Home

Garmin Software Version 0458.01 Cockpit Reference Guide

1. Figure 7 13 Nearest VOR Page View Information on the Nearest VOR 1 With the Nearest VOR Page selected press the VOR softkey 2 Turn either FMS knob to select a VOR Press the ENT key OR Press the MENU key Select the Select VOR Window option and press the ENT key Turn either FMS knob to select a VOR Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 7 7 SECTION 7 NAVIGATION Select and Load a VOR Frequency Select a Nearest User Waypoint 1 With the Nearest VOR Page selected press the 1 With the Nearest User Waypoint Page selected FREQ softkey to highlight the VOR frequency press the FMS knob to activate the cursor OHNE Seleled VOR 2 Press the ENT key to select the Nearest User 2 Press the ENT key The selected VOR frequency Waypoint is placed in the NAV standby frequency field 3 The remaining information on the Nearest User OR Press the MENU key Select the Select Fre Waypoint Page pertains to the selected Nearest quency Window option and press the ENT key User Waypoint Press the ENT key again when the frequency field is highlighted to place the selected VOR 7 13 NEAREST FREQUENCIES frequency in the NAV standby field an 136 975 TH LE er ADCeT ADTI 7 12 NEAREST USER WAYPOINT 17 95 136 975 17 95 ORTH UP K np TARN Figure 7 15 Nearest Frequencies Page Select the Nearest Frequencies Page iam e Figure 7 14 Nearest User Waypoints Page 1 Turn the large
2. 0000esrsrrrseen 12 2 12 2 A36 G36 Aircraft Annunciations amp Alerts 12 3 WARNING Annunciation 12 3 CAUTION ANNUNCIO UON enssins 12 3 ADVISORY Annunciation 12 3 Alert Message scosrsssncteencunctamcuncnisentnctnscensasietianedeatt 12 3 TABLE OF CONTENTS 12 3 AFCS NCIS sieccscsiasicssoccsternecaraiedovenimacinue 12 4 System Status Field ccsssessssessecsecssesssessssssssesseessees 12 4 12 4 G1000 System Annunciations 12 5 WIG N E T 12 5 12 5 G1000 System Alert Messages 12 7 MFD amp PFD Alert Messages csscessesstestecseestesseeseesees 12 8 Database Alert Messages cesseesseesseessesseesesseaseean 12 9 GMA 1347 Alert MeSSAQCS c scesesseesseesseseeseesean 12 10 GIA 63 Alert Messages scesssssessecsesseesseeseesesseean 12 10 GEA 71 Alert Messages s s 12 12 GTX 33 Alert Messages cessssssesstecstesssesseeseesesseean 12 13 GRS 77 Alert Messages c scsssessecstecssessesssesseeseean 12 13 GMU 44 Alert MeSS Q S ccsscesstessesssesseeseesesseean 12 14 GDL 69 Alert Messages essessesstessesssesseeseesesseean 12 14 GDC 74A Alert Messages v ssscesscesstesseesseeseesesseeen 12 14 Miscellaneous Alert Messages sssessessesseesseen 12 15 INDEX Index 1 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 TABLE OF CONTENTS This page intentionally left blank X Garmin G1000 Cockpit Reference Guide for the Beech
3. 3 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 4 With Activate highlighted press the ENT key Figure 8 5 Activate Flight Plan Leg Confirmation 8 9 STOP NAVIGATING A FLIGHT PLAN 1 Press the FPL key and turn the small FMS knob to display the Active Flight Plan Page 2 Press the ENT key to display the Page Menu window SECTION 8 FLIGHT PLANNING Figure 8 6 Delete Flight Plan Turn the large FMS knob to highlight Delete Flight Plan and press the ENT key With OK highlighted press the ENT key to deactivate the flight plan This will not delete the stored flight plan only the active flight plan Delete oll waypoints in Flight plon OK or CANCE 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 origi nal 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 8 Invert Flight Plan Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 SECTION 8 FLIGHT PLANNING 8 4 8 7 Figure 8 9 Invert Flight Plan Confirmation CREATE A NEW FLIGHT PLAN To create a new fligh
4. C Aircraft Wing Tips Q Pitch Scale Slip Skid Indicator E Sky Representation Figure 2 6 Attitude Indicator Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 SECTION 2 FLIGHT INSTRUMENTS 2 3 ALTIMETER MRE Altitude Reference ann Box 3100__ Altitude Trend 30 je Current Altitude Vector Ezeren 2900 2800 Altitude Reference Bug Barometric Setting ELTE Box Figure 2 7 Altimeter Altitude Reference Bug The Altitude Reference Bug can be set to any desired altitude The bug acts as a visual reference to indicate the desired altitude is approaching To set the altitude reference bug 1 Turn the ALT knobs to set the altitude reference bug The small ALT knob sets the hundreds and the large ALT knob sets the thousands This altitude also appears in the altitude reference 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 2 4 VERTICAL DEVIATION GLIDESLOPE INDICATOR The Vertical Deviation Glideslope Indicator appears when an ILS is tuned in the active NAV field 2 5 MARKER BEACON ANNUNCIATIONS Marker Beacon Annunciation Vertical Deviation Glideslope Indicator Figure 2 8 Marker Beacon and Vertical Deviation Garmin G1000 Cock
5. ENGINE Pressing this softkey makes available the LEAN and SYSTEM softkeys which in turn access the Lean Page and the System Page respectively MAP pressing this softkey enables the following softkeys TRAFFIC pressing this softkey displays removes Traffic on the Navigation Map TOPO pressing this softkey displays or removes topographic information on the Navigation Map TERRAIN pressing this softkey displays removes terrain and obstacle data on the Navigation Map Press the BACK softkey on this level to return to the top softkey level y A Press the ENGINE or BACK softkey on any level to return to the default page level optional optional optional j f SECTION 1 SYSTEM OVERVIEW STRMSCP optional pressing this softkey displays removes Stormscope lightning data on the Naviga tion Map NEXRAD optional pressing this softkey displays removes precipitation data on the Navigation Map XM LING optional pressing this softkey displays removes XM Radio lightning data on the Naviga tion Map BACK pressing this softkey displays the ENGINE and MAP top level softkeys DCLTR declutter pressing this softkey removes map information in three levels optional Press to return to the top softkey level gt He O E The DONE softkey changes to UNDO when the checklist item is already checked nG A N nN nae Figure 1 6 MFD Softkeys Garmin G1000 Co
6. G1000 Cockpit Reference Guide for the Beechcraft A36 G36 Copyright 2005 Garmin Ltd or its subsidiaries All rights reserved This manual reflects the operation of System Software version 0458 01 or later for the Beechcraft A36 G36 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 S051 9DL 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 provided 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 u
7. To allow the aircraft to descend power must be reduced The Autopilot maintains 142 knots by controlling pitch 1 Cruise Altitude of 7 000 MSL ko t SECTION 6 AUTOMATIC FLIGHT CONTROL 3 As the aircraft reaches the selected altitude the autopilot changes trom Flight Level Change mode to Altitude Hold mode ALT flashes in green indicating the selected altitude is captured After the capture is finished the autopilot holds the aircraft at the selected altitude 3 Selected Altitude of 3 000 MSL ALT Hold Mode Figure 6 25 FLC Descent Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 6 17 SECTION 6 AUTOMATIC FLIGHT CONTROL ILS Approach 6 18 1 Load the Runway 29R ILS approach for KFAT into the flight plan Vectors to Final is selected for the transition Upon being given vectors from ATC set the Selected Heading to the heading given by ATC and press the HDG key The autopilot turns the aircraft to the desired heading Turn the HDG knob to set the Heading Bug to comply with ATC vectors as requested s Se aa In preparation for the approach and at the pilot s discretion tune the localizer frequency then set the CDI to LOC by pressing the CDI softkey When cleared for the approach press the APR key LOC and GS appear in white in the roll axis and pitch axis modes armed fields respectively The autopilot will calculate wh
8. 6 19 Glideslope 2 2 2 4 6 4 6 8 6 9 6 12 GMA 1347 1 1 Go Around 6 1 6 4 6 8 6 9 6 12 6 19 HDG key 6 10 6 14 6 18 6 19 Heading hold 6 9 Heading indication 2 6 Heading Select 1 3 1 4 6 9 6 10 Heading Select Mode 6 10 Headset s 5 2 Index 1 INDEX Hijack code 4 5 Horizontal situation indicator 2 5 Hurricanes 10 5 ICAO 4 5 ID 4 3 IDENT function 4 5 INTEG 2 7 Interrogations 4 4 K Key s 1 4 L Lightning 1 4 1 7 10 2 10 3 10 5 Load approach 8 5 Load a VOR frequency 7 8 Load departure 8 5 Load the frequency for a controlling agency 7 9 Load the nearest ARTCC frequency 7 9 Loss of communication code 4 5 Manual Electric Trim 6 1 MAP 7 1 Map panning 10 5 Marker beacon 2 4 MET 6 1 6 3 12 4 METAR 10 3 10 5 MFD 1 1 4 4 Military interceptor operations code 4 5 Missed Approach 6 19 MKR MUTE 5 2 Mode selection softkeys 4 4 Morse code identifier 4 3 Nav Com controls 4 1 NAV1 5 2 NAV2 5 2 Navigation 7 1 Navigation Mode 6 11 Navigation status window 2 2 NAV Frequency Window 4 1 Nearest Airports Page 7 3 7 5 7 6 Tf F 67798 Nearest ARTCC amp FSS frequencies 7 8 NEXRAD 1 4 1 7 10 3 10 4 10 5 10 6 10 7 0 OBS 2 7 Obstacles 10 9 10 10 12 9 Operation 5 2 Optional NAV radios 4 3 Overspeed 6 2 P Page group icon 1 8 PFD 1 1 4 1 4 4 PIT 6 3 6 4 6 19 pitch axis modes 6 3 6 4 6 18 Pitch hold 1 4 6 1 6 4 6 8 6 14 6 19
9. Press the TRAFFIC softkey Traffic will now be displayed on the map Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 OEP COMZ sro NORTH UP RML KRAD R3 Non Bearing Traffic Of Scale Tate Traffic Advisories Banner Figure 10 13 TAS Traffic on Navigation Map 10 6 TERRAIN AND OBSTACLE PROXIMITY NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south 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 press the VIEW softkey to access the ARC and 360 softkeys When the ARC softkey is pressed a radar like 120 view is displayed Press 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 RED WARNING Terrain Obstacle at or within 100 below current aircraft altitude YELLOW CAUTION Terrain Obstacle between 100 and 1000 below current aircraft altitude a Aircraft Altitude 4 100 Threshold 1000 AGL Y Displaying Terrain and Obstacles on the Navigation Map 1 With the Navigation Map displayed press the MAP softkey 2 Press the TERRAIN softkey Terrain and obstacle proximity will now be displayed on the m
10. SECTION 5 AUDIO PANEL 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 Figure 5 2 Transceivers 5 2 MARKER BEACON RECEIVER The marker beacon receiver is always ON Figure 5 3 shows the marker beacon annunciators on the PFD Inner Marker Annunciator Middle Marker Annunciator audio returns when the next marker signal is received Marker Beacon Signal Sensitivity The HI SENS key can be pressed for increased marker beacon signal sensitivity y MKR HI SENS MUTE Figure 5 4 Marker Beacon 5 3 NAV RADIO AUDIO SELECTION Pressing DME 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 four keys can be selected individually or together Outer Marker Annunciator Figure 5 3 Marker Beacon Signal Indicator Lights on the PFD When the MKR MUTE key is pressed the key an nunciator is lit and the audio tone can be heard over the speaker or headsets during marker reception When the tone is active pressing the MKR MUTE key mutes the audio but does not affect the annunciato
11. The declutter level appears adjacent to the DCLTR softkey e No declutter All map features are visible Declutter 1 Declutters land data e Declutter 2 Declutters land and SUA data e Declutter 3 Declutters large NAV data remaining removes everything except the active flight plan TRAFFIC Press to display TIS or TAS traffic on the inset map TOPO Press to display topographical data i e coastlines terrain rivers lakes etc and elevation scale on the inset map TERRAIN Press to display terrain information on the inset map STRMSCP optional Press to display the Storm scope lightning data on the inset map within a 200 nm radius of the aircraft NEXRAD optional Press to display NEXRAD precititation data on the inset map XM LTNG optional Press to display the XM Radio lightning data on the inset map BACK Press to return to the previous level softkey configuration PFD Press to display the additional softkeys for additional configurations to the PFD METRIC Press to display the current and refer ence altitudes in meters in addition to feet Pressing the metric softkey also changes the barometric setting to hectopascals DFLTS Press to reset default settings on the PFD DME optional Press to display the DME informa tion window Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 BRG bearing Press to cycle through the follow ing in
12. as shown in Figure 12 3 Pressing the CAUTION softkey acknowledges the presence of the caution alert The softkey has now reverted to the ALERTS softkey label and displays a description of the caution annunciation in the Alerts Window when Figure 12 3 CAUTION Softkey pressed Annunciation e ADVISORY ANNUNCIATION This level of alert provides general information to the pilot that may not need immediate attention An advisory annunciation is displayed in the Annunciation Window as white text An advisory annunciation is DYI SORY also accompanied by a flashing white ADVISORY softkey label as shown in Figure 12 4 Pressing the ADVISORY softkey acknowledges the presence of Figure 12 4 ADVISORY Softkey Annunciation 12 2 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 SECTION 12 ANNUNCIATIONS amp ALERTS 12 2 A36 G36 AIRCRAFT ANNUNCIATIONS amp ALERTS The following alert annunciations are configured specifically for the Beechcraft A36 G36 aircraft See the Beechcraft A36 G36 Pilots Operating Handbook POH for information regarding pilot responses WARNING Annunciation Annunciation Window Text Alerts Window Message Audio Alert Gear up Continuous Tone received through the G1000 audio trom another source Alternator 1 offline Repeating Tone Alternator 2 offline Repeating Tone Alternators 1 and 2 offline Repeating Tone CAUTION Annunciation ADVISORY Annunciation Annunciation Wi
13. maintain the selected altitude Upon reaching the holding pattern set the Selected Heading to 307 degrees using the HDG knob and press the HDG key The HDG knob is used for the remainder of the hold to guide the aircraft SECTION 6 AUTOMATIC FLIGHT CONTROL on Yh Figure 6 27 Go Around Missed Approach Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 6 19 SECTION 6 AUTOMATIC FLIGHT CONTROL This page intentionally left blank 6 20 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 SECTION 7 NAVIGATION SECTION 7 NAVIGATION 7 2 DIRECT TO NAVIGATION Direct to Navigation from the MFD 7 4 NAVIGATION MAP PAGE Identifier ais Fac ILITV i Ty symbol Facility Name MIAMI IN Select the MAP Page Group City a a Flight Plan Field fe acai Nearest Airport 1 Turn the large FMS knob until MAP is high vere lighted in the page group window in the lower l Dette Map of the right of the MFD display Se oe 2 Turn the small FMS knob to select the first MAP Waypoint page indicated by a solid rectangular icon Map Range 3 Press the MAP softkey to display softkeys for the Bearing Region available information which may be displayed Distance T on the map Direct to Activate Field Course WARNING The map display should only be Figure 7 2 MFD Direct to Window used for situational awareness Any map display o indication should be compared with approved To enter a Direct to destinati
14. while the small knob selects the hun dreds Selected altitude provides an altitude setting for the Altitude Capture Hold mode in addition to the stan dard G1000 altitude alerter function 18 AP Key Engages disengages the Autopilot and Flight Director in the default vertical and lateral modes 19 FD Key Activates deactivates the Flight Director only Pressing the FD key turns on the Flight Director in the default vertical and lateral 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 YD Key Engages disengages the Yaw Damper 25 HDG Key Selects deselects the Heading Select mode 26 APR Key Selects deselects the Approach mode 27 28 NOSE UP NOSE DN Keys Controls the ac tive pitch reference for the Pitch Hold Vertical Speed and Flight Level Change modes 1 2 PFD SOFTKEYS oN Softkey ON Softkey OFF optional Figure 1 2 PFD Top Level Softkeys INSET Press to display the Inset Map in the lower left corner of the PFD OFF Press to remove the Inset Map DCLTR 3 Press momentarily to select the desired amount of map detail
