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Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series

Beechcraft King Air 200 · V Speeds Reference

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Overview

This document is a Cockpit Reference Guide for the Beechcraft 200 and B200 series aircraft, specifically detailing the operation of the Garmin G1000 integrated flight deck system. It serves as a resource for pilots to understand the major features and functionalities of the G1000 system, including flight instruments, navigation, and various operational procedures. The guide is intended to complement the G1000 Pilot's Guide and is not a comprehensive operating manual. It includes instructions on configuring V-speed bugs, using the automatic flight control system, and navigating through the flight planning features. The document also emphasizes safety warnings and cautions regarding the use of the G1000 system, ensuring pilots are aware of potential risks and operational limitations.

  • The G1000 system must be operated with updated databases to ensure accuracy.
  • GPS altitude should not be used for vertical navigation; always rely on pressure altitude.
  • Terrain avoidance features are advisory and should not be the sole reference for terrain avoidance.
  • V-speed bugs can be configured individually for precise speed management during flight.
  • The AFCS allows for vertical and lateral flight control modes, enhancing operational safety.

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Document details

Type
V Speeds Reference
Year
2008
Pages
104
File size
5.6 MB
Publisher
static.garmincdn.com
How rare is it?
2Beechcraft King Air 200 registered worldwide · 0 active

Common. Rarer than 17% of the aircraft models we track.

Documentation completeness
3/7

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In this document

Flight Instruments

This section covers the various flight instruments available in the G1000 system, including how to select and synchronize the altimeter barometric pressure settings, change navigation sources, and configure V-speed bugs. It provides step-by-step instructions for pilots to effectively utilize these instruments during flight.

Automatic Flight Control System (AFCS)

The AFCS section details the activation and operation of the flight director, including vertical and lateral modes. It guides pilots on how to engage and manage the autopilot functions, ensuring safe and efficient flight operations.

GPS Navigation

This section explains the GPS navigation features of the G1000, including how to perform direct-to navigation, activate stored flight plans, and manage vertical navigation (VNAV). It provides essential procedures for pilots to follow when using GPS for navigation.

Hazard Avoidance

The hazard avoidance section discusses the customization of hazard displays on the navigation map, including the use of optional features like Stormscope and XM Weather. It emphasizes the importance of using these tools for weather avoidance and situational awareness.

Warnings, Cautions & Notes

This section outlines critical warnings and cautions related to the G1000 system, including the limitations of terrain avoidance features, the importance of using updated databases, and the necessity of cross-checking information from multiple sources during flight.

Safety notes

  • Navigation and terrain separation must not rely solely on the terrain avoidance feature.
  • Always refer to current aeronautical charts for appropriate minimum clearance altitudes.
  • Do not use outdated database information; pilots assume risk when using outdated data.
  • Use of the G1000 for hazardous weather penetration is not recommended.

Full document text

G1000® Integrated Flight Deck Cockpit Reference Guide for the Beechcraft 200/B200 Series System Software 0985.00 or later Flight instruments nav/Com/transponder/audio panel automatiC Flight Control system gps navigation Flight planning proCedures hazard avoidanCe additional Features annunCiations & alerts appendix index Copyright © 2008 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0985.00 or later for the Beechcraft 200 and B200. 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, Liberty House, Bulls Copse Road, Hounsdown Business Park, Southampton, SO40 9RB, 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 unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited. Garmin® and G1000® are registered trademarks of Garmin Ltd. or its subsidiaries. WATCH®, FliteCharts®, and SafeTaxi® are trademarks of Garmin Ltd. or its subsidiaries. These trademarks may not be used without the express permission of Garmin. NavData® is a registered trademark of Jeppesen, Inc.; XM® is a registered trademark of XM Satellite Radio, Inc. November, 2008 190-00929-00 Rev. A Printed in the U.S.A. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A Warnings, Cautions & notes WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance feature. The terrain avoidance feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight. The terrain avoidance feature is only to be used as an aid for terrain avoidance. Terrain data is obtained from third party sources. 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 current aeronautical charts for appropriate minimum clearance altitudes. WARNING: The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and could vary significantly from the altitude displayed by pressure altimeters, such as the GDC 74B 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: Do not use outdated database information. Databases used in the G1000 system must be updated regularly in order to ensure that the information remains current. Pilots using any outdated database do so entirely at their own risk. WARNING: Do not use basemap (land and water data) information for primary navigation. Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness. WARNING: Traffic information shown on system displays 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: XM Weather should not be used for hazardous weather penetration. Weather information provided by the GDL 69A is approved only for weather avoidance, not penetration. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A Warnings, Cautions & notes WARNING: NEXRAD weather data is to be used for long-range planning purposes only. Due to inherent delays in data transmission and the relative age of the data, NEXRAD weather data should not be used for short-range weather avoidance. WARNING: Use of the Stormscope is not intended for hazardous weather penetration (thunderstorm penetration). Stormscope information, as displayed on the G1000 MFD, is to be used only for weather avoidance, not penetration. WARNING: The Garmin G1000, as installed in the Hawker Beechcraft 200/ B200 aircraft, has a very high degree of functional integrity. However, the pilot must recognize that providing monitoring and/or self-test capability for all conceivable system failures is not practical. Although unlikely, it may be possible for erroneous operation to occur without a fault indication shown by the G1000. It is thus the responsibility of the pilot to detect such an occurrence by means of cross-checking with all redundant or correlated information available in the cockpit. WARNING: For safety reasons, G1000 operational procedures must be learned on the ground. WARNING: The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment. Portions of the Garmin G1000 utilize GPS as a

