Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

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. 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 Nav III 190-00384-08 Rev. A 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: The GDU 1040 and GDU 1044B PFD/MFD may require a warm-up time of up to 30 minutes when exposed to -40˚C for an extended period. A warm-up time of up to 15 minutes may be required when exposed to -30˚C for an extended period. 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 Nav III 190-00384-08 Rev. A RR-1 RECORD OF REVISIONS Part Number Change Summary 190-00384-03 (Rev. A) Added XM Radio and XM Weather Added ADF capability Added DME capability Added BRG1/BRG2 pointers Added dual audio panel operation Added C172 parameters Changed Airspeed Trend Vector Changed Altitude Trend Vector Added Checklist capability Added Flight ID capability 190-00384-03 (Rev. B) Updated system software numbers 190-00384-04 (Rev. A) Reformatted manual to new format Added TAS capability 190-00384-04 (Rev. B) Added DONE Softkey, XM-INFORMATION Page, and XM-RADIO Page operation. 190-00384-05 (Rev. A) Added explanation of EIS display behavior upon exceedances Added better explanation of Intercom System Isolation Added Stormscope operation upon loss of heading input Added TAWS-B Added CO Guardian Added new Fuel Totalizer Updated G1000 System Messages 190-00384-06 (Rev A) Added GDU 7.00 (WAAS, VNAV & Charts) software parameters. Added AFCS for the 182 and 206 Added database loading instructions Updated G1000 System Messages Combined previous system software numbers into 0563.00 190-00384-07 Added GDU 8.02 parameters, Airways, and ADS-B 190-00384-08 Added GDU 8.20 parameters, including gradient background on the PFD and GFC 700 for the C172. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A RR-2 RECORD OF REVISIONS Revision Date of Revision Affected Pages Description A November, 2007 i through Index-4 Production release Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A i TABLE OF CONTENTS SECTION 1: SYSTEM OVERVIEW.................................... 1-1 1.1 PFD/MFD Controls................................................... 1-2 1.2 PFD Softkeys............................................................ 1-5 1.3 MFD Softkeys .......................................................... 1-8 1.4 MFD Page Groups ................................................... 1-9 1.5 Vertical Navigation .............................................. 1-10 1.6 Backlighting ........................................................... 1-12 1.7 XM Radio - Automatic Muting ........................... 1-12 1.8 Database Updates ................................................ 1-12 Jeppesen Aviation Database ...................................... 1-12 Garmin Databases ..................................................... 1-13 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 .................................................. 2-3 2.3 Altimeter .................................................................. 2-4 Selected Altitude Bug .................................................. 2-4 Altitude Trend Vector ................................................... 2-4 Barometric Setting Box ................................................ 2-4 Altitude Alerting .......................................................... 2-4 Metric Display ............................................................. 2-5 Low Altitude Annunciation........................................... 2-5 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 ........................... 2-7 2.8 Horizontal Situation Indicator (HSI) ................... 2-8 Course Pointer ............................................................ 2-9 Course Deviation Indicator (CDI) .................................. 2-9 Bearing Pointers and Information Windows ................ 2-11 DME (optional).......................................................... 2-11 Navigation Source ..................................................... 2-11 2.9 Wind Data............................................................... 2-12 2.10 Generic Timer ........................................................ 2-13 SECTION 3: ENGINE INDICATION SYSTEM (EIS).... 3-1 3.1 Engine Display......................................................... 3-1 3.2 Lean Display ............................................................ 3-4 Normally-aspirated Aircraft .......................................... 3-7 Turbocharged Aircraft .................................................. 3-7 3.3 System Display ........................................................ 3-7 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 Optional NAV Radios ............................................. 4-3 DME Radio (optional) .................................................. 4-3 ADF Radio (optional) ................................................... 4-4 4.6 Frequency Auto-tuning ......................................... 4-4 Auto-tuning on the PFD .............................................. 4-4 Auto-tuning on the MFD ............................................. 4-4 4.7 Transponder ............................................................. 4-4 Mode Selection ........................................................... 4-4 Reply Status ................................................................ 4-5 Code Selection ............................................................ 4-5 Flight ID Reporting ...................................................... 4-6 SECTION 5: AUDIO PANEL ................................................ 5-1 5.1 COM Radio Selection ............................................. 5-2 5.2 Cabin Speaker ......................................................... 5-2 5.3 Passenger Address (PA) System (T)182T and (T)206H Only ............................................................ 5-2 5.4 Marker Beacon Receiver ....................................... 5-2 Marker Beacon Signal Sensitivity ................................. 5-2 5.5 Nav Radio Audio Selection ................................... 5-3 5.6 Intercom System (ICS) Isolation .......................... 5-3 5.7 Intercom Squelch Control ..................................... 5-4 5.8 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 ..................................... 6-2 Activating the Flight Director ....................................... 6-2 Command Bars ........................................................... 6-2 AFCS Status Box ......................................................... 6-3 6.3 Flight Director Modes............................................ 6-3 Pitch Modes ................................................................ 6-3 Roll Modes................................................................ 6-17 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A ii TABLE OF CONTENTS 6.4 Autopilot Operation ............................................ 6-22 Flight Control ............................................................ 6-22 Engaging the Autopilot.............................................. 6-22 Control Wheel Steering.............................................. 6-23 Disengaging the Autopilot ......................................... 6-23 6.5 Example Procedures ............................................ 6-24 Departure ................................................................. 