Garmin G1000 Cockpit Reference Guide for the Cessna 350/400

WARNING: The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment. Portions of the Garmin G1000 utilize GPS as a precision 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 Cessna 350/400 Pilot’s Operating Handbook. Thoroughly practice basic operation prior to actual use. During flight operations, carefully compare indications from the G1000 to all available navigation sources, including the information from other NAVAIDs, visual sightings, charts, etc. For safety purposes, always resolve any discrepancies before continuing navigation. WARNING: The illustrations in this guide are only examples. Never use the G1000 to attempt to penetrate a thunderstorm. Both the FAA Advisory Circular, Subject: Thunderstorms, and the 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. Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B WARNINGS, CAUTIONS, & NOTES CAUTION: The Garmin G1000 does not contain any user-serviceable parts. Repairs should only be made by an authorized Garmin service center. Unauthorized repairs or modifications could void both the warranty and the pilot’s authority to operate this device under FAA/FCC regulations. NOTE: When using Stormscope, there are several atmospheric phenomena in addition to nearby thunderstorms that can cause isolated discharge points in the strike display mode. However, clusters of two or more discharge points in the strike display mode do indicate thunderstorm activity if these points reappear after the screen has been cleared. NOTE: All visual depictions contained within this document, including screen images of the G1000 panel and displays, are subject to change and may not reflect the most current G1000 system and aviation databases. Depictions of equipment may differ slightly from the actual equipment. NOTE: This device complies with part 15 of the FCC Rules. Operation is subject to the following two conditions: (1) this device may not cause harmful interference, and (2) this device must accept any interference received, including interference that may cause undesired operation. NOTE: This product, its packaging, and its components contain chemicals known to the 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. Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B RR-1 RECORD OF REVISIONS Part Number Change Summary 190-00567-00 Rev A Rev B Production release. Added C350 parameters, TAWS changes, and Stormscope. 190-00567-01 Rev A Added GDU 8.10 parameters, WAAS, VNAV, Airways, and Charts Revision Date of Revision Affected Pages Description B 12/07 i-Index-4 Changed Columbia references to Cessna Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B RR-2 RECORD OF REVISIONS Blank Page Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B i TABLE OF CONTENTS SECTION 1: SYSTEM OVERVIEW.................................... 1-1 1.1 PFD/MFD Controls................................................... 1-2 1.2 GCU 476 Controls .................................................... 1-5 1.3 PFD Softkeys............................................................ 1-7 1.4 MFD Softkeys ........................................................ 1-10 1.5 MFD Page Groups ................................................. 1-11 1.6 Vertical Navigation .............................................. 1-12 1.7 Backlighting ........................................................... 1-14 1.8 Database Updates ................................................ 1-14 Jeppesen Aviation Database ...................................... 1-14 Garmin Databases ..................................................... 1-15 SECTION 2: FLIGHT INSTRUMENTS .............................. 2-1 2.1 Airspeed Indicator.................................................. 2-3 Speed Indication ......................................................... 2-3 Speed Ranges ............................................................. 2-3 Airspeed Trend Vector ................................................. 2-3 Vspeed References ...................................................... 2-3 2.2 Attitude Indicator .................................................. 2-4 2.3 Altimeter .................................................................. 2-4 Altitude Select Bug ...................................................... 2-4 Altitude Trend Vector ................................................... 2-4 Barometric Setting Box ................................................ 2-5 Altitude Alerting .......................................................... 2-5 Metric Display ............................................................. 2-5 Low Altitude Annunciation (WAAS Only) ...................... 2-6 2.4 Vertical Deviation/Glidepath/Glideslope Indicator ................................................................... 2-6 2.5 Marker Beacon Annunciations ............................ 2-7 2.6 Vertical Speed Indicator ....................................... 2-7 2.7 Barometric Altitude Minimums ........................... 2-8 2.8 Horizontal Situation Indicator (HSI) ................... 2-9 Arc HSI ....................................................................... 2-9 Turn Rate Indicator and Heading Trend Vector ............ 2-10 Course Pointer .......................................................... 2-10 Course Deviation Indicator (CDI) ................................ 2-10 Bearing Pointers and Information Windows ................ 2-11 Navigation Source ..................................................... 2-12 2.9 Wind Data............................................................... 2-13 2.10 Generic Timer ........................................................ 2-13 SECTION 3: ENGINE INDICATION SYSTEM (EIS).... 3-1 3.1 EIS Display................................................................ 3-2 Oxygen System (Optional) ........................................... 3-2 Trim ............................................................................ 3-2 Carbon Monoxide Detection ........................................ 3-2 3.2 Engine Leaning Assist Display ............................. 3-3 Engine Leaning for the Cessna 350.............................. 3-3 Engine Leaning for the Cessna 400.............................. 3-5 3.3 Fuel Calculations .................................................... 3-6 SECTION 4: NAV/COM AND TRANSPONDER .......... 4-1 4.1 Radio Status Indications ....................................... 4-3 4.2 Volume ...................................................................... 4-3 4.3 Automatic Squelch ................................................. 4-3 4.4 Quickly Activating 121.500 MHz .......................... 4-3 4.5 Frequency Auto-tuning ......................................... 4-3 Auto-tuning on the PFD .............................................. 4-3 Auto-tuning on the MFD ............................................. 4-3 4.6 Transponder ............................................................. 4-4 Mode Selection ........................................................... 4-4 Reply Status ................................................................ 