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precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the G1000 can be misused or misinterpreted and, therefore, become unsafe. WARNING: To reduce the risk of unsafe operation, carefully review and understand all aspects of the G1000 Pilot’s Guide documentation and the G1000 Integrated Avionics System and GFC 700 AFCS in Hawker Beechcraft 200 and B200 King Air Airplane Flight Manual Supplement. 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. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A Warnings, Cautions & notes 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 Aeronautical Information Manual (AIM) recommend avoiding “by at least 20 miles any thunderstorm identified as severe or giving an intense radar echo.” WARNING: Lamp(s) inside this product may contain mercury (HG) and must be recycled or disposed of according to local, state, or federal laws. For more information, refer to our website at www.garmin.com/aboutGarmin/ environment/disposal.jsp. WARNING: Because of anomalies in the earth’s magnetic field, operating the G1000 within the following areas could result in loss of reliable attitude and heading indications. North of 70° North latitude and south of 70° South latitude. An area north of 65° North latitude between longitude 75º West and 120º West. An area south of 55° South latitude between longitude 120º East and 165º East. CAUTION: The PFD and MFD displays use a lens coated with a special anti-reflective coating that is very sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI- REFLECTIVE COATING. It is very important to clean the lens using a clean, lint-free cloth and an eyeglass lens cleaner that is specified as safe for anti- reflective coatings. CAUTION: The Garmin G1000 does not contain any user-serviceable parts. 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: 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 and aviation databases. Depictions of equipment may differ slightly from the actual equipment. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A Warnings, Cautions & notes NOTE: This device complies with part 15 of the FCC Rules. Operation is subject to the following two conditions: (1) this device may not cause harmful interference, and (2) this device must accept any interference received, including interference that may cause undesired operation. NOTE: The data contained in the terrain and obstacle databases comes from government agencies. Garmin accurately processes and cross-validates the data, but cannot guarantee the accuracy and completeness of the data. NOTE: This product, its packaging, and its components contain chemicals known to the State of California to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with California’s Proposition 65. If you have any questions or would like additional information, please refer to our web site at www.garmin.com/prop65. NOTE: Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of attitude and heading displays while the aircraft is on the ground. Moving the aircraft more than 100 yards away from the source of the interference should alleviate the condition. NOTE: Use of polarized eyewear may cause the flight displays to appear dim or blank. NOTE: The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system more easily. It is not intended to be a comprehensive operating guide. Complete operating procedures for the system are found in the G1000 Pilot’s Guide for this aircraft. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A Warnings, Cautions & notes Blank Page Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A RR-1 record of revisions part number Change summary 190-00929-00 Initial release revision date of revision affected pages description A November, 2008 All Production release Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A RR-2 record of revisions Blank Page Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A i table of Contents Flight instruments ................................................................................................................ 1 selecting the altimeter Barometric pressure setting ...................................................... 1 selecting standard Barometric pressure (29.92 in hg) .................................................... 1 Change altimeter Barometric pressure setting units ...................................................... 1 synchronizing the altimeter Barometric pressure settings ........................................... 1 synchronize Cdi......................................................................................................................... 1 Change navigation sources ................................................................................................... 2 enable/disable oBs mode While navigating with gps .................................................... 2 generic timer ............................................................................................................................. 2 Configure vspeed Bugs individually ..................................................................................... 2 turn vspeed Bugs on or off by Category............................................................................ 3 set Barometric/radar altimeter minimum descent altitude ......................................... 3 testing the radar altimeter ................................................................................................... 3 displaying Wind data .............................................................................................................. 3 nav/Com/transponder/audio panel......................................................................... 5 adF tuning (optional) .............................................................................................................. 5 dme tuning................................................................................................................................. 5 enter a transponder Code....................................................................................................... 5 activate ads-B transmit ......................................................................................................... 5 selecting a Com radio ............................................................................................................ 5 selecting a nav radio ............................................................................................................. 6 nav/Com tuning ....................................................................................................................... 6 intercom...................................................................................................................................... 6 passenger address (pa) system............................................................................................. 7 Clearance recorder and player ............................................................................................. 7 automatiC Flight Control system ............................................................................ 9 Flight director activation ....................................................................................................... 9 vertical modes ......................................................................................................................... 10 lateral modes .......................................................................................................................... 11 gps navigation ........................................................................................................................ 13 direct-to navigation .............................................................................................................. 13 activate a stored Flight plan ............................................................................................... 14 activate a Flight plan leg ..................................................................................................... 14 stop navigating a Flight plan .............................................................................................. 15 vertical navigation (vnav)................................................................................................... 15 Flight planning ...................................................................................................................... 17 Weight planning ...................................................................................................................... 17 trip planning ............................................................................................................................ 17 Create a new user Waypoint defined by latitude & longitude ................................. 19 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A ii table of Contents Create a new user Waypoint defined by radials from other Waypoints ................. 20 Create a new user Waypoint defined by a radial & distance from another Waypoint................................................................................................................................... 21 delete a user Waypoint ......................................................................................................... 23 Create a new Flight plan ...................................................................................................... 23 import a Flight plan from an sd Card ................................................................................ 24 insert a Waypoint in the active Flight plan ...................................................................... 25 enter an airway in a Flight plan .......................................................................................... 26 invert an active Flight plan.................................................................................................. 26 remove a departure, arrival, approach, or airway from a Flight plan ..................... 27 store a Flight plan .................................................................................................................. 27 edit a stored Flight plan ....................................................................................................... 27 delete a Waypoint from the Flight plan ............................................................................ 28 invert and activate a stored Flight plan ........................................................................... 28 Copy a Flight plan ................................................................................................................... 28 delete a Flight plan ................................................................................................................ 29 graphical Flight plan Creation ............................................................................................. 29 export a Flight plan to an sd Card ..................................................................................... 29 proCedures................................................................................................................................. 31 load and activate a departure procedure ....................................................................... 31 activate a departure leg ..................................................................................................... 31 load an arrival procedure .................................................................................................... 