Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic. WARNING: Use of the Stormscope is not intended for hazardous weather penetration (thunderstorm penetration). Stormscope information, as displayed on the G1000 MFD, is to be used only for weather avoidance, not penetration. WARNING: Do not use datalink weather products (e.g., XM WX Satellite Weather, GFDS World Wide Weather, or FIS-B) for hazardous weather penetration. Weather information provided by these products is aged by up to several minutes and may not depict actual weather conditions as they currently appear. WARNING: NEXRAD weather data is to be used for long-range planning purposes only. Due to inherent delays in data transmission and the relative age of the data, NEXRAD weather data should not be used for short-range weather avoidance. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 Rev. A WARNINGS, CAUTIONS, & NOTES WARNING: The Garmin G1000, as installed in Cessna Nav III aircraft, has a very high degree of functional integrity. However, the pilot must recognize that providing monitoring and/or self-test capability for all conceivable system failures is not practical. Although unlikely, it may be possible for erroneous operation to occur without a fault indication shown by the G1000. It is thus the responsibility of the pilot to detect such an occurrence by means of cross-checking with all redundant or correlated information available in the cockpit. WARNING: For safety reasons, G1000 operational procedures must be learned on the ground. WARNING: The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment. Portions of the Garmin G1000 utilize GPS as a 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 variation in the earth’s magnetic field, operating the system within the following areas could result in loss of reliable attitude and heading indications. North of 72° North latitude at all longitudes. South of 70° South latitude at all longitudes. North of 65° North latitude between longitude 75° W and 120° W. (Northern Canada). North of 70° North latitude between longitude 70° W and 128° W. (Northern Canada). North of 70° North latitude between longitude 85° E and 114° E. (Northern Russia). South of 55° South latitude between longitude 120° E and 165° E. (Region south of Australia and New Zealand). WARNING: Do not use GPS to navigate to any active waypoint identified as a ‘NON WGS84 WPT’ by a system message. ‘NON WGS84 WPT’ waypoints are derived from an unknown map reference datum that may be incompatible with the map reference datum used by GPS (known as WGS84) and may be positioned in error as displayed. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 Rev. A WARNINGS, CAUTIONS, & NOTES CAUTION: The PFD and MFD displays use a lens coated with a special anti-reflective coating that is very sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI-REFLECTIVE COATING. It is very important to clean the lens using a clean, lint-free cloth and an eyeglass lens cleaner that is specified as safe for anti-reflective coatings. CAUTION: The Garmin G1000 does not contain any user-serviceable parts. Repairs should only be made by an authorized Garmin service center. Unauthorized repairs or modifications could void both the warranty and the pilot’s authority to operate this device under FAA/FCC regulations. NOTE: 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: 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 operat- ing guide. Complete operating procedures for the system are found in the G1000 Pilot’s Guide for this aircraft. 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 190-00384-12 Rev. A WARNINGS, CAUTIONS, & NOTES Blank Page Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 Rev. A RR-1 RECORD OF REVISIONS Part Number Change Summary 190-00384-03 (Rev. A) (Rev. B) 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 Updated system software numbers 190-00384-04 (Rev. A) (Rev. B) Reformatted manual to new format Added TAS capability 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 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 Rev. A RR-2 RECORD OF REVISIONS Part Number Change Summary 190-00384-07 (Rev. A) Added GDU 8.02 parameters, Airways, and ADS-B 190-00384-08 (Rev. A) Added GDU 8.20 parameters, including gradient background on the PFD and GFC 700 for the C172. 190-00384-09 (Rev. A) Added GDU 9.03 parameters. Removed gradient background. Added Additional Features section Changed tab structure 190-00384-10 Added GDU 9.15 Added new page navigation Added flight plan import/export Added new EIS displays Added CDI use in Dead Reckoning Mode Various clerical changes 190-00384-11 Added GDU 10.01 Added Auxiliary Video Added AOPA Airport Directory Added Flight Data Logging 190-00384-12 Added GDU 12.02 parameters Added FIS-B Weather Added GTS 800 Added GFDS Weather (GSR 56) Added Arrival Alerts Revision Date of Revision Affected Pages Description A October, 2011 All Production Release Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 Rev. A TOC-1 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 .......................................................... 