4-4 Code Selection ............................................................ 4-5 SECTION 5: AUDIO PANEL ................................................ 5-1 5.1 COM Radio Selection ............................................. 5-2 5.2 Split COM Function ................................................ 5-2 5.3 Marker Beacon Receiver ....................................... 5-2 5.4 Nav Radio Audio Selection ................................... 5-3 5.5 Intercom System (ICS) Isolation .......................... 5-3 5.6 Intercom Squelch Control ..................................... 5-4 5.7 Digital Clearance Recorder and Player ............. 5-4 SECTION 6: AUTOMATIC FLIGHT CONTROL ............. 6-1 6.1 AFCS Controls .......................................................... 6-1 6.2 Flight Director Operation ..................................... 6-1 Activating the Flight Director ....................................... 6-1 Command Bars ........................................................... 6-2 AFCS Status Box ......................................................... 6-2 6.3 Flight Director Modes............................................ 6-3 Pitch Modes ................................................................ 6-3 Roll Modes................................................................ 6-16 6.4 Autopilot Operation ............................................ 6-21 Engaging the Autopilot.............................................. 6-21 Control Wheel Steering.............................................. 6-21 Disengaging the Autopilot ......................................... 6-22 Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B ii TABLE OF CONTENTS 6.5 Example Procedures Using AFCS ....................... 6-23 Departure ................................................................. 6-24 Intercepting a VOR Radial .......................................... 6-25 Flying a Flight Plan/GPS Course ................................. 6-26 Descent .................................................................... 6-27 Approach .................................................................. 6-30 Go Around/Missed Approach ..................................... 6-32 6.6 AFCS Annunciations and Alerts ......................... 6-33 AFCS Status Alerts..................................................... 6-33 Overspeed Protection ................................................ 6-34 SECTION 7: NAVIGATION .................................................. 7-1 7.1 Navigation Map Page ............................................ 7-1 7.2 Direct-to Navigation .............................................. 7-1 Direct-to Navigation from the MFD .............................. 7-1 Direct-to Navigation from the PFD ............................... 7-3 7.3 Navigating an Example Flight Plan .................... 7-5 7.4 Airport Information ............................................. 7-21 7.5 Intersection Information .................................... 7-23 7.6 NDB Information................................................... 7-24 7.7 VOR Information ................................................... 7-24 7.8 User Waypoint Information Page ..................... 7-25 7.9 Nearest Airports ................................................... 7-25 Nearest Airport Information on the MFD .................... 7-25 Nearest Airports Information on the PFD .................... 7-26 7.10 Nearest Intersections .......................................... 7-26 7.11 Nearest NDB .......................................................... 7-27 7.12 Nearest VOR ........................................................... 7-27 7.13 Nearest User Waypoint........................................ 7-28 7.14 Nearest Frequencies ............................................ 7-28 7.15 Nearest Airspaces ................................................. 7-29 SECTION 8: FLIGHT PLANNING ...................................... 8-1 8.1 User Defined Waypoints........................................ 8-1 Select the User WPT Information Page ......................... 8-1 Create User Waypoints from the Navigation Map Page . 8-1 8.2 Viewing the Active Flight Plan ............................ 8-2 8.3 Activate a Stored Flight Plan ............................... 8-2 8.4 Activate a Flight Plan Leg .................................... 8-2 8.5 Stop Navigating a Flight Plan.............................. 8-3 8.6 Invert Active Flight Plan ....................................... 8-3 8.7 Create a New Flight Plan ...................................... 8-3 Create a New Flight Plan Using the MFD ..................... 8-3 Create a New Flight Plan Using the PFD ...................... 8-4 8.8 Enter an Airway in a Flight Plan ......................... 8-4 8.9 Load a Departure ................................................... 8-6 8.10 Load an Arrival ........................................................ 8-6 8.11 Load an Approach .................................................. 8-6 8.12 Remove a Departure, Arrival, Approach, or Airway from a Flight Plan .................................... 8-6 8.13 Store a Flight Plan .................................................. 8-6 8.14 Edit a Stored Flight Plan ....................................... 8-6 8.15 Delete a Waypoint from the Flight Plan............ 8-7 8.16 Invert and Activate a Stored Flight Plan .......... 8-7 8.17 Copy a Flight Plan .................................................. 8-7 8.18 Delete a Flight Plan ............................................... 8-7 8.19 Graphical Flight Plan Creation ............................ 8-8 8.20 Trip Planning............................................................ 8-8 SECTION 9: PROCEDURES ................................................ 9-1 9.1 Arrivals and Departures........................................ 9-1 Load and Activate a Departure Procedure .................... 9-1 Load and Activate An Arrival Procedure ........................ 9-1 9.2 Approaches .............................................................. 9-2 Load and/or Activate an Approach Procedure ............... 9-3 Activate An Approach in the Active Flight Plan ............. 9-3 SECTION 10: HAZARD AVOIDANCE ........................... 10-1 10.1 Customizing the Hazard Displays on the Navigation Map ..................................................... 10-1 10.2 STORMSCOPE® (Optional, 350 only) ........................ 10-1 Displaying Stormscope Lightning Data on the Navigation Map Page ................................................ 10-1 Stormscope Page....................................................... 10-2 10.3 XM ® Weather (Optional) ..................................... 10-3 Displaying METAR and TAF information on the Airport Information Page ........................................... 10-3 Displaying Weather on the Weather Data Link Page ... 10-4 Map Panning Information – Weather Data Link Page . 10-5 Weather Products and Symbols ................................. 10-5 Weather Product Age ................................................ 10-6 10.4 Traffic Information Service (TIS) ....................... 10-7 Displaying Traffic on the Traffic Map Page................... 10-7 Displaying Traffic on the Navigation Map ................... 