6-25 Intercepting a VOR Radial .......................................... 6-26 Flying a Flight Plan/GPS Course ................................. 6-27 Descent .................................................................... 6-28 Approach .................................................................. 6-31 Go Around/Missed Approach ..................................... 6-33 6.6 AFCS Annunciations and Alerts ......................... 6-34 AFCS Status Alerts..................................................... 6-34 Overspeed Protection ................................................ 6-35 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 . 8-2 8.2 Viewing the Active Flight Plan ............................ 8-2 8.3 Activate a Stored Flight Plan ............................... 8-2 8.4 Activate a Flight Plan Leg .................................... 8-3 8.5 Stop Navigating a Flight Plan.............................. 8-3 8.6 Invert Active Flight Plan ....................................... 8-3 8.7 Create a New Flight Plan ...................................... 8-4 Create a New Flight Plan Using the MFD ..................... 8-4 Create a New Flight Plan Using the PFD ...................... 8-4 8.8 Enter an Airway in a Flight Plan ......................... 8-5 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 ....................................... 8-7 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 ............................................... 8-8 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) .................................. 10-1 Displaying Stormscope Lightning Data on the Navigation Map Page ................................................ 10-1 Stormscope Page....................................................... 10-2 10.3 XM Weather (Service 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 & Symbols ..................................... 10-5 Weather Product Age ................................................ 10-6 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A iii TABLE OF CONTENTS 10.4 Traffic Systems ...................................................... 10-7 Traffic Information Service (TIS) .................................. 10-7 Traffic Advisory System (TAS) (Optional) ..................... 10-8 ADS-B Traffic (Optional) ............................................. 10-9 10.5 Terrain and Obstacle Proximity ....................... 10-10 Displaying Terrain and Obstacles on the Terrain Proximity Page ........................................................ 10-10 Displaying Terrain and Obstacles on the Navigation Map........................................................................ 10-11 10.6 Terrain Awareness & Warning System (TAWS) Display (Optional) ................................ 10-11 Displaying Terrain on the TAWS Page ....................... 10-11 Enable/Disable Aviation Data ................................... 10-12 TAWS Inhibit ........................................................... 10-12 Manual System Test ................................................. 10-13 Forward Looking Terrain Avoidance (FLTA) ................ 10-13 Premature Descent Alert (PDA) ................................ 10-13 Excessive Descent Rate Alert (EDR) .......................... 10-14 Negative Climb Rate After TakeoffAlert (NCR) .......... 10-14 “Five-Hundred” Aural Alert...................................... 10-14 Displaying Terrain and Obstacles on the Navigation Map........................................................................ 10-14 Pop-up Alerts .......................................................... 10-15 TAWS Alerts Summary ............................................. 10-16 Alert Annunciations ................................................. 10-17 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 .................................................... 11-3 SECTION 12: ANNUNCIATIONS & ALERTS .............. 12-1 12.1 Alert Level Definitions ........................................ 12-2 12.2 NAV III Aircraft Alerts .......................................... 12-3 WARNING Alerts ....................................................... 12-3 CAUTION Alerts ........................................................ 12-3 CAUTION Alerts (T182, T206, and 206 with Prop De-Ice Only) .............................................................. 12-3 Safe Operating Annunciation (T182, T206, and 206 with Prop De-Ice Only) .............................................. 12-3 12.3 CO Guardian Messages ....................................... 12-3 12.4 AFCS Alerts............................................................. 12-4 System Status Annunciation....................................... 12-4 12.5 TAWS Alerts............................................................ 12-5 12.6 Other G1000 Aural Alerts .................................... 12-6 12.7 G1000 System Annunciations ............................ 12-7 12.8 G1000 System Message Advisories .................. 12-9 MFD & PFD Message Advisories............................... 12-10 Database Message Advisories .................................. 12-11 GMA 1347 Message Advisories ............................... 12-13 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 Miscellaneous Message Advisories ........................... 12-21 INDEX ...................................................................................Index-1 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A iv TABLE OF CONTENTS Blank Page Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A 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 Garmin G1000 Pilot’s Guide for the Cessna Nav III (190- 00498-03). This guide gives the pilot abbreviated operating instructions for the Primary Flight Display (PFD), Multi Function Display (MFD), and the GMA 1347 Audio Panel System. NOTE: The pilot should read and thoroughly understand the Cessna Pilot’s Operating Handbook (POH) for limitations, procedures and operational information not contained in this Cockpit Reference Guide. The Cessna POH always takes precedence over the information found in this guide. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A 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 17 12 13 11 10 27 25 24 28 16 15 14 20 21 19 23 18 22 26 29 GFC 700 AFCS Only Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A 1-3 SECTION 1 SYSTEM OVERVIEW PFD and MFD controls function the same. 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 G1000 displays a list that is too long for the display screen, a scroll bar appears along the right Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A 1-4 SECTION 1 SYSTEM OVERVIEW 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. The following are only available with the GFC 700 AFCS. 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 HDG Key – Selects/deselects the Heading Select Mode. 20 NAV Key – Selects/deselects the Navigation Mode. 21 APR Key – Selects/deselects the Approach Mode. 22 VS Key – Selects/deselects the Vertical Speed Mode. 23 FLC Key – Selects/deselects the Flight Level Change Mode. 24 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. 