15. Comments o GIA1 CONFIG GIA1 configuration error Contig 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 Contig 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 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 12 10 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 GIA 63 Alert Messages Cont SECTION 12 ANNUNCIATIONS amp ALERTS Alerts Window Message Comments o MANIFEST GIA1 software mismatch Communication halted MANIFEST GIA2 software mismatch Communication halted COM1 TEMP COM1 over temp Reducing transmitter power COM2 TEMP CON2 over temp Reducing transmitter power COM1 SERVICE COM needs service Return unit for repair COM2 SERVICE COM2 needs service Return unit for repair COM1 PTT C
16. FLIGHT PLANNING 3 Turn the large FMS knob to highlight the latitude longitude field or the Reference Way points field depending on how the waypoint is to be defined 4 Turn the FMS knobs to enter the position coordinates or the radial and distance from the reference waypoint 5 Press the ENT key to accept the new way point 6 Press the FMS knob to remove the flashing Cursor Create User Waypoints from the Navigation Map Page 1 With the Navigation Map Page displayed push the joystick to activate the panning function The target pointer is displayed at the present aircraft position 2 After placing the pointer at the desired posi tion press the ENT key The User Waypoint Information Page is now displayed with the captured position 3 Turn the FMS knobs to select a waypoint name 4 Press the ENT key to accept the selected name The first reference waypoint field is highlighted 5 If desired 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 6 Press the FMS knob to remove the flashing Cursor Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 SECTION 8 FLIGHT PLANNING Modify a User Waypoint 1 With the User Waypoint Information Page displayed press the FMS knob to activate the Cursor 2 Turn the large FMS knob to move the cursor to the desired field and turn the small F
17. FMS knob to select the NRST page group Select the Nearest User Waypoint Page 2 Turn the small FMS knob to select the sixth 1 Turn the large FMS knob to select the NRST rectangular page icon page group 2 Turn the small FMS knob to select the fifth rectangular page icon 7 8 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 SECTION 7 NAVIGATION Select and Load the Nearest ARTCC FSS or displayed Weather Frequency e Ifthe aircraft is within two nautical miles of an airspace and the current course takes the aircraft 1 With the Nearest Frequencies Page selected inside Ahead lt 2 nm is displayed press the ARTCC FSS or Wx softkey e If the aircraft is within two nautical miles of an airspace and the current course will not take the 2 Turn the large FMS knob to select the fre aircraft inside Within 2 nm is displayed quency Ifthe aircraft has entered an airspace Inside is 3 Press the ENT key to load the frequency into displayed the COM frequency standby field View Additional Details for a Listed Airspace 1 Select the Nearest Airspace Page 7 14 NEAREST AIRSPACES 2 Press the FMS knob to activate the cursor 3 Turn the large FMS knob to scroll through the list highlighting the desired airspace 4 Press the ALERTS softkey and turn either FMS knob to select the desired airspace 5 Press the FMS knob to remove the flashing Cursor View and Quickly Load the Fr
18. MFD Manual disengagement is annunciated by a five second flashing yellow AP in the Autopilot Status field and by a two second Autopilot disconnect aural alert The Yaw Damper will also disengage with the autopilot Manual Disconnect _ ROL LAP YD 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 YD ALT Figure 6 8 CWS Annunciation SECTION 6 AUTOMATIC FLIGHT CONTROL Yaw Damper When the autopilot is engaged the Yaw Damper is au tomatically engaged When the Yaw Damper is active the YD annunciation appears in the Yaw Damper Status field as shown Yaw Damper is active _ HDG JAP YD ALT Figure 6 9 Yaw Damper Active To disengage the Yaw Damper press the YD key or use the MET switch The YD annunciation turns yellow and flashes for five seconds upon disengagement Yaw Damper is disengaging a HDG JAP YD VS 11000r ALT Figure 6 10 Yaw Damper Disengagement 6 4 LOSS OF DATA In general a flashing yellow mode annunciation indi cates either the loss of sensor data AHRS ADC or GIA or loss of na
19. STRMSCP MODE Turn either FMS knob to display the Cell Strike window Turn either FMS knob to select Cell or Strike Press the ENT key Push the FMS knob to return to the Navigation Map Page To clear Stormscope lightning data from the Navigation Map Page P Press the MENU key with the Navigation Map Page displayed Zi Turn either FMS knob to highlight the Clear Lightning Data field and press the ENT key Stormscope Page 1 Turn the large FMS knob until the Map Page group is selected Turn the small FMS knob until the Stormscope Page is selected This is the third rectangular page icon VIEW CLEAR Figure 10 6 Stormscope Page To change the Stormscope lightning mode between cell and strike 1 2 Select the Stormscope Page Press the MODE softkey The CELL and STRIKE softkeys are displayed Press the CELL softkey to display CELL data or press the STRIKE soft key to display STRIKE data CELL or STRIKE is displayed in the mode box located in the upper left corner of the Stormscope Page Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 NOTE Cell mode uses a clustering program to identify clusters of electrical activity that indicate cells To change the viewing mode between 360 10 3 and 120 Select the Stormscope Page Press the VIEW softkey The 360 and ARC soft keys are displayed Press the 360 so
20. Set WPT to Present Position to display P POS Press the ENT key and the flashing cursor moves to the to waypoint field Turn the FMS knobs to enter the identitier of the to waypoint and press the ENT key to accept the waypoint OR SECTION 8 FLIGHT PLANNING For point to point planning turn the FMS knobs to enter the identifier of the trom waypoint Once the waypoints identifier is entered press the ENT key to accept the waypoint The flashing cursor moves to the to waypoint Again turn the FMS knobs to enter the identi fier of the to waypoint and press the ENT key to accept the waypoint OR For flight plan leg planning press the FPL softkey at the bottom of the display and turn the small FMS knob to select the desired flight plan already stored in memory by number 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 Turn the large FMS knob to highlight the depar ture 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 unit 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
21. be smooth Prepare for steep turns ahead and expect noticeable course deviations active proach when required approach to the correct NAV receiver waypoint for navigation xxxx with alternate navigation sources ae Ball sl gic ee The traffic information system TIS has failed The G1000 system should be serviced al EE Stop ene Stormscope has failed The G1000 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 12 16 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 A Abnormal COM operation 11 2 Activate a flight plan 8 3 Active flight plan 8 2 Advisory 12 1 12 2 AFCS 1 1 6 1 6 2 6 4 6 6 6 7 6 9 6 11 6 12 6 13 12 4 Age 10 6 AHRS 12 13 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 Message 12 2 Alert message 12 1 12 8 12 9 12 10 12 11 12 12 12 13 12 14 12 15 12 16 Altitude hold 1 4 6 4 6 5 6 6 6 7 6 8 6 10 6 14 6 17 6 19 Altitude reference bug 2 4 Altitude trend vector 2 4 ALT knob 1 4 Annunciations 12 1 AP 1 4 6 1 6 2 6 3 6 4 6 5 6 6 6 7 6 9 6 14 6 18 6 19 12 4 Approaches 9 2 Approach activation 4 4 Approach markers Signal augmentation 5 2 Approach Mode 6
22. 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 FIS sensor 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 seed Echo Top Cloud Top and Echo Top Mutually Exclusive Figure 10 10 Weather Product Symbols The XM Information Page in the AUX Page Group will display the weather products available for the current sub scription A green box by the weather product means that it is available Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 minutes SIGMETSIAIRMETs fo oo Ciy Forecasts fo wo CountyWamings f o 0 Cyclone Warnings 6o Freezingleves o oo a Surface Analysis fo oo mes Cid a WindsAlft wo ee ee Cloudstops o 10 4 TRAFFIC INFORMATION SERVICE TIS NOTE If the G1000 is configured to use the optional Skywatch Traffic Advisory System TIS will not be available for use NOTE Traffic Information Service TIS is only available when the aircraft is within the service volume of a TIS capable terminal radar site Displaying Traffic on the Traffic Map Page 1 Turn the large FMS knob to select the Map Page Group SECTION 10 HAZARD AVOIDANCE 2 Turn the small FMS knob to select the second rectangular page icon 3 Press the OPERATE softkey to
23. key to display pertinent information for the selected product Note that pressing the ENT key when pan ning over anAIRMET or a SIGMET displays an Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 10 5 SECTION 10 HAZARD AVOIDANCE 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 prod uct is active the product symbol is displayed in the lower right of the screen NEXRAD e Cloud Top Echo Top e XM Lightning e Cell Movement SIGMETs AIRMETs e METARs e City Forecast e Surface Analysis e Freezing Levels e Winds Aloft e County Warnings e Cyclone Warnings NOTE The DONE softkey on the AUX XM INFOR MATION page is used to save the GDL 69 A acti vation data when the XM services are initially set up It is not used during normal operation of the GDL 69 A and it should have no adverse effects if inadvertently selected during flight Refer to the GDL 69 69A XM Satellite Radio Activation Instructions 190 00355 04 Rev E or later for further information Weather Product Age The age
24. model model needs update when practical GEO LIMITS Too far North South no The aircraft is outside geographical limits for approved AHRS operation Heading is magnetic compass flagged as invalid The AHRS has incorrect software installed The G1000 system should be serviced Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 12 13 SECTION 12 ANNUNCIATIONS amp ALERTS GMU 44 Alert Messages Alerts Window Message Comments HDG FAULT A magnetometer fault A fault has occurred in the GMU 44 Heading is flagged as invalid The AHRS uses has occurred GPS for backup mode operation The G1000 system should be serviced MANIFEST GMU1 software mismatch Communication halted GDL 69 Alert Messages Alerts Window Message Comments S 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 Alert Messages 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
25. page while the small knob is used to select individual characters for the highlighted cursor location When the G1000 dis plays a list 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 cat egory Press the FMS PUSH CRSR 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 op tions 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 ar rivals from the flight plan If a flight plan is used avail able 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 se lected 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 Beechcraft A36 G36 SECTION 1 SYSTEM OVERVIEW 16 ENT Key Accepts a menu selection or data entry This key is used to approve an operation or complete data entry It is also used to confirm selections and informa tion entries 17 Dual ALT Knob Sets the reference altitude in the box located above the Altimeter The large knob selects the thousands
26. the selected way point then turn the large FMS knob to highlight the Direct to 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 P 2 i Press the Direct to GE 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 wis Press the FMS CASA knob to return to bose poge Figure 7 3 Canceling Direct to Navigation Direct to Navigation from the PFD WPT Symbol Identifier WPT Location Facility Name JACK IOLE Flight Plan WPT AA cae Nearest WPT Bearing to WPT 43 36 44 EP Distance from WPT Course to Selected WPT ACTIVATE Figure 7 4 PFD Direct to Window Press the Direct to 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 1 2 Press the Direct to eM 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 c
27. time to return to GPS When using GPS as the navigation source the follow ing may appear INTEG RAIM is not available e WARN GPS detects a position error e SUSP Displayed when in OBS Mode indicating GPS navigation is suspended SECTION 2 FLIGHT INSTRUMENTS Figure 2 18 GPS INTEG GPS SUSP LOC1 and VOR2 To enable disable OBS mode while navigating with GPS 1 Z Press the OBS softkey to select OBS Mode Turn the CRS knob to select the desired course TO FROM the waypoint Press the OBS softkey again to return to normal operation Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 2 SECTION 2 FLIGHT INSTRUMENTS This page intentionally left blank 2 8 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 SECTION 3 ENGINE INDICATION SYSTEM EIS 3 1 ENGINE DISPLAY In all cases green indicates normal operation yellow indicates caution and red indicates warning Pressing the ENGINE softkey makes available the LEAN and SYSTEM softkeys which in turn provide ac cess the Lean Page and the System Page respectively Manifold oS 4 quge MAN IN HG woe 27 2 RPM Gauge Fuel Flow Numeric Fuel Flow Readout Indicator Leaning Pointer Cylinder Head Oil Temperature OIL TEMP Temperature Indicator x Indicator OIL PRES Oil Pressure ALT LOAD Indicator Uv Ammeter A BUS VOLTS A Voltmeter FUEL QTY GAL A Fuel Quantity Indicator Figure 3 1 Default En
28. to place the cursor on the desired airport frequency shown in the window Press the ENT key and the selected frequency will become the standby frequency for the active COM Press the Frequency Toggle key to make the frequency the active frequency NEAREST INTERSECTIONS 136 975 MEARE ST IHT Figure 7 11 Nearest Intersections Page Select the Nearest Intersections Page Turn the large FMS knob to select the NRST page group 7 6 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 2 Turn the small FMS knob to select the second rectangular page icon View Information on the Nearest Intersection 1 Press the FMS knob to activate the cursor 2 Turn either FMS knob to select the desired intersection Press the ENT key 7 10 NEAREST NDB T EE 136 975 Figure 7 12 Nearest NDB Page Select the Nearest NDB Page 1 Turn the large FMS knob to select the NRST page group 2 Turn the small FMS knob to select the third rectangular page icon Access Information on a Specific NDB 1 Press the FMS knob to activate the cursor 2 Turn either FMS knob to select the desired NDB Press the ENT key The remaining information SECTION 7 NAVIGATION on the Nearest NDB Page pertains to the selected NDB 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 196 975
29. to the fuel on board field Turn the FMS knobs to modify the fuel on board Press the ENT key when finished Note that in automatic mode this is provided by the system The flashing cursor moves to the calibrated airspeed field Turn the FMS knobs to enter an calibrated airspeed Press the ENT key when finished Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 SECTION 8 FLIGHT PLANNING This page intentionally left blank 8 2 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 9 1 SECTION 9 PROCEDURES ARRIVALS AND DEPARTURES Load and Activate a Departure Procedure 1 With the Navigation Map Page displayed press the FPL key Press the LD DP softkey If a flight plan is active the departure airport will be displayed as the default A list of available departures is also displayed 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 Depar ture 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 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 transiti
30. 0 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 PFD1 terrain database 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 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 DB MISMATCH Terrain database The PFD and MFD have different terrain dat