1-9 1.4 MFD Page Groups ................................................. 1-10 1.5 Vertical Navigation .............................................. 1-11 1.6 Arrival Alerts ......................................................... 1-13 1.7 Backlighting ........................................................... 1-13 1.8 Loading Updated Databases .............................. 1-14 Loading Garmin Database Updates............................ 1-14 Loading the Jeppesen Navigation Database as the Active Navigation Database ............. 1-15 Loading the Jeppesen Navigation Database as the Standby Navigation Database.......................... 1-15 Magnetic Field Variation Database Update ................. 1-16 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 (GFC700 only) ................................... 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 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 190-00384-12 Rev. A TOC-2 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 ................................................................. 6-24 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 Select the MAP Page Group......................................... 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 ............................................. 7-25 Select the Airport Information Page............................ 7-25 Display AOPA Airport Directory Information ................ 7-26 Select an Airport from the Database .......................... 7-26 Select an Airport from the Active Flight Plan............... 7-26 Select a Nearest Airport ............................................. 7-26 Select a Recently Entered Airport Identifier ................. 7-27 Select an Airport by Facility Name or City Location ..... 7-27 7.5 Intersection Information .................................... 7-27 Select the Intersection Information Page .................... 7-27 7.6 NDB Information................................................... 7-28 Select the NDB Information Page ............................... 7-28 7.7 VOR Information ................................................... 7-28 Select the VOR Information Page ............................... 7-28 7.8 User Waypoint Information Page ..................... 7-29 7.9 Nearest Airports ................................................... 7-29 Nearest Airport Information on the MFD .................... 7-29 Nearest Airports Information on the PFD .................... 7-30 7.10 Nearest Intersections .......................................... 7-30 Select the Nearest Intersections Page ......................... 7-30 7.11 Nearest NDB .......................................................... 7-31 Select the Nearest NDB Page ..................................... 7-31 7.12 Nearest VOR ........................................................... 7-31 Select the Nearest VOR Page ..................................... 7-31 7.13 Nearest User Waypoint........................................ 7-32 Select the Nearest User Waypoint Page ...................... 7-32 7.14 Nearest Frequencies ............................................ 7-32 Select the Nearest Frequencies Page .......................... 7-32 7.15 Nearest Airspaces ................................................. 7-33 Select the Nearest Airspaces Page.............................. 7-33 SECTION 8: FLIGHT PLANNING ...................................... 8-1 8.1 User Defined Waypoints........................................ 8-1 Select the User WPT Information Page ......................... 8-1 8.2 Viewing the Active Flight Plan ............................ 8-4 8.3 Activate a Stored Flight Plan ............................... 8-4 8.4 Activate a Flight Plan Leg .................................... 8-5 8.5 Stop Navigating a Flight Plan.............................. 8-5 8.6 Invert Active Flight Plan ....................................... 8-5 8.7 Create a Flight Plan................................................ 8-5 Create a Flight Plan Using the MFD ............................. 8-5 Create a Flight Plan Using the PFD .............................. 8-6 8.8 Import a Flight Plan from an SD Card................ 8-6 8.9 Enter an Airway in a Flight Plan ......................... 8-7 8.10 Load a Departure.................................................... 8-9 8.11 Load an Arrival ........................................................ 8-9 8.12 Load an Approach................................................... 8-9 8.13 Remove a Departure, Arrival, Approach, or Airway from a Flight Plan...............................8-9 8.14 Store a Flight Plan .................................................. 8-9 8.15 Edit a Stored Flight Plan ....................................... 8-9 8.16 Delete a Waypoint from the Flight Plan............ 8-9 8.17 Invert and Activate a Stored Flight Plan......... 8-10 8.18 Copy a Flight Plan ................................................ 8-10 8.19 Delete a Flight Plan.............................................. 8-10 8.20 Graphical Flight Plan Creation .......................... 