25 ALT Key – Selects/deselects the Altitude Hold Mode. 26 VNV Key – Selects/deselects Vertical Navigation Mode. 27 BC Key – Selects/deselects Back Course Mode. 28 29 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 Nav III 190-00384-08 Rev. A 1-5 SECTION 1 SYSTEM OVERVIEW 1.2 PFD SOFTKEYS Softkey OFF Softkey ON Figure 1-2 PFD Top Level Softkeys Press the BACK or OFF Softkey to return to the top-level softkeys. ALERTS STRMSCP DME ALERTS Figure 1-3 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 Nav III 190-00384-08 Rev. A 1-6 SECTION 1 SYSTEM OVERVIEW Figure 1-4 PFD Configuration Softkeys Press the STD BARO or BACK Softkey to return to the top-level softkeys BRG1 (NAV1) BRG1 (GPS) BRG1 (OFF) DME ALT UNIT METERS IN HPA DME ALERTS ALERTS ALERTS ALERTS HSI FRMT ALERTS ARC HSI 360 HSI BRG1 (ADF) BRG2 (NAV2) BRG2 (GPS) BRG2 (OFF) BRG2 (ADF) 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. OPTN 1 – Wind direction arrows with headwind and crosswind components. OPTN 2 – Wind direction arrow and speed. OPTN 3 – Wind direction arrow with direction and speed. OFF – Information not displayed. DME (optional) – Press to display the DME Information Window. 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. ADF – Displays ADF in the BRG1 Information Window when an otional ADF is installed. 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. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A 1-7 SECTION 1 SYSTEM OVERVIEW GPS – Displays GPS waypoint identifier and GPS distance information in the BRG2 Information Window. ADF – Displays ADF in the BRG2 Information Window when an otional ADF is installed. OFF – Removes the BRG2 Information Window. 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. DME (optional) – Press to display the DME Tuning Window. Press the BACK Softkey to return to the top-level softkeys. Press the BACK Softkey to return to the top-level softkeys. ALERTS ALERTS DME ALERTS Figure 1-5 XPDR (Transponder) Softkeys 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). 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. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A 1-8 SECTION 1 SYSTEM OVERVIEW 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. 1.3 MFD SOFTKEYS ENGINE – Pressing this softkey makes available the LEAN and SYSTEM Softkeys which in turn access the Lean Page and the System Page, respectively. Figure 1-6 MFD Softkeys BACK RST FUEL SYSTEM ENGINE LEAN ENGINE MAP DCLTR BACK SYSTEM LEAN ENGINE ENGINE LEAN BACK SYSTEM Press the ENGINE or BACK Softkey to return to the default Engine Page level. TRAFFIC TOPO BACK TERRAIN DCLTR-2 DCLTR-3 DCLTR-1 Press the BACK Softkey on this level to return to the top softkey level. CHKLIST ASSIST CYL SLCT EXIT EMERGCY ENGINE DONE The DONE Softkey changes to UNDO when the checklist item is already checked. (optional) BACK -10 GAL SYSTEM ENGINE LEAN GAL REM -1 GAL XX GAL +10 GAL +1 GAL XX GAL Press the ENGINE Softkey to the default Engine Page level. X = airframe specific values STRMSCP NEXRAD XM LTNG (optional) (optional) (optional) SHW CHRT (optional) AIRWAYS AIRWY LO AIRWAY HI AIRWY ON (Default softkey is dependant on the selection made in the map setup options) Press the BACK Softkey to return to the previous softkey level. 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. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A 1-9 SECTION 1 SYSTEM OVERVIEW 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. 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. ENGINE – Displays engine softkeys. DONE – Pressing this softkey checks off a checklist item. If an item is already checked, an UNDO Softkey is displayed. EXIT – Press to exit the checklist. EMERGCY – Pressing this softkey displays the emergency checklist. Figure 1-7 Page Group Icon Map Page Group Waypoint Page Group Auxiliary Page Group Nearest Group Selected Page Number of Pages in Current Group 1.4 MFD PAGE GROUPS 1) Turn the large FMS Knob until the desired page group is selected. 2) Turn the small FMS Knob to select pages within the group. See Figure 1-7. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A 1-10 SECTION 1 SYSTEM OVERVIEW 1.5 VERTICAL NAVIGATION 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 after the Final Approach Fix. 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 is not 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 are 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 is now 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 when the approach is loaded. These altitudes are also displayed as light blue text. Waypoint altitude constraints designated up to, but not including the FAF. The FAF is always 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 manually. 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 Nav III 190-00384-08 Rev. A 1-11 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 1-8 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 1-9 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 Nav III 190-00384-08 Rev. A 1-12 SECTION 1 SYSTEM OVERVIEW 1.6 BACKLIGHTING 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 small 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 1-10 PFD Setup Menu Window 1.7 XM RADIO - AUTOMATIC MUTING XM Radio audio is automatically muted when the aircraft groundspeed exceeds approximately 30 kts and the airspeed is less than approximately 80 kts. The audio must be manually unmuted once the aircraft is outside the applicable speed range. Refer to the G1000 Optional Equipment section of the pilot’s guide. 1.8 DATABASE UPDATES The G1000 System uses Secure Digital (SD) cards to load and store various types of data. For basic flight op- erations, 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 Nav III 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 1-11 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 Nav III 190-00384-08 Rev. A 1-13 SECTION 1 SYSTEM OVERVIEW Figure 1-12 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 iden- tical 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 1-13 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, press 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 Nav III 190-00384-08 Rev. A 1-14 SECTION 1 SYSTEM OVERVIEW Blank Page Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A 2-1 SECTION 2 FLIGHT INSTRUMENTS SECTION 2: FLIGHT INSTRUMENTS The following discussions pertain to the Primary Flight Display, unless otherwise indicated. 7 8 12 15 16 9 14 13 6 3 4 2 1 17 Figure 2-1 Default PFD Information 15 16 12 14 13 10 7 4 2 6 17 8 3 1 NAV Frequency Box Airspeed Indicator True Airspeed Box Outside Air Temperature Box Selected Altitude Box Horizontal Situation Indicator Heading Box System Time Box Transponder Status Box Barometric Setting Box Vertical Speed Indicator Altimeter COM Frequency Box Navigation Status Box 11 9 Slip/Skid Indicator Turn Rate Indicator 11 10 18 18 Attitude Indicator 5 5 Ground Track Bug Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A 2-2 SECTION 2 FLIGHT INSTRUMENTS Figure 2-2 Additional PFD Information 2 1 5 3 4 8 6 Traffic Annunciation 2 4 3 1 Selected Heading Box 9 Flight Plan Window 10 Barometric Minimums Box 8 BRG2 Information Window Vspeed References 5 Vertical Deviation/Glidepath (WAAS en- abled systems only)/Glidesope Indicator 14 Inset Map Wind Data Window BRG1 Information Window Selected Altitude Bug 11 6 13 Barometric Minimums Bug 15 Marker Beacon Annunciation 12 Selected Course Box 7 7 DME Information Window 10 9 12 14 13 11 15 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 Nav III 190-00384-08 Rev. A 2-3 SECTION 2 FLIGHT INSTRUMENTS 2.1 AIRSPEED INDICATOR Figure 2-4 Airspeed Indicator Actual Airspeed True Airspeed Box Airspeed Trend Vector Speed Ranges Vspeed References Speed Indication The indicated airspeed is displayed inside the black pointer. The pointer becomes red upon reaching Vne. 