31. 12 ANNUNCIATIONS amp ALERTS SECTION 12 ANNUNCIATIONS amp annunciation to accompany an alert During the alert the ALERTS softkey assumes a new label ALERTS 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 press the ALERTS softkey again to view alert text messages A NOTE The Beechcraft A36 G36 Pilot s Operating Handbook POH supersedes information found in this document The G1000 Alerting System conveys alerts to the pilot aa lt lt e System Annunciations Typically a large red X using a combination of the following items appears in a window when a related LRU fails or detects invalid data A red X is accompanied by an alert message in the Alerts Window 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 reversion ary mode All A36 G36 annunciations can be displayed simultaneously A white horizontal line separates annunciations that are acknowledged 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 annun Audio A
32. 12 AP disconnect 6 1 Arrivals 9 1 ASSIST 3 1 Attitude indicator 2 3 Audio alerting system 12 1 Audio panel 4 3 5 1 Audio panel controls Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 DME 5 2 NAV1 5 2 NAV2 5 2 Auto tuning 4 3 4 4 Automatic squelch 4 3 Autopilot 1 3 6 1 6 2 6 3 6 4 6 5 6 6 6 7 6 8 6 9 6 10 6 12 6 13 6 14 6 15 6 16 6 17 6 18 6 19 12 4 Backcourse 6 11 Barometric setting 2 4 Base reflectivity 10 4 BKSP softkey 4 4 BRG1 2 6 BRG2 2 6 C Caution 12 1 12 2 CDI 2 7 12 16 Cell 10 2 Cell mode 10 2 Cell movement 10 5 Cloud tops 10 5 CLR key 1 3 Coast mode 10 7 Codes important 4 5 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 4 6 5 6 6 6 7 6 8 6 9 6 19 Cyclones 10 5 Cylinder select 3 1 CYLSLCT 3 1 INDEX D Departures 9 1 Direct to 7 1 DME 1 6 Dual CDU failure 11 2 E Echo tops 10 5 Edit a flight plan 8 5 Emergency code 4 5 Engine display 3 1 ENGINE softkey 3 1 F FLC 1 4 6 4 6 7 6 17 Flight director 6 1 6 2 6 3 6 4 6 5 6 6 6 7 6 8 6 9 6 10 6 19 Flight ID 4 5 Flight level change 1 4 6 4 6 7 6 11 6 14 6 17 Flight Plan Catalog 9 1 9 2 FPL key 1 3 Freezing level 10 5 Frequency toggle key 1 3 4 3 G GA 6 1 6 3 6 4 6 8 6 9 6 12 6 18
33. 2 and LOC2 which points in the direction of the set course Figure 2 15 Course Pointer 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 the MFD Pilots Guide for more detail Bearing Pointers and Information Windows Pressing the PFD softkey provides access to the BRG1 and BRG2 softkeys The BRG1 pointer is a single line pointer The BRG2 pointer is a double line pointer DME Information Bearing 1 Bearing 2 Window Pointer Pointer CDI Bearing Bearing 2 Information Information Window Window Figure 2 14 HSI with Bearing Information Distance to Bearing Source Waypoint Identifier Bearing Pointer Source Icon Figure 2 15 BRG1 Information Window Distance to Bearing Source VN J 32 4 NH gt _NAV2 Pointer Bearing Icon Source Figure 2 16 BRG2 Information Window Waypoint Identifier Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 DME Radio optional To display the DME Information Window press the PFD softkey followed by the DME softkey Figure 2 17 DME Information Window Navigation Source To change between navigation sources 1 Press the CDI softkey to change trom GPS to VOR1 LOC1 2 Press the CDI softkey again to change from VOR1 LOC1 to VOR2 LOC2 3 Press the CDI softkey a third
34. 3 1 GIIGESIODE E N 6 8 3 3 Engine System Display 3 2 6 6 Roll Axis ModeS 00 eeeesssieeeesssseee 6 9 Roll Hold Mode ROW isc ocsesceaceseiscceniescteonvcnestenen 6 9 SECTION 4 NAV COM AND TRANSPONDER 4 1 Heading Select Mode HDG 6 10 4 1 Radio Status Indications 4 3 Navigation Mode GPS VOR LOC or BC sssssss000 6 11 EE ee 4 3 Navigation Mode Armed 6 11 4 3 Automatic Squeleh cccccssceeen 4 3 Approach Mode GPS VAPP or LOC 6 12 4 4 Quickly Activating 121 500 MHZ 4 3 Go Around GA n 6 12 4 5 Optional NAV Radios ccccccsseeceeeenien 4 3 6 7 Example Procedures Using AFCS 6 13 DME Radio Optional scsssssssssessessessneeseesseesseen 4 3 DSU asinsi adinean 6 14 4 6 Frequency Auto tuning ccccccccin 4 4 Intercepting a VOR Radial 6 15 AO A O ET D iae 4 4 Flying a Flight Plan GPS Course ssssssssssssseeseeeee 6 16 Auto tuning on the MFD sssrin 4 4 Flight Level Change Descent 6 17 A7 Transponder ssirississrssisrsinesisorsanisisinisinnesnisns 4 4 E OO e etien lineece 6 18 Mode Selection sessssecsssssecsssessessseessessessseeesneen 4 4 Go Around Missed Approach 6 19 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 vi TABLE OF CONTENTS SECTION 7 NAVIGATION 7 1 7 4 Navigation Map Pag cc ccccseseeen 7 1 Select the MAP Page GrOUD sssesssesssessess
35. 4 Remove Waypoint Confirmation 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 and press the MENU key to display the Page Menu options Turn the large FMS knob to highlight Invert Flight Plan and press the ENT key The origi nal flight plan remains intact in its flight plan catalog storage location With OK highlighted press the ENT key to invert the flight plan Press the FMS CRSR knob to return to bose poge Figure 8 15 Invert Flight Plan 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 then press the MENU key to display the Flight Plan Catalog Options 8 17 8 18 Turn the large FMS knob to highlight Copy Flight Plan and press the ENT key 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 Press the MENU key to display the Flight Plan Catalog options Turn the large FMS knob to highlight Delete Flight Plan and press
36. 7600 Loss of communication code e 7700 Emergency code e 7777 Military interceptor operations code NEVER ENTER THIS CODE e 000 Code for military use in the U S Flight ID Reporting If so configured the Flight ID may be entered in the Timer Reterence window If configuration is set to SAME AS TAIL the aircraft tail number will always be dis played Ws Vy FLIGHT ID N1294 ee Figure 4 12 Timer References Window Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 4 5 SECTION 4 NAV COM amp TRANSPONDER This page intentionally left blank 4 6 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 SECTION 5 AUDIO PANEL SECTION 5 AUDIO PANEL fa A COMI MIC COMI Transceiver Audio COM 3 is unavailable Transmitters COM3 MIC is unavailable Split COM Not recommended for use Telephone Unavailable in the Beechcraft A36 G36 Passenger Address Speaker Marker Beacon Mute Marker Beacon Signal Sensitivity jaroai Navigation Radio Audio Aircraft Navigation Radio Audio DME optional ADF amp AUX unavailable Manual Squelch fee RELAY Recorded COM Audio Playback CREW PILOT con ICS Isolation ICS ISOLATION PILOT O PASS VOL SO Volume Squelch VOL Annunciation SQ Annunciation Reversionary Mode DISPLAY BACKUP Figure 5 1 Audio Panel Controls Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 5 1
37. ANNUNCIATIONS When an LRU or an LRU function fails a large red X is A NOTE Upon power up of the G1000 system typically displayed on windows associated with the failed certain windows remain invalid as G1000 equip data The following section describes various system an ment begins to initialize All windows should nunciations Refer to the POH for additional information be operational within one minute of power up regarding pilot responses to these annunciations Should any window continue to remain flagged the G1000 system should be serviced by a Garmin authorized repair facility Voice Alerts Voice Alert Alert Trigger Traffic Played when a Traffic Advisory TA is issued Traffic Not Available Traffic Trafic Traffic Advisory System Test Passed Talfic Advisory System Test Failed system Annunciation Commet Attitude and Heading Reference System is aligning Display system is not receiving attitude information from the AHRS Display system is not receiving airspeed input from air data computer Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 12 5 SECTION 12 ANNUNCIATIONS amp ALERTS system Annunciation Commet SS Display is not receiving altitude input from the air data computer Display is not receiving vertical speed input from the air data computer i Display is not receiving valid heading input trom AHRS GPS information is either not present or is inv
38. Beechcraft A36 G36 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 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 i WARNINGS CAUTIONS amp NOTES This page intentionally left blank iv Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 RECORD OF REVISION
39. CONTROL the Airspeed Indicator and in the Airspeed Reference field in the AFCS Status Bar Airspeed may also be changed by pressing and holding the CWS button to manually establish the desired airspeed using the control wheel When the CWS button is released the current airspeed will be maintained This method must be used when using only the flight director Adjust engine power to allow the autopilot to fly the aircraft at a pitch attitude which corresponds to the selected airspeed and the desired flight profile descent or climb 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 at the selected airspeed If only the flight director is engaged pitch and roll commands are given to manually maintain the selected altitude Altitude Hold mode is armed ea oclected Altitude Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 6 SECTION 6 AUTOMATIC FLIGHT CONTROL Go Around Mode GA Glideslope GS Pressing the GA button not located on the MFD en Glideslope is a component of Approach APR mode gages the flight director in a wings level 7 degree pitch up See the discussion on Approach mode later in this sec attitude Go Around mode disengages the autopilot and tion cancels all armed
40. DR softkey 4 4 Y Yaw damper 1 4 6 2 6 3 12 4 YD 1 4 INDEX Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 Index 3 INDEX This page intentionally left blank Index 4 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 2005 Garmin Ltd or its subsidiaries aS Gd IN Garmin International Inc 1200 East 151st Street Olathe KS 66062 U S A p 913 397 8200 f 913 397 8282 hi Garmin AT Inc 2345 Turner Road SE Salem OR 97302 U S A Nooo es 4 503 364 211 38 Garmin Europe Ltd Unit 5 The Quadrangle Abbey Park Industrial Estate Romsey S051 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
41. GDC1 software The GDC 74A has incorrect software installed The G1000 system should be mismatch Communication halted serviced BACKUP PATH Airdata using backup The GDC 74A is using a backup communications data path The G1000 system data path should be serviced when possible Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 SECTION 12 ANNUNCIATIONS amp ALERTS Miscellaneous Alert Messages 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 tind 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 Verity user moditied procedures edited This alert is issued on
42. Hold will not become active and the current vertical speed will be maintained Vertical Speed Reference Vertical Speed mode is active 118 98 ITXD we wwz 115 98 118 98 IIX Figure 6 14 Vertical Speed Hold Mode Altitude Hold is Armed Selected Altitude Selected Vertical Speed Vertical Speed Reference Bug Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 Flight Level Change Mode FLC 1 Selected Airspeed Airspeed Reference Bu Select the desired altitude by turning the ALT knob to set the altitude in the Altitude Select box Press the FLC key The flight director is acti vated if not already active and FLC is now displayed in green in the Active Mode field and the Airspeed Bug will appear on the Airspeed Indicator Pitch and roll commands are given to manually maintain airspeed Press the AP key to engage the autopilot for maintaining the current airspeed Altitude Hold mode is automatically armed with ALT displayed white in the Armed Mode field to the right of the FLC annunciation If the autopilot is engaged the Airspeed Bug can be adjusted in 1 knot increments by pressing the NOSE UP NOSE DN keys to set the desired airspeed The airspeed setting will be displayed in the Selected Airspeed box above Airspeed Reference Flight Level Change mode is active New 113 00 ww2108 00 117 95 Figure 6 15 Flight Level Change Mode SECTION 6 AUTOMATIC FLIGHT
43. MS knob to make changes 3 Press the ENT key to accept the changes 4 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 press the DELETE softkey 2 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 8 2 VIEWING THE ACTIVE FLIGHT PLAN 1 Press the FPL key KSTL Approoch ILS 30R MOODS iof 127 Figure 8 3 Active Flight Plan Window on the PFD 8 3 ACTIVATE A STORED FLIGHT PLAN 1 Press the FPL key and turn the small FMS knob to display the Flight Plan Catalog Page Figure 8 4 Flight Plan Catalog Page 2 Press the FMS knob to activate the cursor 8 9 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 3 Turn the large FMS knob to highlight the desired flight plan and press the ACTIVE softkey 4 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 8 4 ACTIVATE A FLIGHT PLAN LEG 1 From the Active Flight Plan Page press the FMS Knob to activate the cursor and turn the large FMS knob to highlight the desired destination waypoint 2 Press the ACT LEG softkey using MFD only OR
44. Mode is active nav 11 30 114 18 Sielu Flight Director command bars indicating descent on localizer glideslope path LOC2 is the active navigation receiver on the HSI Figure 6 20 Approach Mode If the CDI is not centered deviation gt 1 dot 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 16 depicts the Go Around mode on the PFD Glideslope is active 118 200 121 358 con 136 975 M Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 SECTION 6 AUTOMATIC FLIGHT CONTROL 6 7 EXAMPLE PROCEDURES USING AFCS a A NOTE The diagrams in the following examples This section provides a scenario based set of proce are for instructional purposes only and may not dures showing various autopilot modes used during a be current flight In this scenario the aircraft departs Reid Hillview Airport KRHV from runway 13L enroute to Fresno Yo semite 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 VOR TAC PXN using VOR navigation then fly airway V230 using a GPS fligh
45. OMI push to talk key is stuck COM2 PTT COM2 push to talk key is stuck COM1 RMT XFR COM1 remote transfer key is stuck COM2 RMT XFR COM2 remote transfer key is stuck RAIM UNAVAIL RAIM is not available trom FAF to MAP waypoints The GIA1 and or GIA 2 has incorrect software installed The G1000 system should be serviced The system has detected an over temperature condition in COM1 and or COM2 The transmitter will operate at reduced power If the problem persists the G1000 system should be serviced The system has detected a failure in COM1 and or COM2 COM1 and or COM2 may still be usable The G1000 system should be serviced when possible The COM1 and or COM2 external push to talk switch is stuck in the enable or pressed position Press the PTT switch again to cycle its operation 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 tion Press the transter switch again to cycle its operation If the problem persists the G1000 system should be serviced GPS satellite coverage is insufficient to perform Receiver Autonomous Integrity Monitoring RAIM trom the FAF to the MAP waypoints GPS satellite coverage is insufficient to perform Receiver Autonomous Integrity 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
46. Pitch Hold Mode 6 4 PLAY key 5 4 PROC key 1 3 Red pointer 2 3 Remove departure arrival or approach 8 5 Replies 4 4 Reversionary mode 11 1 Roll Axis Modes 6 2 6 9 Roll Hold 6 9 6 14 6 16 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 4 1 7 Speed ranges 2 3 Squelch 5 3 Store Flight Plan 8 5 Stormscope lightning data 1 4 1 7 10 2 10 3 Strike 10 2 Strike mode 10 2 System annunciations 12 1 12 5 System message advisories 12 7 T TA 10 8 12 5 TAF 10 3 10 4 TAS 1 4 10 8 10 9 12 5 12 13 Terrain 10 9 12 9 Terrain proximity 10 9 TIS 1 4 10 7 10 8 12 16 Tornado 10 5 Traffic Advisory 10 7 10 8 10 9 12 5 Traffic map page 10 7 10 8 10 9 Transponder 4 4 Transponder Status bar 4 4 Trend vector 2 6 Tropical storms 10 5 Turn rate indicator 2 6 TX 4 3 V Vertical Deviation Glideslope indica tor 2 4 Vertical speed 1 4 2 1 2 5 6 4 6 6 6 14 12 1 Vertical Speed Bug 2 5 Vertical Speed Mode 6 6 VFR code 4 5 VHF 4 1 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 Voice alerts 12 5 VOL PUSH ID 4 2 VOL PUSH SQ 4 2 4 3 Volume squelch 5 3 VS 1 4 6 4 6 6 6 14 Vspeeds 2 3 W WARN 2 7 Warning 12 1 12 2 12 4 Weather data link page 10 4 Weather product symbols 10 6 Weather warnings 10 5 Wind direction 10 5 Wind speed 10 5 X XM weather 10 3 10 4 XP
