MUTE Key once when there is no marker indication present or press twice when an indication is present The key annunciator will be extinguished when t
139. 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 If no flight plan is active use the FMS Knobs to enter the identifier of the desired airport Press the ENT Key Turn the large FMS Knob to highlight the Departure field Turn the small FMS Knob to display a list of available departures Turn either FMS Knob to select the desired departure and press the ENT Key AIRPORT KTZD y PUBLIC HEH CENTURY ATRCENTER OLATHE KS DEPARTURE CHIEFS Figure 9 1 Select Departure A list of runways may be displayed for the departure Turn either FMS Knob to select the desired runway and press the ENT Key A list of available transitions is displayed for the departure Turn either FMS Knob to highlight the desired transition waypoint and press the ENT Key 8 SECTION 9 PROCEDURES DEPARTURE CHIEFS RUNWAY ALL TRANSITION CATTS Figure 9 2 Select Departure Transition With LOAD highlighted press the ENT Key The departure will be active when the flight plan is active Load and Activate An Arrival Procedure 1 2 With the Navigation Map Page displayed press the FPL Key Select the LD STAR Softkey If a flight plan is active the destination airport will be displayed as the default A list of available arrivals is also displayed If no flight plan is active use the FMS Knobs to enter the identifier
140. the last peaking cylinder as shown in Figure 3 4 FFLOW GPH TEMPERATURE GEF 1426 1438 1366 4 pea 1g00 1490 1402 1374 15 1750 ate 3 1666 1450 1300 1150 1000 Indicates Last Cylinder to Peak Monitor the A Peak temperature and continue leaning the mixture until reaching the value indicated in the Columbia Airplane Flight Manual AFM Selecting the ASSIST Softkey returns the MFD to the EIS Display Selecting the SYSTEM Softkey exits the Assist Display and returns the MFD to default operation Indicates Difference Between Present and Peak Temperature of the Last Peaked Cylinder CHT F 378 378 372 380 352 gt 00 aot i 300 200 f 100 1 A3456 Figure 3 4 Engine Leaning Assist Display Last Peaked Cylinder Columbia 350 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 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 Indicates Peak TIT Temperature FFLOW GPH ri TEMPERATURE BTF 1706 1571 1634 m 1616 1651 1589 pei 1750 1600 TIT Delta Value LEAN Difference from Peak FEF 1472 1436 1966 1606 sis 1450 13
141. the mixture until one of the cylinder s exhuast temperature peaks This is indicated Engine Leaning for the Columbia 350 by 1st being displayed below the first cylinder to peak A bar is also displayed at that point NOTE The Columbia 350 Airplane Flight Manual on that cylinders bar graph See Figure 3 3 AFM supersedes information found in this 4 Richen the mixture until the A PEAK temperature Feel is rich by the amount indicated in the Columbia Leaning for Best Power Airplane Flight Manual AFM 1 Select the SYSTEM Softkey 2 Select the ASSIST Softkey Indicates Difference Between Present and Peak Temperature of the First Peaked Cylinder FFLOW GPH 13 0 TEMPERATURE s EGT F CHT F 1442 1452 1382 4 pea 378 380 1900 1414 1416 13 74 6 500 314 3 382 3 358 3 1750 1600 1450 1300 1150 1000 Figure 3 3 Engine Leaning Assist Display First Peaked Cylinder Columbia 350 Indicates First Cylinder to Peak Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 23 SECTION 3 ENGINE INDICATION SYSTEM EIS Leaning for Best Economy 3 4 Select the SYSTEM Softkey Select the ASSIST Softkey 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 Continue leaning the mixture until the last of the cylinders peaks This is indicated by Last being displayed below
142. uide for the Columbia 350 400 SECTION 1 SYSTEM OVERVIEW SECTION 1 SYSTEM OVERVIEW This guide gives the pilot abbreviated operating instructions for the Primary Flight Display PFD Multi The purpose of this Cockpit Reference Guide is Function Display MFD GCU 476 MFD PFD Control to provide the pilot a resource with which to find Unit and the GMA 1347 Audio Panel System operating instructions on the major features of the __ _ G1000 system more easily It is not intended to be a A NOTE The pilot should read and thoroughly comprehensive operating guide Complete operating e AT i cir ae s proce 7 f ja procedures for the complete system are found in the and operational information not contained in G1000 Columbia 350 400 Pilots Guide 190 00552 00 this Cockpit Reference Guide The Columbia 350 400 AFM always takes precedence over the information found in this guide A NOTE Speed ranges and V speeds shown in this guide are for example only Refer to the AFM for values pertaining to the Columbia 350 and Columbia 400 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 1 1 SECTION 1 SYSTEM OVERVIEW 1 1 PFD MFD CONTROLS OO O Figure 1 1 PFD MFD Controls D D MFD Only 12 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 PFD and MFD controls function the same with the exception of the dedicated Automatic Flight Control System AFCS keys loc
143. umbia 350 400 8 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 8 20 VERTICAL NAVIGATION VNAV PAGE NOTE An active flight plan or Direct to must be entered in order to utilize VNAV NOTE VNAV is advisory only and cannot be coupled to the autopilot 4 20KT Create a Vertical Navigation Profile 1 2 3 8 8 Press the FPL Key Turn the small FMS Knob to select the third page icon Press the FMS Knob to activate the cursor DTK UP TERRAIN 10 FT 100 FT 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 Press the ENT Key The cursor is now positioned over the Before and After field Turn the small FMS Knob to select whether the previously set distance is Before or After the endpoint Press the ENT Key The cursor is now placed over the VNAV profile endpoint field ARGET POSITION Before KHDN TARGET ALTITUDE 3000FT Above WPT TARGET VERTICAL SPEED 400FPM 4 200NM Figure 8 16 Vertical Navigation VNAV Page STATUS VERTICAL SPEED REQUIRED Begin descent in 1 FPM 00 26 18 LEGEND TARGET ALTITUDE TOP OF DESCENT BOTTOM OF CLIMB