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. Refer to the Pilot’s Operating Handbook (POH) for airspeed limitations and indicator markings. Airspeed Trend Vector The end of the trend vector displays approximately what the airspeed will be in 6 seconds if the current rate of acceleration/deceleration is maintained. Vspeed References Vspeed References are turned on or off in the Timer/References Window. Press the TMR/REF Softkey to display the widow. When active (ON), the Vspeeds are displayed at their respective locations to the right of the airspeed scale. To activate the Vspeed References, display the Timer/Reference Window and turn the large FMS Knob to place the cursor in the ON/OFF field. Turn the small FMS Knob to select ON or OFF. 2.2 ATTITUDE INDICATOR 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 Index Zero 10 10 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. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A 2-4 SECTION 2 FLIGHT INSTRUMENTS 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 Selected Altitude Bug The Selected Altitude Bug is displayed at the Selected Altitude or the edge of the tape (whichever is closer to the current altitude) to provide increased altitude awareness and to set the desired hold altitude for the autopilot. Set the Selected Altitude Bug: Turn the ALT Knobs to set the Selected Altitude 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 six seconds if the current rate of vertical speed is maintained. 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 Altitude Reference Box. Whenever the setting is changed, the Altitude Alerter is reset. The Altitude Alerter is independent of the Automatic Flight Control System. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A 2-5 SECTION 2 FLIGHT INSTRUMENTS 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) Low Altitude Annunciation NOTE: The LOW ALT annunciation is only available in G1000 systems configured with WAAS-capable GPS. Also, 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 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A 2-6 SECTION 2 FLIGHT INSTRUMENTS 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). Figure 2-11 Vertical Deviation Indications Vertical Deviation Indicator VNAV Target Altitude Required Vertical Speed Figure 2-12 Glidepath Indicator Glidepath Indicator The Glideslope Indicator appears when an ILS approach has been activated and an ILS is tuned in the active NAV receiver field (see Figure 2-13). Figure 2-13 Glideslope Indicator Marker Beacon Annunciation Glideslope Indicator Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A 2-7 SECTION 2 FLIGHT INSTRUMENTS 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 Vertical Speed Bug Selected Vertical Speed The actual vertical speed is displayed inside the pointer. When the Flight Director is placed in Vertical Speed Mode (by pressing the VS Key) the Vertical Speed Bug is displayed. Press the NOSE UP or NOSE DN Key to adjust. 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 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 passes 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. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A 2-8 SECTION 2 FLIGHT INSTRUMENTS Figure 2-17 Barometric Minimum Descent Altitude Alerting Visual Annunciations Within 100 ft Altitude Reached Within 2500 ft Barometric Minimum Box Barometric Minimum Bug 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. 2.8 HORIZONTAL SITUATION INDICATOR (HSI) The HSI compass can be displayed as a 360° rose or 140° arc by pressing the PFD Softkey, followed by the HSI FRMT Softkey, followed by the 360 HSI or the ARC HSI Softkey. Figure 2-18 Horizontal Situation Indicator 9 15 10 7 6 5 4 3 1 8 14 13 12 11 Heading Bug 3 4 7 5 6 8 1 Turn Rate Indicator Navigation Source Course Deviation Indicator TO/FROM Indicator Course Pointer Rotating Compass Rose 12 11 13 14 15 10 9 OBS Mode Lateral Deviation Scale Flight Phase Aircraft Symbol Lubber Line Heading Turn Rate and Heading Trend Vector 2 2 Ground Track Bug Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A 2-9 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 2-20 Standard-Rate Turn Indication Turn Rate Trend Vector (standard rate) Figure 2-19 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 2-21 Course Pointer Course Deviation Indicator (CDI) The CDI scale automatically adjusts to the current phase of flight as seen in Figure 2-22. 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 2-23) 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 2-24) Approach (LPV)(WAAS only) Missed Approach 0.3 nm Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A 2-10 SECTION 2 FLIGHT INSTRUMENTS 2.0 nm Enroute (Oceanic if >200 nm from nearest airport) 0.3 nm Missed Approach 1.0 nm Approach 1.0 nm Terminal 1.0 nm Terminal 0.3 nm Departure CDI Full-scale Deflection Refer to accompanying approach CDI scaling figures Drawing not to scale Figure 2-22 Phases of Flight/CDI Scaling 1.0 nm 2 nm 350 ft angle set by system 0.3 nm FAF CDI Full-scale Deflection CDI scale is set to the smaller of 0.3 nm or an angle set by the system CDI scale varies if Vectors-To-Final is activated Drawing not to scale Figure 2-23 Typical LNAV and LNAV+V Approach CDI Scaling 1.0 nm 2 nmFAF 0.3 nm course width Landing Threshold CDI Full-scale Deflection angle based on database information CDI scale varies if Vectors-To-Final is activated Drawing not to scale Figure 2-24 Typical LNAV/VNAV and LPV Approach CDI Scaling (WAAS Systems Only) Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A 2-11 SECTION 2 FLIGHT INSTRUMENTS Bearing Pointers and Information Windows Pressing the PFD Softkey provides access to the BRG1 and BRG2 Softkeys. The BRG1 pointer is a single line pointer. The BRG2 pointer is a double line pointer. Press the BRG1 or BRG2 Softkey to cycle through selecting NAV1/2, GPS, or ADF for display using the corresponding pointer. Bearing 2 Pointer Bearing 1 Information Window Bearing 1 Pointer Bearing 2 Information Window Figure 2-25 HSI with Bearing Information DME Information Window CDI Distance to Bearing Source Waypoint Identifier Bearing Source Pointer Icon Figure 2-26 BRG1 Information Window Distance to Bearing Source Waypoint Identifier Pointer Icon Bearing Source Figure 2-27 BRG2 Information Window DME (optional) To display the DME Information Window, press the PFD Softkey followed by the DME Softkey. Figure 2-28 DME Information Window Navigation Source Change CDI navigation sources: 1) Press the CDI Softkey to change from GPS to VOR1/LOC1. 2) Press the CDI Softkey again to change from VOR1/ LOC1 to VOR2/LOC2. 3) Press the CDI Softkey a third time to return to GPS. When using GPS as the navigation source, the following may appear: • LOI - GPS position integrity is inadequate for the current procedure being flown. If GPS is being used as primary navigation, and LOI is annunciated, other means of primary navigation is required, such as VHF. LOI is also displayed during GPS position initialization. • WARN – GPS detects a position error. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A 2-12 SECTION 2 FLIGHT INSTRUMENTS • OBS – Displayed when operating in OBS Mode. • SUSP – Displayed when in OBS Mode indicating GPS waypoint sequencing is suspended. • DR – Navigating using Dead Reckoning due to an error in the GPS solution. Figure 2-29 GPS LOI, GPS SUSP, LOC1 and VOR2 Enable/disable OBS Mode while navigating with GPS: 1) Press the OBS Softkey to select OBS Mode. 2) Turn the CRS Knob to select the desired course to/from the waypoint. 3) Press the OBS Softkey again to disable OBS Mode. NOTE: The OBS Softkey is only displayed when navigating an active leg using GPS. 2.9 WIND DATA When the window is selected for display, but wind information is invalid or unavailable, the window shows “NO WIND DATA”. Wind data can be displayed in three different ways: • Wind direction arrows with headwind and crosswind components (Option 1) • Wind direction arrow and speed (Option 2) • Wind direction arrow with direction and speed (Option 3) Option 1 Option 2 Option 3 No Data Figure 2-30 Wind Data Window 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 Cessna Nav III 190-00384-08 Rev. A 2-13 SECTION 2 FLIGHT INSTRUMENTS 2.10 GENERIC TIMER Figure 2-31 Timer Status Prompts Change the 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 must be reset manually). Press the CLR Key or the TMR/REF Softkey to remove the window. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A 2-14 SECTION 2 FLIGHT INSTRUMENTS Blank Page Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3-1 SECTION 3: ENGINE INDICATION SYSTEM (EIS) NOTE: Refer to the Pilot’s Operating Handbook (POH) for limitations. EIS information is presented in three displays, accessed using the ENGINE Softkey on the MFD: • Engine Display – Default display, shows all critical engine, fuel, and electrical indicators • Lean Display – Provides engine leaning information • System Display – Shows numeric readouts of critical engine, fuel, and electrical indicators Green and white bands indicate normal ranges of operation; yellow and red bands indicate caution and warning, respectively. If sensory data to an instrument becomes invalid or unavailable, a red “X” is shown across the instrument. 3.1 ENGINE DISPLAY The Engine Display is the default EIS display and can be displayed after viewing other EIS displays by pressing the ENGINE Softkey. The EIS automatically defaults back to the Engine Display from the Lean or System Display when certain parameters are exceeded. Fluctuations in engine speed and fuel quantity above certain levels, depending on the airframe, also cause reversion back to the Engine Display. 1 Engine Manifold Pressure Gauge (MAN IN) Models 182T, T182T, 206H, T206H – Displays engine power in inches of mercury (in Hg). Turbocharged aircraft have a red portion of the gauge indicating the maximum manifold pressure range. A white tick mark is displayed indicating the cruise manifold pressure (Model T182T only). 2 Tachometer (RPM) – Shows propeller speeds in revolutions per minute (rpm). Red range indicates propeller overspeed warning; a white high-rpm range indicates above normal operating speeds (Models 172S, 206H, and T206H) 3 Fuel Flow Indicator (FFLOW GPH) – Shows the current fuel flow in gallons per hour (gph). For turbocharged aircraft, the indicator displays a small stand-alone green band indicating maximum takeoff fuel flow. A white tick mark indicates the maximum cruise fuel flow (Model T182T only). 4 Oil Pressure Indicator (OIL PRES) – Displays pressure of the oil supplied to the engine in pounds per square inch (psi). 5 Oil Temperature Indicator (OIL TEMP) – Displays the engine oil temperature in degrees Fahrenheit (°F). 6 Cylinder Head Temperature Indicator (CHT) Models 182T, T182T, 206H, T206H – Shows the head temperature of the hottest cylinder (number shown in triangular pointer) in degrees Fahrenheit (°F). 7 Exhaust Gas Temperature Indicator (EGT) Normally-aspirated Aircraft – Displays the exhaust gas temperature of the hottest cylinder (number shown in triangular pointer) in degrees Fahrenheit (°F). 8 Turbine Inlet Temperature Indicator (TIT) Turbocharged Aircraft – Displays the temperature at the turbine inlet in degrees Fahrenheit (°F). 9 Vacuum Pressure Indicator (VAC) Models 172R and 172S – Displays vacuum pressure. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3-2 10 Fuel Quantity Indicator (FUEL QTY GAL) – Shows the quantity of fuel in the tanks, in gallons, ranging from zero to full (F) for each fuel tank (left–L and right–R). When full, the indicator displays to 35 gallons per side (26 gallons for the Models 172R and 172S). 11 Engine Hours (Tach) (ENG HRS) Models 172R and 172S – A numeric readout gives the time (in hours) the engine has been in service. Figure 3-1 Engine Display (Normally-aspirated Aircraft) Model 206H 12 10 13 1 5 4 3 2 6 7 Model 172R 9 2 3 4 5 7 13 10 12 11 Model 172S 9 2 3 4 5 7 13 10 12 11 Model 182T 7 6 2 3 4 5 1 13 10 12 12 Voltmeter (M, E BUS VOLTS) – Displays the main and essential bus voltages. 13 Ammeter (M, S BATT AMPS) – Shows the main and standby battery load in amperes. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3-3 Figure 3-2 Engine Display (Turbocharged Aircraft) Model T206H Maximum Takeoff Fuel Flow 8 6 2 3 4 5 1 13 10 12 Model T182T Cruise Fuel Flow Cruise Manifold Pressure 8 6 2 3 4 5 1 13 10 12 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3-4 3.2 LEAN DISPLAY NOTE: The pilot should follow the engine man- ufacturer’s recommended leaning procedures in the Pilot’s Operating Handbook (POH). 1 Engine Manifold Pressure Gauge (MAN IN) Models 182T, T182T, 206H, T206H – Displays engine power in inches of mercury (in Hg). Turbocharged aircraft have a red portion of the gauge indicating the maximum manifold pressure range. A white tick mark is displayed indicating the cruise manifold pressure (Model T182 only). 2 Tachometer (RPM) – Shows propeller speeds in revolutions per minute (rpm). Red range indicates propeller overspeed warning; a white high-rpm range indicates above normal operating speeds (Models 172S, 206H and T206H). 3 Fuel Flow (FFLOW GPH) – Shows the current fuel flow in gallons per hour (gph). 4 Turbine Inlet Temperature Indicator (TIT) Models T182T and T206H – Displays the temperature at the turbine inlet in degrees Fahrenheit (°F). When the ASSIST Softkey is pressed, the TIT deviation from peak (∆PEAK) is displayed below the indicator. 5 Exhaust Gas Temperature Bar Graph (EGT °F) – Displays the exhaust gas temperature of all cylinders in degrees Fahrenheit (°F); a readout for the selected cylinder (by default, the hottest cylinder) is shown below the bar graph. The selected cylinder is indicated in light blue. Cylinders whose EGTs are in the normal range appear in white. Pressing the ASSIST Softkey causes the EGT deviation from peak (∆PEAK) for the selected cylinder to be displayed below the indicator. 6 Cylinder Head Temperature Indicator (CHT) – Shows the head temperatures of all cylinders in degrees Fahrenheit (°F); a readout for the selected cylinder (by default, the hottest cylinder) is shown below the bar graph. The selected cylinder is indicated in light blue. Cylinders whose CHTs are in the normal range appear in white. Cylinders whose CHTs enter the caution and warning ranges appear in yellow and red, respectively. 