47. Pressing this knob toggles the tuning cursor light blue box between the COM1 and COM2 fields 8 COM Frequency Toggle Key Toggles 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 destina tion waypoint and establish a direct course to the selected destination specified by the identifier chosen from the active route or taken from the map cursor 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 can cels 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 dif ferent windows using the small and large knobs The large knob is used to move the cursor on the
48. S Part Number Change Summary 190 00525 00 Initial release Revision Date of evsion fected Pages 7 05 Initial release Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 V RECORD OF REVISIONS This page intentionally left blank vi Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 TABLE OF CONTENTS SECTION 1 SYSTEM OVERVIEW 1 1 Ground Mode AULOMATIC sosassevssnurissnnsintsossssssas 4 4 1 1 PFD MFD Controls cccccccccssssssssscesssssseee 1 2 REDY SATUS ax stnansssstncntacatescncenercacsncsstlaveiesiivet 4 4 1 2 PFD Softkeys ccssssssssssssssssssssssssssssssseseeen 1 4 COVE SeT sosen 4 4 1 3 MFD Softkeys oo ccs 1 7 PIQMIE IE ROOTING satssctscassnssstadinsbdintonscesbhinthadstinesethless 4 5 15 Backlghting yg SECTION 5 AUDIO PANEL 5 5 1 COM Radio Selection 0 cece 5 2 SECTION 2 FLIGHT INSTRUMENTG 2 1 5 2 Marker Beacon Receiver Ded 2 1 Airspeed Indicator 2 3 Marker Beacon Signal Sensitivity ccsceseseeseeseeren 5 2 Speed Indication vv 2 3 5 3 Nav Radio Audio Selection ccccce 5 2 Speed RANGES v s 2 3 5 4 Intercom System ICS Isolation 0 5 3 Airspeed Trend Vector nssr 2 3 5 5 Intercom Squelch Control 0 0 0 0 5 3 Vspeed References s is 2 3 5 6 Digital Clearance Recorder with Playback 2 2 Attitude Indicator cccccccccccccsssssseeeeeeeeeeee 2 3 CODA ii contesatixstdrivini
49. S NAV1 and NAV2 DME optional Press to display the DME Tuning window XPDR Press to display the transponder mode selec tion softkeys STBY Press to select standby mode ON Press to select mode A ALT Press to select altitude reporting mode VFR Press to automatically squawk 1200 only in the U S A refer to ICAO standards for VFR codes in other countries CODE Press to display transponder code selection softkeys 0 7 0 through 7 Press numbers to enter code Ja rn to return softkeys a a a ol a ol A CDI VOR2 F Press the BACK softkey IDENT Press to provide special aircraft position identification to Air Traffic Control ATC BKSP Press to remove numbers entered one at a time BACK Press to return to the previous level softkeys IDENT Press to provide special aircraft position identification to Air Tratfic Control ATC BACK Press to return to the previous level softkeys IDENT Press to provide special aircraft position identification to Air Traffic Control ATC TMR REF Press to display the Timer References window NRST Press to display the Nearest Airports window ALERTS Press to display the Alerts window n D to the top level Press the BACK softkey to return to the top level softkeys ee ee ee De nN Figure 1 5 PFD Softkey Flow Chart 3 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 1 3 MFD SOFTKEYS
50. TE Fuel calculations do not use the aircraft fuel quantity indicators and are calculated from the last time the fuel was reset SYSTEM System OIL C 90 Information DAES FUEL CALC FFLOW GPH 14 2 GAL REM 0 0 Fuel Calculation 0 0 Information 0 ELECTRICAL 1 ALT LOAD _2 44 6 Flectrical Information 1 BUS VOLTS 2 28 0 274 Figure 3 3 SYSTEM Engine Page Any exceedance of default Engine Page parameters while viewing the System Engine Page will cause the dis play to automatically switch back to the default Engine Page 3 2 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 SECTION 4 NAV COM amp TRANSPONDER SECTION 4 NAV COM AND TRANSPONDER The Nav Com controls and frequency windows are lo cated on the Primary Flight Display and the Multi Func tion Display in the same locations NAV COM Controls NAV Frequency Window COM Frequency Window Controls navi 113 25 110 90 ors 199m o 095 me 095 118 900 gt 133 000 com vous Navz11 80 110 98 f p124 908 135 325 conz 7000 6300 ee USI 1 2 CRS 4 BARO TORT are 6500 Jkh 15TH LP OR RLI 07 10 15 INSET FD CD XPDR IDENT THR REF NRST ALERTS Figure 4 1 G1000 VHF NAV COM Interface PFD Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 4 1 SECTION 4 NAV COM amp TRANSPONDER Standby NAV Selected NAV Selected COM Standby COM Frequency Field Frequency Navi
51. TE The Beechcraft A36 G36 Pilot s Operating Handbook POH 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 Beechcraft A36 G36 11 1 SECTION 11 ABNORMAL OPERATION 11 2 ABNORMAL COM OPERATION When a COM tuning failure is detected by the system the emergency frequency 121 500 MHz is automatically loaded into the active frequency field of the COM radio for which the tuning failure was detected In the event of a dual display failure the emergency frequency 121 500 MHz automatically becomes the active frequency to the pilot through the pilot headset 11 3 UNUSUAL ATTITUDES The PFD will declutter when the aircraft enters an un usual attitude Only the basic primary functions will be displayed in these situations 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 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 en sure that the strike and or cell positions are depicted ac curately in relation to the nose of the aircraft 11 2 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 SECTION
52. TROL Flying a Flight Plan GPS Course gt 1 The aircraft is currently tracking inbound on the 116 degree radial of Panoche VORTAC Enter Panoche VORTAC PXN and Clovis VORTAC CZQ into the GPS flight plan in preparation to intercept this leg 2 With the flight plan activated press the CDI softkey to set the CDI to GPS This cancels VOR mode and the autopilot loses the VOR signal As a result the VOR annunciation flashes yellow and the autopilot reverts to default Roll Hold ROL mode Flashes for ten seconds then transitions to ROL 23 0 lt _ G PS D Ode Panoche VORTAC PXN Now press the NAV key to reactivate the auto pilot using GPS guidance At this moment the autopilot couples to GPS guidance and steers the aircraft toward the active flight plan leg Once the flight plan leg is intercepted the autopilot continues to track GPS guidance to the end of the flight plan 23 0 27 Clovis Figure 6 24 Transition to GPS Flight Plan 6 16 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 Flight Level Change Descent 1 In preparation for the approach to KFAT set Selected Altitude to 3 000 feet using the ALT knob Press the FLC key FLC is annunciated with the airspeed reference which defaults to the current aircraft airspeed Altitude Hold mode is armed automatically The current cruise speed of 142 knots will be used for the descent a ALT 2
53. abase 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 Beechcraft A36 G36 12 9 SECTION 12 ANNUNCIATIONS amp ALERTS GMA 1347 Alert Messages 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 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 using The audio panel is using a backup communication path The G1000 system should backup data path be serviced when possible GIA 63 Alert Messages Alerts Window Message
54. ages the autopilot Pressing it also acknowledges an autopilot disconnect e CWS Control Wheel Steering Button Located on the pilots control wheel pressing and holding the CWS button disengages the control surface servos without disengaging the autopi lot If the flight director has not been activated pressing the CWS button will activate the flight director in the default pitch and roll hold modes GA Go Around Button Located on the sub panel or throttle lever the GA button disengages the autopilot and selects the Go Around Pitch and Roll wings level modes e MET Manual Electric Trim Switch This switch is used to operate manual electric pitch trim Moving both switches forward simultane ously trims the aircraft nose down Moving both switches aft simultaneously trims the aircraft nose up The left switch is the ARM contact and the right switch controls the up down trim Pressing the ARM switch disengages the autopilot if cur rently engaged If one side of the switch is active for more than three seconds without the other side also being active PTRM is displayed in the AFCS System Status field on the PFD Pressing SECTION 6 AUTOMATIC FLIGHT CONTROL the MET ARM switch also acknowledges an auto pilot disconnect Figure 6 1 AFCS Keys Pressing the FD key activates only the flight director in the default Pitch Hold Roll modes without engaging the autopilot Pressing the AP key activates the f
55. alid for navigation use Note that AHRS utilizes GPS inputs during normal operation AHRS opera tion may be degraded if GPS signals are not present see POH Display is not receiving valid transponder information np A red X through any other display field such as engine instrumentation LEAO EG A aE fields indicates that the field is not receiving valid data 12 6 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 A red X may be the result of an LRU or an LRU func tion failure The Figure 12 6 illustrates all possible flags and the responsible LRUs GIA 63 Integrated Avionics Units GEA 71 Engine Airframe Unit R O GIA 63 Integrated Avionics Unit FUEL FLOW GPH CHT T r OIL TEMP _ OIL PRES r AMPS a VOLTS ENGINE GDC 74A Air Data Computer t INTEG SECTION 12 ANNUNCIATIONS amp ALERTS ar GIA 63 Integrated Avionics Units GDC 74A Air Data Computer GRS 77 AHRS OR GMU 44 Magnetometer GIA 63 Integrated Avionics Units XPDR IDENT TMREREF NRST ALERTS Figure 12 6 G1000 System Failure Annunciations 12 5 G1000 SYSTEM ALERT MESSAGES This section describes various G1000 system alert mes sages Certain messages are issued due to an LRU or an LRU function failure Such messages are displayed in the Alerts Window and are normally accompanied by a cor responding red X annunciation as shown previously in the G1000 System Annunciation sectio
56. ancel the direct to Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 7 3 AIRPORT INFORMATION Figure 7 5 Airport Information Page Select the Airport Information Page 1 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 1 Press the FMS knob to activate the cursor 2 Turn the large FMS knob to select the facility name or location city field 3 Turn the small FMS knob to select the desired character 4 Turn the large FMS knob to select the next character field 5 Repeat steps 3 and 4 until the facility name or location is selected then press the ENT key It there are duplicate names in the database a list is displayed from which to chose the desired location SECTION 7 NAVIGATION 7 To remove the flashing cursor press the FMS knob Access Runway Information 1 Press the FMS knob to activate the cursor 2 Turn the large FMS knob to place the cursor on the Runways field 3 Turn the small FMS knob to display the next runway for the selected airport 4 Continue turning the small FMS knob to select the desired runway 5 To remove the flashing cursor press the FMS knob Access Frequency Information 1 Press the FMS knob to activate the cursor 2 Turn the large FMS knob to move the cursor to the Frequencies window Turn either FMS knob to scroll t
57. ap Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 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 Maximum o of 181 LEa topograph f presently fa displayed on screen Minimum a of topograph fs presently isplayed on screen Aircraft altitude pane of topography eleva Ground elevation tion a y dis at present aircraft played on screen position Figure 10 16 Topography Scale 10 10 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 SECTION 11 ABNORMAL OPERATION 11 1 REVERSIONARY MODE Should a system detected failure occur in either dis play 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 ac tivated 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 reversion ary mode A NO
58. ated airspeed is displayed inside the black pointer The pointer will become red upon reaching Vne Figure 2 5 Red Pointer at Vne Speed Ranges The color coded speed range strip denotes flaps op erating range normal operating range and never exceed speed Vne A red range is also present for low speed awareness Refer to the Pilots Operating Handbook POH 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 SECTION 2 FLIGHT INSTRUMENTS Vspeed References Vspeed References are turned on or off in the Timer References window Press 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 dis play 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 point er 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 tra ditional slip skid indicator D Roll Pointer 2 Roll Scale G Horizon Line 4 Aircraft Symbol G Land Representation Roll Index
59. ay still be available Elevator Mistrim Up TELE 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 Elevator Mistrim Down IF A condition has developed causing the pitch servo to provide a sustained force Be prepared to apply nose down control wheel force upon autopilot disconnect Aileron Mistrim Lett P A condition has developed causing the roll servo to provide a sustained left force En sure the slip skid indicator is centered and observe any maximum fuel imbalance limits Aileron Mistrim Right A condition has developed causing the roll servo to provide a sustained right force En sure the slip skid indicator is centered and observe any maximum fuel imbalance limits Rudder Mistrim Left Di A condition has developed causing the yaw servo to provide a sustained force Ensure the slip skid indicator is centered and observe any maximum fuel imbalance limits Rudder Mistrim Right A condition has developed causing the yaw servo to provide a sustained force Ensure the slip skid indicator is centered and observe any maximum fuel imbalance limits Preflight Test PFT Performing preflight system test Upon completion the aural alert will be heard PET Preflight system test has tailed Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 SECTION 12 ANNUNCIATIONS amp ALERTS 12 4 G1000 SYSTEM
60. begin displaying traffic TIS OPERATIING is displayed in the Traffic mode field 4 Press 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 for a period longer than 6 sec onds 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 sec onds traffic will be removed from the display Taf Mode descending movieg in the drecion H 17 95 BEXIE Last data update Traffic 1600 above amp is older than 6 altitude level flight amp moving climbing moving in the Proximity Traffic at same sec resulting in in the direction of the line Coast mode direction of the line Figure 10 11 Traffic Map Page Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 SECTION 10 HAZARD AVOIDANCE Displaying Traffic on the Navigation Map 1 Ensure TIS is operating With the Navigation Map displayed press the MAP softkey 2 Press the TRAFFIC softkey Traffic will now be displayed on the map TIS Audio Alert When a Traffic Advisory TA is displayed an audio alert Traffic is gi
61. ced error Contig service req d SW MISMATCH GDU software The MFD and PFD have different sottware 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 overheating 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 12 8 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 SECTION 12 ANNUNCIATIONS amp ALERTS Database Alert Messages Alerts Window Message Comments MFD1 DB ERR MFD1 aviation database error exists The MFD and or PFD detected a failure in the aviation database Attempt to reload PFD1 DB ERR PFD1 aviation the aviation database It problem persists the G100
