Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca

WARNING: Do not use basemap (land and water data) information for primary navigation. Basemap data is intended only to supplement other approved navigation data sources and should be considered only an aid to enhance situational awareness. WARNING: Do not rely solely upon the display of traffic information for collision avoidance maneuvering. The traffic display does not provide colli- sion avoidance resolution advisories and does not under any circumstances or conditions relieve the pilot’s responsibility to see and avoid other aircraft. WARNING: Do not rely solely upon the display of traffic information to accurately depict all of the traffic within range of the aircraft. Due to lack of equipment, poor signal reception, and/or inaccurate information from aircraft or ground stations, traffic may be present that is not represented on the display. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A Warnings, Cautions & Notes WARNING: Do not use data link weather information for maneuvering in, near or around areas of hazardous weather. Information contained within data link weather products may not accurately depict current weather condi- tions. WARNING: Do not use the indicated data link weather product age to determine the age of the weather information shown by the data link weather product. Due to time delays inherent in gathering and processing weather data for data link transmission, the weather information shown by the data link weather product may be significantly older than the indicated weather product age. WARNING: Do not rely on information from the lightning detection system display as the sole basis for hazard weather avoidance. Range limitations and interference may cause the system to display inaccurate or incomplete information. Refer to the documentation from the lightning detection system manufacturer for detailed information about the system. WARNING: The Garmin system, as installed in this aircraft, has a very high degree of functional integrity. However, the pilot must recognize that provid- ing monitoring and/or self-test capability for all conceivable system failures is not practical. WARNING: Do not use the system until carefully reviewing, and gaining a thorough understanding of all aspects of the system’s Pilot’s Guide docu- mentation and the Airplane Flight Manual. Do not attempt to learn system operational procedures while the aircraft is in the air. For safety reasons, system 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 system utilize GPS as a precision elec- tronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the system can be misused or misinterpreted and, therefore, become unsafe. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A Warnings, Cautions & Notes WARNING: To reduce the risk of unsafe operation, carefully review and understand all aspects of the Pilot’s Guide documentation and the Airplane Flight Manual. Thoroughly practice basic operation prior to actual use. During flight operations, carefully compare indications from the system to all avail- able navigation sources, including the information from other NAVAIDs, visual sightings, charts, etc. For safety purposes, always resolve any discrepancies before continuing navigation. WARNING: Do not use the system to attempt to penetrate a thunderstorm. The illustrations in this guide are only examples. Both the FAA Advisory Circular, Subject: Thunderstorms, and the Aeronautical Information Manual (AIM) recommend avoiding any thunderstorm identified as severe of giving intense radar echo by at least 20 miles. WARNING: Lamp(s) inside this product 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/environ- ment/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 Piper PA-34-220T Seneca 190-01405-00 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 clean- ers. 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 coat- ings. CAUTION: The system 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 thunderstorm 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 cleaned. NOTE: Do not rely upon data link services to provide Temporary Flight Restriction (TFR) information. Always confirm TFR information through official sources such as Flight Service Stations or Air Traffic Control. NOTE: All visual depictions contained within this document, including screen images of the panel and displays, are subject to change and may not reflect the most current system and 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 harm- ful interference, and (2) this device must accept any interference received, including interference that may cause undesired operation. NOTE: This product, its packaging, and its components contain chemicals known to the State of California to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with California’s Proposition 65. If you have any questions or would like additional information, please refer to our web site at www.garmin.com/prop65. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A RR-11 Record of Revisions NOTE: Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of attitude and heading displays while the aircraft is on the ground. Moving the aircraft more than 100 yards away from the source of the interference should alleviate the condition. NOTE: Use of polarized eyewear may cause the flight displays to appear dim or blank. NOTE: Garmin requests the flight crew report any observed discrepancies related to database information. These discrepancies could come in the form of an incorrect procedure; incorrectly identified terrain, obstacles and fixes; or any other displayed item used for navigation or communication if the air or on the ground. Go to FlyGarmin.com and select Aviation Data Error Report. NOTE: The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system more easily. It is not intended to be a comprehensive operating guide. Complete operating procedures for the system are found in the G1000 Pilot’s Guide for this aircraft. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A RR-12 Record of Revisions Blank Page Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A RR-1 Record of Revisions Part Number Change Summary 190-01405-00 Initial release Revision Date of Revision Affected Pages Description A May, 2013 All Production release Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A RR-2 Record of Revisions Blank Page Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A i Table of Contents FLIGHT INSTRUMENTS ................................................................................................................ 1 Selecting the Altimeter Barometric Pressure Setting ...................................................... 1 Selecting Standard Barometric Pressure (29.92 in Hg) .................................................... 1 Change Altimeter Barometric Pressure Setting Units ...................................................... 1 Synchronizing the Altimeter Barometric Pressure Settings ........................................... 1 Synchronize CDI......................................................................................................................... 1 Change Navigation Sources ................................................................................................... 2 Enable/Disable OBS Mode While Navigating with GPS .................................................... 2 Generic Timer ............................................................................................................................. 2 Turn Individual Vspeed Bugs On or Off ................................................................................ 2 Turn ALL Vspeed Bugs On or Off ............................................................................................ 3 Set Barometric Altimeter Minimum Descent Altitude ..................................................... 3 Displaying Wind Data .............................................................................................................. 3 ENGINE INDICATION .................................................................................................................... 5 Engine Display ........................................................................................................................... 5 Engine Page................................................................................................................................ 7 Flap Indications ....................................................................................................................... 10 Landing Gear Indications ...................................................................................................... 11 NAV/COM/TRANSPONDER/AUDIO PANEL....................................................................... 13 Enter a Transponder Code..................................................................................................... 13 DME Tuning............................................................................................................................... 13 Selecting a COM Radio .......................................................................................................... 13 Selecting a NAV Radio ........................................................................................................... 13 NAV/COM Tuning ..................................................................................................................... 14 Digital Clearance Recorder and Player .............................................................................. 14 Intercom System (ICS) Isolation .......................................................................................... 15 GPS NAVIGATION ........................................................................................................................ 17 Direct-to Navigation .............................................................................................................. 