7 Fuel Quantity Indicator (FUEL QTY GAL) – Shows the quantity of fuel in the left and right fuel tanks (left–L and right–R). When full, the indicator displays to 35 gallons per side (26 gallons for the Models 172R and 172S). Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3-5 Figure 3-3 Lean Display (Normally-aspirated Aircraft) Model 206H 6 3 1 2 5 7 Hollow Block Represents Peak Model 172R 7 2 3 6 5 Model 172S 2 5 3 7 6 Model 182T 6 3 1 2 5 7 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3-6 Model T206H 6 3 4 1 2 5 7 Cruise Manifold Pressure Model T182T 6 3 4 1 2 5 7 Figure 3-4 Lean Display (Turbocharged Aircraft) The Lean Display is accessed by pressing the ENGINE Softkey followed by the LEAN Softkey and provides information for performing engine leaning. From the Lean Display, the pilot can utilize the CYL SLCT and ASSIST softkeys to obtain information about specific cylinders. Pressing the CYL SLCT (Cylinder Select) Softkey cycles through the cylinders (i.e., changes the cylinder indicated on the bar graphs in light blue). This softkey is disabled when the ASSIST Softkey is pressed or when a cylinder experiences a caution or warning condition; the softkey remains disabled until the temperature returns to normal. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3-7 The ASSIST Softkey aids in the leaning process by identifying the peak of the first cylinder whose temperature falls. If the temperature of the peaked cylinder exceeds the peak value, the peak value is not updated. Press the ASSIST Softkey to stop peak monitoring. Normally-aspirated Aircraft For normally-aspirated aircraft, when a cylinder peaks, its peak is represented by a hollow block on the EGT Bar Graph. The EGT readout for the peaked cylinder, indicat- ed on the bar graph in light blue, appears directly beneath the bar graph. The system automatically switches to the first peak obtained and displays the temperature deviation from peak (∆PEAK) in degrees Fahrenheit (°F) below the EGT readout. Turbocharged Aircraft Leaning for turbocharged aircraft is done with refer- ence to the Turbine Inlet Temperature (TIT). When the temperature peaks, the numeric readout (∆PEAK) appears below the TIT Indicator and displays the difference be- tween peak and current TITs, in degrees Fahrenheit (°F). If a peak is not displayed, underscores are shown until one is established. 3.3 SYSTEM DISPLAY NOTE: Fuel calculations do not use the aircraft fuel quantity indicators and are calculated from the last time the fuel was reset. NOTE: The pilot should refer to the Pilot’s Operating Handbook (POH) for fuel values and limitations. The displayed fuel remaining can be adjusted up to 53 gal (Models 172R, 172S) or 87 gal (Models 182T, T182T, 206H, T206H). The System Display is accessed by pressing the ENGINE Softkey followed by the SYSTEM Softkey and shows critical engine, fuel, and electrical parameters. Fuel calculations are based on the fuel flow totalizer and the displayed fuel remaining, adjusted by the pilot using the following softkeys: • RST FUEL – Resets totalizer-based fuel remaining (GAL REM) to zero and the fuel used (GAL USED) to zero • GAL REM – Gives access to softkeys for adjusting the amount of fuel remaining for purposes of fuel calculations Fuel remaining can be adjusted in one or ten-gallon increments using the appropriate softkeys. Softkeys also allow entering the full tank quantity for the aircraft or the tab quantity, which is 35 gallons (Models 172R and 172S) or 64 gallons (Models 182T, T182T, 206H, and T206H). Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3-8 1 Engine Manifold Pressure Gauge (MAN IN) Models 182, T182, 206, T206 – Displays engine power in inches of mercury (in Hg). Turbocharged aircraft have a red portion of the gauge indicating the maximum manifold pressure range. A white tick mark is displayed indicating the cruise manifold pressure (Model T182 only). 2 Tachometer (RPM) – Shows propeller speeds in revolutions per minute (rpm). Red range indicates propeller overspeed warning; a white high-rpm range indicates above normal operating speeds (Models 172S, 206 and T206). 3 Oil Pressure (OIL PSI) – Displays pressure of the oil supplied to the engine in pounds per square inch (psi). 4 Oil Temperature (OIL °F) – Displays the engine oil temperature in degrees Fahrenheit (°F). 5 Engine Hours (Tach) (ENG HRS) Models 182, T182, 206, T206 – A numeric readout gives the time (in hours) the engine has been in service. 6 Vacuum Pressure Indicator (VAC) Models 182, T182, 206, T206 – Displays vacuum pressure. 7 Fuel Flow (FFLOW GPH) – Shows the current fuel flow in gallons per hour (gph). 8 Calculated Fuel Used (GAL USED) – Shows quantity of fuel used in gallons based on fuel flow since last reset. 9 Set Fuel Remaining (GAL REM) – Shows current fuel remaining in gallons as set by the pilot and adjusted for fuel burn since last set. 10 Fuel Quantity Indicator (FUEL QTY GAL) – Shows the quantity of fuel in the tanks, in gallons, ranging from zero to full (F) for each fuel tank (left–L and right–R). When full, the indicator displays to 35 gallons per side (26 gallons for the Models 172R and 172S). 11 Voltmeter (M, E BUS VOLTS) – Displays the main and essential bus voltages. 12 Ammeter (M, S BATT AMPS) – Shows the main and standby battery load in amperes. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3-9 Figure 3-5 System Display (Normally-aspirated Aircraft) Model 182T 1 8 10 9 5 4 3 2 6 7 11 12 Model 172S 12 7 4 3 2 8 9 10 11 Model 172R 12 7 4 3 2 8 9 10 11 Model 206H 1 8 10 9 5 4 3 2 6 7 11 12 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3-10 Figure 3-6 System Display (Turbocharged Aircraft) Model T206H 1 8 10 9 5 4 3 2 6 7 11 12 Model T182T 1 8 10 9 5 4 3 2 6 7 11 12 Cruise Manifold Pressure Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A 4-1 SECTION 4 – NAV/COM & TRANSPONDER SECTION 4: NAV/COM AND TRANSPONDER The NAV/COM controls and frequency boxes share the same locations on the on the Primary Flight Display and the Multi-Function Display. Figure 4-1 G1000 VHF NAV/COM Interface (PFD shown) DME Tuning Window NAV Controls COM Controls NAV Frequency Box COM Frequency Box Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A 4-2 SECTION 4 – NAV/COM & TRANSPONDER Standby NAV Frequency Field Active NAV Frequency Field Active COM Frequency Field Standby COM Frequency Field Figure 4-2 Frequency Fields Selected NAV Frequency Tuning Box Tuning Box Selected COM Frequency Frequency Transfer Arrow Tuning Box Figure 4-3 Frequency Transfer Arrow and Tuning Box Figure 4-4 NAV/COM Controls Frequency Transfer Key Dual NAV Knob Dual COM Knob VOL/PUSH ID Knob VOL/PUSH SQ Knob NAV Controls COM Controls • Turn to tune in desired frequencies. • Press to change tuning box positions. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A 4-3 SECTION 4 – NAV/COM & TRANSPONDER 4.1 RADIO STATUS INDICATIONS • RX – When a COM signal is received, a white ‘RX’ appears by the active COM frequency during signal reception. • TX – When a COM radio is transmitting, a white ‘TX’ indication appears to the right of the corresponding COM frequency. • ID – When the Morse code identifier is ON for a NAV radio, a white ‘ID’ indication appears to the left of the corresponding active NAV frequency. The Morse code identifier can be heard if the corresponding NAV radio is selected on the audio panel. Figure 4-5 Radio Status Indications 4.2 VOLUME ‘VOLUME’ is displayed in place of the associated radio name (i.e., ‘COM1’ or ‘NAV2’) for two seconds after the volume level is last changed. The percentage of maximum volume is displayed in place of the standby frequency selected by the tuning box. Figure 4-6 COM Volume Level 4.3 AUTOMATIC SQUELCH Automatic squelch can be disabled for a COM radio by pressing the COM Knob to place the tuning box on the desired COM’s standby frequency, then by pressing the VOL/PUSH SQ Knob. When Automatic Squelch is disabled, a white ‘SQ’ appears next to the COM frequency. Squelch Indication Figure 4-7 Squelch Indication 4.4 QUICKLY ACTIVATING 121.500 MHZ Pressing and holding the COM Frequency Transfer Key for approximately two (2) seconds automatically tunes the selected COM radio to the emergency frequency. 4.5 OPTIONAL NAV RADIOS DME Radio (optional) The DME Tuning Window is displayed by pressing the DME Softkey. Figure 4-8 Radio Tuning Window Changing the DME tuning source: 1) From the tuning window, turn the large FMS Knob to highlight the DME source field. 2) Turn the small FMS Knob to display the selection window. Turn the FMS Knob to select the desired mode and press the ENT Key. Figure 4-9 DME Selection Window Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A 4-4 SECTION 4 – NAV/COM & TRANSPONDER ADF Radio (optional) The G1000 does not support tuning of the ADF in Nav III aircraft. ADF tuning is accomplished through the Bendix/King KR 87 ADF Radio. ADF volume must also be adjusted through the KR 87. 4.6 FREQUENCY AUTO-TUNING Auto-tuning on the PFD Figure 4-10 Nearest Airports Window (PFD) 1) Press the NRST Softkey to display the Nearest Airports Window. 2) Turn either FMS Knob to highlight the desired frequency. 3) Press the ENT Key to place the frequency in the standby field of the active COM. 4) Press the Frequency Transfer Key to place the frequency in the active field. NAV frequencies are entered automatically in the NAV frequency active or standby field (depending in CDI selection) upon approach loading or approach activation. Auto-tuning on the MFD Auto-tuning on the MFD is done in much the same way as on the PFD. Use the FMS Knobs to select the desired frequency on any of the information pages. Pressing the ENT Key then loads the selected frequency in the tuning box as a standby frequency. 4.7 TRANSPONDER Mode Selection The STBY, ON, ALT, GND, VFR, CODE, and IDENT Softkeys can be accessed by pressing the XPDR Softkey. Ground Mode (Automatic or Manual) GND is displayed when the aircraft is on the ground or when the GND Softkey is pressed. The transponder does not allow Mode A and Mode C replies, but it does permit acquisition squitter and replies to discretely address Mode S interrogations. Figure 4-11 Ground Mode Standby Mode (Manual) Press the STBY Softkey. In Standby Mode, the tran- sponder does not reply to interrogations, but new codes can be entered. STBY Mode (White Code Number and Mode) Figure 4-12 Standby Mode Manual ON Mode Press the ON Softkey. ON Mode generates Mode A and Mode S replies, but Mode C altitude reporting is in- hibited. ON Mode (No Altitude Reporting) Figure 4-13 ON Mode Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A 4-5 SECTION 4 – NAV/COM & TRANSPONDER Altitude Mode (Automatic or Manual) Altitude Mode is automatically selected when the aircraft becomes airborne. Altitude Mode may also be selected manually by pressing the ALT Softkey. All transponder replies requesting altitude information are provided with pressure altitude information. ALT Mode (Mode C Altitude Reporting) Figure 4-14 Altitude Mode Reply Status When the transponder sends replies to interrogations, an “R” indication appears momentarily in the reply status field. Figure 4-15 Reply Indication Reply Indication Code Selection VFR Code Selection 1) Press the XPDR Softkey to display the transponder Mode Selection softkeys. 2) Press the VFR Softkey to enter the VFR code. Pressing the VFR Softkey again restores the previous identification code. NOTE: The pre-programmed VFR Code is set at the factory to 1200. Enter Code Using Softkeys 1) Press the XPDR Softkey to display the transponder Mode Selection softkeys. 2) Press the CODE Softkey to display the transponder Code Selection softkeys, which includes the digit softkeys. 3) Press the appropriate digit softkeys to enter the code in the four-digit code field of the Transponder Status Box. When the last digit is entered, the transponder code becomes active. When entering a code, press the BKSP Softkey as needed to back up and change code digits. Enter Code Using the FMS Knob 1) Press the XPDR Softkey to display the transponder Mode Selection softkeys. 2) Press the CODE Softkey to display the transponder Code Selection softkeys, which includes the digit softkeys. 3) Turn the small FMS Knob to enter the first two digits. 4) Turn the large FMS Knob to place the cursor in position to change the second two digits. 5) Turn the small FMS Knob to enter the second two digits. 6) Press the ENT Key to activate the code immediately, or wait 10 seconds and the code will become active. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A 4-6 SECTION 4 – NAV/COM & TRANSPONDER Flight ID Reporting If so configured, the Flight ID may be entered in the Timer/Reference Window. Figure 4-16 Timer/References Window Flight ID 1) Press the TMR/REF Softkey to display the Timer/ References Window. 2) Turn the large FMS Knob to place the cursor in the Flight ID field. 3) Turn the small FMS Knob to enter the desired first character. 4) Turn the large FMS Knob to place the cursor in the next desired field. 5) Turn the small FMS Knob to enter the next desired character. 6) Repeat steps 4 and 5 until the desired Flight ID is entered. 7) Press the ENT Key. ‘updating’ is displayed as the Flight ID is loaded into the system. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A 5-1 SECTION 5 – AUDIO PANEL SECTION 5: AUDIO PANEL Transmitters Receiver Audio Marker Beacon/Mute Marker Beacon Signal Sensitivity Cabin Speaker VOL/SQ Manual Squelch Aircraft Navigation Radio Audio (Optional, disabled if ADF and/or DME are not installed) Reversionary Mode Aircraft Navigation Radio Audio Figure 5-1 Front Panel Controls ICS Isolation VOL Annunciation SQ Annunciation Disabled Disabled Digital Clearance Recorder Play Key Passenger Address (Disabled on 172R/S) Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A 5-2 SECTION 5 – AUDIO PANEL 5.1 COM RADIO SELECTION Pressing the COM1 MIC or COM2 MIC Key selects the active transmitter (i.e., microphone). The associated receiver audio (COM1 or COM2) also becomes selected when the COM MIC Key is pressed. To prevent deselecting the desired received audio when pressing another COM MIC Key, press the already selected COM1 or COM2 Key before pressing the other COM MIC Key. Figure 5-2 Transceivers 5.2 CABIN SPEAKER Pressing the SPKR Key selects and deselects the cabin speaker. All of the radios can be heard over the cabin speaker. Speaker audio is muted when the PTT is pressed. Certain aural alerts and warnings (autopilot, traffic, altitude) are always heard on the speaker, even when the speaker is not selected. Figure 5-3 Passenger Address and Speaker Keys 5.3 PASSENGER ADDRESS (PA) SYSTEM (T)182T AND (T)206H ONLY A passenger address system is available for delivering voice messages over the cabin speaker. When the PA Key is selected on the Audio Panel, the COM MIC Annunciator is extinguished, and the active COM frequency changes to white, indicating that there is no COM selected. A Push-to- Talk (PTT) must be pressed to deliver PA announcements. The PA Annunciator flashes about once per second while the PTT is depressed. 