62. ckpit Reference Guide for the Beechcraft A36 G36 1 7 SECTION 1 SYSTEM OVERVIEW 1 4 MFD PAGE GROUPS 1 Turn the large FMS knob until the desired page group is selected 2 Turn the small FMS knob to select pages within the group See Figure 1 7 Nearest Group Auxiliary Page Group Number of Pages in Current Group Waypoint Page Group Map Page Group Figure 1 7 Page Group Icon Selected Page 1 5 BACKLIGHTING To manually adjust the backlight for the PFD and MFD 1 Press the MENU key on the PFD to display the PFD Setup Menu window 2 Press the small FMS knob to activate the cursor PFD DSPL gt AUTO is now high lighted 3 Turn the small FMS knob to display the selection window Figure 1 8 PFD Setup Menu Window 4 Turn the FMS knob to select MANUAL then press the ENT key 5 With the intensity value now highlighted turn the small FMS knob to select the desired backlighting 6 Turn the large FMS knob to highlight MFD DSPL gt AUTO and repeat steps 3 through 5 PFD DSPL MFD DSPL 1 8 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 SECTION 2 FLIGHT INSTRUMENTS SECTION 2 FLIGHT INSTRUMENTS navi 113 25 110 90 aT DIS DTK TRE 118 988 133 888 com NAVZ 116 98 124 308 COH 195 yt ET INSET PFD CDI DHE MPDR IDENT TWR REF NRST ALERTS O NAV Frequency Window E Turn Rate Indicator 2 Airspeed Indicator Barometric Setti
63. control SFC pressing the SFC softkey for Surface Analysis shows current or forecast conditions Forecasts SECTION 10 HAZARD AVOIDANCE are available for intervals of Current 12 24 36 and 48 hours Press the softkey corresponding to the desired forecast The closest city forecast information is displayed in the legend The dis play is updated every 12 minutes FRZ LVL press the FRZ LVL softkey to display contour lines for freezing levels The display is updated every 12 minutes WIND press 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 incre ments After pressing the WIND softkey press the softkey corresponding to the desired winds aloft altitude The display is updated every 12 minutes COUNTY pressing 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 every 5 minutes CYCLONE pressing the CYCLONE softkey shows the current location of cyclones hurricanes and tropical storms and their projected track at vari ous time intervals The update rate is every 12 minutes Map Panning Information Weather Data Link Page ik Push in the joystick to display the panning arrow Move the joystick to place the panning arrow onAIRMETs TFRs METARs or SIGMETs Press the ENT
64. craft A36 G36 SECTION 1 SYSTEM OVERVIEW SECTION 1 SYSTEM OVERVIEW This guide gives the pilot abbreviated operating in structions for the Primary Flight Display PFD Multi The purpose of this Cockpit Reference Guide is to Function Display MFD and the GMA 1347 Audio Panel provide the pilot a resource with which to find operat System ing instructions on the major features of the G1000 e system more easily It is not intended to be a A NOTE The pilot should read and thoroughly comprehensive operating guide Complete operat understand the Beechcraft A36 G36 Pilot s Oper ating Handbook POH for limitations procedures and operational information not contained in this Cockpit Reference Guide The Beechcraft e G1000 Primary Flight Display Pilots Guide A36 G36 POH always takes precedence over the e G1000 VHF NAV COM Pilots Guide information found in this guide e G1000 Transponder Pilots Guide e G1000 GMA 1347 Audio Panel Pilots Guide and Supplement e G1000 Engine Indication System Pilots Guide e Gl1000 AFCS Pilots Guide e G1000 Multi Function Display Pilots Guide e G1000 Optional Equipment Pilots Guide ing procedures for the complete system are found in the following documents Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 1 1 SECTION 1 SYSTEM OVERVIEW 1 1 PFD MFD CONTROLS O 0 0 Oo 0O 00 a Figure 1 3 PFD MFD Controls OOG 000 PUSH CRSA MFD Only ie Garmin G1000 Cock
65. ctive and ALT is now displayed in green in the Active Mode field with the cur rent altitude displayed in the Altitude Reference field 2 Pitch and roll commands will be given to manu ally maintain the current altitude Press the AP key to engage the autopilot for maintaining the current altitude Altitude Hold mode is active na 113 00 116 98 ITXD w 118 96 IT Flight Director command bars hold pitch attitude to maintain the altitude reference SECTION 6 AUTOMATIC FLIGHT CONTROL To change aircraft altitude press and hold the CWS button and manually maneuver to the desired altitude Upon reaching the desired altitude release the CWS button for at least one second Momentarily press the CWS button a second time to synchronize the autopilot to the new altitude This new altitude is now displayed in the Altitude Reference field The autopilot will now hold the aircraft at this altitude Altitude Reference 118 788 cont 123 888 Figure 6 13 Altitude Hold Mode Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 SECTION 6 AUTOMATIC FLIGHT CONTROL Vertical Speed Mode VS 6 6 1 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 Soeed Bug will appear on the Ve
66. de erissa 10 2 10 3 XM Weather Optional 0 0 0 10 3 Displaying METAR and TAF information on the Airport Information Page c scssessessessesseseesesssen 10 3 Displaying Weather on the Weather Data Link Page 10 4 NEXRAD Umat inienn 10 4 Map Panning Information Weather Data Link Page 10 5 Weather Products and Symbols csseseseeseeseesen 10 6 Weather Product Age ssesssssssssesssssssssssesseen 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 8 TIS Audio Alert vo eescesscesseesssessessseesessessesssesneesneeseen 10 8 10 5 Skywatch Traffic Advisory System TAS Optional 0 0 0 0 cesses 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 Proximity PA casts screredtetntat tee ayinnte araccacuannoccetaoins 10 9 Displaying Terrain and Obstacles on the Navigation MaD sranane 10 9 SECTION 11 ABNORMAL OPERATION 11 1 11 1 Reversionary Mode 0 ccccseeeeeen 11 1 11 2 Abnormal COM Operation 0 0 000 11 2 11 3 Unusual Attitudes ccs 11 2 11 4 Stormscope Operation with Loss of Heading Input ccs 11 2 SECTION 12 ANNUNCIATIONS amp ALERTS 12 1 12 1 Alert Level Definitions
67. dow when pressed The G1000 Alerting System as installed in Beechcraft A36 G36 aircraft uses four alert levels e WARNING This level of alert is time critical and requires immediate pilot attention A warning annunciation is displayed in the Annunciation Window as red text A warning annunciation is ALERT MESSAGE These messages are provided to make the pilot aware of G1000 system problems or status and may not require pilot action An alert message is accompanied by a flashing white also accompanied by a flashing red WARNING ADVISORY softkey label as shown in Figure 12 4 soltkey label as shown in Figure 12 2 Pressing Pressing the ADVISORY softkey acknowledges the the WARNING softkey acknowledges the presence presence of the advisory alert The softkey has now of the warning alert and stops the aural tone if reverted to the ALERTS softkey label and displays applicable The softkey has now reverted to the ALERTS softkey label and displays a description of the warning annunciation in the Alerts Window when pressed a description of the alert message in the Alerts Window when pressed e CAUTION This level of alert indicates the exis tence of abnormal conditions on the aircraft that may require pilot intervention A caution annunciation Figure 12 2 WARNING Softkey Annunciation is displayed in the Annunciation Window as yellow text A caution annunciation is also accompanied by a flashing yellow WARNING softkey label
68. e a New Flight Plamn 0 cces 8 4 Create a new flight plan using the PFD 8 4 8 8 Load a Departure 0 cesses 8 5 8 9 Load an Arrival cccccesessessessseesseessessees 8 5 8 10 Load an Approach ose 8 5 8 11 Remove a Departure Arrival or Approach from a Flight Plan cscs 8 5 8 12 Store a Flight Pham cscs 8 5 8 13 Edit a Stored Flight Plan cee 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 essen 8 6 8 18 Graphical Flight Plan Creation 8 6 8 19 Trip PlaNMing ccs teases 8 7 SECTION 9 PROCEDURES 0 oc 9 1 9 1 Arrivals and Departures 5511151111111111112 9 1 Load and Activate a Departure Procedure cscse 9 1 Load and Activate An Arrival Procedure 9 1 9 2 Approaches 00 0 ccc 9 2 Load and or Activate an Approach Procedure 9 2 Activate An Approach in the Active Flight Plan 9 3 viii Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 SECTION 10 HAZARD AVOIDANCE 00000 10 1 10 1 Customizing the Hazard Displays on the Navigation Map 0 ccccccssseseseseesen 10 1 10 2 Stormscope Optional 0 0 10 1 Displaying Stormscope Lightning Data on the Navigation Map Page csssssssssssssssesensees 10 1 SOS COPE Fa
69. e desired identifier is entered Press the ENT key and the cursor is now ready for entering of the next flight plan waypoint Repeat steps 2 through 5 to enter the identifier for each additional flight plan waypoint Once all waypoints have been entered press the FMS knob to return to the Active Flight Plan Window Figure 8 12 Creating Flight Plan on the PFD Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 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 8 12 REMOVE A DEPARTURE ARRIVAL OR APPROACH FROM A FLIGHT PLAN With the Active or Stored Flight Plan Page dis played press the small 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 FLIGHT PLAN From the Flight Plan Page press the FMS knob to activate the cursor Turn the large FMS knob to highlight the desired flight plan and press the MENU key to di
70. e of the GDL 69 Weather Interface for hazardous weather penetration is prohibited Weather information provided by the GDL 69 is approved only for weather avoidance not penetration Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 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 Beechcraft A36 G36 aircraft has a very high degree of func tional 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 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
71. electronic NAVI gation 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 Beechcraft A36 G36 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 aN 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 1043 MFD displays use a lens coated with a special anti reflective coating that is very sensitive to skin oils waxes and abrasive cleaners CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI REFLECTIVE COATING It is very important to clean the lens using a clean lint free cloth and an eyeglass lens cleaner that is specified as safe for anti reflective coatings ii Garmin G1000 Cockpit Reference Guide for the
72. en to begin the turn to intercept the final approach course From this point the autopilot flies the ILS At the Decision Height press the AP DISC button and land the aircraft or press the GA button to execute a missed approach Figure 6 26 ILS Approach to KFAT Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 Go Around Missed Approach 1 When the decision is made to execute a missed approach apply full power and press the GA button The autopilot will disconnect and the flight director command bars will establish a 7 degree nose up climb Note when the autopilot disconnects the AP annunciation flashes yellow for five seconds Manually fly the aircraft to the command bars Following the published Missed Approach Pro cedure climb to the prescribed altitude Press the AP key re engaging the autopilot To have the autopilot fly to the hold point set the CDI to GPS by pressing the CDI softkey then press the NAV key The autopilot flies direct to Clovis VORTAC according to the loaded approach while maintaining the current attitude During the climb set a desired hold altitude in the Selected Altitude box by turning the ALT knob The CWS button may be used to manu ally set a new pitch attitude Doing this causes the autopilot to revert to the default Pitch Hold PIT mode and Altitude Hold is armed When the selected altitude is reached Altitude Hold mode will become active and the autopilot will
73. equency for a Controlling Agency 1 Select the Nearest Airspaces Page 2 Press the FREQ softkey and turn either FMS knob to select the desired trequency Press the Figure 7 16 Nearest Airspaces Page ENT key to load the frequency into the COM frequency standby field 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 Ifthe projected course takes the aircraft inside an airspace within the next ten minutes Ahead is Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 7 9 SECTION 7 NAVIGATION This page intentionally left blank 7 10 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 SECTION 8 FLIGHT PLANNING 8 1 USER DEFINED WAYPOINTS 17 95 136 975 T wa Sar Mal me Figure 8 1 User WPT Information Page Select the User WPT Information 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 Create a New User Waypoint 1 With the User Waypoint Information Page displayed press the FMS knob to activate the cursor 2 Turnthe FMS knobs to enter a name for the new waypoint and press the ENT key The message Are you sure you want to create the new user waypoint is displayed With YES highlighted press the ENT key SECTION 8
74. esseereeen 7 1 7 2 Direct to Navigation seen 7 1 Direct to Navigation from the MFD v s essen 1 1 Direct to Navigation from the PFD s s s 1 2 7 3 Airport Information 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 INTOrMatiOn cesccesessessessesseeseesees 7 3 7 4 Intersection Information 00 cccce 7 4 Select the Intersection Information Page seseseeee 7 4 Access Information on an Intersection csssseeseeerees 1 4 7 5 NDB Information 0 0 0 cccccs cesses 7 4 Select the NDB Information Page 7 4 View Information on a Specific NDB cesscesssesseeseesees 1 4 7 6 VOR Information 7 5 Select the VOR Information Page 7 5 Access Information ON AVOR ssesssessesssessseesseensees 1 5 7 7 User Waypoint Information Page 7 5 7 8 Nearest Airports uu tessa 7 5 Nearest Airport Information on the MPD sss 7 5 Nearest Airports Information on the PFD 7 6 7 9 Nearest Intersections 0 ccc 1 6 Select the Nearest Intersections Page 7 6 View Information on the Nearest Intersection 1 1 7 10 Nearest NDB ou ccsseesestesnssesesneesneeeens a Select the Nearest NDB Page sssesssessessneesneeen 1 1 Access Information on a Specific NDB cesscesseesseessees 1 1 7 11 Nearest VOR cece il Select the Nearest VOR Page csssesssess
75. evel at the new heading The same practice applies to holding roll attitude GPS Arm Capture Track APR VOR Approach Arm Capture Track ILS Approach Arm Capture Track Glideslope pitch mode automatically armed 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 activa tion is maintained by the autopilot If only the flight director is active command bars indicate the proper roll attitude Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 6 9 SECTION 6 AUTOMATIC FLIGHT CONTROL Heading Select Mode HDG 6 10 1 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 It the autopilot is engaged the aircraft will begin to turn toward the selected heading When the selected heading is reached the aircraft will main
76. formation NAVI Displays NAV1 waypoint frequency or identifier and DME information in the BRG1 information window GPS Displays GPS waypoint identifier and GPS distance information in the BRG1 information SECTION 1 SYSTEM OVERVIEW NAV2 Displays NAV2 waypoint frequency or identifier and DME information 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 window OFF Removes the BRGI information STD BARO Press to set the barometric pressure window to 29 92 inches of mercury 1013 hPa by pressing the METRIC softkey BRG2 bearing Press to cycle through the follow BACK Press to return to the previous level ing information softkeys INSET A optional optional optional nonrunonkink D S D Press the BACK or OFF softkey to return to the top level softkeys Figure 1 3 PFD Softkey Flow Chart 1 PFD optional a O O I O I L 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 4 PFD Softkey Flow Chart 2 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 1 5 SECTION 1 SYSTEM OVERVIEW OBS Press to select OBS mode on the CDI when navigating by GPS only available with active leg CDI Press to change navigation mode on the CDI between GP