17 Activate a Stored Flight Plan ............................................................................................... 18 Activate a Flight Plan Leg ..................................................................................................... 18 Stop Navigating a Flight Plan .............................................................................................. 19 Vertical Navigation (VNAV)................................................................................................... 19 FLIGHT PLANNING ...................................................................................................................... 23 Weight Planning ...................................................................................................................... 23 Trip Planning ............................................................................................................................ 23 Create a User Waypoint Defined by Latitude & Longitude ........................................... 25 Create a User Waypoint Defined by Radials from Other Waypoints ........................... 26 Create a User Waypoint Defined by a Radial & Distance from Another Waypoint.. 28 Create a User Waypoint using the Map Pointer............................................................... 29 Delete a User Waypoint ......................................................................................................... 30 Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A ii Table of Contents Create a Flight Plan ................................................................................................................ 30 Import a Flight Plan from an SD Card ................................................................................ 31 Insert a Waypoint in the Active Flight Plan ...................................................................... 32 Enter an Airway in a Flight Plan .......................................................................................... 33 Creating a User-Defined Hold at an Active Flight Plan Waypoint................................ 33 Creating a User-Defined Hold at the Aircraft Present Position .................................... 34 Removing a User-Defined Hold (Created at the Aircraft P.POS) .................................. 34 Removing a User-Defined Hold (Created at an Active Waypoint) ............................... 35 Invert An Active Flight Plan.................................................................................................. 35 Remove a Departure, Arrival, Approach, or Airway from a Flight Plan ..................... 35 Store a Flight Plan .................................................................................................................. 36 Edit a Stored Flight Plan ....................................................................................................... 36 Delete a Waypoint from the Flight Plan ............................................................................ 36 Invert and Activate a Stored Flight Plan ........................................................................... 37 Copy a Flight Plan ................................................................................................................... 37 Delete a Flight Plan ................................................................................................................ 37 Graphical Flight Plan Creation ............................................................................................. 38 Export a Flight Plan to an SD Card ..................................................................................... 38 PROCEDURES................................................................................................................................. 39 Load and Activate a Departure Procedure ....................................................................... 39 Activate A Departure Leg ..................................................................................................... 39 Load An Arrival Procedure .................................................................................................... 39 Activate An Arrival Leg ......................................................................................................... 40 Load and/or Activate an Approach Procedure ................................................................. 40 Activate An Approach in the Active Flight Plan ............................................................... 41 Activate a Vector to Final Approach Fix ............................................................................ 42 Activate A Missed Approach in the Active Flight Plan ................................................... 42 Temperature Compensated Altitude .................................................................................. 42 HAZARD AVOIDANCE ................................................................................................................ 45 Customizing the Hazard Displays on the Navigation Map ............................................ 45 STORMSCOPE® (Optional) ..................................................................................................... 45 SiriusXM Weather (Optional) ............................................................................................... 47 Connext Weather (Optional) ................................................................................................ 50 Traffic Advisory System (TAS) .............................................................................................. 62 Terrain And Obstacle Proximity ........................................................................................... 64 Terrain-SVS ............................................................................................................................... 64 Terrain Awareness & Warning System (TAWS-B) Display (Optional) ........................... 66 Airborne Color Weather Radar ............................................................................................ 68 ADDITIONAL FEATURES ........................................................................................................... 71 Synthetic Vision (Optional) ................................................................................................... 71 Terminal Procedure Charts ................................................................................................... 72 Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A iii Table of Contents Airport Directory .................................................................................................................... 74 SiriusXM Radio Entertainment (Optional) ........................................................................ 75 ABNORMAL OPERATION.......................................................................................................... 77 Reversionary Mode ................................................................................................................ 77 Abnormal COM Operation .................................................................................................... 77 Hazard Displays with Loss of GPS Position ....................................................................... 78 Unusual Attitudes ................................................................................................................... 78 Dead Reckoning ...................................................................................................................... 79 ANNUNCIATIONS & ALERTS................................................................................................... 81 G1000 System Annunciations ............................................................................................... 81 G1000 System Annunciations (Cont.) ................................................................................. 82 CAS Annunciations.................................................................................................................. 83 System Messages .................................................................................................................... 85 Comparator Annunciations................................................................................................... 85 Reversionary Sensor Annunciations ................................................................................... 85 Voice Alerts .............................................................................................................................. 86 Terrain-SVS Alerts ................................................................................................................... 87 Terrain-SVS System Status Annunciations ........................................................................ 87 TAWS-B Alerts .......................................................................................................................... 88 TAWS-B System Status Annunciations ............................................................................... 90 MFD & PFD Message Advisories .......................................................................................... 91 Database Message Advisories ............................................................................................. 93 GMA 1347 Message Advisories ............................................................................................ 96 GIA 63W Message Advisories ............................................................................................... 97 GEA 71 Message Advisories................................................................................................ 100 GTX 33 & 33 w/ES Message Advisories ............................................................................ 