10-7 TIS Audio Alert .......................................................... 10-7 10.5 Ryan ® 9900BX Traffic Advisory System (TAS) (Optional) ............................................................... 10-8 Displaying Traffic on the Traffic Map Page................... 10-8 Displaying Traffic on the Navigation Map ................... 10-8 Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B iii TABLE OF CONTENTS 10.6 Terrain And Obstacle Proximity ........................ 10-9 Displaying Terrain and Obstacles on the Terrain Proximity Page .......................................................... 10-9 Displaying Terrain and Obstacles on the Navigation Map.......................................................................... 10-9 10.7 Terrain Awareness & Warning System (TAWS) Display (Optional) ................................ 10-10 Displaying Terrain on the TAWS Page ....................... 10-10 Enable/Disable Aviation Data ................................... 10-11 TAWS Inhibit ........................................................... 10-11 Manual System Test ................................................. 10-12 Forward Looking Terrain Avoidance (FLTA) ................ 10-12 Premature Descent Alert (PDA) ................................ 10-12 Excessive Descent Rate Alert (EDR) .......................... 10-13 Negative Climb Rate After Takeoff Alert (NCR).......... 10-13 “Five-Hundred” Aural Alert...................................... 10-13 Pop-up Alerts .......................................................... 10-14 Displaying Terrain and Obstacles on the Navigation Map........................................................................ 10-14 Alert Annunciations ................................................. 10-14 TAWS Alerts Summary ............................................. 10-15 SECTION 11: ABNORMAL OPERATION ..................... 11-1 11.1 Reversionary Mode .............................................. 11-1 11.2 Abnormal COM Operation .................................. 11-2 11.3 Unusual Attitudes ................................................. 11-2 11.4 Stormscope operation with loss of Heading Input ........................................................................ 11-2 11.5 Hazard Displays with Loss of GPS Position .... 11-2 11.6 Dead Reckoning .................................................... 11-2 SECTION 12: ANNUNCIATIONS & ALERTS .............. 12-1 12.1 Alert Level Definitions ........................................ 12-2 12.2 Aircraft Alerts ........................................................ 12-3 WARNING Alerts ....................................................... 12-3 CAUTION Alerts ........................................................ 12-3 Annunciation Advisory ............................................... 12-4 Message Advisory Alerts ............................................ 12-4 12.3 CO Guardian Messages ....................................... 12-4 12.4 AFCS Alerts............................................................. 12-5 System Status Annunciation....................................... 12-5 12.5 TAWS ALERTS ......................................................... 12-6 TAWS System Status Annunciations ........................... 12-7 12.6 G1000 System Annunciations ............................ 12-7 12.7 G1000 System Message Advisories .................. 12-9 MFD & PFD Message Advisories............................... 12-10 Database Message Advisories .................................. 12-11 GMA 1347 Message Advisories ............................... 12-12 GIA 63 Message Advisories ..................................... 12-13 GIA 63W Message Advisories .................................. 12-16 GEA 71 Message Advisories .................................... 12-18 GTX 33 Message Advisories..................................... 12-19 GRS 77 Message Advisories..................................... 12-19 GMU 44 Message Advisories ................................... 12-20 GDL 69A Message Advisories .................................. 12-20 GDC 74A Message Advisories.................................. 12-20 GCU 476 Message Advisories .................................. 12-20 Miscellaneous Message Advisories ........................... 12-21 INDEX ...................................................................................Index-1 Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B iv TABLE OF CONTENTS Blank Page Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B 1-1 SECTION 1 SYSTEM OVERVIEW 1-1 SECTION 1: SYSTEM OVERVIEW The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system more easily. It is not intended to be a comprehensive operating guide. Complete operating procedures for the complete system are found in the G1000 Cessna 350/400 Pilot’s Guide (190-00552-01): This guide gives the pilot abbreviated operating instructions for the Primary Flight Display (PFD), Multi Function Display (MFD), GCU 476 MFD/PFD Control Unit, and the GMA 1347 Audio Panel System. NOTE: The pilot should read and thoroughly understand the Cessna 350/400 Airplan Flight Manual (AFM) for limitations, procedures and operational information not contained in this Cockpit Reference Guide. The Cessna 350/400 AFM always takes precedence over the information found in this guide. NOTE: Speed ranges and V-speeds shown in this guide are for example only. Refer to the AFM for values pertaining to the Cessna 350 and Cessna 400. Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B 1-2 SECTION 1 SYSTEM OVERVIEW 1.1 PFD/MFD CONTROLS Figure 1-1 PFD/MFD Controls 4 2 1 6 5 7 9 8 3 12 13 11 10 16 15 14 MFD Only 17 27 26 25 28 18 19 23 22 21 20 24 Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B 1-3 SECTION 1 SYSTEM OVERVIEW PFD and MFD controls function the same with the exception of the dedicated Automatic Flight Control System (AFCS) keys located only on the MFD bezel. 1 NAV VOL/ID Knob – Controls the NAV audio level. Press to turn the Morse code identifier ON and OFF. Volume level is shown in the field as a percentage. 2 NAV Frequency Transfer Key – Transfers the standby and active NAV frequencies. 3 Dual NAV Knob – Tunes the MHz (large knob) and kHz (small knob) standby frequencies for the NAV receiver. Press to switch the tuning box (light blue box) between the NAV1 and NAV2 fields. 4 Heading Knob – Turn to manually select a heading on the HSI. When pressed, it synchronizes the heading bug with the compass lubber line. Selected Heading provides the heading reference to the Flight Director while operating in Heading Select Mode. 5 Joystick – Changes the map range (distance top to bottom of map display) when rotated. Activates the map pointer when pressed. 6 CRS/BARO Knob – The large knob sets the altimeter barometric pressure and the small knob adjusts the course. The course is only adjustable when the HSI is in VOR1, VOR2, or OBS/SUSP Mode. Pressing this knob centers the CDI on the currently selected VOR. Selected Course provides course reference to the Flight Director when operating in Navigation and Approach Modes. 