31 activate an arrival leg ......................................................................................................... 32 load and/or activate an approach procedure ................................................................. 32 activate an approach in the active Flight plan ............................................................... 33 activate a vector to Final approach Fix ............................................................................ 33 activate a missed approach in the active Flight plan ................................................... 33 hazard avoidanCe ................................................................................................................ 35 Customizing the hazard displays on the navigation map ............................................ 35 stormsCope® (optional) ..................................................................................................... 35 xm Weather (optional) .......................................................................................................... 37 traffic systems ........................................................................................................................ 38 terrain awareness & Warning system (taWs) display................................................... 40 airborne Color Weather radar ............................................................................................ 42 additional Features ........................................................................................................... 45 synthetic vision....................................................................................................................... 45 terminal procedure Charts ................................................................................................... 46 xm® radio entertainment..................................................................................................... 48 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A iii table of Contents annunCiations & alerts................................................................................................... 51 advisory annunciations......................................................................................................... 51 Comparator annunciations................................................................................................... 51 reversionary sensor annunciations ................................................................................... 52 aFCs alerts ............................................................................................................................... 52 taWs alerts .............................................................................................................................. 53 aural alerts .............................................................................................................................. 55 mFd & pFd message advisories .......................................................................................... 56 database message advisories ............................................................................................. 57 gma 1347d message advisories ......................................................................................... 60 gia 63W message advisories ............................................................................................... 61 gea 71 message advisories.................................................................................................. 64 gtx 33 message advisories .................................................................................................. 64 grs 77 message advisories .................................................................................................. 65 gmu 44 message advisories ................................................................................................ 67 gdl 69a message advisories ............................................................................................... 67 gWx 68 alert messages ......................................................................................................... 68 gdC 74B message advisories ............................................................................................... 68 gCu 477 message advisories ............................................................................................... 69 gmC 710 message advisories .............................................................................................. 69 miscellaneous message advisories..................................................................................... 70 appendix ....................................................................................................................................... 75 pFd softkey map .................................................................................................................... 75 mFd softkey map ................................................................................................................... 80 index .........................................................................................................................................Index-1 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A iv table of Contents Blank Page Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 1 Flight instruments Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index Flight instruments seleCting the altimeter BarometriC pressure setting Turn the BARO Knob to select the desired setting. seleCting standard BarometriC pressure (29.92 in hg) Push the BARO Knob to select standard pressure. Change altimeter BarometriC pressure setting units 1) Press the PFD Softkey to display the second-level softkeys. 2) Press the ALT UNIT Softkey. 3) Press the IN Softkey to display the barometric pressure setting in inches of mercury (in Hg). Or: Press the HPA Softkey to display the barometric pressure setting in hectopascals. 4) Press the BACK Softkey to return to the top-level softkeys. synChronizing the altimeter BarometriC pressure settings 1) Select the AUX-SYSTEM SETUP Page on the MFD. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight BARO in SYNCHRONIZATION Window. 4) Turn the small FMS Knob clockwise to ON or counterclockwise to OFF. synChronize Cdi 1) Select the AUX-SYSTEM SETUP Page on the MFD. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight CDI in SYNCHRONIZATION Window. 4) Turn the small FMS Knob clockwise to ON or counterclockwise to OFF. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 2 Flight instruments Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index Change navigation sourCes 1) Press the CDI Softkey to change from GPS to VOR1 or LOC1. This changes the NAV1 standby frequency in the upper left corner of the PFD to light blue, indicating this is the frequency selected for tuning. 2) Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2. This changes the NAV2 standby frequency in the upper left corner of the PFD to light blue, indicating this is the frequency selected for tuning. 3) Press the CDI Softkey a third time to return to GPS. enaBle/disaBle oBs mode While navigating With gps 1) Press the OBS Softkey to select OBS Mode. 2) Turn a CRS Knob to select the desired course to/from the waypoint. Press a CRS Knob to synchronize the Selected Course with the bearing to the next waypoint. 3) Press the OBS Softkey again to disable OBS Mode. generiC timer 1) Press the TMR/REF Softkey, then turn the large FMS Knob to select the time field (hh/mm/ss). Turn the FMS Knobs to set the desired time, then press the ENT Key. The UP/DOWN field is now highlighted. 2) Turn the small FMS Knob to display the UP/DOWN window. Turn the FMS Knob to select ‘UP’ or ‘DOWN’, then press the ENT Key. ‘START?’ is now highlighted. 3) Press the ENT Key to START, STOP, or RESET the timer (if the timer is counting DOWN, it will start counting UP after reaching zero). Press the CLR Key or the TMR/REF Softkey to remove the window. ConFigure vspeed Bugs individually 1) Press the TMR/REF Softkey. 2) Turn the large FMS Knob to highlight the desired Vspeed. 3) Use the small FMS Knob to change the Vspeed in 1-kt increments (when a speed has been changed from a default value, an asterisk appears next to the speed). 4) Press the ENT Key or turn the large FMS Knob to highlight the ON/OFF field Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 3 Flight instruments Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index 5) Turn the small FMS Knob clockwise to ON or counterclockwise to OFF. 6) To remove the window, press the CLR Key or the TMR/REF Softkey. turn vspeed Bugs on or oFF By Category 1) Press the TMR/REF Softkey. 2) Press the MENU Key. 3) Turn the FMS Knob to highlight the desired option. 4) Press the ENT Key. Press the TMR/REF Softkey to remove the window. set BarometriC/radar altimeter minimum desCent altitude 1) Press the TMR/REF Softkey. 2) Turn the large FMS Knob to highlight the OFF/BARO/RAD ALT field to the right of ‘MINIMUMS’. 3) Turn the small FMS Knob clockwise to select BARO or RAD ALT. 4) Press the ENT Key. 5) Use the small FMS Knob to enter the desired altitude. 6) Press the ENT Key. 7) To remove the window, press the CLR Key or the TMR/REF Softkey. testing the radar altimeter 1) Select the AUX-SYSTEM STATUS Page on the MFD. 2) Select the RA TEST Softkey. The Radar Altitude window displays 50 feet, indicating a properly functioning system. 3) Selecting the RA TEST Softkey again, or exiting the System Status Page cancels the test. displaying Wind data 1) Press the PFD Softkey. 2) Press the WIND Softkey to display wind data below the Selected Heading. 3) Press one of the OPTN softkeys to change how wind data is displayed. 4) To remove the Wind Data Window, press the OFF Softkey. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 4 Flight instruments Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index Blank Page Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 5 nav/Com/xpdr/audio panel Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index nav/Com/transponder/audio panel adF tuning (optional) Tune the ADF using the remote ADF control head. dme tuning 1) Press the DME Softkey. 2) Turn the large FMS to select the DME source field. 3) Turn the small FMS Knob to select the desired Nav radio. 4) Press the ENT Key to complete the selection. enter a transponder Code 1) Press the XPDR Softkey to display the transponder mode selection softkeys. 2) Press the XPDR1 or XPDR2 Softkey to select the active transponder. 3) Press the CODE Softkey to display the transponder code selection softkeys, for digit entry. 4) Press the digit softkeys to enter the code in the code field. When entering the code, the next key in sequence must be pressed within 10 seconds, or the entry is cancelled and restored to the previous code. Five seconds after the fourth digit has been entered, the transponder code becomes active. aCtivate ads-B transmit 1) Press the XPDR Softkey to display the transponder mode selection softkeys. 2) Press the ADS-B TX Softkey to enable transmission of three-dimensional aircraft position and aircraft heading. 3) Press the ADS-B TX Softkey again to disable transmission. seleCting a Com radio transmit/receive Press the COM1 MIC, COM2 MIC, or COM3 MIC Key (optional COM, if installed) on the audio panel. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 6 nav/Com/xpdr/audio panel Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index receive only Press the COM1, COM2, or COM3 Key (optional COM, if installed) on the audio panel. seleCting a nav radio 1) Press the CDI Softkey to select NAV1 (VOR1/LOC1) or NAV2 (VOR2/LOC2). 