100 GRS 77 Message Advisories ................................................................................................ 101 GMU 44 Message Advisories .............................................................................................. 102 GDL 69A Message Advisories ............................................................................................. 103 GDC 74A Message Advisories............................................................................................. 103 GWX 68 Alert Messages ....................................................................................................... 104 Miscellaneous Message Advisories................................................................................... 104 Flight Plan Import/Export Messages ................................................................................ 108 APPENDIX ..................................................................................................................................... 111 PFD Softkey Map .................................................................................................................. 111 MFD Softkey Map ................................................................................................................. 117 Loading Updated Databases .............................................................................................. 120 INDEX .........................................................................................................................................Index-1 Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A iv Table of Contents Blank Page Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 1 Flight Instruments Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index FLIGHT INSTRUMENTS SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING Turn the BARO Knob to select the desired setting. SELECTING STANDARD BAROMETRIC PRESSURE (29.92 IN HG) Press the BARO Knob. CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS 1) Press the PFD Softkey to display the second-level softkeys. 2) Press the ALT UNIT Softkey. 3) Press the IN Softkey to display the barometric pressure setting in inches of mercury (in Hg). Or: Press the HPA Softkey to display the barometric pressure setting in hectopascals. 4) Press the BACK Softkey to return to the top-level softkeys. SYNCHRONIZING THE ALTIMETER BAROMETRIC PRESSURE SETTINGS 1) Select the AUX-SYSTEM SETUP Page on the MFD. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight BARO in the SYNCHRONIZATION Window. 4) Turn the small FMS Knob clockwise to ON or counterclockwise to OFF. SYNCHRONIZE CDI 1) Select the AUX-SYSTEM SETUP Page on the MFD. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight CDI in SYNCHRONIZATION Window. 4) Turn the small FMS Knob clockwise to ON or counterclockwise to OFF. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 2 Flight Instruments Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index CHANGE NAVIGATION SOURCES 1) Press the CDI Softkey to change from GPS to VOR1 or LOC1. This places the light blue tuning box over the NAV1 standby frequency in the upper left corner of the PFD. 2) Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2. This places the light blue tuning box over the NAV2 standby frequency. 3) Press the CDI Softkey a third time to return to GPS. ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS 1) Press the OBS Softkey to select OBS Mode. 2) Turn a CRS Knob to select the desired course to/from the waypoint. Press the CRS Knob to synchronize the Selected Course with the bearing to the next waypoint. 3) Press the OBS Softkey again to disable OBS Mode. GENERIC TIMER 1) Press the TMR/REF Softkey, then turn the large FMS Knob to select the time field (hh/mm/ss). Turn the FMS Knobs to set the desired time, then press the ENT Key. The UP/DOWN field is now highlighted. 2) Turn the small FMS Knob to display the UP/DOWN window. Turn the FMS Knob to select ‘UP’ or ‘DOWN’, then press the ENT Key. ‘START?’ is now highlighted. 3) Press the ENT Key to START, STOP, or RESET the timer (if the timer is counting DOWN, it will start counting UP after reaching zero). Press the CLR Key or the TMR/REF Softkey to remove the window. TURN INDIVIDUAL VSPEED BUGS ON OR OFF 1) Press the TMR/REF Softkey. 2) Turn the large FMS Knob to highlight the desired Vspeed. 3) Turn the small FMS Knob clockwise to ON or counterclockwise to OFF. 4) To remove the window, press the CLR Key or the TMR/REF Softkey. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 3 Flight Instruments Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index TURN ALL VSPEED BUGS ON OR OFF 1) Press the TMR/REF Softkey. 2) Press the MENU Key. 3) Turn the FMS Knob to highlight the desired option. 4) Press the ENT Key. Press the TMR/REF Softkey to remove the window. SET BAROMETRIC ALTIMETER MINIMUM DESCENT ALTITUDE 1) Press the TMR/REF Softkey. 2) Turn the large FMS Knob to highlight the OFF/BARO/TEMP COMP field to the right of ‘MINIMUMS’. 3) Turn the small FMS Knob clockwise to select BARO or TEMP COMP. Selecting TEMP COMP will allow the system to use an altitude compensated for temperature. 4) Press the ENT Key. 5) Use the small FMS Knob to enter the desired altitude. 6) Press the ENT Key. 7) To remove the window, press the CLR Key or the TMR/REF Softkey. 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 Piper PA-34-220T Seneca 190-01405-00 Rev. A 4 Flight Instruments Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index Blank Page Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 5 EIS Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index ENGINE INDICATION ENGINE DISPLAY Engine Display when Engine Page is displayed Engine Display 8 1 9 10 11 2 3 4 5 6 7 13 12 Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 6 EIS Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index 1 Engine Manifold Pressure Gauge (MAN IN HG) Displays manifold pressure in inches of Mercury (in Hg) to indicate engine power 2 Tachometer (RPM) Displays propeller speed in revolutions per minute (rpm) 3 Propeller Sync Indicator Points towards the higher-speed propeller when the propellers are out of sync. 4 Turbo Inlet Temperature Indicator (TIT °F) Displays the temperature for the right and left turbo inlets in °F 5 Fuel Flow Indicator (FFLOW GPH) Displays fuel flow in gallons per hour (gph) 6 Oil Pressure Indicator (OIL PSI) Displays oil pressure in pounds per square inch (psi) 7 Oil Temperature Indicator (OIL °F) Displays oil temperature in degrees Fahrenheit (°F) 8 Alternator Current(ALTR AMPS) Displays each alternator current in amperes 9 Voltage (VOLTS) Displays the bus voltage. 10 Battery Current(BATT AMPS) Displays the battery current in amperes 11 Fuel Quantity Indicator (FUEL QTY GAL) Displays the amount of fuel in gallons (gal) for each side of a standard fuel tank. 12 Flap Position (FLAPS) Displays flap position in degrees 13 Landing Gear Status (LANDING GEAR) Displays landing gear status Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 7 EIS Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index ENGINE PAGE Press the ENGINE Softkey or turn the large FMS Knob and select the EIS - Engine Page. 1 Engine Page 4 5 6 7 8 9 3 2 14 15 13 11 12 10 1 Engine Manifold Pressure Gauge (MAN IN HG) Displays manifold pressure in inches of Mercury (in Hg) to indicate engine power 2 Tachometer (RPM) Displays propeller speed in revolutions per minute (rpm) 3 Propeller Sync Indicator Points towards the higher-speed propeller when the propellers are out of sync. 4 Turbo Inlet Temperature Indicator (TIT °F) Displays the temperature for the right and left turbo inlets in °F Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 8 EIS Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index 5 Fuel Flow Indicator (FFLOW GPH) Displays fuel flow in gallons per hour (gph) 6 Oil Pressure Indicator (OIL PSI) Displays oil pressure in pounds per square inch (psi) 7 Oil Temperature Indicator (OIL °F) Displays oil temperature in degrees Fahrenheit (°F) 8 Flap Position (FLAPS) Displays flap position in degrees 9 Landing Gear Status (LANDING GEAR) Displays landing gear status 10 Fuel Calculations Group (FUEL CALC) Displays calculated fuel used (GAL USED), endurance (ENDUR), and range (in nautical miles, RANGE NM), and fuel efficiency (in nautical miles per gallon, NMPG) based on the displayed fuel remaining (GAL REM) and the fuel flow totalizer 11 Systems Group (SYSTEMS) Displays oxygen in pounds per square inch (OXYGEN PSI), vacuum in inches of Mercury (VACUUM IN HG), and propeller heat in amperes (PROP HEAT AMPS) 12 Engine Hours (TACH TIME) Displays the total time in hours the engine has been in service 13 Cylinder Head Temperature Bar Graph (CHT °F) Displays head temperatures for all cylinders in °F 14 Electrical Group (ELECTRICAL) Displays alternator (ALTR AMPS) and battery (BATT AMPS) currents in amperes and bus voltage (VOLTS) 15 Fuel Quantity Gauges (L/R FUEL QTY GAL) Displays the total amount of fuel and the amount of fuel in gallons (gal) for each side of a standard fuel tank Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 9 EIS Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index Fuel Calculations NOTE: Fuel calculations do not use the aircraft fuel quantity indicators and are calculated from the last time the fuel was reset. Fuel used (GAL USED), endurance (ENDUR), range (in nautical miles, RANGE NM), and fuel efficiency (in nautical miles per gallon, NMPG) are calculated based on the displayed fuel remaining (GAL REM) and the fuel flow totalizer. The calculated range also takes into account the aircraft’s heading and the wind direction and speed. Adjusting the fuel totalizer quantity: On the Engine Page, use the DEC FUEL and INC FUEL softkeys to obtain the desired fuel remaining (GAL REM). Each press of the softkey increments or decrements in one gallon increments. Resetting the fuel totalizer: On the Engine Page, select the RST FUEL Softkey; this resets displayed fuel remaining (GAL REM) to the maximum fuel capacity for the aircraft and fuel used to zero. Fuel Calculations Group Fuel Efficiency Calculated Range Calculated Endurance Calculated Fuel Used Set Fuel Remaining Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 10 EIS Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index FLAP INDICATIONS Flap positions are labeled 0°, 10°, 25°, and 40°. An invalid flap position is dis- played as ‘--’. Indication Description Flaps normal (EIS) Flaps normal (Engine Page displayed) Invalid flap position (EIS) Invalid flap position (Engine Page displayed) Flap Indications Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 11 EIS Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index LANDING GEAR INDICATIONS Landing Gear statuses are shown using the indications in the following table. Position EIS Engine Page Up & Locked In Transition Down and Locked Warning Landing Gear Indications Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 12 EIS Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index Blank Page Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 13 Nav/Com/XPDR/Audio Panel Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index NAV/COM/TRANSPONDER/AUDIO PANEL ENTER A TRANSPONDER CODE 1) Press the XPDR Softkey to display the transponder mode selection softkeys. 