7 Dual COM Knob – Tunes the MHz (large knob) and kHz (small knob) standby frequencies for the COM transceiver. Pressing this knob switches the tuning box (light blue box) between the COM1 and COM2 fields. 8 COM Frequency Transfer Key – Transfers the standby and active COM frequencies. Pressing and holding this key for two seconds automatically tunes the emergency frequency (121.5 MHz) in the active frequency field. 9 COM VOL/SQ Knob – Controls COM audio level. Pressing this knob turns the COM automatic squelch ON and OFF. Audio volume level is shown in the field as a percentage. 10 Direct-to Key – Allows the user to enter a destination waypoint and establish a direct course to the selected destination (specified by the identifier, chosen from the active route, or taken from the map pointer position). 11 FPL Key – Displays the active Flight Plan Page for creating and editing the active flight plan, or for accessing stored flight plans. 12 CLR Key (DFLT MAP) – Erases information, cancels an entry, or removes page menus. To display the Navigation Map Page immediately, press and hold CLR (MFD only). 13 Dual FMS Knob – Used to select the page to be viewed (only on the MFD). The large knob selects a page group (MAP, WPT, AUX, NRST), while the small knob selects a specific page within the page group. Pressing the small knob turns the selection cursor ON and OFF. When the cursor is ON, data may be entered in the different fields using the small and large knobs. The large knob is used to move the cursor on the page, while the small knob is used to select individual characters for the highlighted cursor location. When the Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B 1-4 SECTION 1 SYSTEM OVERVIEW G1000 displays a list that is too long for the display screen, a scroll bar appears along the right side of the display, indicating the availability of additional items within the selected category. Press the small FMS Knob to activate the cursor and turn the large FMS Knob to scroll through the list. 14 MENU Key – Displays a context-sensitive list of options. This list allows the user to access additional features, or to make setting changes that relate to certain pages. 15 PROC Key – Selects approaches, departures and arrivals from the flight plan. If a flight plan is used, available procedures for the departure and/ or arrival airport are automatically suggested. If a flight plan is not used, the desired airport and the desired procedure may be selected. This key selects IFR departure procedures (DPs), arrival procedures (STARs) and approaches (IAPs) from the database and loads them into the active flight plan. 16 ENT Key – Accepts a menu selection or data entry. This key is used to approve an operation or complete data entry. It is also used to confirm selections and information entries. 17 Dual ALT Knob – Sets the selected altitude in the box located above the Altimeter. The large knob selects the thousands, while the small knob selects the hundreds. Altitude Select is used by the Automatic Flight Control System in certain modes, in addition to the standard G1000 Altitude Alerter function. 18 AP Key – Engages/disengages the Autopilot and Flight Director. Pressing the AP Key activates the Flight Director and engages the Autopilot in the default pitch axis and roll axis modes. Pressing the AP Key again disengages the autopilot and deactivates the Flight Director. 19 FD Key – Activates/deactivates the Flight Director only. Pressing the FD Key turns on the Flight Director in the default pitch axis and roll axis modes. Pressing the FD Key again deactivates the Flight Director and removes the command bars, unless the Autopilot is engaged. If the Autopilot is engaged, the FD Key is disabled. 20 NAV Key – Selects/deselects the Navigation Mode. 21 ALT Key – Selects/deselects the Altitude Hold Mode. 22 VS Key – Selects/deselects the Vertical Speed Mode. 23 FLC Key – Selects/deselects the Flight Level Change Mode. 24 HDG Key – Selects/deselects the Heading Select Mode. 25 APR Key – Selects/deselects the Approach Mode. 26 VNV Key (WAAS only)– Selects/deselects Vertical Navigation Mode. 27 28 NOSE UP/NOSE DN Keys – Controls the active pitch reference for the Pitch Hold, Vertical Speed, and Flight Level Change Modes. Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B 1-5 SECTION 1 SYSTEM OVERVIEW 1.2 GCU 476 CONTROLS The indicators above the PFD, MFD, NAV, and COM Keys are lit when the respective control mode key is pressed. The unit is in MFD Control Mode by default, until the PFD Control Mode selection key is pressed. Many of the controls duplicate the controls on the PFD and MFD. The discussions later in this manual are cen- tered around using the controls on the PFD and/or MFD. When reading these discussions, keep in mind that many of the operations may also be performed on the GCU 476. Figure 1-2 MFD/PFD Control Unit (GCU 476) 2 1 4 3 5 6 7 8 9 11 10 12 13 15 14 16 17 18 19 1 FPL Key – Displays the active Flight Plan Page for creating and editing the active flight plan. 2 Direct-to Key – Allows the user to enter a destination waypoint and establish a direct course to the selected destination (the destination is either specified by the identifier, chosen from the active route, or taken from the map pointer position). 3 MENU Key – Displays a context-sensitive list of options. This list allows the user to access additional features or make setting changes that relate to particular pages. 4 PROC Key – Gives access to IFR departure procedures (DPs), arrival procedures (STARs) and approach procedures (IAPs) for a flight plan. If a flight plan is used, available procedures for the departure and/or arrival airport are automatically suggested and can be loaded into the active flight plan. If a flight plan is not used, both the desired airport and the desired procedure may be selected. 5 Joystick – Changes the map range (distance top to bottom of map display) when rotated; activates the map pointer when pressed. 6 Alphanumeric Keys – Allow data entry without using the GDU FMS Knob to select individual characters. 7 BKSP Key – Moves the cursor back one character space. 8 SPC Key – Adds a space. Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B 1-6 SECTION 1 SYSTEM OVERVIEW 9 ENT Key – Validates or confirms a menu selection or data entry. 10 CLR Key – Erases information, cancels entries, or removes page menus. Press and hold to immediately display the Navigation Map Page. 11 SEL Key – The center of this key activates the selected softkey, while the right and left arrows move the softkey selection box (light blue box around the softkey label) to the right and left, respectively. 12 Decimal Key – Enters a decimal point. 13 Plus-Minus (±) Key – Switches entry between the + and - characters. 14 NAV Key – Selects NAV Radio Control Mode. The FMS Knob will now control the NAV radios. 15 COM Key – Selects COM Radio Control Mode. The FMS Knob will now control the COM radios. 16 Frequency Transfer Key – Switches between active and standby selected COM or NAV tuning frequencies. Pressing and holding this key while in COM radio control mode tunes the COM radio to 121.50 MHz, the emergency COM frequency. 17 PFD Key – Selects PFD Control Mode. The FMS Knob will now control PFD functions. 