2) Pressing the NAV1, NAV2, DME, or ADF Key on the audio panel selects and deselects the navigation radio audio source. All radio keys can be selected individually or together. nav/Com tuning 1) Press the small tuning knob to select the desired radio for tuning. A light blue box highlights the radio frequency to be tuned. 2) Turn the respective tuning knobs to enter the desired frequency into the standby frequency field. The large knob enters MHz and the small knob enters kHz. 3) Press the Frequency Transfer Key to place the frequency into the active frequency field. interCom Pressing the INTR COM Key on either Audio Panel selects and deselects the intercom on both Audio Panels. The annunciator is lit when the intercom is active. The intercom connects the pilot and copilot together. Either the pilot or copilot may select or deselect the intercom. The CABIN Key initiates two way communication between the pilot or copilot and the passengers in the cabin. The annunciator is lit when the cabin intercom is active on either Audio Panel. The MAN SQ Key allows either automatic or manual control of the intercom squelch setting. Pressing the MAN SQ Key enables manual squelch control, indicated by the MAN SQ annunciator. During manual squelch operation, pressing the ICS Knob switches between volume and squelch adjustment, lighting the associated annunciator beneath the knob. When the MAN SQ annunciator is lit, the ICS Knob controls both volume and squelch. When the MAN SQ annunciator is extinguished, the ICS Knob controls only volume. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 7 nav/Com/xpdr/audio panel Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index passenger address (pa) system A passenger address system is provided by pressing the PA Key to deliver messages to the passengers. The message is heard by the other pilot on the headset only if the PA Key is enabled on both audio panels. PA messages are one way from the flight deck to the passengers. ClearanCe reCorder and player NOTE: Pressing the play key on the pilot’s Audio Panel plays recorded audio to the Pilot. Pressing the play key on the Copilot’s Audio Panel plays recorded audio to the Copilot. Recorded COM audio is stored in separate memory blocks. Once 2.5 minutes of recording time have been reached, the recorder begins recording over the stored memory blocks, starting from the oldest block. The PLAY Key controls the play function. The PLAY annunciator is illuminated to indicate when play is in progress. The PLAY annunciator extinguishes after playback is finished. Pressing the PLAY Key once plays the latest recorded memory block and then returns to normal operation. Pressing the PLAY Key again during play of a memory block stops play. If a COM input signal is detected during play of a recorded memory block, play is halted. Pressing the PLAY Key twice within one-half second while audio is playing plays the previous block of recorded audio. Each subsequent two presses of the PLAY Key within one-half second backtracks through the recorded memory blocks to reach and play any recorded block. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 8 nav/Com/xpdr/audio panel Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index Blank Page Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 9 aFCs Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index automatiC Flight Control system NOTE: If sensor information (other than attitude) required for a flight director mode becomes invalid or unavailable, the flight director automatically reverts to the default mode for that axis. NOTE: If the attitude information required for the default flight director modes becomes invalid or unavailable, the autopilot automatically disengages. Flight direCtor aCtivation An initial press of a key listed in the following table (when the flight director is not active) activates the pilot-side flight director in the listed modes. Control Pressed Modes Selected Lateral Vertical FD Key Roll Hold (default) ROL Pitch Hold (default) PIT AP Key Roll Hold (default) ROL Pitch Hold (default) PIT CWS Button Roll Hold (default) ROL Pitch Hold (default) PIT GA Switch Takeoff (on ground) Go Around (in air) TO GA Takeoff (on ground) Go Around (in air) TO GA ALT Key Roll Hold (default) ROL Altitude Hold ALT VS Key Roll Hold (default) ROL Vertical Speed VS VNV Key Roll Hold (default) ROL Vertical Path Tracking* VPTH NAV Key Navigation** GPS VOR LOC Pitch Hold (default) PIT BC Key Backcourse*** BC Pitch Hold (default) PIT APR Key Approach** GPS VAPP LOC Pitch Hold (default) Glidepath Glideslope PIT GP GS HDG Key Heading Select HDG Pitch Hold (default) PIT *Valid VNV flight plan must be entered before VNV Key press activates flight director. **The selected navigation receiver must have a valid VOR or LOC signal or active GPS course beforeNAV or APR Key press activates flight director. ***The selected navigation receiver must have a valid LOC signal before BC Key press activates flight director. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 10 aFCs Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index vertiCal modes Vertical Mode Description Control Annunciation Pitch Hold Holds the current aircraft pitch attitude; may be used to climb/descend to the Selected Altitude (default) PIT Selected Altitude Armed AFCS armed to capture the altitude displayed in the Selected Altitude window * ALTS Altitude Hold Holds the current Altitude Reference ALT Key ALT nnnnn fT Vertical Speed Maintains the current aircraft vertical speed; may be used to climb/descend to the Selected Altitude VS Key VS nnnn fpm Flight Level Change, IAS Hold Maintains the current aircraft airspeed (in IAS or Mach) while the aircraft is climbing/descending to the Selected Altitude. Press the SPD Key to switch between IAS and MACH. FLC Key FLC nnn kT Flight Level Change, Mach Hold FLC M .nnn VNAV Captures and tracks the VNAV flight path VNV Key VPTH VNAV Target Altitude Armed AFCS armed to capture the altitude displayed in the VNAV Target Altitude window ** ALTV Glidepath Captures and tracks the WAAS glidepath on approach APR Key GP Glideslope Captures and tracks the ILS glideslope on approach GS Takeoff (on ground) Disengages the autopilot and commands a constant pitch angle and wings level in the air on the ground in preparation for takeoff GA Switch TO Go Around (in air) Disengages the autopilot and commands a constant pitch attitude and wings level in the air GA * ALTS armed automatically when PIT, VS, FLC, TO, or GA active, and under VPTH when Selected Altitude is to be captured instead of VNAV Target Altitude ** ALTV armed automatically under VPTH when VNAV Target Altitude is to be captured instead of Selected Altitude Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 11 aFCs Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index lateral modes Lateral Mode Description Control Annunciation Roll Hold Holds current aircraft roll attitude or rolls wings level, depending on commanded bank angle (default) ROL Low Bank Limits maximum commanded roll angle BANK Key * Heading Select Captures and tracks Selected Heading HDG Key HDG Navigation, GPS Arm/ Capture/Track Captures and tracks selected navigation source (GPS, VOR, LOC) NAV Key GPS Navigation, VOR Enroute Arm/Capture/Track VOR Navigation, LOC Arm/ Capture/Track (No Glideslope) LOC Backcourse Arm/Capture/ Track Captures and tracks a localizer signal for backcourse approaches BC Key BC Approach, GPS Arm/ Capture/Track Captures and tracks selected navigation source (GPS, VOR, LOC) APR Key GPS Approach, VOR Arm/ Capture/Track VAPP Approach, ILS Arm/ Capture/Track (Glideslope Mode automatically armed) LOC Takeoff (on ground) Disengages autopilot and commands a constant pitch angle and wings level in preparation for takeoff GA Switch TO Go Around (in air) Disengages autopilot and commands a constant pitch angle and wings level in the air GA * No annunciation appears in the AFCS Status Box. The acceptable bank angle range is indicated in green along the Roll Scale of the Attitude Indicator. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 12 aFCs Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index Blank Page Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 13 gps navigation Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index gps navigation direCt-to navigation direct-to navigation from the mFd 1) Press the Direct-to ( ) Key on the Control Unit. 2) Enter the waypoint identifier. 3) Press the ENT Key to confirm the identifier. The ‘Activate?’ field is highlighted. 4) If no altitude constraint or course is desired, press the ENT Key to activate. To enter an altitude constraint, proceed to step 5. 5) Turn the large FMS Knob to place the cursor over the ‘VNV’ altitude field. 6) Enter the desired altitude. 7) Press the ENT Key. If the waypoint entered is an airport, the option to select MSL or AGL is now displayed. If the waypoint is not an airport, proceed to step 9. 8) Turn the small FMS Knob to select ‘MSL’ or ‘AGL’. 9) Press the ENT Key. The cursor is now flashing in the VNV offset distance field. 10) Enter the desired offset distance before (-) or after (+) the waypoint. 11) Press the ENT Key. The ‘Activate?’ field is highlighted. 12) Press the ENT Key to activate. direct-to navigation from the pFd 1) Press the Direct-to Key ( ) on the PFD. 2) Turn the large FMS Knob to place the cursor in the desired selection field. 3) Turn the small FMS Knob to begin selecting the desired identifier, location, etc. 4) Press the ENT Key. 5) The cursor is now flashing on ‘ACTIVATE?’. If no altitude constraint or course is desired, press the ENT Key to activate. To enter an altitude constraint, proceed to step 6. 6) Turn the large FMS Knob to place the cursor over the ‘ALT’ altitude field. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 14 gps navigation Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index 7) Turn the small FMS Knob to enter the desired altitude. 8) Press the ENT Key. If the waypoint entered is an airport, the option to select MSL or AGL is now displayed. If the waypoint is not an airport, proceed to step 10. 9) Turn the small FMS Knob to select ‘MSL’ or ‘AGL’. 10) Press the ENT Key. The cursor is placed in the ‘OFFSET’ offset distance field. 11) Turn the small FMS Knob to enter the desired target altitude offset from the selected Direct-to. 12) Press the ENT Key to highlight ‘Activate?’ or turn the large FMS Knob to highlight the ‘CRS’ field. 13) Turn the small FMS Knob to enter the desired course to the waypoint. 14) Press the ENT Key to highlight ‘ACTIVATE?’. 15) Press the ENT again to activate the Direct-to. aCtivate a stored Flight plan 1) Press the FPL Key on the Control Unit and turn the small FMS Knob to display the Flight Plan Catalog Page. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the desired flight plan 4) Select the ACTIVE Softkey. The confirmation window is now displayed. 5) 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. 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 waypoint. 2) Select the ACT LEG Softkey. OR Press the MENU Key, select the ‘Activate Leg’ option from the page menu and press the ENT Key. This step must be used when activating a leg from the PFD. 3) With ‘Activate’ highlighted, press the ENT Key. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 15 gps navigation Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index stop navigating a Flight plan 1) Press the FPL Key on the Control Unit to display the Active Flight Plan Page. 2) Press the MENU Key to display the Page Menu Window. 