2) Press the CODE Softkey to display the transponder code selection softkeys, for digit entry. 3) Press the digit softkeys to enter the code in the code field. When entering the code, the next key in sequence must be pressed within 10 seconds, or the entry is cancelled and restored to the previous code. Five seconds after the fourth digit has been entered, the transponder code becomes active. DME TUNING 1) Press the DME Softkey. 2) Turn the large FMS to select the DME source field. 3) Turn the small FMS Knob to select the desired Nav radio. 4) Press the ENT Key to complete the selection. SELECTING A COM RADIO Transmit/Receive Press the COM1 MIC, COM2 MIC, or COM3 MIC Key (optional COM, if installed) on the audio panel. Receive Only Press the COM1, COM2, or COM3 Key (optional COM, if installed) on the audio panel. SELECTING A NAV RADIO 1) To begin navigating using a navigation radio, press the CDI Softkey on the PFD to select VOR1/LOC1 (NAV1) or VOR2/LOC2 (NAV2). 2) Press the NAV1, NAV2, DME, or ADF Key on the audio panel to select or deselect the navigation radio audio source. All radio keys can be selected individually or together. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 14 Nav/Com/XPDR/Audio Panel Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index NAV/COM TUNING 1) Press the small tuning knob to select the desired radio for tuning. A light blue box highlights the radio frequency to be tuned. 2) Turn the respective tuning knobs to enter the desired frequency into the standby frequency field. The large knob enters MHz and the small knob enters kHz. 3) Press the Frequency Transfer Key to place the frequency into the active frequency field. DIGITAL CLEARANCE RECORDER AND PLAYER NOTE: Only the audio for the selected COM MIC Key is recorded. Audio is not recorded for COM3 MIC. • Pressing the PLAY Key once plays the latest recorded memory block, then returns to normal operation. • Pressing the MKR/MUTE Key while playing a memory block stops play. • Pressing the PLAY Key during play begins playing the previously recorded memory block. Each subsequent press of the PLAY Key begins playing the next previously recorded block. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 15 Nav/Com/XPDR/Audio Panel Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index INTERCOM SYSTEM (ICS) ISOLATION Press the PILOT and/or COPLT Key to select those isolated from hearing the Nav/ Com radios and music. Mode PILOT KEY ANNUNCIATOR COPLT KEY ANNUNCIATOR Pilot Hears Copilot Hears Passenger Hears ALL OFF OFF Selected radios; pilot; copilot; passengers; music Selected radios; pilot; copilot; passengers; music Selected radios; pilot; copilot; passengers; music PILOT ON OFF Selected radios; pilot Copilot; passengers; music Copilot; passengers; music COPILOT OFF ON Selected radios; pilot; passengers; music Copilot Selected radios; pilot; passengers; music CREW ON ON Selected radios; pilot; copilot Selected radios; pilot; copilot Passengers; music Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 16 Nav/Com/XPDR/Audio Panel Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index Blank Page Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 17 GPS Navigation Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index GPS NAVIGATION DIRECT-TO NAVIGATION Direct-to Navigation using the MFD 1) Press the Direct-to ( ) Key on the MFD. 2) Enter the waypoint identifier. 3) Press the ENT Key to confirm the identifier. The ‘Activate?’ field is highlighted. 4) If no altitude constraint or course is desired, press the ENT Key to activate. To enter an altitude constraint, proceed to step 5. 5) Turn the large FMS Knob to place the cursor over the ‘VNV’ altitude field. 6) Enter the desired altitude. 7) Press the ENT Key. If the waypoint entered is an airport, the option to select MSL or AGL is now displayed. If the waypoint is not an airport, proceed to step 9. 8) Turn the small FMS Knob to select ‘MSL’ or ‘AGL’. 9) Press the ENT Key. The cursor is now flashing in the VNV offset distance field. 10) Enter the desired offset distance before (-) the waypoint. 11) Press the ENT Key. The ‘Activate?’ field is highlighted. 12) Press the ENT Key to activate. Direct-to Navigation using the PFD 1) Press the Direct-to Key ( ) on the PFD. 2) Turn the large FMS Knob to place the cursor in the desired selection field. 3) Turn the small FMS Knob to begin selecting the desired identifier, location, etc. 4) Press the ENT Key. 5) The cursor is now flashing on ‘ACTIVATE?’. If no altitude constraint or course is desired, press the ENT Key to activate. To enter an altitude constraint, proceed to step 6. 6) Turn the large FMS Knob to place the cursor over the ‘ALT’ altitude field. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 18 GPS Navigation Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index 7) Turn the small FMS Knob to enter the desired altitude. 8) Press the ENT Key. If the waypoint entered is an airport, the option to select MSL or AGL is now displayed. If the waypoint is not an airport, proceed to step 10. 9) Turn the small FMS Knob to select ‘MSL’ or ‘AGL’. 10) Press the ENT Key. The cursor is placed in the ‘OFFSET’ field. 11) Turn the small FMS Knob to enter the desired target altitude offset from the selected Direct-to. 12) Press the ENT Key to highlight ‘Activate?’ or turn the large FMS Knob to highlight the ‘CRS’ field. 13) Turn the small FMS Knob to enter the desired course to the waypoint. 14) Press the ENT Key to highlight ‘ACTIVATE?’. 15) Press the ENT Key again to activate the Direct-to. ACTIVATE A STORED FLIGHT PLAN 1) Press the FPL Key on the MFD and turn the small FMS Knob to display the Flight Plan Catalog Page. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the desired flight plan 4) Press the ACTIVE Softkey. The confirmation window is now displayed. 5) With ‘OK’ highlighted, press the ENT Key to activate the flight plan. To cancel the flight plan activation, turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key. ACTIVATE A FLIGHT PLAN LEG 1) From the Active Flight Plan Page, press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the desired waypoint. 2) Press the ACT LEG Softkey. OR Press the MENU Key, select the ‘Activate Leg’ option from the page menu and press the ENT Key. This step must be used when activating a leg from the PFD. 3) With ‘Activate’ highlighted, press the ENT Key. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 19 GPS Navigation Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index STOP NAVIGATING A FLIGHT PLAN 1) Press the FPL Key to display the Active Flight Plan Page. 2) Press the MENU Key to display the Page Menu Window. 3) Turn the large FMS Knob to highlight ‘Delete Flight Plan’ and press the ENT Key. With ‘OK’ highlighted, press the ENT Key to deactivate the flight plan. This will not delete the stored flight plan, only the active flight plan. VERTICAL NAVIGATION (VNAV) The navigation database only contains altitudes for procedures that call for “Cross at” altitudes. If the procedure states “Expect to cross at,” the altitude is not in the database. In this case the altitude may be entered manually. Large Light Blue Text Small White Text with Altitude Restriction Bar Large White Text Small Light Blue Subdued Text Small Light Blue Text Insertion Point Indicator Cross AT or ABOVE 5,000 ft Cross AT or BELOW 3,000 ft Cross AT 2,300 ft Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 20 GPS Navigation Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index Altitudes associated with arrival and approach procedures are “manually- designated”. This means the system will not use the altitudes loaded with the procedure for giving vertical flight path guidance until designated to do so by the pilot. Note that these altitudes are initially displayed as white text. These altitudes may be “designated” by placing the cursor over the desired altitude and pressing the ENT Key. After designation, the text changes to light blue. Altitudes that have been designated for use in vertical navigation may also be made “non-designated” by placing the cursor over the desired altitude and pressing the CLR Key. The altitude is now displayed only as a reference. It will not be used to give vertical flight path guidance. Other displayed altitudes may change due to re-calculations or rendered invalid as a result of manually changing an altitude to a non-designated altitude. NOTE: Making course changes greater than 90° during a descent with vertical guidance may cause excessive and rapid movement of the vertical deviation indicator, and SVT Pathways. The system updates vertical path guidance continuously using ground speed and the calculated distance to the Bottom of Descent (BOD). Due to turn anticipation guidance (turn-smoothing), distance to the BOD can be affected by course changes greater than approximately 5 degrees. Ground speed can be affected by factors such as shifts in wind direction, aircraft power management, pitch angle, and course changes. Abrupt and/or substantial changes to either the distance to the BOD, ground speed, or both can cause similarly abrupt/substantial changes in vertical path guidance. Because of turn-smoothing, changes to both distance to the BOD and ground speed tend to be more extreme when the BOD is also a waypoint that marks a large course change. These speed and distance changes will be accounted for in the computed required vertical path and reflected in the vertical guidance indications. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 21 GPS Navigation Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index White Text Light Blue Text Light Blue Subdued Text Large Text Altitude calculated by the system estimating the altitude of the aircraft as it passes over the navigation point. This altitude is provided as a reference and is not designated to be used in determining vertical flight path guidance. Altitude has been entered by the pilot. Altitude is designated for use in giving vertical flight path guidance. Altitude does not match the published altitude in navigation database or no published altitude exists. The system cannot use this altitude in determining vertical flight path guidance. Small Text Altitude is not designated to be used in determining vertical flight path guidance. Altitude has been retrieved from the navigation database and is provided as a reference. Altitude is designated for use in giving vertical flight path guidance. Altitude has been retrieved from the navigation database or has been entered by the pilot and matches a published altitude in the navigation database. The system cannot use this altitude in determining vertical flight path guidance. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 22 GPS Navigation Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index Blank Page Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 23 Flight Planning Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index FLIGHT PLANNING WEIGHT PLANNING All procedures apply to the MFD and the Control Unit unless otherwise stated. Entering Weight Parameters The Weight Planning Page is displayed after system power-up. If it is necessary to return to this page, turn the large FMS Knob to select the ‘AUX’ page group. Turn the small FMS Knob to select the Weight Planning Pge. 1) Select the EMPTY WT Softkey to place the cursor in the Basic Empty Weight field. 2) Enter the desired aircraft empty weight. 3) Press the ENT Key. The cursor is now over the ‘PILOT & STORES’ field. 4) Enter the desired weight of Pilot & Stores. 5) Press the ENT Key. 6) Continue repeating these steps until all desired weights have been entered. Entering Fuel Parameters 1) Press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to place the cursor in the ‘FUEL ON BOARD’ field. 3) Turn the small FMS Knob to enter the desired fuel quantity. 4) Press the ENT Key. The cursor is now in the ‘FUEL RESERVES’ field. 5) Turn the small FMS Knob to enter the desired reserve fuel quantity. 6) Press the FMS Knob to remove the cursor. 7) Press the ENT Key. TRIP PLANNING 1) Turn the large FMS Knob to select the ‘AUX’ page group. 2) Turn the small FMS Knob to select the Trip Planning Page. 3) The current ‘PAGE MODE’ is displayed at the top of the page: ‘AUTOMATIC’ or ‘MANUAL’. To change the page mode, press the AUTO or MANUAL Softkey. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 24 Flight Planning Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index 4) For Direct-to planning: a) Press the WPTS Softkey and verify that the starting waypoint field indicates ‘P.POS’ (present position). b) If necessary, press the MENU Key and select ‘Set WPT to Present Position’ to display ‘P.POS’. c) Press the ENT Key and the flashing cursor moves to the ending waypoint field. d) Enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint. Or: For point-to-point planning: a) Enter the identifier of the starting waypoint. b) Once the waypoint’s identifier is entered, press the ENT Key to accept the waypoint. The flashing cursor moves to the ending waypoint. c) Again, enter the identifier of the ending waypoint. d) Press the ENT Key to accept the waypoint. Or: For flight plan leg planning: a) Press the FPL Softkey (at the bottom of the display). b) Turn the small FMS Knob to select the desired flight plan (already stored in memory), by number. c) Turn the large FMS Knob to highlight the ‘LEG’ field. d) Turn the small FMS Knob to select the desired leg of the flight plan, or select ‘CUM’ to apply trip planning calculations to the entire flight plan. Selecting ‘FPL 00’ displays the active flight plan. If an active flight plan is selected, ‘REM’ will be an available option to display planning data for the remainder of the flight plan. NOTE: The page mode must be set to ‘MANUAL’ to perform the following steps. 5) Turn the large FMS Knob to highlight the departure time (DEP TIME) field. NOTE: The departure time on the Trip Planning Page is used for preflight planning. Refer to the Utility Page for the actual flight departure time. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 25 Flight Planning Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index 6) Enter the departure time. Press the ENT Key when finished. Departure time may be entered in local or UTC time, depending upon system settings. 7) The flashing cursor moves to the ground speed (GS) field. Enter the ground speed. Press the ENT Key when finished. Note that in ‘automatic’ page mode, ground speed is provided by the system. 8) The flashing cursor moves to the fuel flow field. Enter the fuel flow. Press the ENT Key when finished. Note that in ‘AUTOMATIC’ page mode, fuel flow is provided by the system. 9) The flashing cursor moves to the fuel onboard field. Enter the fuel onboard. Press the ENT Key when finished. Note that in ‘AUTOMATIC’ page mode, fuel onboard is provided by the fuel totalizer. 10) The flashing cursor moves to the calibrated airspeed (CALIBRATED AS) field. Enter the calibrated airspeed. Press the ENT Key when finished. Note that in ‘AUTOMATIC’ page mode, calibrated airspeed is provided by the system. 11) The flashing cursor moves to the altitude (IND ALTITUDE) field. Enter the altitude. Press the ENT Key when finished. Note that in ‘AUTOMATIC’ page mode, altitude is provided by the system. 12) The flashing cursor moves to the barometric setting (PRESSURE) field. Enter the desired baro setting. Press the ENT Key when finished. Note that in ‘AUTOMATIC’ page mode, the baro setting is provided by the setting entered on the PFD. 13) The flashing cursor moves to the air temperature (TOTAL AIR TEMP) field. Enter the desired air temperature. Press the ENT Key when finished. Note that in ‘AUTOMATIC’ page mode, air temperature is provided by the system outside air temperature. CREATE A USER WAYPOINT DEFINED BY LATITUDE & LONGITUDE 1) Turn the large FMS Knob on the MFD to select the ‘WPT’ page group. 2) Turn the small FMS Knob to select the User WPT Information Page. 3) Press the NEW Softkey. A waypoint is created at the current aircraft position. 4) Enter the desired waypoint name. 5) Press the ENT Key. 6) The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint can be made temporary (deleted automatically when the system is turned off). If the waypoint is to remain in the system, proceed to step 7. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 26 Flight Planning Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index a) Turn the large FMS Knob one click to the left to highlight ‘TEMPORARY’. b) Press the ENT Key to place a check-mark in the box. Turn the large FMS Knob to place the cursor back in the ‘WAYPOINT TYPE’ field. 7) With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to display a list of waypoint types. 8) Turn the small FMS Knob to select LAT/LON (latitude and longitude). 9) Press the ENT Key. CREATE A USER WAYPOINT DEFINED BY RADIALS FROM OTHER WAYPOINTS 1) Turn the large FMS Knob on the MFD to select the ‘WPT’ page group. 2) Turn the small FMS Knob to select the User WPT Information Page. 3) Press the NEW Softkey. A waypoint is created at the current aircraft position. 4) Enter the desired waypoint name. 5) Press the ENT Key. 6) The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint can be made temporary (deleted automatically when the system is turned off). If the waypoint is to remain in the system, proceed to step 7. a) Turn the large FMS Knob one click to the left to highlight ‘TEMPORARY’. b) Press the ENT Key to place a check-mark in the box. Turn the large FMS Knob to place the cursor back in the ‘WAYPOINT TYPE’ field. 7) With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to display a list of waypoint types. 8) Turn the small FMS Knob to select RAD/RAD (radial/radial). 9) Press the ENT Key. 10) The cursor moves to the ‘REFERENCE WAYPOINTS’ field. With the first waypoint name highlighted, use the FMS Knobs to enter the desired waypoint name. Waypoints may also be selected as follows: a) When a flight plan is active, turning the small FMS Knob to the left will display a list of the flight plan waypoints. b) Turn the large FMS Knob to select the desired waypoint. c) Press the ENT Key. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 27 Flight Planning Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index Or: a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed. b) Turn the small FMS Knob to the right to display the ‘NRST’ airports to the aircraft’s current position. c) Turn the large FMS Knob to select the desired waypoint. d) Press the ENT Key. Or: a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed. b) Turn the small FMS Knob to the right to display the ‘RECENT’ waypoints. c) Turn the large FMS Knob to select the desired waypoint. d) Press the ENT Key. Or: a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed. b) Turn the small FMS Knob to the right to display the ‘USER’ waypoints. c) Turn the large FMS Knob to select the desired waypoint. d) Press the ENT Key. 11) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter the desired radial from the reference waypoint. 12) Press the ENT Key. 13) Repeat step 10 to enter the next waypoint name. 14) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field for the second waypoint. Enter the desired radial from the reference waypoint. 15) Press the ENT Key. 16) Press the FMS Knob to remove the flashing cursor. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 28 Flight Planning Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index CREATE A USER WAYPOINT DEFINED BY A RADIAL & DISTANCE FROM ANOTHER WAYPOINT 1) Turn the large FMS Knob on the MFD to select the ‘WPT’ page group. 2) Turn the small FMS Knob to select the User WPT Information Page. 3) Press the NEW Softkey. A waypoint is created at the current aircraft position. 4) Enter the desired waypoint name. 5) Press the ENT Key. 6) The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint can be made temporary (deleted automatically when the system is turned off). If the waypoint is to remain in the system, proceed to step 7. a) Turn the large FMS Knob one click to the left to highlight ‘TEMPORARY’. b) Press the ENT Key to place a check-mark in the box. Turn the large FMS Knob to place the cursor back in the ‘WAYPOINT TYPE’ field. 7) With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to display a list of waypoint types. 8) Turn the small FMS Knob to select RAD/DIS (radial/distance). 9) Press the ENT Key. 10) The cursor moves to the ‘REFERENCE WAYPOINTS’ field. With the first waypoint name highlighted, use the FMS Knobs to enter the desired waypoint name. Waypoints may also be selected as follows: a) When a flight plan is active, turning the small FMS Knob to the left will display a list of the flight plan waypoints. b) Turn the large FMS Knob to select the desired waypoint. c) Press the ENT Key. Or: a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed. b) Turn the small FMS Knob to the right to display the ‘NRST’ airports to the aircraft’s current position. c) Turn the large FMS Knob to select the desired waypoint. d) Press the ENT Key. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 29 Flight Planning Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index Or: a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed. b) Turn the small FMS Knob to the right to display the ‘RECENT’ waypoints. c) Turn the large FMS Knob to select the desired waypoint. d) Press the ENT Key. Or: a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed. b) Turn the small FMS Knob to the right to display the ‘USER’ waypoints. c) Turn the large FMS Knob to select the desired waypoint. d) Press the ENT Key. 11) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter the desired radial from the reference waypoint. 12) Press the ENT Key. 13) The cursor is now displayed in the ‘DIS’ (distance) field. Enter the desired distance from the reference waypoint. 14) Press the ENT Key. 15) Press the FMS Knob to remove the flashing cursor. CREATE A USER WAYPOINT USING THE MAP POINTER 1) Press the Joystick to activate the panning function and pan to the map location of the desired user waypoint. 2) Press the ENT Key. The User Waypoint Information Page is displayed with the captured position. NOTE: If the pointer has highlighted a map database feature, one of three things happens upon pressing the ENT Key: 1) information about the selected feature is displayed instead of initiating a new waypoint, 2) a menu pops up allowing a choice between ‘Review Airspaces’ or ‘Create User Waypoint’, or 3) a new waypoint is initiated with the default name being the selected map item. 3) Enter a user waypoint name (up to six characters). Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 30 Flight Planning Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index 4) Press the ENT Key to accept the selected name. 5) If desired, define the type and location (i.e., LAT/LON, RAD/RAD or RAD/ DIS) of the waypoint. 6) Press the ENT Key to accept the new waypoint. 7) If desired, change the storage method of the waypoint to “TEMPORARY” or “NORMAL” by moving the cursor to “TEMPORARY” and selecting the ENT Key to check or uncheck the box. 8) Press the FMS Knob to remove the flashing cursor. 9) Press the GO BACK Softkey to return to the map page. DELETE A USER WAYPOINT 1) Turn the large FMS Knob to select the ‘WPT’ page group. 2) Turn the small FMS Knob to select the User WPT Information Page. 3) Press the FMS Knob to activate the cursor. 4) Turn the large FMS Knob to the place the cursor in the ‘USER WAYPOINT LIST’ field. 5) Turn the small FMS Knob to highlight the desired waypoint. 6) Press the DELETE Softkey. 7) The message ‘Would you like to delete the user waypoint?’ is displayed. With ‘YES’ highlighted, press the ENT Key. CREATE A FLIGHT PLAN NOTE: When creating a flight plan in the Active Flight Plan Window, the first leg is activated automatically after it is created. Creating an active flight plan: 1) Press the FPL Key. 2) Press the FMS Knob to activate the cursor (only on MFD). 3) Turn the small FMS Knob to display the Waypoint Information Window. (Turning it clockwise displays a blank Waypoint Information Window, turning it counter-clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan, nearest, recent, user, or airway waypoints). Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 31 Flight Planning Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index 4) Enter the identifier, facility, or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key. The active flight plan is modified as each waypoint is entered. 5) Repeat step numbers 3 and 4 to enter each additional flight plan waypoint. 6) When all waypoints have been entered, press the FMS Knob to remove the cursor. Creating a stored flight plan: 1) Press the FPL Key. 2) Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page. 3) Select the NEW Softkey; or press the MENU Key, highlight ‘Create New Flight Plan’, and press the ENT Key to display a blank flight plan for the first empty storage location. 4) Turn the small FMS Knob to display the Waypoint Information Window. (Turning it clockwise displays a blank Waypoint Information Window, turning it counter-clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan, nearest, recent, user, or airway waypoints). 5) Enter the identifier, facility, or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key. 6) Repeat step numbers 4 and 5 to enter each additional flight plan waypoint. 7) When all waypoints have been entered, press the FMS Knob to return to the Flight Plan Catalog Page. The new flight plan is now in the list. IMPORT A FLIGHT PLAN FROM AN SD CARD 1) Insert the SD card containing the flight plan in the top card slot on the MFD. 2) Press the FPL Key on the MFD to display the Active Flight Plan Page on the MFD. 3) Turn the small FMS Knob to select the Flight Plan Catalog Page. 4) Press the FMS Knob to activate the cursor. 5) Turn either FMS Knob to highlight an empty or existing flight plan. 6) Press the IMPORT Softkey. If an empty flight plan is selected, a list of the available flight plans on the SD card will be displayed. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 32 Flight Planning Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index Or: If an existing flight plan is selected, an ‘Overwrite existing flight plan? OK or CANCEL’ prompt is displayed. Press the ENT Key to choose to overwrite the selected flight plan and see a list of the available flight plans on the SD card. If overwriting the existing flight plan is not desired, select ‘CANCEL’ using the FMS Knob, press the ENT Key, select another existing or empty flight plan, and again press the IMPORT Softkey. 7) Turn the small FMS Knob to highlight the desired flight plan for importing. 8) Press the ENT Key. INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN 1) Press the FPL Key to display the active flight plan. 2) If necessary, press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the desired flight plan waypoint. The new waypoint is inserted before the highlighted waypoint (shown by the insertion point indicator). 4) Turn the small FMS Knob. The Waypoint Information Window is now displayed. 5) Enter the new flight plan waypoint by one of the following: a) Enter the user waypoint identifier, facility, or city. b) Press the ENT Key. Or: a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed. b) Turn the small FMS Knob to the right to display the ‘NRST’ airports to the aircraft’s current position. c) Turn the large FMS Knob to select the desired waypoint. d) Press the ENT Key. Or: a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed. b) Turn the small FMS Knob to the right to display the ‘RECENT’ waypoints. c) Turn the large FMS Knob to select the desired waypoint. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 33 Flight Planning Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index d) Press the ENT Key. Or: a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed. b) Turn the small FMS Knob to the right to display the ‘USER’ waypoints. c) Turn the large FMS Knob to select the desired user waypoint. d) Press the ENT Key. 6) Press the ENT Key again to “accept” the waypoint. ENTER AN AIRWAY IN A FLIGHT PLAN 1) Press the FPL Key. 2) Press the FMS Knob to activate the cursor (not required on the PFD). 