8-10 8.21 Trip Planning.......................................................... 8-11 8.22 Export a Flight Plan to an SD Card ................... 8-12 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 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 Rev. A TOC-3 TABLE OF CONTENTS Activate An Approach in the Active Flight Plan ............. 9-4 Activate A Missed Approach in the Active Flight Plan.... 9-4 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 Displaying TFR Data:.................................................. 10-5 Enabling/disabling winds aloft data display in Profile View: .............................................................. 10-6 Weather Products & Symbols ..................................... 10-6 Weather Product Age ................................................ 10-7 10.4 FIS-B Weather (Optional) .................................... 10-7 Accessing FIS-B Weather Products ............................. 10-7 Setting Up and Customizing the FIS-B Weather Data Link Page ........................................... 10-8 Restoring Default FIS-B Weather Data Link Page Settings ............................................. 10-9 Switching Between FIS-B, GFDS and XM WX Sources . 10-9 Viewing Legends for Displayed FIS-B Weather Products...................................................... 10-9 Setting Up and Customizing Weather Data for the Navigation Map Page............................. 10-9 FIS-B Weather Products ........................................... 10-10 Displaying Precipitation Weather Information ........... 10-11 10.5 Worldwide Weather (Optional) ....................... 10-12 Registering with Garmin Flight Data Services ........... 10-12 Switching Between GFDS, FIS-B and XM WX Sources 10-13 Accessing GFDS Worldwide Weather Products .......... 10-13 Setting Up and Customizing the GFDS Weather Data Link Page ................................. 10-14 Restoring Default GFDS Weather Data Link Page Settings ............................. 10-14 Viewing Legends for Displayed GFDS Weather Products.................................................... 10-15 Setting Up and Customizing Weather Data for the Navigation Map Page ............. 10-15 GFDS Weather Data Requests .................................. 10-16 Worldwide Weather Products................................... 10-19 10.6 Traffic Systems .................................................... 10-23 Traffic Information Service (TIS) ................................ 10-23 Traffic Advisory Systems (Optional) ........................... 10-24 ADS-B Traffic GDL 90 (Optional) .............................. 10-27 10.7 Terrain and Obstacle Proximity ....................... 10-28 Displaying Terrain and Obstacles on the Terrain Proximity Page ............................................ 10-28 Displaying Terrain and Obstacles on the Navigation Map ...................................................... 10-28 10.8 TERRAIN-SVS Display (Optional) ..................... 10-29 Displaying Terrain on the TERRAIN-SVS Page ............ 10-29 Enable/Disable Aviation Data ................................... 10-30 TERRAIN-SVS Alerts................................................. 10-30 Terrain Inhibit .......................................................... 10-33 Forward Looking Terrain Avoidance (FLTA) ................ 10-33 Displaying Terrain and Obstacles on the Navigation Map ...................................................... 10-34 10.9 Terrain Awareness & Warning System (TAWS) ...... Display (Optional)...............................................10-34 Displaying Terrain on the TAWS-B Page .................... 10-34 Enable/Disable Aviation Data ................................... 10-35 TAWS Inhibit ........................................................... 10-35 Manual System Test ................................................. 10-35 Forward Looking Terrain Avoidance (FLTA) ................ 10-36 Premature Descent Alert (PDA) ................................ 10-36 Excessive Descent Rate Alert (EDR) .......................... 10-36 Negative Climb Rate After Takeoff Alert (NCR).......... 10-36 “Five-Hundred” Aural Alert...................................... 10-37 Displaying Terrain and Obstacles on the Navigation Map ...................................................... 10-37 Pop-up Alerts .......................................................... 10-37 TAWS Alerts Summary ............................................. 10-38 Alert Annunciations ................................................. 10-39 SECTION 11: ADDITIONAL FEATURES....................... 11-1 11.1 Synthetic Vision System (SVS) (Optional) ....... 11-1 SVS Operation ........................................................... 11-1 SVS Features ............................................................. 11-2 Field of View ............................................................. 11-9 11.2 SafeTaxi ................................................................ 11-10 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 Rev. A TOC-4 TABLE OF CONTENTS 11.3 ChartView (Optional) ......................................... 