144. us annunciations may also be issued PFD MFD TAWS Alert Type Page Annunciation MFD Pop Up Alert Aural Message TAWS System Test Fail ec TAWS System Failure No GPS position or excessively degraded ITAWS NAA None TAWS Not Available GPS signal TAWS Availble will be heard when sufficient GPS signal is re established System Test pass None TAWS System Test OK Alert Annunciations Alert Annunciation TERRAIN 100F1 l 1000Ff1 PULL UP Figure 10 25 Alert Annunciation on the PFD Alert Annuncia Figure 10 24 Alert Annunciation on the TAWS Page 10 16 Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 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 Reversionary display mode can also be manually activated by the pilot if the system fails to detect a display problem The reversionary mode is activated manually by pressing the red DISPLAY BACKUP button on the bottom of the audio panel GMA 1347 Pressing the red DISPLAY BACKUP button again deactivates reversionary mode NOTE The Columbia 350 400 Airplane Flight Manual AFM
145. ve been entered press the FMS Knob to return to the Flight Plan Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 8 8 LOAD A DEPARTURE See the Procedures section for a discussion on loading and activating departure procedures 8 9 LOAD AN ARRIVAL See the Procedures section for a discussion on loading and activating arrival procedures 8 10 LOAD AN APPROACH See the Procedures section for a discussion on loading and activating approach procedures 8 11 REMOVE A DEPARTURE ARRIVAL OR APPROACH FROM A FLIGHT PLAN With the Active or Stored Flight Plan Page displayed press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the title for the approach departure or arrival to be deleted Titles appear in white directly above the procedure s waypoints Press the CLR Key to display a confirmation window With OK highlighted press the ENT Key to remove the selected procedure STORE A NEWLY CREATED FLIGHT PLAN After creating a flight plan on either the PFD or MFD it may be saved by pressing the MENU Key Turn the large FMS Knob to highlight Store Flight Plan and press the ENT Key With OK highlighted press the ENT Key to store the flight plan SECTION 8 FLIGHT PLANNING Figure 8 13 Store Flight Plan Confirmation EDIT A STORED FLIGHT PLAN Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page Press the FMS Knob
146. vided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited Garmin and G1000 are registered trademarks of Garmin Ltd or its subsidiaries These trademarks may not be used without the express permission of Garmin NavData is a registered trademark of Jeppesen Inc Stormscope is a registered trademarks of L 3 Communications and XM is a registered trademark ot XM Satellite Radio Inc Ryan is a registered trademark of Avidyne Corporation June 2006 190 00567 00 Rev B Printed in the U S A Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 WARNINGS CAUTIONS amp 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 Terrain data is obtained from third party sources Garmin is not able to independently verify the accuracy of the terrain data WARNING The displayed minimum saf
147. wer down the G1000 GARHIN CORPORATION 1395 2003 Land and woter data is provided only as a general reference to your surroundings HH Terroin Database Version 2 40 Copyright 2003 Garnin Ltd or its subs Terrain data is provided only as on oid to situational quareness US Obstocle Dotobose Version 2 08 Figure 1 12 Power Up Splash Screen Window Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 SECTION 2 FLIGHT INSTRUMENTS SECTION 2 FLIGHT INSTRUMENTS The following discussions pertain to the Primary Flight Display unless otherwise indicated nav1 188 88 De RK 118 888 com NAVZ 136 975 COM INSET PFD NBS CD Tah a aa ALERTS C1 NAV Frequency Box E Turn Rate Indicator 2 Airspeed Indicator Barometric Setting Box G True Airspeed Box Vertical Speed Indicator Heading Box Altimeter G Horizontal Situation Indicator 13 Selected Altitude Box 6 Outside Air Temperature Box COM Frequency Box Q System Time Box 1s Navigation Status Box Transponder Status Box Slip Skid Indicator Attitude Indicator Figure 2 1 Default PFD Information Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 2 1 2 2 SECTION 2 FLIGHT INSTRUMENTS navi 1 17 88 HPT NAVZ 113 00 0 tonk IL LOW FUEL Low fuel in left tank bd R LOW FUEL Low fuel in right z ne FD cor GUS EE ESOP ALERTS Traffic Annunciation 6
148. while playing play is halted and the new COM input signal is recorded as the latest block Garmin G1000 Cockpit Reference Guide for the Columbia 350 400 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 e AP DISC Autopilot Disconnect Button Located on the pilots control stick pressing this button disengages the autopilot Pressing it also acknowledges an autopilot disconnect e CWS Control Wheel Steering Button Located on the pilots control stick pressing and holding the CWS button disengages the control surface servos without disengaging the autopilot If the flight director has not been activated pressing the CWS button will activate the flight director in the detault pitch and roll hold modes GO AROUND Button Located on the instrument panel the Go Around Button disengages the autopilot and selects the Go Around wings level mode e MET Manual Electric Trim Switch This switch is used to operate manual electric pitch trim Moving the switch forward trims the aircraft nose down Moving the switch aft trims the aircraft nose up SECTION 6 AUTOMATIC FLIGHT CONTROL Figure 6 1 AFCS Keys Pressing the FD Key activates only the flight director in the default Pitch Hold Roll mo

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