18 MFD Key – Selects MFD Control Mode. The FMS Knob will now control MFD functions. 19 Dual FMS–NAV/COM Knob (Multifunction Control Knob) – With the MFD indicator illuminated, the FMS-NAV/COM Knob performs the same functions as a the FMS, NAV, and COM Knobs on the MFD. With the PFD indicator illuminated, the FMS- NAV/COM Knob performs the same functions as a the FMS, NAV, and COM Knobs on the PFD. Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B 1-7 SECTION 1 SYSTEM OVERVIEW 1.3 PFD SOFTKEYS Softkey OFF Softkey ON Figure 1-3 PFD Top Level Softkeys Press the BACK or OFF Softkey to return to the top-level softkeys. ALERTS STRMSCP ALERTS Figure 1-4 INSET Softkeys INSET – Press to display the Inset Map in the lower left corner of the PFD. OFF – Press to remove the Inset Map. DCLTR (3) – Press momentarily to select the desired amount of map detail. The declutter level appears adjacent to the DCLTR Softkey. - No declutter: All map features are visible. - Declutter – 1: Declutters land data. - Declutter – 2: Declutters land and SUA data. - Declutter – 3: Declutters large NAV data remaining (removes everything except the active flight plan). TRAFFIC – Press to display traffic on the map. TOPO – Press to display topographical data (i.e., coastlines, terrain, rivers, lakes, etc.) and elevation scale on the Inset Map. TERRAIN – Press to display terrain information on the Inset Map. STRMSCP (optional) – Press to display the Stormscope lightning data on the Inset Map (within a 200 nm radius of the aircraft). NEXRAD (optional) – Press to display NEXRAD weather and coverage information on the Inset Map. XM LTNG (optional) – Press to display XM lightning information on the Inset Map. BACK – Press to return to the previous level softkey configuration. Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B 1-8 SECTION 1 SYSTEM OVERVIEW Figure 1-5 PFD Configuration Softkeys Press the STD BARO or BACK Softkey to return to the top-level softkeys BRG1 (NAV1) BRG1 (GPS) BRG1 (OFF) ALT UNIT METERS IN HPA ALERTS ALERTS ALERTS ALERTS HSI FRMT ALERTS ARC HSI 360 HSI BRG2 (NAV2) BRG2 (GPS) BRG2 (OFF) PFD – Press to display the additional softkeys for additional configuration of the PFD. DFLTS – Press to reset default settings on the PFD. WIND – Displays softkeys to select wind data parameters. O P T N 1 – L o n g i t u d i n a l a n d l a t e r a l components. OPTN 2 – Total direction and speed. OPTN 3 – Total direction with headwind and crosswind speed components. OFF – Information not displayed. BRG1 (bearing) – Press to cycle through the following Nav sources, making the pointer the indicator for the corresponding source and displaying the appropriate information. NAV1 – Displays NAV1 waypoint frequency or identifier and DME information in the BRG1 Information Window. GPS – Displays GPS waypoint identifier and GPS distance information in the BRG1 Information Window. OFF – Removes the BRG1 Information Window. HSI FRMT – Press to display the HSI formatting softkeys. 360 HSI – Press to display the HSI in a 360 degree format. ARC HSI – Press to display the HSI in an arc format. BRG2 (bearing) – Press to cycle through the following Nav sources, making the pointer the indicator for the corresponding source and displaying the appropriate information. NAV2 – Displays NAV2 waypoint frequency or identifier and DME information in the BRG2 Information Window. GPS – Displays GPS waypoint identifier and GPS distance information in the BRG2 Information Window. OFF – Removes the BRG2 Information Window. Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B 1-9 SECTION 1 SYSTEM OVERVIEW ALT UNIT – Displays softkeys for setting the altimeter and BARO settings to metric units: METERS – When enabled, displays altimeter in meters. IN – Press to display the BARO setting as inches of mercury. HPA – Press to display the BARO setting as hectopacals. STD BARO – Press to set the barometric pressure to standard pressure. BACK – Press to return to the previous level softkeys. ALERTS – Press to display the Alerts Window. OBS – Press to select OBS Mode on the CDI when navigating by GPS (only available with active leg). CDI – Press to change navigation mode on the CDI between GPS, VOR1, and VOR2. XPDR – Press to display the transponder mode selection softkeys. STBY – Press to select Standby Mode. ON – Press to select Mode A. ALT – Press to select Altitude Reporting Mode. GND – Press to select Ground Mode. VFR – Press to automatically squawk 1200 (only in the U.S.A., refer to ICAO standards for VFR codes in other countries). Press the BACK Softkey to return to the top-level softkeys. Press the BACK Softkey to return to the top-level softkeys. ALERTS ALERTS ALERTS Figure 1-6 XPDR (Transponder) Softkeys CODE – Press to display transponder code selection softkeys 0-7. 0 through 7 – Press numbers to enter code. IDENT – Press to provide special aircraft position identification to Air Traffic Control (ATC). BKSP – Press to remove numbers entered one at a time. BACK – Press to return to the previous level softkeys. IDENT – Press to provide special aircraft position identification to Air Traffic Control (ATC). BACK – Press to return to the previous level softkeys. ALERTS – Press to display the Alerts Window. IDENT – Press to provide special aircraft position identification to Air Traffic Control (ATC). TMR/REF – Press to display the Timer/References Window. NRST – Press to display the Nearest Airports Window. ALERTS – Press to display the Alerts Window. Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B 1-10 SECTION 1 SYSTEM OVERVIEW 1.4 MFD SOFTKEYS SYSTEM – Selecting this softkey makes available the Engine Display functions. Refer to the Engine Indication System section. MAP – Pressing this softkey enables the following softkeys: TRAFFIC – Pressing this softkey displays/removes Traffic on the Navigation Map. TOPO – Pressing this softkey displays or removes topographic information on the Navigation Map. TERRAIN – Pressing this softkey displays/removes terrain and obstacle data on the Navigation Map. Figure 1-7 MFD Softkeys MAP DCLTR DCLTR-2 DCLTR-3 DCLTR-1 CHKLIST EXIT EMERGCY SYSTEM DONE The DONE Softkey changes to UNDO when the checklist item is already checked SYSTEM (optional) TRAFFIC TOPO BACK TERRAIN Press the BACK Softkey on this level to return to the top softkey level. STRMSCP NEXRAD XM LTNG (optional) (optional) (optional) AIRWAYS AIRWY LO AIRWAY HI AIRWY ON (Default softkey is dependant on the selection made in the map setup options) SHW CHRT (optional) Press the SYSTEM Softkey to return to the default page level. DCLTR SYSTEM ASSIST OXYGEN DEC FUEL INC FUEL RST FUEL CO RST AIRWAYS – Pressing this softkey displays/removes airways information. The default is dependent on map setup option selected. Pressing cycles through all airways displayed (AIRWY ON), low altitude airways only (AIRWY LO), and high altitude airways only (AIRWY HI). STRMSCP (optional) – Pressing this softkey displays/ removes Stormscope lightning data on the Navigation Map. NEXRAD (optional) – Pressing this softkey displays/ removes precipitation data on the Navigation Map. XM LTNG (optional) – Pressing this softkey displays/ removes XM Radio lightning data on the Navigation Map. Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B 1-11 SECTION 1 SYSTEM OVERVIEW BACK – Pressing this softkey displays the ENGINE and MAP top level softkeys. DCLTR (declutter) – Pressing this softkey removes map information in three levels. SHW CHRT (Show Chart)(optional) – Pressing this softkey displays optional FliteCharts or ChartView charts. CHKLIST (checklist)(optional) – Pressing the CHKLIST Softkey displays the Checklist Page. SYSTEM – Displays engine softkeys. DONE – Pressing this softkey checks off a checklist item. If an item is already checked, an UNDO Softkey will be displayed. EXIT – Press to exit the checklist. EMERGCY – Pressing this softkey displays the emergency checklist. Figure 1-8 Page Group Icon Map Page Group Waypoint Page Group Auxiliary Page Group Nearest Group Selected Page Number of Pages in Current Group 1.5 MFD PAGE GROUPS 1) Turn the large FMS Knob until the desired page group is selected. 2) Turn the small FMS Knob to select pages within the group. See Figure 1-8. Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B 1-12 SECTION 1 SYSTEM OVERVIEW 1.6 VERTICAL NAVIGATION In WAAS capable installations, one of two altitude sources is used by the G1000 when giving vertical navigation guidance. WAAS GPS altitude is used when giving guidance for a WAAS approach. Baro corrected altitude is used when vertical guidance is given in all other situations and in non-WAAS systems. The G1000 system can use altitude constraints associated with lateral waypoints to give guidance for vertical navigation. These altitudes are, depending on the specific instance, entered by the pilot or retrieved from the published altitudes in the navigation database. The navigation database only contains altitudes for procedures that call for “Cross at” altitudes. If the procedure states “Expect to cross at,” then the altitude will not be in the database. In this case the altitude may be entered manually. NOTE: All arrival procedure altitudes contained in the navigation database are for turbojet aircraft only. Alter or enter altitudes as desired to comply with the ATC clearance. When activating or loading an arrival or approach procedure into an active flight plan, the VNV ‘ALT’ fields will be populated with any altitudes that can be retrieved from the navigation database. Since altitudes loaded with an arrival procedure are published only for turbojet aircraft, the altitudes are displayed as white text indicating that the altitudes are displayed for reference only. An arrival waypoint altitude may be used (or “designated”) as is, or changed to a different altitude. An altitude is designated by pressing the FMS Knob and turning the large FMS Knob to place the cursor on the desired altitude and pressing the ENT Key or entering a different value and pressing the ENT Key. The altitude will now be displayed as light blue text, indicating that the altitude is now designated to give vertical speed and deviation guidance. Approach waypoint altitude constraints are automatically designated for use when the approach is loaded. These altitudes will be displayed as light blue text indicating the altitudes will be used in vertical guidance calculations. Waypoint altitude constraints may be designated up to, but not including the FAF. The FAF will always be a “reference only” altitude and cannot be designated, unless the selected approach does not provide vertical guidance. In this case, the FAF altitude can be designated. Altitudes that have been designated for use in vertical guidance may also be made “non-designated” by placing the cursor over the desired altitude and pressing the CLR Key. 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. To help interpret the meanings of how the altitudes are presented, keep the following points in mind: • When the altitude is displayed in light blue, the system is using that altitude (designated) to determine vertical speed and deviation guidance. • When the altitude is displayed in white, it is not being used by the system (non-designated) to determine the vertical speed and deviation guidance. • An altitude displayed as small text is an altitude that is published in the navigation database. • Altitudes displayed as a light blue subdued text cannot be used in the current vertical navigation calculations. Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B 1-13 SECTION 1 SYSTEM OVERVIEW 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 speed and deviation guidance. Altitude has been entered by the pilot. Altitude is designated for use in giving vertical speed and deviation 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 speed and deviation guidance. Small Text Altitude is not designated to be used in determining vertical speed and deviation guidance. Altitude has been retrieved from the navigation database and is provided as a reference. Altitude is designated for use in giving vertical speed and deviation 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 speed and deviation guidance. Table 1-1 VNV Altitude Text Size and Color Refer to Figure 1-8 and Table 1-1 for more detail regarding the significance of text size and color. Figure 1-9 VNAV Altitudes Large Light Blue Text Small White Text with Altitude Restriction Bar Large White Text Small Light Blue Subdued Text Small Light Blue Text Some altitudes retrieved from the database have associated restrictions indicating to stay ‘At’, ‘At or Above’, or ‘At or Below’ a specific altitude. These restrictions are indicated using a ‘bar’ above and/or below the appropriate altitude as shown in Figure 1-9. Cross AT or ABOVE 5,000 ft Cross AT or BELOW 3,000 ft Cross AT 2,300 ft Figure 1-10 Altitude Restrictions See Section 7 - Navigation, for a sample flight plan which further illustrates vertical navigation in more detail. Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B 1-14 SECTION 1 SYSTEM OVERVIEW 1.7 BACKLIGHTING When system power is turned off, all manual backlighting settings will return to the factory default settings. Manually adjust the backlight for the PFD and MFD: 1) Press the MENU Key on the PFD to display the PFD Setup Menu Window. 2) Press the small FMS Knob to activate the cursor. ‘PFD DSPL > AUTO’ is now highlighted. 3) Turn the small FMS Knob to display the selection window. 4) Turn the FMS Knob to select ‘MANUAL’, then press the ENT Key. 5) With the intensity value now highlighted, turn the small FMS Knob to select the desired backlighting. 6) Turn the large FMS Knob to highlight ‘MFD DSPL > AUTO’ and repeat steps 3 through 5. Figure 1-11 PFD Setup Menu Window 1.8 DATABASE UPDATES The G1000 System uses Secure Digital (SD) cards to load and store various types of data. For basic flight operations, SD cards are required for database storage as well as Jeppesen aviation and ChartView database updates. The following procedures pertain to updating the G1000 system with SD cards as outlined in Appendix B of the G1000 Cessna 350/400 Pilot’s Guide. Jeppesen Aviation Database NOTE: After the aviation database is installed, the card may be removed after loading the update to each LRU. Updating the Jeppesen aviation database: 1) With the G1000 System OFF, insert the SD card containing the aviation database update into the top card slot of the PFD to be updated (Label of SD card facing left). 