11-11 Chart Options ......................................................... 11-12 Day/Night View ....................................................... 11-13 11.4 FliteCharts ............................................................ 11-14 Chart Options ......................................................... 11-15 Day/Night View ....................................................... 11-15 11.5 AOPA Airport Directory ..................................... 11-15 11.6 XM Radio Entertainment (Service Optional) 11-16 Using XM Radio ...................................................... 11-16 Automatic Audio Muting ......................................... 11-18 11.7 Scheduler.............................................................. 11-18 11.8 Electronic Checklists .......................................... 11-20 11.9 Flight Data Logging ........................................... 11-23 11.10 Auxiliary Video (Optional)............................... 11-24 Video Setup ............................................................ 11-25 Display Selection ..................................................... 11-25 Input Selection ........................................................ 11-25 Zoom/Range ........................................................... 11-26 SECTION 12: ABNORMAL OPERATION ..................... 12-1 12.1 Reversionary Mode .............................................. 12-1 12.2 Abnormal COM Operation .................................. 12-2 12.3 Unusual Attitudes ................................................. 12-2 12.4 Stormscope Operation with loss of Heading Input .......................................... 12-2 12.5 Hazard Displays with Loss of GPS Position .... 12-2 12.6 Dead Reckoning .................................................... 12-3 SECTION 13: ANNUNCIATIONS & ALERTS .............. 13-1 13.1 Alert Level Definitions ........................................ 13-2 13.2 NAV III Aircraft Alerts .......................................... 13-3 WARNING Alerts (172R, 172S, 182T, T182T, 206H, and T206H) ........... 13-3 CAUTION Alerts (172R, 172S, 182T, T182T, 206H, and T206H) ............ 13-3 CAUTION Alerts (T182, T206, and 206 with Prop De-Ice Only)............. 13-3 Safe Operating Annunciation (T182, T206, and 206 with Prop De-Ice Only)............. 13-3 13.3 CO Guardian Messages........................................ 13-3 13.4 AFCS Alerts............................................................. 13-4 System Status Annunciation....................................... 13-4 13.5 Terrain-SVS Alerts................................................. 13-5 13.6 TAWS Alerts............................................................ 13-6 13.7 Other G1000 Aural Alerts .................................... 13-8 13.8 G1000 System Annunciations ............................ 13-9 13.9 G1000 System Message Advisories ................ 13-12 MFD & PFD Message Advisories............................... 13-12 Database Message Advisories .................................. 13-13 GMA 1347 Message Advisories ............................... 13-16 GIA 63 Message Advisories ..................................... 13-16 GIA 63W Message Advisories .................................. 13-19 GEA 71 Message Advisories .................................... 13-22 GSR 56 Message Advisories..................................... 13-22 GDC 74A Message Advisories.................................. 13-22 GTX 33 Message Advisories..................................... 13-23 GRS 77 Message Advisories..................................... 13-23 GMU 44 Message Advisories ................................... 13-24 GDL 69/69A Message Advisories ............................. 13-24 Miscellaneous Message Advisories ........................... 13-24 13.10 Flight Plan Import/Export Messages ............ 13-27 INDEX ...................................................................................Index-1 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 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- 00498-07). 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 190-00384-12 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 190-00384-12 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, FPL, 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 190-00384-12 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 (500m for metric), while the small knob selects the hundreds (50m for metric). 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 190-00384-12 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 Softkey to return to the top-level softkeys. STRMSCP ALERTS ALERTS DME TRFC-1 TRFC-2 WX LGND METAR or PRECIP or DL LTNG Figure 1-2 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). WX LGND – Displays icon and age on the Inset Map for the selected weather products (optional) TRAFFIC – Cycles through traffic display options: - TRFC-1: Traffic displayed on inset map - TRFC-2: Traffic Map Page is displayed in the inset map window 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. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 Rev. A 1-6 SECTION 1 SYSTEM OVERVIEW STRMSCP (optional) – Press to display the Stormscope lightning data on the Inset Map (within a 200 nm radius of the aircraft). NEXRAD/PRECIP (optional) – Press to display NEXRAD weather and coverage information on the Inset Map or FIS-B/GFDS precipitation on the Inset Map XM LTNG/DL LTNG (optional) – Press to display XM/DL lightning information on the Inset Map. METAR (optional) – Press to display METAR flags for the airport symbols on the Inset Map BACK – Press to return to the previous level softkey configuration. Figure 1-3 PFD Configuration Softkeys Press the 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) SYN VIS SYN TERR HRZN HDG PATHWAY APTSIGNS ALERTS PFD – Press to display the additional softkeys for additional configuration of the PFD. DFLTS – Press to reset default settings on the PFD. SYN VIS – Displays the softkeys for enabling or disabling Synthetic Vision features. PATHWAY – Displays rectangular boxes representing the horizontal and vertical flight path of the active flight plan. SYN TERR – Enables synthetic terrain depiction. HRZN HDG – Displays compass heading along the Zero-Pitch line. APTSIGNS – Displays position markers for airports within approximately 15 nm of the current aircraft position. Airport identifiers are displayed when the airport is within approximately 9 nm. 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. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 Rev. A 1-7 SECTION 1 SYSTEM OVERVIEW 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 optional 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. GPS – Displays GPS waypoint identifier and GPS distance information in the BRG2 Information Window. ADF – Displays ADF in the BRG2 Information Window when an optional 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 hectopascals. 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. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 Rev. A 1-8 SECTION 1 SYSTEM OVERVIEW 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 or use the small FMS knob to enter the first two digits then turn the large FMS knob to move the curser. Again using the small FMS knob enter the second two digits. IDENT – Press to provide special aircraft position identification to Air Traffic Control (ATC). . Press the BACK Softkey to return to the top-level softkeys. Press the BACK Softkey to return to the previous softkey level. ALERTS ALERTS DME ALERTS Figure 1-4 XPDR (Transponder) Softkeys BKSP – Press to remove numbers entered one at a time. BACK – Press to return to the previous level softkeys IDENT – Press to provide special aircraft position identification to Air Traffic Control (ATC). BACK – Press to return to the previous level softkeys. ALERTS – Press to display the Alerts Window. IDENT – Press to provide special aircraft position identification to Air Traffic Control (ATC). TMR/REF – Press to display the Timer/References Window. NRST – Press to display the Nearest Airports Window. ALERTS/ADVISORY – Press to display the Alerts/ Advisory Window. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 Rev. A 1-9 SECTION 1 SYSTEM OVERVIEW 1.3 MFD SOFTKEYS Figure 1-5 MFD Softkeys BACK RST FUEL SYSTEM ENGINE LEAN ENGINE MAP DCLTR ENGINE LEAN BACK SYSTEM 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 EXIT EMERGCY ENGINE CHECK The CHECK Softkey changes to UNCHECK when the checklist item is already checked. (optional) BACK SYSTEM LEAN ENGINE Press the ENGINE or BACK Softkey to return to the default Engine Page level. ASSIST CYL SLCT GAL REM STRMSCP NEXRAD XM LTNG (optional) SHW CHRT (optional) AIRWAYS AIRWY LO AIRWAY HI AIRWY ON (Default softkey is dependant on the selection made in the map setup options) BACK -10 GAL SYSTEM ENGINE LEAN -1 GAL XX GAL +10 GAL +1 GAL XX GAL Press the ENGINE Softkey to the default Engine Page level. X = airframe specific values Press the BACK Softkey to return to the previous softkey level. (optional) or PRECIP METAR LEGEND PROFILE or DL LTNG (optional) ENGINE – Pressing this softkey makes available the LEAN and SYSTEM Softkeys which in turn access the Lean Page and the System Page, respectively. MAP – Pressing this softkey enables the following softkeys: TRAFFIC – Pressing this softkey displays/removes Traffic on the Navigation Map. PROFILE – Pressing this softkey displays/removes Profile view 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. 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/PRECIP (optional) – Pressing this softkey displays/removes precipitation data on the Navigation Map. XM LTNG/DL LTNG (optional) – Pressing this softkey displays/removes XM/DL lightning data on the Navigation Map. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 Rev. A 1-10 SECTION 1 SYSTEM OVERVIEW METAR – Pressing this softkey displays METAR flags on airport symbols on the Navigation flag. LEGEND – Pressing this softkey displays the Legend 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. CHECK – Pressing this softkey checks off a checklist item. If an item is already checked, an UNCHECK Softkey is displayed. EXIT – Press to exit the checklist. EMERGCY – Pressing this softkey displays the emergency checklist. Figure 1-6 Page Groups Map Page Group Waypoint Page Group Auxiliary Page Group Flight Plan Page Group Nearest Page Group Turn Large FMS Knob to Select Page Group Pages Within Selected Page Group (Map Pages Selected) Turn Small FMS Knob to Select Pages 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 190-00384-12 Rev. A 1-11 SECTION 1 SYSTEM OVERVIEW 1.5 VERTICAL NAVIGATION One of two altitude sources is used by the G1000 when giving vertical navigation guidance. SBAS GPS altitude is used when giving guidance for an SBAS approach after the Final Approach Fix. Baro corrected altitude is used when vertical guidance is given in all other situations and in non-SBAS 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 are 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. Refer to Figure 1-8 and Table 1-1 for more detail regarding the significance of text size and color. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 Rev. A 1-12 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 Figure 1-7 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 190-00384-12 Rev. A 1-13 SECTION 1 SYSTEM OVERVIEW 1.6 ARRIVAL ALERTS The Arrival Alert Box on the System Setup Page allows the Alerts Window arrival alert to be turned ON/OFF. The alert trigger distance (up to 99.9 units) may also be set for alerts in the Alerts Window and the PFD Navigation Status Box. An arrival alert can be set to notify the pilot with a message upon reaching a user-specified distance from the final destination (the direct-to waypoint or the last waypoint in a flight plan). When an Arrival Alert is set to ON, and the set distance is reached, an “Arrival at waypoint” message is displayed in the PFD Navigation Status Box, and a “WPT ARRIVAL - Arriving at waypoint - [xxxx]” is displayed in the Alerts Window. When Arrival Alert is set to OFF, only the PFD Navigation Status Box message “Arriving at waypoint” is displayed, and it is displayed when the time to the final destination is approximately ten seconds. Figure 1-8 Arrival Alert Settings (System Setup Page) 1.7 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 1-9 PFD Setup Menu Window Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 Rev. A 1-14 SECTION 1 SYSTEM OVERVIEW 1.8 LOADING UPDATED DATABASES CAUTION: Never disconnect power to the system when loading a database. Power interruption during the database loading process could result in maintenance being required to reboot the system. NOTE: When loading database updates, the ‘DB Mismatch’ message will be displayed until database synchronization is complete, followed by turning system power off, then on. Synchro- nization can be monitored on the AUX-SYSTEM STATUS Page. In some cases it may be necessary to obtain an unlock code from Garmin in order to make the database product functional. It may also be necessary to have the system configured by a Garmin authorized service facility in order to use some database features. If an error occurs during synchronization, an error message will be displayed, followed by the affected display in the Sync Status section of the Database Window. If synchronization completes on one display, but an error occurs on another, the error message will be displayed with the affected displays listed after it. When an error message is displayed, the problem must be corrected before synchronization can be completed. A power cycle is required to restart synchronization when ‘Card Full’ or ‘Err’ is shown. Error Message Description Canceled Database synchronization has been canceled by removing the bottom SD card in display being updated Card Full SD card does not contain sufficient memory Error Message Description Err Displayed for all other errors that may cause the synchronization process to be halted Timeout System timed-out prior to the database transfer completing Table 1-2 Database Error Messages Loading Garmin Database Updates 1) With system power OFF, remove the MFD database card from the bottom card slot of the MFD. 2) Update the Garmin databases on the MFD card. 3) Insert the MFD database card into the bottom card slot of the MFD. 4) Apply power to the system, check that the databases are initialized and displayed on the power-up screen. When updating the terrain and FliteCharts databases, a ‘Verifying’ message may be seen. If this message is present, wait for the system to finish loading before proceeding to step 5. 5) Acknowledge the Power-up Page agreement by pressing the ENT Key or the right most softkey. 6) Turn the large FMS Knob to select the AUX Page group on the MFD. 7) Turn the small FMS Knob to select the System Status Page. 8) Monitor the Sync Status in the Database Window. Wait for all databases to complete synching, indicated by ‘Complete’ being displayed. 9) Remove and reapply power to the system. 10) Turn the large FMS Knob to select the AUX Page group on the MFD. 11) Turn the small FMS Knob to select the System Status Page. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 Rev. A 1-15 SECTION 1 SYSTEM OVERVIEW 12) Press the Display Database Selection Softkey to show database information for each display (MFD1 DB, PFD1 DB). Verify the correct database cycle information is shown for each database for each display. Loading the Jeppesen Navigation Database as the Active Navigation Database NOTE: Loading the Jeppesen navigation data- base as the active database prior to its effective date will result in the expiration date on the power-up screen and the effective date on the AUX-System Status Page being displayed in yellow. NOTE: After the navigation database is loaded or copied, the top SD card may be removed. 1) With the system OFF, insert the SD card containing the new navigation database version into the top card slot of the display (PFD or MFD) to be updated (label of SD card facing left). 2) Turn the system ON. A prompt is displayed in the upper left corner of the display: 3) Press the NO Softkey to proceed to loading the active database. 4) A prompt similar to the following is displayed. Press the YES Softkey to update the active navigation database. 5) After the update completes, the display starts in normal mode. 6) Turn the system OFF and remove the SD card from the top card slot. 7) Repeat steps 1 through 6 for the other displays (PFD or MFD). 8) Apply power to the system and press the ENT Key to acknowledge the startup screen. 9) Turn the large FMS Knob to select the AUX Page group on the MFD. 10) Turn the small FMS Knob to select the System Status Page. 11) Press the Display Database Selection Softkey to show active navigation database information for each display (MFD1 DB, PFD1 DB). Verify the correct active navigation database cycle information is shown for each display. Loading the Jeppesen Navigation Database as the Standby Navigation Database NOTE: After the navigation database is loaded or copied, the top SD card may be removed. 1) With the system OFF, insert the SD card containing the new navigation database version into the top card slot of the MFD. 2) Verify that an SD card is inserted in the bottom slot of each PFD and the MFD. 3) Turn the system ON. A prompt is displayed. 4) Press the YES Softkey. The navigation database is copied to the SD card in the bottom card slot of the MFD. 5) After the navigation database files are copied to the bottom SD card, press any key to continue, as instructed. 6) Again, press any key to continue as instructed on the display. 7) Press the NO Softkey. The display now starts in normal mode. Since the database effective date is not yet valid, it should not be loaded as the active database. The display now starts in normal mode. Do not remove power while the display is starting. 8) Press the ENT Key to acknowledge the startup screen. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 Rev. A 1-16 SECTION 1 SYSTEM OVERVIEW 9) Turn the large FMS Knob to select the AUX Page group on the MFD. 10) Turn the small FMS Knob to select the System Status Page. 11) The new database is copied to the SD card in the bottom card slot of each PFD. Progress can be monitored in the SYNC STATUS field. When copying is finished, ‘Complete’ is displayed. NOTE: During the synchronization process, version differences between standby navigation databases will exist. This will result in the system displaying a ‘DB Mismatch’ alert for the standby navigation databases. This alert will remain until the next power cycle. 12) Turn system power OFF. 13) Remove the SD card from the top card slot of the MFD. 14) Turn system power ON. 15) Press the ENT Key to acknowledge the startup screen. 16) Turn the large FMS Knob to select the AUX Page group on the MFD. 17) Turn the small FMS Knob to select the System Status Page. 18) Press the Display Database Selection Softkey to show standby navigation database information for each display (MFD1 DB, PFD1 DB). Verify the correct standby navigation database cycle information is shown for each display. Magnetic Field Variation Database Update At startup, the system compares this version of the MV DB with that presently being used by the AHRS (GRS). If the system determines the MV DB needs to be updated, a prompt is displayed on the Navigation Map Page, as shown in Figure 1-10. Figure 1-10 GRS Magnetic Field Variation Database Update Prompt Loading the magnetic field variation data- base update: With ‘OK’ highlighted, as shown in the previous figure, press the ENT Key on the MFD. A progress monitor is displayed as shown in Figure 1-11. Figure 1-11 Uploading Database to GRS When the upload is complete, the system is ready for use. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 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 Current Track Indicator Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 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 (SBAS enabled systems only)/Glideslope 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 190-00384-12 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 190-00384-12 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 (50m for metric) and the large ALT Knob sets the thousands (500m for metric). 