77. ftkey to display a 360 viewing are or press the ARC softkey to display a 120 viewing area Press the CLEAR softkey to remove all Storm scope lightning data trom the display XM WEATHER OPTIONAL WARNING Use of XM weather for hazard ous weather penetration is not recommended Weather information provided by XM Radio Service is approved only for weather avoidance not penetration Press the MAP softkey Press the NEXRAD or XM LING softkey to dis play the desired weather Press the applicable softkey again to remove weather data from the Navigation Map Page SECTION 10 HAZARD AVOIDANCE BACK Figure 10 7 Navigation Map Page Displaying NEXRAD Weather Displaying METAR and TAF information on the Airport Information Page To display METAR and TAF text on the Air port 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 Press the WX softkey to display METAR and TAF text METAR and TAF intormation is updated every 12 minutes Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 10 3 SECTION 10 HAZARD AVOIDANCE NORTH UP AIRPORT KMSP UBLIC METAR Text TAF Text m APR JATI PAP eee r E vi STG ATR u AR Ezra W Er X iCELL Y ws t z Ai CIL Figure 10 9 Weather Data Link Page WX Softkey Figure 10 8 METAR and TAF Text Displayed on the Airport Weather Information Pa
78. ftware installed The G1000 system should be Communication halted serviced BACKUP PATH Transponder using The transponder is using a backup communications path The G1000 system should backup data path be serviced when possible GRS 77 Alert Messages Alerts Window Message Comments S AHRS TAS AHRS not receiving The AHRS is not receiving true airspeed from the air data computer The AHRS relies airspeed on GPS information to augment the lack of airspeed The G1000 system should be serviced AHRS GPS AHRS using backup GPS The AHRS is using the backup GPS path Primary GPS path has failed The G1000 source system should be serviced when possible AHRS GPS AHRS not receiving any The AHRS is not receiving any or any useful GPS information Check AFMS limita GPS information tions The G1000 system should be serviced AHRS GPS AHRS not receiving The AHRS is not receiving backup GPS information The G1000 system should be backup GPS information serviced AHRS GPS AHRS operating The 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 AHRS using backup The AHRS is using a backup communications data path The G1000 system should data path be serviced when possible AHRS SERVICE AHRS Magnetic field The AHRS earth magnetic field model is out of date Update magnetic field
79. gation Status Window Frequency Frequency Field gt 118 500 com 116 60 CKY VOR IRMATION 118 400 COM2 Figure 4 2 Frequency Fields Tuning Box Active NAV Active COM Tuning Box Frequency Field Frequency Field 135 100 COMI gt 121 900 conz Frequency Toggle Arrow Tuning Box Figure 4 3 Frequency Toggle Arrow and Tuning Box NAV Controls COM Controls VOL PUSH VOL PUSH ID Knob SQ Knob Frequency Toggle 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 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 4 1 RADIO STATUS INDICATIONS e TX When a COM radio is keyed a white TX indication appears to the right of the corresponding COM frequency ID When the Morse code identifier is ON for a 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 correspond ing NAV radio is selected on the audio panel 121 988 118 608 con TX COM2 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 EDA ES 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 select the desired COM sub window t
80. ge NEXRAD press 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 Certain limitations exist regarding the NEXRAD radar displays Some but not all are listed here Displaying Weather on the Weather Data Link Page To select the Weather Data Link Page 1 Turn the large FMS knob to select the Map Page Group 2 Turn the small FMS knob to select the fourth e NEXRAD base reflectivity does not provide suf rectangular page icon ficient information to determine cloud layers or precipitation characteristics hail vs rain etc e An individual NEXRAD site cannot depict high alti tude storms at close ranges and has no information 3 Press the available softkeys to select the desired XM weather product 4 Press the LEGEND softkey to view the legends about storms directly over the site for the selected products If necessary turn The resolution of displayed NEXRAD data is 2 kilo either FMS knob to scroll through the list Press meters Therefore when zoomed in on the display the small FMS knob or the ENT softkey to return each square block is 2 kilometers The intensity to the map level reflected by the square will be the highest level sampled within the 2 kilometer square area ECHO TOP press the ECHO TOP softkey to show 10 4 Garmin G1000 Cockpit Reference Gu
81. gine Page In a maximum power climb or cruise climb engine leaning may be done using the Leaning Pointer as a refer ence when adjusting fuel mixture SECTION 3 ENGINE INDICATION SYSTEM EIS 3 2 LEAN ENGINE DISPLAY we a IN HG 21 2 16 ae 5 Fuel Flow RPM 30909 Numeric 2350 Readout FFLOW GPH 14 8 Cylinder peak Difference temperature between peak and current Exhaust Gas temperature of Temperature selected cylinder Bar Graph EGT Readout For Selected Cylinder Cylinder Head Temperature Bar Graph CHT Readout For Selected Cylinder Figure 3 2 LEAN Engine Page Press the CYL SLCT softkey to select the desired cyl inder for monitoring The CYL SLCT softkey becomes disabled when the ASSIST softkey is pressed Pressing the ASSIST softkey causes the first cylinder that peaks to become highlighted and information for that cylinder to be displayed Any exceedance of default Engine Page parameters while viewing the Lean Engine Page will cause the display to automatically switch back to the detault Engine Page NOTE The pilot should follow the engine manufacturer s recommended leaning procedures in the Pilot s Operating Handbook POH Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 SECTION 3 ENGINE INDICATION SYSTEM EIS 3 3 ENGINE SYSTEM DISPLAY It desired use the DEC FUEL INC FUEL and RST FUEL softkeys to adjust the amount of fuel remaining for totalizer calculations A NO
82. hen by pressing the VOL PUSH SQ knob 4 4 QUICKLY ACTIVATING 121 500 MHZ Pressing and holding the COM Frequency Toggle key for approximately two 2 seconds automatically tunes the selected COM radio to the emergency frequency 4 5 SECTION 4 NAV COM amp TRANSPONDER OPTIONAL NAV RADIOS DME Radio optional The Tuning window is displayed by pressing the DME softkey DME Figure 4 7 Radio Tuning Window To change the DME tuning source 1 From the Tuning window turn the large FMS knob to highlight the DME source field Turn the small FMS knob to display the selec tion window Turn the FMS knob to select the desired mode and press the ENT key Figure 4 8 DME Selection Window Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 4 3 SECTION 4 NAV COM amp TRANSPONDER 4 6 FREQUENCY AUTO TUNING Auto tuning on the PFD IDENT TMR REF Figure 4 9 Nearest Airports Window PFD 1 Press 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 Toggle key to place the frequency in the active field NAV frequencies are entered automatically in the NAV window 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 t
83. hrough the list placing the cursor on the desired frequency UJ 4 Press the ENT key to place the selected fre quency in the standby field of the COM or NAV window 5 To remove the flashing cursor press the FMS Knob e TX transmit only RX receive only e PT part time frequency e additional information exists press the ENT key If a listed frequency has sector or altitude restrictions the frequency is preceded by an info designation Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 r3 SECTION 7 NAVIGATION 7 4 INTERSECTION INFORMATION 7 5 Select the Intersection Information Page 1 Turn the large FMS knob to select the WPT page group 2 Turn the small FMS knob to select the second rectangular page icon Figure 7 6 Intersection Information Page Access Information on an Intersection 1 With the Intersection Information Page dis played press the FMS knob to activate the cursor 2 2 Turn the FMS knobs to enter a name for the identifier and press the ENT key 3 Press the FMS knob to remove the flashing Cursor NDB INFORMATION Figure 7 7 NDB Information Page Select the NDB Information Page 1 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 With the NDB Information Page displayed press the FMS knob to ac
84. i ated by the green ALT flashing for ten sec onds Upon reaching the selected altitude the auto pilot completes the capture process and levels the aircraft From this point the autopilot continues to operate in Altitude Hold mode 70 ALT Mode 5 6 14 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 SECTION 6 AUTOMATIC FLIGHT CONTROL Intercepting a VOR Radial 3 The system calculates the point at which the After climbout the autopilot continues to fly the aircraft au pel or Uien e o vay on a heading of 070 degrees at an altitude of 7 000 feet en h enine o m a i Next intercept airway V107 to Panoche VORTAC PXN S A Hi vans field The autopilot begins turning to intercept 1 Tune the VOR f th t the CDI t SE a ea le Oe re 2 the selected course VOR by pressing the CDI softkey Fa Set the Selected Course to 116 degrees using the CRS knob Note the autopilot is still in 4 The autopilot continues the turn until the Heading mode and continues to fly a heading aircraft is established on the selected course of 070 degrees 2 Press the NAV key This arms the Naviga tion mode and the white annunciation VOR appears to the left of the active Heading mode VOR HDG JAP YD ALT 7000er HDG Mode VOR Armed 4 Panoche VORTAC PXN Figure 6 23 Intercepting a VOR Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 6 15 SECTION 6 AUTOMATIC FLIGHT CON
85. ide for the Beechcraft A36 G36 the location elevation and direction the high est 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 descrip tion of the ECHO TOPS coding The display is updated every 7 5 minutes CLD TOP press the CLD TOP softkey to show the cloud top altitude determined from satellite imagery The display is updated every 15 minutes LING pressing the LTNG softkey shows the location of cloud to ground lightning strikes The display is updated every five minutes A NOTE Strikes depicted represent cloud to ground strikes within a 2 km radius of the actual strike location Therefore the exact location of the strike is not displayed CELL MOV pressing the CELL MOV softkey shows storm cell movement by displaying an arrow point ing in the direction of predicted movement The display is updated every 12 minutes SIG AIR pressing the SIG AIR softkey shows SIGMET and AIRMET information The display is updated every 12 minutes METAR press the METAR softkey to graphically dis play METARs METARS are shown as colored flags at airports providing METAR reports The display is updated every 12 minutes MORE WX press the MORE WX softkey to display the following group of softkeys for additional weather
86. ight Director command bars maintain desired pitch reference Altitude Hold mode is automatically armed with ALT displayed white in the Armed Mode field to the right of the PIT annunciation If the autopilot is engaged pitch attitude can be adjusted in 0 5 degree increments by press ing the NOSE UP NOSE DN keys Aircraft pitch may also be changed by press ing and holding the CWS button to manually establish the desired pitch using the control wheel When the CWS button is released the current pitch angle will be maintained This method must be used when using only the flight director If desired entered an altitude in the Selected Altitude Box by turning the ALT knob With mode armed 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 signals the altitude capture is complete and the selected altitude will be maintained Altitude Hold mode is armed 118 700 cons 123 800 A Figure 6 12 Pitch Hold Mode Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 If only the flight director is engaged pitch and roll commands are given to manually maintain the selected altitude If no altitude has been selected Altitude Hold will not become active and the current pitch attitude will be maintained Altitude Hold Mode ALT 1 Press the ALT key The flight director is activated if not already a
87. ircraft heading A NOTE When making a backcourse approach set Selected Course to the localizer front course Navigation Mode is active using GPS source 113 68 117 95 nov2 108 08 Flight Director command bars indicating a left turn to track GPS course and a climb to intercept Selected Altitude Figure 6 19 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 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 Flight Level Change mode is active Altitude Hold is armed 133 558 121 988 128 058 cons Selected Course GPS is active navigation receiver on the HSI Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 6 11 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 am NOTE The Glideslope mode is automatically armed when LOC mode is selected on the HSI Approach
88. lerting System The G1000 system issues audio alert tones when specific system conditions are met See the Alert Levels Definitions section for more information ciation is displayed at the top of the Annunciation System Annunciation Window Red X e Alerts Window The Alerts Window displays annunciation and alert message text Up to 64 a Annunciation prioritized alerts can be displayed in the Alerts AFI DOOR Window Window Pressing the ALERTS softkey displays as the Alerts Window Pressing the ALERTS softkey LERTS AVIONICS FAN Cooling fon for again removes the Alerts Window from the display ais eet ea Me E Alerts Window When the Alerts Window is displayed the pilot may TRAFFIC FAIL Traffic device use the large FMS knob to scroll through the alert has Failed list Higher priority alerts are displayed at the top SUAS GHAT is inoperative WARNING of the window Lower priority alerts are displayed CAUTION S ADVISORY and at the bottom of the window ALERTS Softkey Annunciation When an alert is issued the ALERTS softkey is used as a flashing ALERTS Softkey Figure 12 1 G1000 Alerting System Annunciation Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 12 1 SECTION 12 ANNUNCIATIONS amp ALERTS 12 1 ALERT LEVEL DEFINITIONS the advisory alert The softkey has now reverted to the ALERTS softkey label and displays a description of the advisory annunciation in the Alerts Win
89. light director and yaw damper and engages the autopilot When only the flight director is engaged pressing the FD key disen gages 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 in valid or unavailable the command bars are removed from the display Figure 6 2 Command Bars 6 1 MODE ANNUNCIATIONS Mode annunciations are displayed on the PFD Figure 6 3 shows the AFCS Status Bar 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 dis played in green Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 6 1 SECTION 6 AUTOMATIC FLIGHT CONTROL Active Mode Armed Mode GPS ROLJAP YD Autopilot Status Roll Axis Modes Yaw Damper Status Mode Reference Active Mode Armed Mode ALT Pitch Axis Modes AFCS Status Bar nevi 113 08 118 9 Jera xD wf 118 98 11x0 System Status Field see Annunciations amp Alerts Aircraft Attitude Symbol Flight Director Command Bars 6 2 OVERSPEED PROTECTION An overspeed annunciation flashing inverse video is displayed above the airspeed tape Figure 6 4 Overspeed Annunciation When an overspeed caution occurs red
90. ly after an aviation database update Verity that the user moditied procedures in stored flight plans are correct and up to date 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 pl RGAE np hoecing rele Aircraft is approaching target altitude Prepare to level aircraft Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 12 15 SECTION 12 ANNUNCIATIONS amp ALERTS Miscellaneous Alert Messages Cont Alerts Window Message Comments S 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 aa Seen i Arriving at waypoint xxx 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 ARSPC AHEAD Airspace ahead less Special use airspace is ahead of aircraft The aircraft will penetrate the airspace than 10 minutes within 10 minutes than 2 nm not