3) Turn the large FMS Knob to highlight the waypoint after the desired airway entry point. The airway is inserted before the highlighted waypoint (as shown by the insertion point indicator). If this waypoint is not a valid airway entry point, a valid entry point should be entered at this time. 4) Turn the small FMS Knob one click clockwise and press the LD AIRWY Softkey, or press the MENU Key and press “Load Airway”. The Select Airway Page is displayed. The LD AIRWY Softkey or the “Load Airway” menu item is available only when an acceptable airway entry waypoint has been chosen (the waypoint ahead of the cursor position as indicated by the insertion point indicator). 5) Turn the FMS Knob to select the desired airway from the list, and press the ENT Key. Low altitude airways are shown first in the list, followed by “all” altitude airways, and then high altitude airways. 6) Turn the FMS Knob to select the desired airway exit point from the list, and press the ENT Key. ‘LOAD?’ is highlighted. 7) Press the ENT Key. The system returns to editing the flight plan with the new airway inserted. CREATING A USER-DEFINED HOLD AT AN ACTIVE FLIGHT PLAN WAYPOINT 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the FMS Knob to activate the cursor (not required on the PFD) and turn the large FMS Knob to highlight the waypoint for the hold. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 34 Flight Planning Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index 3) Press the MENU Key, highlight ‘Hold At Wpt’, and press the ENT Key. The HOLD AT window appears with the course field highlighted. 4) Use the FMS Knobs to edit the entry course, and press the ENT Key. 5) Use the small FMS Knob to select ‘INBOUND’ or ‘OUTBOUND’ course direction, and press the ENT Key. 6) Use the small FMS Knob to select ‘TIME’ or ‘DIST’ length mode, and press the ENT Key. 7) Use the FMS Knobs to edit the length, and press the ENT Key. 8) Use the small FMS Knob to select ‘RIGHT’ or ‘LEFT’ turn direction, and press the ENT Key. 9) Use the FMS Knobs to edit the Expect Further Clearance Time (EFC TIME), and press the ENT Key. 10) Press the ENT Key while ‘LOAD?’ is highlighted to add the hold into the flight plan. CREATING A USER-DEFINED HOLD AT THE AIRCRAFT PRESENT POSITION 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the MENU Key, highlight ‘Hold At Present Position’, and press the ENT Key. The HOLD AT window appears with the Length mode highlighted. 3) Use the small FMS Knob to select ‘TIME’ or ‘DIST’ length mode, and press the ENT Key. 4) Use the FMS Knobs to edit the length, and press the ENT Key. 5) Use the small FMS Knob to select ‘RIGHT’ or ‘LEFT’ turn direction, and press the ENT Key. 6) Use the FMS Knobs to edit the Expect Further Clearance Time (EFC TIME), and press the ENT Key. 7) Press the ENT Key while ‘ACTIVATE?’ is highlighted to immediately activate the hold. REMOVING A USER-DEFINED HOLD (CREATED AT THE AIRCRAFT P.POS) 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the FMS Knob to activate the cursor (not required on the PFD) and turn the large FMS Knob to highlight the PPOS-H waypoint. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 35 Flight Planning Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index 3) Press the CLR Key. A “Remove Holding Pattern?” confirmation window is displayed. 4) Select ‘OK’ and press the ENT Key. The holding pattern is removed from the active flight plan. Select ‘CANCEL’ and press the ENT Key to cancel the removal of the holding pattern. REMOVING A USER-DEFINED HOLD (CREATED AT AN ACTIVE WAYPOINT) 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the FMS Knob to activate the cursor (not required on the PFD) and turn the large FMS Knob to highlight the HOLD waypoint. 3) Press the CLR Key. A ‘Remove Holding Pattern?’ confirmation window is displayed. 4) Select ‘OK’ and press the ENT Key. The holding pattern is removed from the active flight plan. Select ‘CANCEL’ and press the ENT Key to cancel the removal of the holding pattern. INVERT AN ACTIVE FLIGHT PLAN 1) Press the FPL Key to display the active flight plan. 2) Press the MENU Key to display the Page Menu. 3) Turn the large FMS Knob to highlight ‘Invert Flight Plan’. 4) Press the ENT Key. The original flight plan remains intact in its flight plan catalog storage location. 5) With ‘OK’ highlighted, press the ENT Key to invert the flight plan. REMOVE A DEPARTURE, ARRIVAL, APPROACH, OR AIRWAY FROM A FLIGHT PLAN 1) Press the FPL Key to display the active flight plan. Press the FMS Knob to activate the cursor. Or, for a stored flight plan: a) Press the MFD FPL Key and turn the small FMS Knob to select the Flight Plan Catalog Page. b) Press the FMS Knob to activate the cursor. c) Turn the large FMS Knob to highlight the desired flight plan. d) Press the EDIT Softkey. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 36 Flight Planning Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index 2) Turn the large FMS Knob to highlight the title for the approach, departure, arrival, or airway to be deleted. Titles appear in white directly above the procedure’s waypoints. 3) Press the CLR Key to display a confirmation window. 4) With ‘OK’ highlighted, press the ENT Key to remove the selected procedure or airway. STORE A FLIGHT PLAN 1) After creating a flight plan on either the PFD or MFD, it may be saved by pressing the MENU Key. 2) Turn the large FMS Knob to highlight ‘Store Flight Plan’ and press the ENT Key. 3) With ‘OK’ highlighted, press the ENT Key to store the flight plan. EDIT A STORED FLIGHT PLAN 1) Press the FPL Key for the MFD and turn the small FMS Knob to display the Flight Plan Catalog Page. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the desired flight plan. 4) Press the EDIT Softkey. 5) Turn the large FMS Knob to place the cursor in the desired location. 6) Enter the changes, then press the ENT Key. 7) Press the FMS Knob to return to the Flight Plan Catalog Page. DELETE A WAYPOINT FROM THE FLIGHT PLAN 1) Press the FPL Key to display the active flight plan. Press the FMS Knob to activate the cursor. Or, for a stored flight plan: a) Press the FPL Key of the MFD and turn the small FMS Knob to select the Flight Plan Catalog Page. b) Press the FMS Knob to activate the cursor. c) Turn the large FMS Knob to highlight the desired flight plan. d) Press the EDIT Softkey. 2) Turn the large FMS Knob to highlight the waypoint to be deleted. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 37 Flight Planning Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index 3) Press the CLR Key to display a ‘REMOVE (Wpt Name)?’ confirmation window. 4) With ‘OK’ highlighted, press the ENT Key to remove the waypoint. To cancel the delete request, turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key. 5) Once all changes have been made, press the FMS Knob to remove the cursor. INVERT AND ACTIVATE A STORED FLIGHT PLAN 1) Press the FPL Key for the MFD. 2) Turn the small FMS Knob to select the Flight Plan Catalog Page. 3) Press the FMS Knob to activate the cursor. 4) Turn the large FMS Knob to highlight the desired flight plan. 5) Press the INVERT Softkey. ‘Invert and activate stored flight plan?’ is displayed. 6) With ‘OK’ highlighted, press the ENT Key. The selected flight plan is now inverted and activated. The original flight plan remains intact in its flight plan catalog storage location. COPY A FLIGHT PLAN 1) Press the FPL Key for the MFD. 2) Turn the small FMS Knob to select the Flight Plan Catalog Page. 3) Press the FMS Knob to activate the cursor. 4) Turn the large FMS Knob to highlight the flight plan to be copied. 5) Press the COPY Softkey. A ‘Copy to flight plan #?’ confirmation window is displayed. 6) With ‘OK’ highlighted, press the ENT Key to copy the flight plan. To cancel, turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key. DELETE A FLIGHT PLAN 1) Press the FPL Key for the MFD. 2) Turn the small FMS Knob to select the Flight Plan Catalog Page. 3) Press the FMS Knob to activate the cursor. 4) Turn the large FMS Knob to highlight the flight plan to be deleted. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 38 Flight Planning Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index 5) Press the DELETE Softkey. A ‘Delete flight plan #?’ confirmation window is displayed. 6) With ‘OK’ highlighted, press the ENT Key to delete the flight plan. To cancel, turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key. GRAPHICAL FLIGHT PLAN CREATION 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Press the Joystick to activate the map pointer. Use the Joystick to move the pointer to the desired point on the map to be inserted as a waypoint in the flight plan. 3) The default insertion point is at the end of the flight plan. If the selected waypoint is to be placed anywhere other than the end of the flight plan, press the FMS Knob to activate the cursor. Waypoints are inserted ABOVE the cursor (as indicated by the insertion point indicator). Turn the large FMS Knob to select the desired insertion point. 4) Press the LD WPT Softkey. The selected waypoint is inserted at the selected point. The default user waypoint naming is USR000, USR001, USR002, and so on. 5) To change the user waypoint name, follow the procedure for modifying a user waypoint. EXPORT A FLIGHT PLAN TO AN SD CARD 1) Insert the SD card into the top card slot on the MFD. 2) Press the FPL Key on the Control Unit to display the Active Flight Plan Page on the MFD. 3) Turn the small FMS Knob to select the Flight Plan Catalog Page. 4) Press the FMS Knob to activate the cursor. 5) Turn the large FMS Knob to highlight the flight plan to be exported. 6) Press the EXPORT Softkey. 7) Press the ENT Key to confirm the export. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 39 Procedures Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index PROCEDURES LOAD AND ACTIVATE A DEPARTURE PROCEDURE 1) Press the PROC Key. 2) Turn the large FMS Knob to highlight ‘SELECT DEPARTURE’. 3) Press the ENT Key. The cursor is displayed in the ‘DEPARTURE’ field with a list of available departures. 4) Turn the large FMS Knob to highlight the desired departure. 5) Press the ENT Key. A list of runways may be displayed for the departure. If so, turn either FMS Knob to select the desired runway. 