3) 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. vertiCal navigation (vnav) The navigation database only contains altitudes for procedures that call for “Cross at” altitudes. If the procedure states “Expect to cross at,” the altitude is not in the database. In this case the altitude may be entered manually. Large Light Blue Text Small White Text with Altitude Restriction Bar Large White Text Small Light Blue Subdued Text Small Light Blue Text Cross AT or ABOVE 5,000 ft Cross AT or BELOW 3,000 ft Cross AT 2,300 ft Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 16 gps navigation Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index Altitudes associated with arrival and approach procedures are “auto-designated”. This means the system will automatically use the altitudes loaded with the arrival or approach for giving vertical flight path guidance outside the FAF. Note that these altitudes will be displayed as small light blue text. Altitudes that have been designated for use in vertical navigation may also be made “non-designated” by placing the cursor over the desired altitude and pressing the CLR Key. The altitude is now displayed only as a reference. It will not be used to give flight path vertical guidance. Other displayed altitudes may change due to re-calculations or rendered invalid as a result of manually changing an altitude to a non-designated altitude. White Text Light Blue Text Light Blue Subdued Text Large Text Altitude calculated by the system estimating the altitude of the aircraft as it passes over the navigation point. This altitude is provided as a reference and is not designated to be used in determining vertical flight path guidance. Altitude has been entered by the pilot. Altitude is designated for use in giving vertical flight path guidance. Altitude does not match the published altitude in navigation database or no published altitude exists. The system cannot use this altitude in determining vertical flight path guidance. Small Text Altitude is not designated to be used in determining vertical flight path guidance. Altitude has been retrieved from the navigation database and is provided as a reference. Altitude is designated for use in giving vertical flight path guidance. Altitude has been retrieved from the navigation database or has been entered by the pilot and matches a published altitude in the navigation database. The system cannot use this altitude in determining vertical flight path guidance. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 17 Flight planning Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index Flight planning Weight planning All procedures apply to the MFD and the Control Unit unless otherwise stated. entering Weight parameters The Weight Planning Page is displayed after system power-up. If it is necessary to return to this page, turn the large FMS Knob to select the ‘AUX’ page group. Turn the small FMS Knob to select the Weight Planning Pge. 1) Select the EMPTY WT Softkey to place the cursor in the Basic Empty Weight field. 2) Enter the desired aircraft empty weight. 3) Press the ENT Key. The cursor is now over the ‘PILOT & STORES’ field. 4) Enter the desired weight of Pilot & Stores. 5) Press the ENT Key. 6) Continue repeating these steps until all desired weights have been entered. entering Fuel parameters 1) Press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to place the cursor in the ‘FUEL ON BOARD’ field. 3) Turn the small FMS Knob to enter the desired fuel quantity. 4) Press the ENT Key. The cursor is now in the ‘FUEL RESERVES’ field. 5) Turn the small FMS Knob to enter the desired reserve fuel quantity. 6) Press the FMS Knob to remove the cursor. 7) Press the ENT Key. trip planning 1) Turn the large FMS Knob on the Control Unit to select the ‘AUX’ page group. 2) Turn the small FMS Knob to select the Trip Planning Page. 3) The current ‘PAGE MODE’ is displayed at the top of the page: ‘AUTOMATIC’ or ‘MANUAL’. To change the page mode, select the AUTO or MANUAL Softkey. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 18 Flight planning Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index 4) For Direct-to planning: a) Select the WPTS Softkey and verify that the starting waypoint field indicates ‘P.POS’ (present position). b) If necessary, press the MENU Key and select ‘Set WPT to Present Position’ to display ‘P.POS’. c) Press the ENT Key and the flashing cursor moves to the ending waypoint field. d) Enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint. Or: For point-to-point planning: a) Enter the identifier of the starting waypoint. b) Once the waypoint’s identifier is entered, press the ENT Key to accept the waypoint. The flashing cursor moves to the ending waypoint. c) Again, enter the identifier of the ending waypoint. d) Press the ENT Key to accept the waypoint. Or: For flight plan leg planning: a) Select the FPL Softkey (at the bottom of the display). b) Turn the small FMS Knob to select the desired flight plan (already stored in memory), by number. c) Turn the large FMS Knob to highlight the ‘LEG’ field. d) Turn the small FMS Knob to select the desired leg of the flight plan, or select ‘CUM’ to apply trip planning calculations to the entire flight plan. Selecting ‘FPL 00’ will display the active flight plan. If an active flight plan is selected, ‘REM’ will be an available option to display planning data for the remainder of the flight plan. NOTE: The page mode must be set to ‘MANUAL’ to perform the following steps. 5) Turn the large FMS Knob to highlight the departure time (DEP TIME) field. NOTE: The departure time on the Trip Planning Page is used for preflight planning. Refer to the Utility Page for the actual flight departure time. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 19 Flight planning Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index 6) Enter the departure time. Press the ENT Key when finished. Departure time may be entered in local or UTC time, depending upon system settings. 7) Enter the fuel flow. Press the ENT Key when finished. Note that in ‘AUTOMATIC’ page mode, fuel flow is provided by the system. 8) The flashing cursor moves to the fuel onboard field. Modify the fuel onboard. Press the ENT Key when finished. In ‘AUTOMATIC’ mode, fuel onboard is provided by the entry made on the Weight Planning Page. 9) The flashing cursor moves to the calibrated airspeed field. Enter a calibrated airspeed. Press the ENT Key when finished. Create a neW user Waypoint deFined By latitude & longitude 1) Turn the large FMS Knob on the Control Unit to select the ‘WPT’ page group. 2) Turn the small FMS Knob to select the User WPT Information Page. 3) Press the NEW Softkey. A waypoint is created at the current aircraft position. 4) Enter the desired waypoint name. 5) Press the ENT Key. 6) The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint can be made temporary (deleted automatically when the system is turned off). If the waypoint is to remain in the system, proceed to step 7. a) Turn the large FMS Knob one click to the left to highlight ‘TEMPORARY’. This list is populated only when there is an active flight plan. b) Press the ENT Key to place a check-mark in the box. 7) The cursor is now in the ‘WAYPOINT TYPE’ field. Turn the small FMS Knob to display a list waypoint types. 8) Turn the small FMS Knob to select LAT/LON (latitude and longitude). 9) Press the ENT Key. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 20 Flight planning Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index Create a neW user Waypoint deFined By radials From other Waypoints 1) Turn the large FMS Knob on the Control Unit to select the ‘WPT’ page group. 2) Turn the small FMS Knob to select the User WPT Information Page. 3) Press the NEW Softkey. A waypoint is created at the current aircraft position. 4) Enter the desired waypoint name. 5) Press the ENT Key. 6) The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint can be made temporary (deleted automatically when the system is turned off). If the waypoint is to remain in the system, proceed to step 7. a) Turn the large FMS Knob one click to the left to highlight ‘TEMPORARY’. This list is populated only when there is an active flight plan. b) Press the ENT Key to place a check-mark in the box. 7) The cursor is now in the ‘WAYPOINT TYPE’ field. Turn the small FMS Knob to display a list waypoint types. 8) Turn the small FMS Knob to select RAD/RAD (radial/radial). 9) Press the ENT Key. 10) The cursor moves to the ‘REFERENCE WAYPOINTS’ field. With the first waypoint name highlighted, use the FMS Knobs to enter the desired waypoint name. Waypoints may also be selected as follows: a) When a flight plan is active, turning the small FMS Knob to the left will display a list of the flight plan waypoints. b) Turn the large FMS Knob to select the desired waypoint. c) Press the ENT Key. Or: a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed. b) Turn the small FMS Knob to the right to display the ‘NRST’ waypoints to the aircraft’s current position. c) Turn the large FMS Knob to select the desired waypoint. d) Press the ENT Key. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 21 Flight planning Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index Or: a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed. b) Turn the small FMS Knob to the right to display the ‘RECENT’ waypoints. c) Turn the large FMS Knob to select the desired waypoint. d) Press the ENT Key. Or: a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed. b) Turn the small FMS Knob to the right to display the ‘USER’ waypoints. c) Turn the large FMS Knob to select the desired waypoint. d) Press the ENT Key. 11) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter the desired radial from the reference waypoint. 12) Press the ENT Key. 13) Repeat step 10 to enter the next waypoint name. 14) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field for the second waypoint. Enter the desired radial from the reference waypoint. 15) Press the ENT Key. 16) Press the FMS Knob to remove the flashing cursor. Create a neW user Waypoint deFined By a radial & distanCe From another Waypoint 1) Turn the large FMS Knob on the MFD Control Unit to select the ‘WPT’ page group. 2) Turn the small FMS Knob to select the User WPT Information Page. 3) Press the NEW Softkey. A waypoint is created at the current aircraft position. 4) Enter the desired waypoint name. 5) Press the ENT Key. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 22 Flight planning Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index 6) The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint can be made temporary (deleted automatically when the system is turned off). If the waypoint is to remain in the system, proceed to step 7. a) Turn the large FMS Knob one click to the left to highlight ‘TEMPORARY’. This list is populated only when there is an active flight plan. b) Press the ENT Key to place a check-mark in the box. 7) The cursor is now in the ‘WAYPOINT TYPE’ field. Turn the small FMS Knob to display a list waypoint types. 8) Turn the small FMS Knob to select RAD/DIS (radial/distance). 9) Press the ENT Key. 10) The cursor moves to the ‘REFERENCE WAYPOINTS’ field. With the first waypoint name highlighted, use the FMS Knobs to enter the desired waypoint name. Waypoints may also be selected as follows: a) When a flight plan is active, turning the small FMS Knob to the left will display a list of the flight plan waypoints. b) Turn the large FMS Knob to select the desired waypoint. c) Press the ENT Key. Or: a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed. b) Turn the small FMS Knob to the right to display the ‘NRST’ waypoints to the aircraft’s current position. c) Turn the large FMS Knob to select the desired waypoint. d) Press the ENT Key. Or: a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed. b) Turn the small FMS Knob to the right to display the ‘RECENT’ waypoints. c) Turn the large FMS Knob to select the desired waypoint. d) Press the ENT Key. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 23 Flight planning Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index Or: a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed. b) Turn the small FMS Knob to the right to display the ‘USER’ waypoints. c) Turn the large FMS Knob to select the desired waypoint. d) Press the ENT Key. 11) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter the desired radial from the reference waypoint. 12) Press the ENT Key. 13) The cursor is now displayed in the ‘DIS’ (distance) field. Enter the desired distance from the reference waypoint. 14) Press the ENT Key. 15) Press the FMS Knob to remove the flashing cursor. delete a user Waypoint 1) Turn the large FMS Knob to select the ‘WPT’ page group. 2) Turn the small FMS Knob to select the User WPT Information Page. 3) Press the FMS Knob to activate the cursor. 4) Turn the large FMS Knob to the place the cursor in the ‘USER WAYPOINT LIST’ field. 5) Turn the small FMS Knob to highlight the desired waypoint. 6) Select the DELETE Softkey. 7) The message ‘Would you like to delete the user waypoint?’ is displayed. With ‘YES’ highlighted, press the ENT Key. Create a neW Flight plan using the mFd 1) Press the FPL Key on the Control Unit. 2) Turn the small FMS Knob to display the Flight Plan Catalog Page. 3) Select the NEW Softkey to display a blank flight plan for the first empty storage location. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 24 Flight planning Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index 4) Turn the small FMS Knob to display the Waypoint Information Window. 5) Enter the identifier of the departure waypoint. 6) Press the ENT Key. 7) Repeat step number 4, 5, and 6 to enter the identifier for each additional flight plan waypoint. 8) 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. using the pFd NOTE: If a flight plan is active, an additional flight plan cannot be entered using the PFD. NOTE: After the first leg is entered (using the PFD only) it is immediately activated. 1) Press the FPL Key on the PFD. 2) Press the FMS Knob to activate the cursor. 3) Turn the small FMS Knob to enter the first letter of the destination waypoint identifier. 4) Turn the large FMS Knob to the right to move the cursor to the next character position. 5) Repeat step 3 and 4 to spell out the rest of the waypoint identifier. 6) Press the ENT Key and the cursor is now ready for entering of the next flight plan waypoint. 7) Repeat steps 3 through 6 to enter the identifier for each additional flight plan waypoint. 8) Once all waypoints have been entered, press the FMS Knob to remove the cursor. The new flight plan is now active. import a Flight plan From an sd Card 1) Insert the SD card containing the flight plan in the top card slot on the MFD. 2) Press the FPL Key on the Control Unit to display the Active Flight Plan Page on the MFD. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 25 Flight planning Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index 3) Turn the small FMS Knob to select the Flight Plan Catalog Page. 4) Press the FMS Knob to activate the cursor. 5) Turn either FMS Knob to highlight an empty or existing flight plan. 6) Press the IMPORT Softkey. If an empty flight plan is selected, a list of the available flight plans on the SD card will be displayed. or: If an existing flight plan is selected, an ‘Overwrite existing flight plan? OK or CANCEL’ prompt is displayed. Press the ENT Key to choose to overwrite the selected flight plan and see a list of the available flight plans on the SD card. If overwriting the existing flight plan is not desired, select ‘CANCEL’ using the FMS Knob, press the ENT Key, select another existing or empty flight plan, and again press the IMPORT Softkey. 7) Turn the small FMS Knob to highlight the desired flight plan for importing. 8) Press the ENT Key. insert a Waypoint in the aCtive Flight plan 1) Press the FPL Key on the Control Unit to display the active flight plan. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the desired flight plan waypoint. The new waypoint will be inserted before the highlighted waypoint. 4) Turn the small FMS Knob. The Waypoint Information Window is now displayed. 5) Enter the new flight plan waypoint by one of the following: a) Enter the user waypoint identifier, facility, or city. b) Press the ENT Key. Or: a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed. b) Turn the small FMS Knob to the right to display the ‘NRST’ airport waypoints to the aircraft’s current position. c) Turn the large FMS Knob to select the desired waypoint. d) Press the ENT Key. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 26 Flight planning Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index Or: a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed. b) Turn the small FMS Knob to the right to display the ‘RECENT’ waypoints. c) Turn the large FMS Knob to select the desired waypoint. d) Press the ENT Key. enter an airWay in a Flight plan 1) Press the FPL Key on the Control Unit. 2) Press the FMS Knob to activate the cursor (not required on the PFD). 3) Turn the large FMS Knob to highlight the waypoint after the desired airway entry point. If this waypoint is not a valid airway entry point, a valid entry point should be entered at this time. 4) Turn the small FMS Knob one click clockwise and press the LD AIRWY Softkey, or press the MENU Key and select “Load Airway”(required on the PFD). The Select Airway Page is displayed. The LD AIRWY Softkey or the “Load Airway” menu item is available only when an acceptable airway entry waypoint has been chosen (the waypoint ahead of the cursor position). 5) Turn the FMS Knob to select the desired airway from the list, and press the ENT Key. Low altitude airways are shown first in the list, followed by “all” altitude airways, and then high altitude airways. 6) Turn the FMS Knob to select the desired airway exit point from the list, and press the ENT Key. ‘LOAD?’ is highlighted. 7) Press the ENT Key. The system returns to editing the flight plan with the new airway inserted. invert an aCtive Flight plan 1) Press the FPL Key to display the active flight plan. 2) Press the MENU Key to display the Page Menu. 3) Turn the large FMS Knob to highlight ‘Invert Flight Plan’. 4) Press the ENT Key. The original flight plan remains intact in its flight plan catalog storage location. 5) With ‘OK’ highlighted, press the ENT Key to invert the flight plan. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 27 Flight planning Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index remove a departure, arrival, approaCh, or airWay From a Flight plan 1) Press the FPL Key on the Control Unit to display the active flight plan. Press the FMS Knob to activate the cursor. Or: a) Turn the small FMS Knob to select the Flight Plan Catalog Page. b) Press the FMS Knob to activate the cursor. c) Turn the large FMS Knob to highlight the desired flight plan. d) Select the EDIT Softkey. 2) Turn the large FMS Knob to highlight the title for the approach, departure, arrival, or airway to be deleted. Titles appear in white directly above the procedure’s waypoints. 3) Press the CLR Key to display a confirmation window. 4) With ‘OK’ highlighted, press the ENT Key to remove the selected procedure or airway. store a Flight plan 1) After creating a flight plan on either the PFD or MFD, it may be saved by pressing the MENU Key. 2) Turn the large FMS Knob to highlight ‘Store Flight Plan’ and press the ENT Key. 3) With ‘OK’ highlighted, press the ENT Key to store the flight plan. edit a stored Flight plan 1) Press the FPL Key on the Control Unit and turn the small FMS Knob to display the Flight Plan Catalog Page. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the desired flight plan. 4) Select the EDIT Softkey. 5) Turn the large FMS Knob to place the cursor in the desired location. 6) Enter the changes, then press the ENT Key. 7) Press the FMS Knob to return to the Flight Plan Catalog Page. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 28 Flight planning Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index delete a Waypoint From the Flight plan 1) Press the FPL Key to display the active flight plan. Press the FMS Knob to activate the cursor. Or: a) Turn the small FMS Knob to select the Flight Plan Catalog Page. b) Press the FMS Knob to activate the cursor. c) Turn the large FMS Knob to highlight the desired flight plan. d) Select the EDIT Softkey. 2) Turn the large FMS Knob to highlight the waypoint to be deleted. 3) Press the CLR Key to display a ‘REMOVE (Wpt Name)?’ confirmation window. 4) 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. 5) Once all changes have been made, press the FMS Knob to remove the cursor. invert and aCtivate a stored Flight plan 1) Press the FPL Key on the Control Unit. 2) Turn the small FMS Knob to select the Flight Plan Catalog Page. 3) Press the FMS Knob to activate the cursor. 4) Turn the large FMS Knob to highlight the desired flight plan. 5) Select the INVERT Softkey. ‘Invert and activate stored flight plan?’ will be displayed. 6) With ‘OK’ highlighted, press the ENT Key. The selected flight plan is now inverted and activated. The original flight plan remains intact in its flight plan catalog storage location. Copy a Flight plan 1) Press the FPL Key on the Control Unit. 2) Turn the small FMS Knob to select the Flight Plan Catalog Page. 3) Press the FMS Knob to activate the cursor. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 29 Flight planning Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index 4) Turn the large FMS Knob to highlight the flight plan to be copied. 5) Select the COPY Softkey. A ‘Copy to flight plan #?’ confirmation window is displayed. 6) 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 1) Press the FPL Key on the Control Unit. 2) Turn the small FMS Knob to select the Flight Plan Catalog Page. 3) Press the FMS Knob to activate the cursor. 4) Turn the large FMS Knob to highlight the flight plan to be deleted. 5) Select the DELETE Softkey. A ‘Delete flight plan #?’ confirmation window is displayed. 6) 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 1) Press the FPL Key on the Control Unit to display the Active Flight Plan Page. 2) 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. 3) The default insertion point is at the end of the flight plan. If the selected waypoint is to be placed anywhere other than the end of the flight plan, press the FMS Knob to activate the cursor. Waypoints are inserted ABOVE the cursor. Turn the large FMS Knob to select the desired insertion point. 4) Select the LD WPT Softkey. The selected waypoint will be inserted at the selected point. The default user waypoint naming is USR000, USR001, USR002, and so on. 5) To change the user waypoint name, follow the procedure for modifying a user waypoint. export a Flight plan to an sd Card 1) Insert the SD card into the top card slot on the MFD. 2) Press the FPL Key on the Contol Unit to display the Active Flight Plan Page on the MFD. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 30 Flight planning Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index 3) Turn the small FMS Knob to select the Flight Plan Catalog Page. 4) Press the FMS Knob to activate the cursor. 