5.4 MARKER BEACON RECEIVER The marker beacon receiver is always on. Only the marker beacon audio can be turned off. Figure 5-4 shows the marker beacon annunciators on the PFD. When the MKR/MUTE Key is pressed, the key an- nunciator is lit and the audio tone can be heard over the speaker or headsets during marker beacon reception. When the tone is active, pressing the MKR/MUTE Key once mutes the audio but does not affect the marker an- nunciator. The audio returns when the next marker signal is received. To turn off the marker beacon audio, press the MKR/ MUTE Key once when there is no marker indication pres- ent, or press twice when an indication is present. The key annunciator extinguishes when the marker beacon audio is turned off. Outer Marker Inner Marker Altimeter Middle Marker Figure 5-4 Marker Beacon Annunciators on the PFD Marker Beacon Signal Sensitivity The HI SENS Key can be pressed for increased marker beacon signal sensitivity. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A 5-3 SECTION 5 – AUDIO PANEL Figure 5-5 Marker Beacon 5.5 NAV RADIO AUDIO SELECTION Pressing DME, ADF, NAV1, or NAV2 selects and deselects the audio source and activates the annunciator. Selected audio can be heard over the headset and the speakers. These four keys can be selected individually or together. Figure 5-6 Navigation Radios PILOT KEY Annunciator COPLT KEY Annunciator Pilot Hears Copilot Hears Passenger Hears OFF OFF Selected radios, aural alerts, pilot, copilot, passengers, music Selected radios, aural alerts, pilot, copilot, passengers, music Selected radios, aural alerts, pilot, copilot, passengers, music ON OFF Selected radios, aural alerts, pilot Copilot, passengers, music Copilot, passengers, music OFF ON Selected radios, aural alerts, pilot, passengers, music Copilot Selected radios, aural alerts, pilot, passengers, music ON ON Selected radios, aural alerts, pilot, copilot Selected radios, aural alerts, pilot, copilot Passengers, music Table 5-1 ICS Isolation Modes 5.6 INTERCOM SYSTEM (ICS) ISOLATION Press the PILOT and/or COPLT Key to select who is isolated from hearing the Nav/Com radios and music. Selection scenarios are addressed in Table 5-1. Figure 5-7 ICS Isolation Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A 5-4 SECTION 5 – AUDIO PANEL 5.7 INTERCOM SQUELCH CONTROL Select manual squelch for intercom audio by pressing the MAN SQ Key to light the annunciator. Pressing the small VOL/SQ Knob now switches be- tween volume and squelch adjustment by lighting VOL or SQ respectively. Figure 5-8 Volume/Squelch Control 5.8 DIGITAL CLEARANCE RECORDER AND PLAYER Each reception of primary active COM audio is automatically recorded in a memory block. When the next transmission is received, it is recorded in the next memory block, and so on. Once the 2.5 minutes of recording time has been reached, the recorder begins recording over the stored memory blocks, starting from the oldest block. Powering off the unit automatically clears all recorded blocks. Figure 5-9 Clearance Recorder Play Key • Pressing the PLAY Key once plays the latest recorded memory block, then returns to normal operation. • Pressing the MKR/MUTE Key while playing a memory block stops play. • Pressing the PLAY Key during play begins playing the previously recorded memory block. Each subsequent press of the PLAY Key begins playing the next previously recorded block. If a COM input signal is detected while playing, play is halted and the new COM input signal is recorded as the latest block. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-1 SECTION 6: AUTOMATIC FLIGHT CONTROL NOTE: The Aircraft Flight Manual (AFM) always supersedes the information in this guide. This section only applies to the GFC 700 Automatic Flight Control System (AFCS). 6.1 AFCS CONTROLS The following dedicated AFCS keys are located on the bezels of the PFD and MFD: Figure 6-1 Dedicated AFCS Controls The following AFCS controls are located in the cockpit separately from the MFD: • AP DISC Switch (Autopilot Disconnect) Disengages the autopilot and interrupts pitch trim operation. The red AP DISC Switch is located forward of the MET Switch on the pilot’s control wheel left grip. This switch may be used to acknowledge an autopilot disconnect and mute the associated aural tone. • CWS Button (Control Wheel Steering) Momentarily disengages the autopilot and synchronizes the flight director’s Command Bars with the current aircraft pitch (if not in Glideslope Mode) and roll (if in Roll Hold Mode). The CWS Button is located on the top of the pilot’s control wheel right grip. Upon release of the CWS Button, the flight director may establish new reference points, depending on the current pitch and roll modes. • GA Switch (Go-Around) Disengages the autopilot, selects flight director Go- Around Mode, and activates the missed approach. The GA Switch is located on the instrument panel above the throttle. • MET Switch (Manual Electric Trim) The MET Switch is located on the pilot’s control wheel left grip. This composite switch is split into left and right sides. The left switch is the ARM contact and the right switch controls the DN (forward) and UP (rearward) contacts. The MET ARM switch can be used to disengage the autopilot and to acknowledge an autopilot disconnect alert and mute the associated aural tone. Manual trim commands are generated only when both sides of the switch are operated simultaneously. If either side of the switch is active separately for more than three seconds, MET function is disabled and ‘PTRM’ is displayed as the AFCS Status Annunciation on the PFD. The function remains disabled until both sides of the switch are inactivated. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-2 6.2 FLIGHT DIRECTOR OPERATION With the flight director activated, the aircraft can be hand-flown to follow the path shown by the Command Bars. Maximum commanded pitch (+20°/-15°) and bank (22°) angles, vertical acceleration, and roll rate are limited to values established during AFCS certification. The flight director also provides commands to the autopilot. Activating the Flight Director Pressing the FD or AP Key (when the flight director is not active) activates the flight director in default pitch/roll modes. Pushing the GA Switch or any flight director mode key activates the flight director in the respective mode(s). AFCS Status Box Roll Modes Active Autopilot Status Active Pitch Modes Armed Mode Reference Armed Selected Altitude Command Bars Figure 6-3 PFD AFCS Display GPS is Selected Navigation Source Selected Course Selected Heading The flight director may be turned off by pressing the FD Key. Command Bars Upon activation of the flight director, Command Bars are displayed on the PFD as a single cue. If the attitude information sent to the flight director becomes invalid or unavailable, the Command Bars are removed from the display. The Command Bars do not override the aircraft symbol. Figure 6-2 Command Bars Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev. A SECTION 6