2) Turn the G1000 System ON. A prompt similar to the following is displayed in the upper left corner of the PFD: Figure 1-12 Database Update Prompt 3) Press the ENT Key to start the database update. A prompt similar to the following is displayed: Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B 1-15 SECTION 1 SYSTEM OVERVIEW Figure 1-13 Database Update Confirmation 4) After the update completes, the PFD starts in normal mode. 5) Turn the G1000 System OFF and remove the SD card. 6) Repeat steps 1 through 4 for the MFD. The MFD and PFD databases are now updated. Remove the SD card when finished. 7) Verify that the correct update cycle is loaded during startup of the MFD. Garmin Databases Since these databases are not stored internally in the MFD or PFD, a Supplemental Data Card containing identical database versions must be kept in each display unit. 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. 1) Insert one SD card in the bottom card slot of the MFD and one in the bottom card slot of the PFD. The SD card containing the ChartView or FliteCharts database must be inserted into the bottom slot on the MFD. 2) Apply power to the G1000 System. View the MFD power-up splash screen. Check that the databases are initialized and displayed on the scrolling window of the splash screen. When updating the terrain and FliteCharts databases, an ‘in progress’ message may be seen. If this message is present, wait for the system to finish loading before verifying the correct databases are initialized, then proceed to step 3. Figure 1-14 Power-Up Splash Screen Window 3) Acknowledge the Power-up Page agreement by pressing the ENT Key or the right most softkey. 4) At the MAP – NAVIGATION MAP Page, select the MAP Softkey and check to make sure that the TOPO and TERRAIN Softkeys are available (not dimmed) and other database features are functioning. 5) Power down the G1000. Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B 1-16 SECTION 1 SYSTEM OVERVIEW Blank Page Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B 2-1 SECTION 2 FLIGHT INSTRUMENTS SECTION 2: FLIGHT INSTRUMENTS The following discussions pertain to the Primary Flight Display, unless otherwise indicated. The gradient color background shown in the following illustrations, is used in WAAS capable systems. A solid blue and brown background will be seen in non-WAAS systems 8 7 16 13 12 11 1 19 17 20 21 9 5 6 2 4 3 15 10 14 18 1 NAV Frequency Box 2 Airspeed Indicator 3 True Airspeed 4 Current Heading 5 Horizontal Situation Indicator ( HSI) 6 Outside Air Temperature (OAT) 7 Softkeys 8 System Time 9 Transponder Data Box 10 Selected Heading Bug 11 Turn Rate Indicator 12 Altimeter Barometric Setting 13 Vertical Speed Indicator (VSI) 14 Selected Altitude Bug 15 Altimeter 16 Selected Altitude 17 COM Frequency Box 18 AFCS Status Box 19 Navigation Status Box 20 Slip/Skid Indicator 21 Attitude Indicator Figure 2-1 Primary Flight Display (Default) Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B 2-2 SECTION 2 FLIGHT INSTRUMENTS 7 9 8 2 4 3 1 12 5 6 13 10 11 1 Traffic Annunciation 2 Vspeed References 3 Selected Heading 4 Wind Data 5 Inset Map 6 Bearing Information Windows 7 Selected Course 8 Alerts Window 9 Barometric Minimum Descent Altitude 10 Annunciation Window 11 Vertical Deviation/Glideslope Indicator 12 Marker Beacon Annunciation 13 AFCS Status Annunciation Figure 2-2 Additional PFD Information Figure 2-3 PFD Navigation Status Box Active Flight Plan Leg Distance to Next Waypoint Bearing to Next Waypoint Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B 2-3 SECTION 2 FLIGHT INSTRUMENTS 2.1 AIRSPEED INDICATOR Figure 2-4 Airspeed Indicator Actual Airspeed Airspeed Trend Vector True Air- speed Vspeed References Speed Ranges Speed Indication The indicated airspeed is displayed inside the black pointer. The pointer will become red upon reaching Vne. At altitudes above 12,000 feet, Vno and Vne will vary with altitude. Refer to the Airplane Flight Manual (AFM). Figure 2-5 Red Pointer at VNE Speed Ranges The color coded speed range strip denotes flaps operating range, normal operating range, and never exceed speed (Vne). A red range is also present for low speed awareness. At altitudes above 12,000 feet, caution and excessive speed range markings will vary with altitude. Refer to the Airplane Flight Manual (AFM) for airspeed limitations and indicator markings. Airspeed Trend Vector The end of the trend vector displays approximately what the airspeed will be in 6 seconds if the current rate of acceleration/deceleration is maintained. Vspeed References Vspeed References are turned on or off in the Timer/References Window. Select the TMR/REF Softkey to display the widow. When active (ON), the Vspeeds are displayed at their respective locations to the right of the airspeed scale. To activate the Vspeed References, display the Timer/Reference Window and turn the large FMS Knob to place the cursor in the ON/OFF field. Turn the small FMS Knob to select ON or OFF. Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B 2-4 SECTION 2 FLIGHT INSTRUMENTS 2.2 ATTITUDE INDICATOR The Slip/Skid Indicator is located under the Roll Pointer and moves laterally away from the pointer to indicate lateral acceleration. One Slip/Skid indicator displacement is equal to one ball displacement when compared to a traditional slip/skid indicator. Figure 2-6 Attitude Indicator 3 2 1 9 8 7 6 5 4 1 2 3 4 5 Roll Scale Horizon Line Aircraft Symbol Land Representation Roll Pointer 6 7 8 9 Aircraft Wing Tips Pitch Scale Sky Representation Slip/Skid Indicator Roll Scale Zero 10 10 2.3 ALTIMETER Altitude Reference Box Altitude Trend Vector Current Altitude Barometric Setting Box Altitude Reference Bug Figure 2-7 Altimeter Barometric Altitude Minimums Bug Altitude Select Bug The Altitude Select Bug is displayed at the selected altitude or, if the selected altitude is beyond the altitudes currently displayed, the bug is displayed at the top or bottom of the display (whichever is closest to the selected altitude). Set the Selected Altitude Bug: Turn the ALT Knobs to set the Altitude Select Bug. The small ALT Knob sets the hundreds and the large ALT Knob sets the thousands. This altitude also appears in the Selected Altitude Box above the Altimeter. Altitude Trend Vector The end of the trend vector displays approximately what the altitude will be in 6 seconds if the current rate of vertical speed is maintained. Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B 2-5 SECTION 2 FLIGHT INSTRUMENTS Barometric Setting Box Select barometric pressure: Turn the BARO Knob to select the desired setting. Quickly enter standard pressure: 1) Press the PFD Softkey. 2) Press the STD BARO Softkey. Altitude Alerting Figure 2-8 Altitude Alerting Visual Annunciations Within 1000 ft Within 200 ft Deviation of ±200 ft Visual annunciations appear in the Selected Altitude Box. Whenever the Selected Altitude is changed, the Altitude Alerter is reset. The Altitude Alerter is independent of the Automatic Flight Control System. An aural tone is heard when the aircraft is within 200 feet of acquiring the selected altitude or when deviating beyond 200 feet of the acquired selected altitude. Metric Display Display altitude in meters and barometric pressure in hectopascals: 1) Press the PFD Softkey to display the second level softkeys. 