5) Turn the large FMS Knob to highlight the flight plan to be exported. 6) Press the EXPORT Softkey. 7) Press the ENT Key to confirm the export. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 31 procedures Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index proCedures load and aCtivate a departure proCedure 1) Press the PROC Key. 2) Turn the large FMS Knob to highlight ‘SELECT DEPARTURE’. 3) Press the ENT Key. The cursor is displayed in the ‘DEPARTURE’ field with a list of available departures. 4) Turn the large FMS Knob to highlight the desired departure. 5) Press the ENT Key. A list of runways may be displayed for the departure. If so, turn either FMS Knob to select the desired runway. 6) Press the ENT Key. The cursor is displayed in the ‘TRANSITION’ field with a list of available transitions. 7) Turn the large FMS Knob to highlight the desired transition. 8) Press the ENT Key. 9) With ‘LOAD?’ highlighted, press the ENT Key. The departure will be active when the flight plan is active. aCtivate a departure leg 1) Press the FPL Key to display the active flight plan. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the desired waypoint within the departure. 4) Select the ACT LEG Softkey. A confirmation window showing the selected leg will be displayed. 5) With ‘ACTIVATE’ highlighted, press the ENT Key. load an arrival proCedure 1) Press the PROC Key. 2) Turn the large FMS Knob to highlight ‘SELECT ARRIVAL’. 3) Press the ENT Key. The cursor is displayed in the ‘ARRIVAL’ field with a list of available arrivals. 4) Turn the large FMS Knob to highlight the desired arrival. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 32 procedures Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index 5) Press the ENT Key. A list of transitions is displayed for the selected arrival. 6) Turn either FMS Knob to select the desired transition. 7) Press the ENT Key. A list of runways is displayed for the selected arrival. 8) Turn the large FMS Knob to highlight the desired runway. 9) Press the ENT Key. 10) With ‘LOAD?’ highlighted, press the ENT Key. 11) The arrival will become part of the active flight plan. aCtivate an arrival leg 1) Press the FPL Key on the Control Unit to display the active flight plan. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the desired waypoint within the arrival. 4) Select the ACT LEG Softkey. A confirmation window showing the selected leg is displayed. 5) With ‘ACTIVATE’ highlighted, press the ENT Key. load and/or aCtivate an approaCh proCedure NOTE: If certain GPS parameters (WAAS, RAIM, etc.) are not available, some published approach procedures for the desired airport may not be displayed in the list of available approaches. 1) Press the PROC Key. 2) Turn the large FMS Knob to highlight ‘SELECT APPROACH’. 3) Press the ENT Key. A list of available approaches for the destination airport is displayed. 4) Turn either FMS Knob to highlight the desired approach. 5) Press the ENT Key. A list of available transitions for the selected approach procedure is now displayed. 6) Turn either FMS Knob to select the desired transition. 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 200/B200 Series 190-00929-00 Rev. A 33 procedures Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index 7) Press the ENT Key. The cursor moves to the MINIMUMS field. 8) If desired, the DA/MDA for the selected approach procedure may be entered and displayed on the PFD. Turn the small FMS Knob in the direction of the green arrow to change the display from OFF to BARO. 9) Press the ENT Key. The cursor moves to the altitude field. Turn the small FMS Knob to enter the published DA/MDA for the selected approach procedure. 10) Press the ENT Key. ‘LOAD? or ACTIVATE?’ is now displayed with ‘LOAD?’ highlighted. 11) Turn the large FMS Knob to select either ‘LOAD?’ or ‘ACTIVATE?’. Selecting ‘LOAD?’ enters the selected approach procedure into the active flight plan, but is not currently active. Selecting ‘ACTIVATE?’ enters the selected approach procedure into the active flight plan and is immediately activated. 12) Press the ENT Key. aCtivate an approaCh in the aCtive Flight plan 1) Press the PROC Key. 2) Turn the large FMS Knob to highlight ‘ACTIVATE APPROACH’. 3) Press the ENT Key. aCtivate a veCtor to Final approaCh Fix 1) Press the PROC Key. 2) Turn the large FMS Knob to highlight ‘ACTIVATE VECTOR-TO-FINAL’. 3) Press the ENT Key. 4) The final approach course becomes the active leg. aCtivate a missed approaCh in the aCtive Flight plan 1) Press the PROC Key. 2) Turn the large FMS Knob to highlight ‘ACTIVATE MISSED APPROACH’. 3) Press the ENT Key. A confirmation window will be displayed. 4) With ‘ACTIVATE’ highlighted, press the ENT Key. Or: Press the go-around button. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 34 procedures Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index Blank Page Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 35 hazard avoidance Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index hazard avoidanCe Customizing the hazard displays on the navigation map 1) With the Navigation Map Page displayed, press the MENU Key to display the Navigation Map Page Menu. The cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Menu is displayed. Turn the small FMS Knob to select ‘Weather’ to customize 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. stormsCope® (optional) WARNING: The Stormscope system is not intended to be used for hazardous thunderstorm penetration. Weather information on the G1000 MFD is approved for weather avoidance only. Refer to the WX-500 Pilot’s Guide for detailed operation. displaying stormscope lightning data on the navigation map page 1) Press the MAP Softkey. 2) Press the STRMSCP Softkey. Press the STRMSCP Softkey again to remove Stormscope Lightning Data from the Navigation Map Page. 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 Select ‘Cell’ or ‘Strike’ as the Stormscope Lightning Mode 1) With the Weather Group selected, press the ENT Key. The cursor flashes on ‘STRMSCP LTNG’. 2) Turn the large FMS Knob to select ‘STRMSCP MODE’. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 36 hazard avoidance Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index 3) Turn the small FMS Knob to display the ‘Cell/Strike’ window. 4) Turn either FMS Knob to select ‘Cell’ or ‘Strike’. Press the ENT Key. 5) Push the FMS Knob to return to the Navigation Map Page. Clear Stormscope Lightning Data from the Navigation Map Page 1) Press the MENU Key (with the Navigation Map Page displayed). 2) Turn either FMS Knob to highlight the ‘Clear Stormscope® Lightning’ field and press the ENT Key. NOTE: If heading input is lost, strikes and/or cells must be cleared manually after the execution of each turn. This is to ensure that the strike and/or cell positions are depicted accurately in relation to the nose of the aircraft. stormscope page 1) Turn the large FMS Knob until the Map Page group is selected. 2) Turn the small FMS Knob select the Stormscope Page. Change the Stormscope Lightning Mode Between ‘Cell’ and ‘Strike’ 1) Select the Stormscope Page. 2) Press the MODE Softkey. The CELL and STRIKE Softkeys are displayed. Press the CELL Softkey to display ‘CELL’ data or press the STRIKE Softkey to display ‘STRIKE’ data. ‘CELL’ or ‘STRIKE’ is displayed in the mode box located in the upper left corner of the Stormscope Page. NOTE: “Cell mode” uses a clustering program to identify clusters of electrical activity that indicate cells. Change the Viewing Mode Between 360˚ and 120˚ 1) Select the Stormscope Page. 2) Press the VIEW Softkey. The 360 and ARC Softkeys are displayed. Press the 360 Softkey to display a 360˚ viewing area or press the ARC Softkey to display a 120˚ viewing area. Press the CLEAR Softkey to remove all Stormscope lightning data from the display. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 37 hazard avoidance Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index xm Weather (optional) WARNING: Use of XM weather for hazardous weather penetration is not recommended. Weather information provided by XM Radio Service is approved only for weather avoidance, not penetration. displaying xm Weather on the navigation map page 1) Press the MAP Softkey. 2) Press the NEXRAD or XM LTNG Softkey to display the desired weather. Press the applicable softkey again to remove weather data from the Navigation Map Page. display metar and taF information on the airport information page 1) Turn the large FMS Knob to select the WPT Page Group. 2) Turn the small FMS Knob to select the Airport Information Page. 3) Select the WX Softkey to display METAR and TAF text (METAR and TAF information is updated every 12 minutes). displaying Weather on the Weather data link page 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Weather Data Link Page. 3) Select the available softkeys to select the desired XM weather product. 4) Select the LEGEND Softkey to view the legends for the selected products. If necessary, turn either FMS Knob to scroll through the list. Press the small FMS Knob or the ENT Key to return to the map. map panning information – Weather data link page 1) Push in the Joystick to display the panning arrow. 2) Move the Joystick to place the panning arrow on AIRMETs, TFRs, METARs, or SIGMETs. 3) Press the ENT Key to display pertinent information for the selected product. Note that pressing the ENT Key when panning over an AIRMET or a SIGMET displays an information box that shows the text of the report. Panning over an airport with METAR information does not display more Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 38 hazard avoidance Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index 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 Echo Top (Cloud Top and Echo Top Mutually Exclusive) NEXRAD Cloud Top XM Lightning Cell Movement SIGMETs/AIRMETs METARs City Forecast Surface Analysis Freezing Levels Winds Aloft County Warnings Turbulence PIREPs AIREPs Cyclone Warnings Icing Potential traFFiC systems • If Traffic information Service (TIS) is configured, a STANDBY, OPERATE, and TNA MUTE Softkey will be displayed. • If a Traffic Advisory System (TAS) is configured, a STANDBY, OPERATE, TEST, and ALT MODE Softkey will be displayed. Traffic Symbol Description Non-Threat Traffic (intruder is beyond 5 nm and greater than 1200’ vertical separation) Proximity Advisory (PA)(TAS only, not available with TIS) (intruder is within 5 nm and less than 1200’ vertical separation) Traffic Advisory (TA) (closing rate, distance, and vertical separation meet TA criteria) Traffic Advisory Off Scale Traffic Symbol Description traffic information service (tis) NOTE: If the G1000 is configured to use an optional Traffic Advisory System (TAS), TIS is not available for use. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 39 hazard avoidance Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index NOTE: Traffic Information Service (TIS) is only available when the aircraft is within the service volume of a TIS capable terminal radar site. Displaying Traffic on the Traffic Map Page 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Traffic Map Page. 3) Select the OPERATE Softkey to begin displaying traffic. ‘OPERATING’ is displayed in the Traffic Mode field. 4) Select the STANDBY Softkey to place the system in the Standby Mode. ‘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. Displaying Traffic on the Navigation Map 1) Ensure TIS is operating. With the Navigation Map displayed, press the MAP Softkey. 2) Select the TRAFFIC Softkey. Traffic will now be displayed on the map. traffic advisory system (tas) (optional) System Self Test 1) Set the range to 2/6 nm. 2) Press the STANDBY Softkey. 