91. modes including Altitude Hold Other roll axis modes may be selected after Go Around mode engagement Subsequent autopilot engagement is also al lowed If the pitch attitude is changes manually e g with CWS button or the NOSE UP NOSE DN keys Pitch Hold mode will automatically be selected Autopilot disconnect annunciation Go Around mode is ac flashes yellow for 5 seconds tive in both pitch axis amp roll axis modes 114 18 socl wr DIS DTk Rx ee 121 358 com 136 4 15 m nove 108 00 Flight Director command bars indicating climb Figure 6 16 Go Around Mode 6 8 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 SECTION 6 AUTOMATIC FLIGHT CONTROL 6 6 ROLL AXIS MODES If the aircraft bank angle is lt 6 degrees when the key is pressed the aircraft will be main tained at wings level If only the flight direc tor is active command bars give guidance to AFCS a maintain wings level Roll Hold mode is annunciated by ROL a ROL T Heading Select HDG Figure 6 17 Roll Hold Mode VOR Enroute Arm Capture Track 2 Anew heading can be established by pressing GPS Arm Capture Track and holding the CWS button and manually Mode annunciations for active roll axis modes are shown in green during normal operation BC Arm Capture Track turning the aircraft to the desired new heading LOC Arm Capture Track Release the CWS button and the aircraft will No Glideslope NAV maintain wings l
92. n GTX 33 Transponder OR GIA 63 Integrated Avionics Units NOTE This section provides information regard ing G1000 alert messages that may be displayed by the system Knowledge of the aircraft systems flight conditions and other existing operational priorities must be considered when responding to a message Always use sound pilot judgment The Beechcraft A36 G36 Pilot s Operating Hand book POH takes precedence over any conflicting guidance found in this section Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 12 7 SECTION 12 ANNUNCIATIONS amp ALERTS MFD amp PFD Alert Messages 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 servi
93. nauthorized commercial distribution of this manual or any revision hereto is strictly prohibited Garmin is a registered trademark of Garmin Ltd or its subsidiaries and G1000 is a trademark 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 and SkyWatch are registered trademarks of L 3 Communica tions and XM is a registered trademark of XM Satellite Radio Inc July 2005 190 00525 00 Rev A Printed in the U S A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 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 safe 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 cu
94. ndow Text Alerts Window Message Audio Alert BUSES TIED Bus 2 is tied to Bus 1 Alert Message Alerts Window Message Audio Alert PFD FAN FAIL The cooling fan for the PFD is inoperative MFD FAN FAIL The cooling fan for the MFD is inoperative AVIONICS FAN The cooling fan for remote avionics is inoperative Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 12 3 SECTION 12 ANNUNCIATIONS 12 4 amp ALERTS 12 3 AFCS ALERTS System Status Field System Status Field T z The following AFCS alert annunciations appear in the AFCS System Status field on the PFD WARNING Red annunciation is time critical and Ti indicates an abnormal AFCS condition requiring Figure 12 5 AFCS System Status Field immediate pilot attention e CAUTION Yellow annunciation indicates the existence of abnormal AFCS conditions that may require pilot intervention 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 Yaw Damper Failure Yaw Damper control failure System Failure AFCS AP and MET are unavailable FD m
95. ng Box G True Airspeed Box Vertical Speed Indicator 4 Heading Box 12 Altimeter Horizontal Situation Indicator 13 Altitude Reference Box 6 Outside Air Temperature Box COM Frequency Window 7 System Time Box 15 Navigation Status Bar Transponder Status Bar Slip Skid Indicator Figure 2 1 Default PFD Information Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 Ij SECTION 2 FLIGHT INSTRUMENTS nav1 188 08 PT DIS DTK TRE 118 688 con HAVZ 136 975 coMZ ALERTS Alternator 1 offline ALT 2 SWITCH Alternotor 2 lsvitch disconnected TRAFFIC FAIL Troffie device hos Foiled NAV2 ipo Le 09 34 45 XPDR TENT THR REF NRST MARNING Traffic Annunciation 7 Alerts Window 2 Selected Heading Box Selected Course Box G Inset Map C Annunciation Window 4 BRGI Information Window Vertical Deviation Glideslope Indicator DME Information Window Marker Beacon Annunciation 6 BRG2 Information Window 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 Window default 19 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 2 1 AIRSPEED INDICATOR Airspeed Trend ector Actual Airspeed Speed Range flap speed range Vspeed References True Airspeed best glide Box Figure 2 4 Airspeed Indicator Speed Indication The indic
96. nintinnscctsepnininioerindanensatic 5 4 Pe nitude RlonceBu a4 SECTION 6 AUTOMATIC FLIGHT CONTROL Alita TARE VECIOR cocsecsteecocccoseoseceesnscnescceecs 2 4 6 1 Mode Annunciations 0 0 0 cece 6 1 Barometric Setting BOX scesscesseesssesessessessesseeseesven 2 4 6 2 Overspeed Protection E headed 6 2 2 4 Vertical Deviation Glideslope Indicator 2 4 6 3 AP Engagement Disengagement 6 2 2 5 Marker Beacon Annunciations 2 4 Automatic Disengagement ssssssssssrstsrstssttsrrterrtessreerets 6 3 2 6 Vertical Speed Indicator 0 ccceees 2 5 Manual Disengagement aaa 6 3 2 7 Horizontal Situation Indicator HS 2 5 Control Wheel Steering 6 3 COUN POME cesgaseniaena in 2 6 Vaw DAMPET erevesvevssisieienananananananananininin 6 3 Course Deviation Indicator CDI 2 6 6 4 Loss of Data A a as 6 3 Bearing Pointers and Information WindOWS 0 2 6 6 5 Pitch AXIS Modes srsrvresrnrenenieneninnenn 6 3 DME Radio Optional csscsscesesseseeseseeseseeseeseen 2 7 Pitch Hold Mode PIT ssststsesstseseisnneseintneseie 0 4 Navigation SOUPE i Altitude Hold Mode ALT enn 6 5 Vertical Speed Mode VS cesccescesseestesseessesseesteaseeseeaees 6 6 SECTION 3 ENGINE INDICATION SYSTEM EIS 3 1 Flight Level Change Mode FLC ssssssssssssseesseesssssen 6 7 3 1 Engine Display cccccccsssseeen 3 1 Go Around Mode GA siisii 6 8 3 2 Lean Engine Display
97. o select the de sired frequency on any of the information pages Pressing the ENT key then loads the selected frequency into the standby frequency window of the appropriate radio 4 7 TRANSPONDER Mode Selection The STBY ON and ALT softkeys can be accessed by pressing the XPDR softkey Ground Mode Automatic GND is displayed when the aircraft is on the ground Figure 4 10 Ground Mode Reply Status When the transponder sends replies to interrogations an R indication appears momentarily in the reply status field Figure 4 11 Reply Indication Code Selection 1 Press the XPDR softkey to display the transpon der Mode Selection softkeys 2 Press the CODE softkey to display the transpon der 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 bar Five seconds after the fourth digit has been entered the transponder code becomes activated When entering a code press the BKSP soft key as needed to back up and change code digits Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 SECTION 4 NAV COM amp TRANSPONDER Following is a list of important codes e 1200 VFR code in the U S please refer to the ICAO standards for VFR codes in other countries e 7000 VFR code commonly used in Europe please refer to the ICAO standards e 7500 Hijack code e
98. ocedure 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 Load and or Activate an Approach Procedure 1 APPROACHES With the Navigation Map Page displayed press the FPL key Press the LD APR softkey If a flight plan is active the destination airport will be displayed as the default A list of available approaches 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 Approach field Turn the small FMS knob to display a list of available approaches Figure 9 6 Selecting an Approach Procedure Turn either FMS knob to highlight the desired approach Press the ENT key 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 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 SECTION 9 PROCEDURES Figure 9 7 Selecting an Approach Transition 7 Turn the large FMS knob to highlight Activate and press the ENT key to activate the approach Selecting Load will add the p
99. on navigation sources 1 Press the Direct to E8 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 way point identifier 4 Press the ENT key to confirm the identifier The Activate field is highlighted 5 Press the ENT key to activate To select a Direct to destination to a flight plan waypoint or nearest airport 1 Press the Direct to E key 2 Turn the large FMS knob to highlight the Flight Plan Field or Nearest Airport Field Figure 7 1 Navigation Map Page 3 Turn the small FMS knob to display a list way points or airports Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 7 1 SECTION 7 NAVIGATION 4 Continue turning the small FMS knob to scroll through the list and highlight the desired waypoint or airport Press the ENT key to contirm the selection Press ENT again to activate a Direct to To re center the CDI HSI needle to the same destination waypoint 1 Press the Direct to key followed by pressing the ENT key twice NOTE If a missed approach point MAP is the current destina tion the approach will be canceled To manually define the Direct to course i 2 Press the Direct to 8 key Turn the FMS knobs to select the destination waypoint Press the ENT key to confirm
100. on waypoint and press the ENT key 8 SECTION 9 PROCEDURES DEPARTURE RUNEA 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 With the Navigation Map Page displayed press the FPL key Press 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 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 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 9 1 SECTION 9 PROCEDURES 6 9 2 A second window is displayed listing available transitions for the arrival Turn either FMS knob to highlight the desired transition waypoint and press the ENT key Figure 9 4 Select Arrival Transition A third window is displayed listing the available runways Turn either FMS knob to select the desired runway and press the ENT key Figure 9 5 Select Arrival Runway With LOAD highlighted press the ENT key If a flight plan is active the selected arrival pr
101. pit Reference Guide for the Beechcraft A36 G36 Functionality of the PFD and MFD controls are the same with the exception of the dedicated autopilot keys located only on the MFD bezel 1 NAV VOL ID Knob Controls the NAV audio level Press to toggle the Morse code identifier ON and OFF Volume level is shown in the field as a percentage 2 NAV Frequency Toggle Key Toggles the standby and active NAV frequencies 3 Dual NAV Knob Tunes the MHz large knob and kHz small knob standby frequencies for the NAV re ceiver Press to toggle the tuning cursor light blue box between the NAV 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 pro vides the heading reference to the Flight Director while operating in Heading Select mode 5 Joystick Changes the map range when rotated Ac tivates the map pointer when pressed 6 CRS BARO Knob The large knob sets the altim eter 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 trans ceiver
102. pit Reference Guide for the Beechcraft A36 G36 SECTION 2 FLIGHT INSTRUMENTS 2 6 VERTICAL SPEED INDICATOR 2 7 HORIZONTAL SITUATION INDICATOR HSI Selected Vertical Speed Vertical Speed Bug Vertical Speed Pointer Figure 2 9 Vertical Speed Indicator The actual vertical speed is displayed inside the point O a ake or Pressing the VS key will display the Vertical Speed Bug Lateral Deviation Scale Press the NOSE UP or NOSE DN key to adjust G Navigation Source 4 Aircraft Symbol Course Deviation Indicator 6 Rotating Compass Rose Q OBS Mode TO FROM Indicator C Heading Bug 10 Course Pointer Flight Phase cr Turn Rate and Heading Trend Vector 13 Heading Lubber Line Figure 2 10 Horizontal Situation Indicator Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 15 SECTION 2 FLIGHT INSTRUMENTS Turn Rate Indicator and Heading Trend Vector Each tick mark is at 9 half standard rate tick mark and 18 standard rate tick mark degrees to the left and right of the lubber line A wide magenta line displays the current turn rate up to 24 degrees A magenta arrow head appears at 25 degrees This trend vector provides the pilot with a prediction of what the heading will be in 6 seconds at the present turn rate Figure 2 14 Turn Rate Indicator and Heading Trend Vector Course Pointer The course pointer is a single line arrow GPS VORI and LOC1 or double line arrow VOR
103. r The Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 SECTION 5 AUDIO PANEL 5 5 INTERCOM SQUELCH CONTROL Select manual squelch for intercom audio by pressing the MAN SQ key to light the annunciator Pressing the small VOL SQ knob now toggles be tween volume and squelch adjustment by lighting VOL or SQ respectively Figure 5 5 Navigation Radios wv 5 4 INTERCOM SYSTEM ICS ISOLATION Press the PILOT and or COPLT key to select who is isolated from hearing the Nav Com radios and music Se ee lection scenarios are addressed in Table 5 1 PLAY PILOT COPLT ICS ISOLATION PILOT O PASS lt CREW w PILOT COPLT ICS ISOLATION Figure 5 6 ICS Isolation so Figure 5 7 Volume Squelch Control ANNUNCIATOR ANNUNCIATOR Hears Selected radios Selected radios Selected radios OFF pilot copilot pilot copilot pilot copilot passengers passengers passengers MUSIC 1 MUSIC 1 MUSIC 2 Selected radios copie cope PILOT ilot passengers passengers P MUSIC 1 MUSIC 2 Selected radios Selected radios COPILOT pilot passengers Copilot pilot passengers MUSIC 1 MUSIC 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 Beechcraft A36 G36 5 3 SECTION 5 AUDIO PANEL 5 6 DIGITAL CLEARANCE RECORDER WITH PLAYBACK CAPABILITY Each reception of primary acti
104. rocedure to the flight plan without immediately using it for navigation guidance Activate An Approach in the Active Flight Plan 1 With the Navigation Map Page displayed press the PROC key 2 Turn the large FMS knob to highlight ACTIVATE APPROACH 3 Press the ENT key The approach procedure is now active Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 9 3 SECTION 9 PROCEDURES This page intentionally left blank 9 4 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 SECTION 10 HAZARD AVOIDANCE 10 2 STORMSCOPE OPTIONAL 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 WARNING Use of the Stormscope system for hazardous thunderstorm penetration is prohib ited Weather information on the G1000 MFD is approved for weather avoidance only Refer to the WX 500 Pilot s Guide for detailed opera tion Setup option 2 Press the ENT key The Map Setup Menu is displayed Turn the small FMS knob to select the Weather or Traffic group to customize 1 the display of weather features Select Traffic to customize the display of traffic 3 Press the small FMS knob to return to the Navigation Map Page Displaying Stormscope Lightning Data on the Navigation Map Page Press the MAP softke
105. rrent 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 navi gational 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 interface for hazardous weather penetration thunderstorm penetration is prohibited Weather information on the G1000 MFD is approved only for weather avoidance not penetra tion WARNING Us
106. rti cal Speed Indicator Pitch and roll 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 If the autopilot is engaged the Vertical Speed Bug can be adjusted in 100 fpm 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 Speed box above the VSI and in the Vertical Speed Reference field in the AFCS Status Bar Vertical speed may also be changed by pressing and holding the CWS button to manually estab lish the desired vertical speed using the control wheel When the CWS button is released the current vertical speed will be maintained This method must be used when using only the flight director 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 Acitve 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 and roll commands are given to manually maintain the selected altitude If no altitude has been selected Altitude