2) Press the ALT UNIT Softkey. 3) Press the METERS Softkey to display altitude in meters. 4) Press the HPA Softkey to display the barometric setting in hectopascals. Press the IN Softkey to display the barometric setting in inches of mercury. 5) Press the BACK Softkey to return to the previous level softkeys. Figure 2-9 Altimeter (Metric) Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B 2-6 SECTION 2 FLIGHT INSTRUMENTS Low Altitude Annunciation (WAAS Only) NOTE: The LOW ALT annunciation is not available when the G1000 is configured with TAWS (Terrain Awareness & Warning System), unless TAWS is inhibited. When the Final Approach Fix (FAF) is the active waypoint in a GPS WAAS approach using vertical guidance, a LOW ALT (Low Altitude) annunciation may appear if the current aircraft altitude is at least 164 feet below the prescribed altitude at the FAF. The annunciation initially flashes. After a few seconds the flashing stops and the annunciation is displayed as shown in Figure 2-10. Figure 2-10 Low Altitude on GPS Approach Low Altitude Annunciation 2.4 VERTICAL DEVIATION/GLIDEPATH/ GLIDESLOPE INDICATOR The Vertical Deviation and Required Vertical Speed Indicators appear when vertical guidance is being given prior to executing an approach (see Figure 2-11). In systems that are WAAS enabled, the Glidepath Indicator appears at a point prior to the FAF when executing an LPV, LNAV/VNAV, or LNAV+V approach (see Figure 2-12). Vertical Deviation Indicator Required Vertical Speed Vertical Speed Pointer Vertical Speed Indicator VNV Target Altitude Figure 2-11 Vertical Speed and Devia- tion Indicators (VSI and VDI) Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B 2-7 SECTION 2 FLIGHT INSTRUMENTS Glidepath Indicator Figure 2-12 Glidepath Indicator The Glideslope Indicator appears when an ILS is tuned in the active NAV receiver field (see Figure 2-13). Glideslope Indicator Marker Beacon Annunciation Figure 2-13 Glideslope Indicator 2.5 MARKER BEACON ANNUNCIATIONS Figure 2-14 Marker Beacon Annunciations Outer Marker Middle Marker Inner Marker Altimeter 2.6 VERTICAL SPEED INDICATOR Figure 2-15 Vertical Speed Indicator Vertical Speed Pointer The actual vertical speed is displayed inside the pointer. Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B 2-8 SECTION 2 FLIGHT INSTRUMENTS 2.7 BAROMETRIC ALTITUDE MINIMUMS The desired barometric altitude minimums can be set in the Timer/References Window. The altitude ranges from 0 to 16,000 feet in 10-foot increments. The minimums are reset anytime the power is cycled. Figure 2-16 Barometric Minimum Descent Altitude Settings Set the barometric altitude minimums: 1) Press the TMR/REF Softkey. 2) Turn the large FMS Knob to highlight the ‘Minimums’ field (Figure 2-16). 3) Turn the small FMS Knob to select BARO. OFF is selected by default. Press the ENT Key or turn the large FMS Knob to highlight the next field. 4) Use the small FMS Knob to enter the desired altitude (from zero to 16,000 feet). 5) To remove the window, press the CLR Key or the TMR/REF Softkey. The desired barometric minimum descent altitude (MDA, or Decision Height, DH) can be set in the Timer/ References Window. Visual annunciations alert the pilot when approaching the MDA: • When the aircraft altitude descends to within 2500 feet of the MDA setting, the Barometric Minimum Box appears with the altitude in light blue text. The bug appears on the tape in light blue once in range. • When the aircraft descends through 100 feet of the MDA, the bug and text turn white. • Once the aircraft descends past the MDA, the bug and text turn yellow and the aural alert, “Minimums Minimums”, is generated. Alerting is inhibited while the aircraft is on the ground. If the aircraft climbs after having reached the MDA, once it reaches 50 feet above the MDA, alerting is disabled. Figure 2-17 Barometric Minimum Descent Altitude Alerting Visual Annunciations Within 100 ft Altitude Reached Within 2500 ft Barometric Minimum Box Barometric Minimum Bug Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B 2-9 SECTION 2 FLIGHT INSTRUMENTS 2.8 HORIZONTAL SITUATION INDICATOR (HSI) Figure 2-18 Horizontal Situation Indicator (360˚) 8 14 9 6 5 4 3 2 1 7 13 12 11 10 Heading Bug 2 3 6 4 5 7 1 Turn Rate Indicator Navigation Source Course Deviation Indicator TO/FROM Indicator Course Pointer Rotating Compass Rose 11 10 12 13 14 9 8 OBS Mode Lateral Deviation Scale Flight Phase Aircraft Symbol Lubber Line Heading Turn Rate and Heading Trend Vector Arc HSI NOTE: When the Arc HSI is displayed the BRG1 and BRG2 Information Windows and pointers are disabled. NOTE: If the pilot makes a heading change greater than 105˚ with respect to the course, the CDI switches to the opposite side of the deviation scale and displays reverse sensing. The Arc HSI is a 140˚ expanded section of the compass rose. The Arc contains a Course Pointer arrow, the TO/FROM indicator, a sliding deviation indicator (the TO/FROM and sliding deviation indicators are one and the same), and a deviation scale. Upon station passage, the TO/FROM indicator flips and points to the tail of the aircraft, just like the conventional TO/FROM flag. Depending on the navigation source, the CDI on the Arc HSI can appear in two different ways: • GPS, OBS, VOR – Arrowhead • Localizer – Diamond Lateral Deviation Scale Course Deviation and TO/FROM Indicator Figure 2-19 Arc HSI Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev. B 2-10 SECTION 2 FLIGHT INSTRUMENTS Turn Rate Indicator and Heading Trend Vector Tick marks to the left and right of the lubber line denote half-standard and standard turn rates. A magenta turn rate trend vector shows the current turn rate. The end of the trend vector gives the heading predicted in six seconds, based on the present turn rate. At rates greater than 4 deg/sec, an arrowhead appears at the end of the magenta trend vector and the prediction is no longer valid. Figure 2-21 Standard-Rate Turn Indication Turn Rate Trend Vector (standard rate) Figure 2-20 Turn Rate Indicator and Trend Vector Half-Standard Turn Rate Tick Mark Standard Turn Rate Tick Mark Turn Rate Trend Vector (rate > 4 deg/sec) Course Pointer The Course Pointer is a single line arrow (GPS, VOR1 and LOC1) or double line arrow (VOR2 and LOC2) which points in the direction of the set course. Figure 2-22 Course Pointer Course Deviation Indicator (CDI) The CDI scale automatically adjusts to the current phase of flight as seen in Figure 2-23. Scaling may be selected manually from the MFD System Setup Page. Flight Phase Automatic CDI Full-scale Deflection Departure (DRPT) 0.3 nm Terminal (TERM) 1.0 nm Enroute (ENR) 2.0 nm Oceanic (OCN) 2.0 nm Approach (LNAV) 1.0 nm decreasing to 350 feet depending on variables (see Figure 2-24) Approach (LNAV+V) (WAAS systems only)) Approach (LNAV/ VNAV)(WAAS only) 1.0 nm decreasing to a specified course width, then 0.3 nm, depending on variables (see Figure 2-25) Approach (LPV)(WAAS only) Missed Approach 0.3 nm