3) Press the TEST Softkey. 4) Self test will take approximately eight seconds to complete. When completed successfully, traffic symbols will be displayed and a voice alert appropriate for the installed system will be heard indicating the test passed (see Annuciations & Alerts section). If the self test fails, the system will revert to Standby Mode and a voice alert appropriate for the installed system will be heard indicating the test failed. 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. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 40 hazard avoidance Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index 3) Press the OPERATE Softkey to begin displaying traffic. ‘OPERATING’ is displayed in the Traffic Mode field. 4) Press the ALT MODE Softkey to change the altitude display volume. Select the desired altitude volume by pressing the BELOW, NORMAL, ABOVE, or UNREST (unrestricted) Softkey. The selection is displayed in the Altitude Mode field. 5) Press the STANDBY Softkey to place the system in the Standby Mode. ‘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. Displaying Traffic on the Navigation Map 1) With the Navigation Map displayed, press the MAP Softkey. 2) Press the TRAFFIC Softkey. Traffic will now be displayed on the map. terrain aWareness & Warning system (taWs) display NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south. NOTE: TAWS operation is only available when the G1000 is configured for a TAWS-B installation. manual system test 1) While the TAWS Page is displayed, press the MENU Key. 2) Turn the small FMS Knob to select ‘Test TAWS System’. 3) Press the ENT Key. During the test ‘TAWS TEST’ is displayed in the center of the TAWS Page. When all is in working order, “TAWS System Test, OK” will be heard. display terrain on the taWs page 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the TAWS Page. 3) If desired, select the VIEW Softkey to access the ARC and 360 softkeys. When the ARC Softkey is selected, a radar-like 120° view is displayed. Select the 360 Softkey to return to the 360° default display. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 41 hazard avoidance Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index 4) Rotate the Joystick clockwise to display a larger area or rotate counter- clockwise to display a smaller area. Color Terrain/Obstacle Location Red Terrain/Obstacle above or within 100’ below current aircraft altitude. Yellow Terrain/Obstacle between 100’ and 1000’ below current aircraft altitude. Black Terrain/Obstacle is more than 1000’ below aircraft altitude. enable/disable aviation data 1) While the TAWS Page is displayed, press the MENU Key. 2) Turn the small FMS Knob to select “Show (or Hide) Aviation Data”. 3) Press the ENT Key. taWs inhibit Inhibit TAWS While the TAWS Page is displayed, press the INHIBIT Softkey. Or: 1) Press the MENU Key. 2) Turn the small FMS Knob to select ‘Inhibit TAWS’. 3) Press the ENT Key. Enable TAWS While the TAWS Page is displayed, press the INHIBIT Softkey. or: 1) While the TAWS Page is displayed, press the MENU Key. 2) Turn the small FMS Knob to select ‘Enable TAWS’. 3) Press the ENT Key. NOTE: If TAWS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS WAAS approach, a LOW ALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 42 hazard avoidance Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index airBorne Color Weather radar WARNING: Begin transmitting only when it is safe to do so. If it is desired to transmit while the aircraft is on the ground, no personnel or objects should be within 11 feet of the antenna. CAUTION: In Standby Mode, the antenna is parked at the center line. It is always a good idea to put the radar in Standby Mode before taxiing the aircraft to prevent the antenna from bouncing on the bottom stop and possibly causing damage to the radar assembly. displaying Weather on the Weather radar page 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Weather Radar Page. 3) Select the MODE Softkey. 4) If the aircraft is on the ground, select the STANDBY Softkey to initiate the one minute warm-up period. After the warm-up is complete, the radar will enter the Standby Mode. After the aircraft is airborne, select the WEATHER Softkey. or: If the aircraft is already airborne, select the WEATHER or GROUND Softkey. The one-minute warm-up period will be initiated, after which the radar will begin transmitting. The horizontal scan is initially displayed. 5) Turn the Joystick to select the desired range. 6) If desired, select the VERTICAL Softkey for vertical scanning. adjusting antenna tilt Move the Joystick up or down to adjust the tilt of the antenna up or down. Moni- tor the displayed tilt value in the TILT field. When scanning vertically, a Tilt Line may be displayed to aid in positioning the tilt of the antenna. If the Tilt Line is not displayed, perform the following steps: 1) Press the MENU Key 2) Turn the large FMS Knob to select ‘Show Tilt Line’. 3) Press the ENT Key. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 43 hazard avoidance Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index adjusting antenna Bearing Move the Joystick right or left to adjust the azimuth position of the antenna right or left. Monitor the displayed bearing value in the BEARING field. When scanning horizontally, a Bearing Line may be displayed to aid in positioning the antenna for the vertical scan. If the Bearing Line is not displayed, perform the following steps: 1) Press the MENU Key 2) Turn the large FMS Knob to select ‘Show Bearing Line’. 3) Press the ENT Key. Vertically Scan a Storm Cell 1) While in the Horizontal Scan view, move the Joystick to place the Bearing Line on the desired storm cell, or other area, to be vertically scanned. 2) Select the VERTICAL Softkey. A vertical ‘slice’ of the selected area will now be displayed. 3) Move the Joystick right or left to move the scanned “slice” a few degrees right or left. 4) Turn the Joystick to adjust the range. 5) To select a new area to be vertically scanned, select the HORIZON Softkey to return to the Horizontal Scan view and repeat the previous steps. adjusting gain WARNING: Changing the gain in Weather Mode will cause precipitation intensity to be displayed as a color not representative of the true intensity. Remember to return the gain setting to ‘Calibrated’ for viewing the actual intensity of precipitation. 1) Select the GAIN Softkey to activate the cursor in the ‘GAIN’ field. 2) Turn the small FMS Knob to adjust the gain for the desirable level. The gain setting is visible in the gain field as a movable horizontal bar in a flashing box. The line pointer is a reference depicting the calibrated position. 3) Press the FMS Knob to remove the cursor. 4) Select the GAIN Softkey again to recalibrate the gain. ‘CALIBRATED’ will be displayed in the ‘GAIN’ field. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 44 hazard avoidance Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index ground mapping 1) Select the MODE Softkey. 2) Select the GROUND Softkey to place the radar in Ground Map Mode. 3) Select the BACK Softkey. sector scan 1) While in the Horizontal Scan Mode, move the Joystick right or left to place the Bearing Line in the desired position. The location of the Bearing Line will become the center point of the Sector Scan. 2) Press the FMS Knob to display the cursor. 3) Turn the large FMS Knob to place the cursor in the SECTOR SCAN field. 4) Turn the small FMS Knob to select FULL, 60˚, 40˚, or 20˚ scan. 5) If desired, readjust the Bearing Line with the Joystick to change the center of the Sector Scan. 6) Press the FMS Knob to remove the cursor. antenna stabilization 1) To activate or deactivate the antenna stabilization, select the MODE Softkey. 2) Select the STAB ON Softkey to activate antenna stabilization or select the STAB OFF Softkey to deactivate. The current stabilization condition is shown in the upper right of the weather radar display. Weather attenuated Color highlight (WatCh®) To activate or deactivate the WATCh® feature, select the WATCH Softkey. This feature is only available in the horizontal Scan Mode. Weather alert To activate or deactivate Weather Alert, select the WX ALRT Softkey. Activating and deactivating will also enable or inhibit the alert on the PFD. automatic standby When the weather radar system is in the Weather or Ground Map Mode, upon landing the system will automatically switch to Standby Mode. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 45 additional Features Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index additional Features synthetiC vision WARNING: Use appropriate primary systems for navigation, and for terrain, obstacle, and traffic avoidance. SVS is intended as an aid to situational aware- ness only and may not provide either the accuracy or reliability upon which to solely base decisions and/or plan maneuvers to avoid terrain, obstacles, or traffic. Synthetic Vision System (SVS) functionality is offered as an optional enhancement to the G1000 system. SVS is primarily comprised of a computer-generated forward-looking, attitude aligned view of the topography immediately in front of the aircraft from the pilot’s perspective. SVS information is shown on the primary flight display (PFD). In addition to SVS enhancement to the PFD, the following features have been added to the PFD: • Pathways • Flight Path Marker • horizon heading Marks • Terrain and Obstacle Alerting • Three-dimensional Traffic • Airport Signs • Runway Display displaying svs terrain 1) Press the PFD Softkey. 2) Press the SYN VIS Softkey. 3) Press the SYN TERR Softkey. 4) Press the BACK Softkey to return to the previous page. displaying pathways 1) Press the PFD Softkey. 2) Press the SYN VIS Softkey. 3) If not already enabled, press the SYN TERR Softkey. 4) Press the PATHWAY Softkey. 5) Press the BACK Softkey to return to the previous page. Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-00929-00 Rev. A 46 additional Features Flight Instruments Nav/Com/ XPDR/Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Annun/Alerts Appendix Index displaying heading on the horizon 1) Press the PFD Softkey. 2) Press the SYN VIS Softkey. 3) If not already enabled, press the SYN TERR Softkey. 4) Press the HRZN HDG Softkey. 5) Press the BACK Softkey to return to the previous page. displaying airport signs 1) Press the PFD Softkey. 2) Press the SYN VIS Softkey. 3) If not already enabled, press the SYN TERR Softkey. 4) Press the APTSIGNS Softkey. 5) Press the BACK Softkey to return to the previous page. terminal proCedure Charts NOTE: With the availability of SafeTaxi®, ChartView, or FliteCharts® in electronic form, it is still advisable to carry another source of charts on-board the aircraft. safetaxi® SafeTaxi® is an enhanced feature that gives greater map detail as the map range is adjusted in on the airport. The airport display on the map reveals runways with numbers, taxiways identifiers, and airport landmarks including ramps, buildings, control towers, and other prominent features. Resolution is greater at lower map ranges. The aircraft symbol provides situational awareness while taxiing. Pressing the DCLTR Softkey (declutter) once removes the taxiway markings and airport identification labels. Pressing the DCLTR Softkey twice removes VOR station ID, the VOR symbol, and intersection names if within the airport plan view. Pressing the DCLTR Softkey a third time removes the airport runway layout, unless the airport in view is part of an active route structure. Pressing the DCLTR Softkey again cycles back to the original map detail. The SafeTaxi database contains detailed airport