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. STD BARO will now be displayed in the Barometric Setting Box. Altitude Alerting (GFC700 only) 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 190-00384-12 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 SBAS-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 SBAS 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 190-00384-12 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 SBAS 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 is tuned in the active NAV receiver field, selected for display on the HSI, and the aircraft heading is within 105º of the approach course (see Figure 2-13). Figure 2-13 Glideslope Indicator Marker Beacon Annunciation Glideslope Indicator Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 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, DA, 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 190-00384-12 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 Current Track Indicator Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 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) (SBAS systems only) Approach (LNAV/ VNAV)(SBAS only) 1.0 nm decreasing to a specified course width, then 0.3 nm, depending on variables (see Figure 2-24) Approach (LPV) (SBAS only) Missed Approach 0.3 nm Table 2-1 CDI Scale Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 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 (SBAS Systems Only) Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 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 190-00384-12 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 190-00384-12 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 190-00384-12 Rev. A 2-14 SECTION 2 FLIGHT INSTRUMENTS Blank Page Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 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. The 172R, 172S, 182T, 206H, T182T, and T206H dis- play the following: • 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). Model 172S – When ascending through 5300 ft, the upper end of the green arc displays 2600 rpm and ascending through 10,300 displays 2700 rpm. When descending below 9700 ft, the upper end of the green arc returns to 2600 rpm and descending below 4700 ft returns to 2500 rpm. 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). Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 Rev. A SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3-2 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 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. 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). Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 Rev. A SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3-3 11 Engine Hours (Tach) (ENG HRS) Models 172R and 172S – A numeric readout gives the time (in hours) the engine has been in service. 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. 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 190-00384-12 Rev. A SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3-4 3.2 LEAN DISPLAY NOTE: The pilot should follow the engine manu- facturer’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 (DPEAK) 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 by a light blue box around the cylinder number. Cylinders whose EGTs are in the normal range appear in white. For normally aspirated models, pressing the ASSIST Softkey causes the EGT deviation from peak (DPEAK) 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 by a light blue box around the cylinder number. Cylinders whose CHTs are in the normal range appear in white. Cylinders whose CHTs enter the warning ranges appear in red. 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 190-00384-12 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 Blue 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 190-00384-12 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., places a light blue box around the cylinder number). 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 190-00384-12 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 (DPEAK) 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 (DPEAK) 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). 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). Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 Rev. A SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3-8 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 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. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 Rev. A SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3-9 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 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 (24 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 190-00384-12 Rev. A SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3-10 Blank Page Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 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 190-00384-12 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 Frequenc