107. sessessesseesneeen 7 7 View Information on the Nearest VOR fo Select and Load a VOR Frequency s s s 7 8 7 12 Nearest User Waypoint 0 ccccceeeeen 7 8 Select the Nearest User Waypoint Page esesnecen 7 8 Select a Nearest User Waypoint c csceseeseesesseeseean 1 8 7 13 Nearest Frequencies cccccceseseeseseeen 7 8 Select the Nearest Frequencies Page sesesesrneeen 7 8 Select and Load the Nearest ARTCC FSS or Weather ESOO e PA 19 7 14 Nearest Airspace 7 9 Select the Nearest Airspaces Page 7 9 Airspace Alerts BOX scssssssssesssssessssssesssessesssesseesees 7 9 View Additional Details for a Listed Airspace 1 9 View and Quickly Load the Frequency for a Controlling a EEA N TETEN 1 9 SECTION 8 FLIGHT PLANNING 00000000 8 1 8 1 User Defined Waypoints 00ssss1111111111 8 1 Select the User WPT Information Page sesecseceen 8 1 Create a New User Waypoint 8 1 Create User Waypoints from the Navigation DEE E aona 8 1 Modify a User Waypoint c scsscesssessessessessessseessen 8 2 Delete a User Waypoint cesssesssesssessessessneesneeseessen 8 2 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 0 0 0 8 3 8 5 Stop Navigating a Flight Plan 8 3 8 6 Invert Active Flight Plan ees 8 3 8 7 Creat
108. splay The first airport in the nearest airports list is highlighted 2 Turn the large FMS knob to highlight the desired airport Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 7 5 SECTION 7 NAVIGATION Access Runway Information for the Selected Airport 1 Press the RNWY softkey located at the bottom of the display 2 Turn the small FMS knob to select the desired runway Quickly Tune the COM Transceiver to a Nearby Airport Frequency 1 Press the FREQ softkey located at the bottom of the display 2 Turn either FMS knob to select the desired frequency 3 Press the ENT key The selected frequency is placed in the standby frequency tuning box 4 Press the Frequency Toggle key to place the frequency in the active field Nearest Airports Information on the PFD Bearing TO Distance Airport Symbol Identifier MULTICOM 122 900 RNWY 35 Runway Lengin TOWER 118 500 RNWY JF 11 H UNICOM 122 800 RNWY Primary COM Frequency Figure 7 10 Nearest Airports Window 1 Press the NRST softkey to display the PFD Near est Airports Window View Information on a Specific Airport in the List 1 Turn the large FMS knob to place the cursor on the desired airport identifier Press the ENT key to display airport informa tion Press the ENT key again cursor is on BACK to return to the list Load an Airport COM Frequency into the Active COM 1 1 Turn the large FMS knob
109. splay the Flight Plan Page options Turn the large FMS knob to highlight Store Flight Plan and press the ENT key 8 14 SECTION 8 FLIGHT PLANNING With OK highlighted press the ENT key to store the flight plan 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 to activate the cursor Turn the large FMS knob to highlight the desired flight plan and press the ENT key 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 Press the FPL key and turn the small FMS knob to display the Flight Plan Catalog Page Press the FMS knob 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 select the waypoint to be deleted and press the CLR key to display a REMOVE WAYPOINT contirmation window 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 Once all changes have been made press the FMS knob to return to the Flight Plan Page Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 8 5 SECTION 8 FLIGHT PLANNING 8 6 8 15 8 16 Figure 8 1
110. system no longer GPS position is in error provides GPS based guidance DGRD GPS ACC GPS position E accuracy degraded amp RAIM unavailable GPS position accuracy has been degraded and RAIM is not available RAIM UNAVAIL RAIM is not available GPS1 FAIL GPS1 is inoperative GPS2 FAIL GPS2 is inoperative A failure has been detected in the GPS1 and or GPS2 receiver The receiver is unavailable The G1000 system should be serviced Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 12 11 SECTION 12 ANNUNCIATIONS amp ALERTS GIA 63 Alert Messages Cont Alerts Window Message Comments S GPS1 SERVICE GPS1 needs service 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 RMTXFR NAV1 remote a transfer key is stuck The remote NAV1 and or NAV2 transfer switch is stuck in the enabled or pressed s 5 state Press the transfer switch again to cycle its operation If the problem persists NAV RMTXFR NAV2 remote the G1000 system should be ser
111. t 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 missed approach KRHV X YQ 2 Clovis VORTAC o CZQ Panoche k VORTAC 8 Gh PXN Figure 6 21 Flight Plan Overview Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 6 13 SECTION 6 AUTOMATIC FLIGHT CONTROL Departure To Climb to Selected Altitude and Fly an Assigned Heading 1 Upon takeoff set the Selected Altitude to 7 000 feet using the ALT knob To have the autopilot capture this altitude select 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 fpm press the VS key Altitude Hold mode is armed automatically ee RONG ALT 3 After reaching the minimum engage altitude and activating Vertical Soeed mode press the AP key engaging the autopilot in detault Roll Hold and Vertical Soeed modes 6 ALT HDG Mode 3 Oo me Selected Altitude of 7 000 MSL Figure 6 22 Departure With the autopilot engaged in a climb set Selected Heading to 070 degrees using the HDG knob then press the HDG key The autopi lot turns the aircraft to the desired heading o HDG AP YD ALT As the aircraft climbs to the selected altitude the autopilot changes from Vertical Speed mode to Altitude Hold mode This is annunc
112. t plan using the MFD 1 4 J Press the FPL key and turn the small FMS knob to display the Flight Plan Catalog Page Press the NEW softkey to display a blank flight plan page for the first empty storage loca tion Figure 8 10 Create FPL on MFD Turn the small FMS knob to display the Way point Information Page Turn the small FMS knob to enter the first character of the identifier of the departure waypoint Turn the large FMS knob to move the cursor to the next character field Repeat using the FMS knobs until the desired identifier has been entered WAYPOINT INFORHATION IDENT FACILITY CITY Figure 8 11 Waypoint Info Window Press the ENT key Repeat step number 3 to enter the identifier for each additional flight plan waypoint When all waypoints have been entered press the FMS knob to return to the Flight Plan Catalog Page The new flight plan is now in the list Create a new flight plan using the PFD NOTE A flight plan cannot be entered using the PFD if another flight plan is active NOTE After the first leg is entered using the PFD only it is immediately activated Press the FPL key and press the small FMS knob to activate the cursor Turn the small FMS knob to enter the first character of the flight plan starting identifier Turn the large FMS knob to move the cursor to the next character field Turn the small FMS knob to enter the next char acter Continue this process until th
113. tain 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 nant 113 868 nov2 108 00 117 95 Flight Director command bars tracking Selected Heading Selected Heading Box 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 it the heading bug is moved more than 340 degrees at a time a turn reversal will be the result Altitude Hold mode is active 133 558 128 858 cons 121 988 Selected Heading Bug Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 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 a
114. the ENT key 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 Press the LD WPT softkey The selected way point will be inserted at the end of the flight plan If the selected waypoint is to be placed else where in the flight plan press the FMS knob to activate the cursor Waypoints are inserted ABOVE the cursor Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 5 After placing the cursor at the desired point in the list of waypoints press the LD WPT soft key 8 19 TRIP PLANNING 1 Turn the large FMS knob to select the AUX page group 2 Turn the small FMS knob to select the first rectangular page icon 3 The current page mode is displayed at the top of the page AUTOMATIC or MANUAL To change the page mode press the AUTO or MANUAL softkey OEL Lar PALL WETS Figure 8 16 Trip Planning Page 4 For Direct to planning press the WPTS softkey and verity that the trom waypoint field indi cates P POS present position If necessary press the MENU key and select
115. tivate the cursor Turn the large FMS knob to highlight the desired selection field identifier name or clos est city Turn the FMS knobs to enter an identitier name or city and press the ENT key Press the FMS knob to remove the flashing Cursor 7 4 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 7 6 VOR INFORMATION 17 95 Figure 7 8 VOR Information Page Select the VOR Information Page 1 Turn the large FMS knob to select the WPT page group 2 Turn the small FMS knob to select the fourth rectangular page icon Access Information on a VOR 1 With the VOR Information Page displayed press the FMS knob to activate the cursor 2 Turn the large FMS knob to highlight the desired selection field identifier name or clos est city 3 Turn the FMS knobs to enter an identifier name or city and press the ENT key 4 Press the FMS knob to remove the flashing Cursor SECTION 7 NAVIGATION 7 7 USER WAYPOINT INFORMATION PAGE See the Flight Planning section for a discussion on cre ating and modifying user defined waypoints 7 8 NEAREST AIRPORTS 17 95 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 Access Information on a Specific Airport 1 Press the APT softkey located at the bottom of the di
116. uce engine power and or adjust the pitch reference to slow the air craft Figure 6 3 PFD AFCS Display Selected Altitude Box 6 3 AP ENGAGEMENT DISENGAGEMENT When the key is pressed the system engages the auto pilot If the flight director is not already active it is also engaged when the AP key is pressed If the yaw damper is not already active it too is engaged when the AP key pressed Autopilot engagement is displayed in the Autopilot Status field of the AFCS Status Bar Autopilot engagement is indicated by a green AP Autopilot Engaged _ ROL LAP YD ALT Figure 6 5 Autopilot Engaged Annunciation 6 2 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 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 discon nect aural alert will be heard Both the annunciation and the aural alert will continue until acknowledged by press ing the AP DISC button or the MET ARM switch The Yaw Damper may or may not disengage depending on the cause of the automatic AP disengagement Automatic Disconnect ROL M ALT Figure 6 6 Automatic Disconnect Annunciation Manual Disengagement The autopilot may also be manually disengaged by pressing the AP DISC button the GA button the MET ARM switch or by pressing the AP key on the
117. ve COM audio is auto matically recorded in a memory block When the next transmission is received it is recorded in the next memory block and so on Once the 2 5 minutes of recording time has been reached the recorder begins recording over the stored memory blocks starting from the oldest block Powering off the unit automatically clears all recorded blocks v v MAN SQ PLAY Figure 5 8 Playback e Pressing PLAY once plays back the latest recorded memory block then returns to normal operation e Pressing PLAY during playback of a memory block halts the playback of this block and plays back the preceding recorded block The PLAY key can be used to backtrack through the recorded memory blocks to reach and play back any desired block Pressing the MKR MUTE key during playback halts playback and returns the recorder playback to normal operation If a COM input signal is detected during playback playback is halted and the new COM input signal is re corded as the latest block 5 4 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 SECTION 6 AUTOMATIC FLIGHT CONTROL In addition to the AFCS Automatic Flight Control Sys tem keys on the MFD as discussed in the System Over view section the following buttons and switches used by the AFCS are located in the cockpit separately from the PFD and MFD AP DISC Autopilot Disconnect Button Located on the pilots control wheel pressing this button diseng
118. ven Traffic Not Available will be heard whenever TIS ser vice becomes unavailable 10 5 SKYWATCH TRAFFIC ADVISORY SYSTEM TAS OPTIONAL Refer to the SkyWatch pilots guide for a detailed dis cussion of the SkyWatch system Displaying Traffic on the Traffic Map Page 1 Turn the large FMS knob to select the Map Page Group 2 Turn the small FMS knob to select the second rectangular page icon 3 Press the OPERATE softkey to begin displaying traffic TAS OPERATING is displayed in the Traffic mode field 4 Press the ALT MODE softkey to change the altitude volume Select the desired altitude volume by pressing the the BELOW NORMAL ABOVE or UREST unrestricted softkey The selection is displayed in the Altitude mode field 5 Press the STANDBY softkey to place the system in the Standby mode TAS STANDBY will be displayed in the Traffic mode field 6 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Traffic Advisory aircraft is 400 a E Out of Traffic Mode Altitude Mode climbing Range Proximity Traffic 00 above amp descending Non Bearing Traffic ans is unable to determine bearing 10 distance is 8 0 nm 1190 above and descending Figure 10 12 Traffic Map Page Displaying Traffic on the Navigation Map 1 Ensure the SkyWatch system is operating With the Navigation Map displayed press the MAP softkey 2
119. viced transfer 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 Alert Messages Alerts Window Message Comments GEA1 CONFIG GEA1 configuration The GEA 71 configuration settings do not match those of backup configuration error 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 12 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 SECTION 12 ANNUNCIATIONS amp ALERTS GTX 33 Alert Messages Alerts Window Message Comments XPDR1 CONFIG XPDR1 contig error The transponder configuration settings do not match those of backup configuration Contig service req d memory The G1000 system should be serviced MANIFEST GTX1 software mismatch The transponder has incorrect so
120. vigation data VOR LOC or GPS required to compute commands When such a loss occurs the system automatically re verts to the default mode for the affected axis 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 Figure 6 11 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 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 6 3 6 4 SECTION 6 AUTOMATIC FLIGHT CONTROL AFCS Key AFCS Mode FD AP only Pitch Hold Default i A 7 Atitude Hold Vertical Speed ight Level Change APR GA Glideslope vertical com ponent of Approach GA GoAround GA 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 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 Bar 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 novi 113 08 110 90 ITXD w DIS 1186 98 IIx Fl
121. y 2 Press the STRMSCP softkey Press the STRMSCP softkey again to remove Stormscope Lightning Data from the Navigation Map Page 196 975 ERMA CITY iL NORTH UP PAGE MHENU OPT DONS Press the FMS CRSA knob to return to bose poge Figure 10 1 Page Menu HAP SETUP GROUP Tar eae TU EJIE STRASCP LTHG STRHSCP HODE STRHSCP SHEL NEXRAD DATA MH LTNG CELL HOWEHENT MEI PET NEXRAD YH LTNG T BAC Figure 10 2 Map Setup Menu Figure 10 4 In Flight Navigation Map Page Displaying Stormscope Lightning Data Figure 10 3 Map Setup Group List Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 10 1 SECTION 10 HAZARD AVOIDANCE 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 At a map range of less than 25 nm Stormscope light ning data is not displayed but can still be present The presence of Stormscope lightning data is indicated by the annunciation LING lt 25 nm in the upper right corner NORTH UP LTNING i el MODE CELI Haaf Donn boa Haaa 7h Fe AT T Figure 10 5 Lightning Display Range Annunciation To select cell or strike as the Stormscope lightning mode 1 With the Weather Group selected press the ENT key The cursor flashes on STRMSCP LING Turn the large FMS knob to select

Garmin Software Version 0458.01 Cockpit Reference Guide

Contents

Download Pdf Manuals

Related Search

Related Contents