6) Press the ENT Key. The cursor is displayed in the ‘TRANSITION’ field with a list of available transitions. 7) Turn the large FMS Knob to highlight the desired transition. 8) Press the ENT Key. 9) With ‘LOAD?’ highlighted, press the ENT Key. The departure is active when the flight plan is active. ACTIVATE A DEPARTURE LEG 1) Press the FPL Key for the MFD to display the active flight plan. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the desired waypoint within the departure. 4) Press the ACT LEG Softkey. A confirmation window showing the selected leg is displayed. 5) With ‘ACTIVATE’ highlighted, press the ENT Key. LOAD AN ARRIVAL PROCEDURE 1) Press the PROC Key. 2) Turn the large FMS Knob to highlight ‘SELECT ARRIVAL’. 3) Press the ENT Key. The cursor is displayed in the ‘ARRIVAL’ field with a list of available arrivals. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 40 Procedures Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index 4) Turn the large FMS Knob to highlight the desired arrival. 5) Press the ENT Key. A list of transitions is displayed for the selected arrival. 6) Turn either FMS Knob to select the desired transition. 7) Press the ENT Key. A list of runways may be displayed for the selected arrival. 8) Turn the large FMS Knob to highlight the desired runway. 9) Press the ENT Key. 10) With ‘LOAD?’ highlighted, press the ENT Key. 11) The arrival becomes part of the active flight plan. ACTIVATE AN ARRIVAL LEG 1) Press the FPL Key to display the active flight plan. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the desired waypoint within the arrival. 4) Press the ACT LEG Softkey. A confirmation window showing the selected leg is displayed. 5) With ‘ACTIVATE’ highlighted, press the ENT Key. LOAD AND/OR ACTIVATE AN APPROACH PROCEDURE NOTE: If certain GPS parameters (SBAS, RAIM, etc.) are not available, some published approach procedures for the desired airport may not be displayed in the list of available approaches. 1) Press the PROC Key. 2) Turn the large FMS Knob to highlight ‘SELECT APPROACH’. 3) Press the ENT Key. A list of available approaches for the destination airport is displayed. 4) Turn either FMS Knob to highlight the desired approach. 5) Press the ENT Key. A list of available transitions for the selected approach procedure is now displayed. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 41 Procedures Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index 6) Turn either FMS Knob to select the desired transition. The “Vectors” option assumes vectors will be received to the final course segment of the approach and will provide navigation guidance relative to the final approach course. 7) Press the ENT Key. The cursor moves to the MINIMUMS field. 8) If desired, the DA/MDA for the selected approach procedure may be entered and displayed on the PFD. Turn the small FMS Knob in the direction of the green arrow to change the display from OFF to BARO or TEMP COMP. 9) Press the ENT Key. The cursor moves to the altitude field. Turn the small FMS Knob to enter the published DA/MDA for the selected approach procedure. 10) Press the ENT Key. If BARO or OFF was selected step 8, proceed to step 11. If TEMP COMP was selected in step 8, the cursor moves to the ‘TEMP AT....” field. Turn the small FMS Knob to enter the temperature at the destination airport. The temperature compensated altitude minimum is displayed below the previously enter minimum altitude value. 11) Press the ENT Key. ‘LOAD? or ACTIVATE?’ is now displayed with ‘LOAD?’ highlighted. 12) Turn the large FMS Knob to select either ‘LOAD?’ or ‘ACTIVATE?’. Selecting ‘LOAD?’ enters the selected approach procedure into the active flight plan, but is not currently active. Selecting ‘ACTIVATE?’ enters the selected approach procedure into the active flight plan and activates the first leg of the approach. 13) Press the ENT Key. ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN 1) Press the PROC Key. 2) Turn the large FMS Knob to highlight ‘ACTIVATE APPROACH’. 3) Press the ENT Key. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 42 Procedures Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index ACTIVATE A VECTOR TO FINAL APPROACH FIX 1) Press the PROC Key. 2) Turn the large FMS Knob to highlight ‘ACTIVATE VECTOR-TO-FINAL’. 3) Press the ENT Key. 4) The final approach course becomes the active leg. ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN 1) Press the PROC Key. 2) Turn the large FMS Knob to highlight ‘ACTIVATE MISSED APPROACH’. 3) Press the ENT Key. A confirmation window is displayed. 4) With ‘ACTIVATE’ highlighted, press the ENT Key. Or: Press the go-around button: TEMPERATURE COMPENSATED ALTITUDE When temperature compensated altitude is enabled for the loaded approach, the altitudes associated with the approach waypoints are displayed in slanted text. Altitudes Displayed Without Temperature Compensation Altitudes Displayed With Temperature Compensation Enabling temperature compensated altitude: 1) From the Active Flight Plan Page, press the MENU Key. The Page Menu is displayed. 2) Turn the FMS Knob to highlight ‘Temperature Compensation’. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 43 Procedures Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index 3) Press the ENT Key. The TEMPERATURE COMPENSATION Window is displayed. 4) Use the small FMS Knob to select the temperature at the <airport>. The compensated altitude is computed as the temperature is selected. 5) Press the ENT Key. ‘ACTIVATE COMPENSATION?’ is highlighted. 6) Press the ENT Key. The compensated altitudes for the approach are shown in the flight plan. Disabling temperature compensated altitude: 1) From the Active Flight Plan Page, press the MENU Key. The Page Menu is displayed. 2) Turn the FMS Knob to highlight ‘Temperature Compensation’. 3) Press the ENT Key. The TEMPERATURE COMPENSATION Window is displayed. 4) Press the ENT Key. ‘CANCEL COMPENSATION?’ is highlighted. 5) Press the ENT Key. The temperature compensated altitude at the FAF is cancelled. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 44 Procedures Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index Blank Page Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 45 Hazard Avoidance Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index HAZARD AVOIDANCE Customizing THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1) With the Navigation Map Page displayed, press the MENU Key to display the Navigation Map Page Menu. The cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Menu is displayed. Turn the small FMS Knob to select ‘Weather’ to customize the display of weather features. Select ‘Traffic’ to customize the display of traffic. 3) Press the small FMS Knob to return to the Navigation Map Page. STORMSCOPE® (OPTIONAL) WARNING: Do not rely on information from the lightning detection system display as the sole basis for hazard weather avoidance. Range limitations and interference may cause the system to display inaccurate or incomplete information. Refer to the documentation from the lightning detection system manufacturer for detailed information about the system. Displaying Stormscope Lightning Data on the Navigation Map Page 1) Press the MAP Softkey. 2) Press the STRMSCP Softkey. Press the STRMSCP Softkey again to remove Stormscope Lightning Data from the Navigation Map Page. Lightning Age Symbol Strike is less than 6 seconds old Strike is between 6 and 60 seconds old Strike is between 1 and 2 minutes old Strike is between 2 and 3 minutes old Select ‘Cell’ or ‘Strike’ as the Stormscope Lightning Mode 1) Press the MENU Key (with the Navigation Map Page displayed). 2) Turn either FMS Knob to highlight ‘Map Setup’. 3) Press the ENT Key. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 46 Hazard Avoidance Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index 4) Turn the small FMS Knob to highlight ‘Weather’. 5) Press the ENT Key. 6) Turn the large FMS Knob to place the cursor in the ‘STRMSCP MODE’ field. 7) Turn the small FMS Knob to display the ‘Cell/Strike’ window. 8) Turn either FMS Knob to select ‘Cell’ or ‘Strike’. Press the ENT Key. 9) Push the FMS Knob to return to the Navigation Map Page. Clear Stormscope Lightning Data from the Navigation Map Page 1) Press the MENU Key (with the Navigation Map Page displayed). 2) Turn either FMS Knob to highlight the ‘Clear Stormscope® Lightning’ field and press the ENT Key. NOTE: If heading input is lost, strikes and/or cells must be cleared manually after the execution of each turn. This is to ensure that the strike and/or cell positions are depicted accurately in relation to the nose of the aircraft. Stormscope Page 1) Turn the large FMS Knob until the Map Page group is selected. 2) Turn the small FMS Knob until the Stormscope Page is selected. Change the Stormscope Lightning Mode Between ‘Cell’ and ‘Strike’ 1) Select the Stormscope Page. 2) Press the MODE Softkey. The CELL and STRIKE Softkeys are displayed. Press the CELL Softkey to display ‘CELL’ data or press the STRIKE Softkey to display ‘STRIKE’ data. ‘CELL’ or ‘STRIKE’ is displayed in the mode box located in the upper left corner of the Stormscope Page. NOTE: “Cell mode” uses a clustering program to identify clusters of electrical activity that indicate cells. Change the Viewing Mode Between 360˚ and 120˚ 1) Select the Stormscope Page. 2) Press the VIEW Softkey. The 360 and ARC Softkeys are displayed. Press the 360 Softkey to display a 360˚ viewing area or press the ARC Softkey to display a 120˚ viewing area. Press the CLEAR Softkey to remove all Stormscope lightning data from the display. Garmin G1000 Cockpit Reference Guide for the Piper PA-34-220T Seneca 190-01405-00 Rev. A 47 Hazard Avoidance Flight Instruments EIS Nav/Com/ XPDR/Audio GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/Alerts Appendix Index SIRIUSXM WEATHER (OPTIONAL) WARNING: Do not use data link weather information for maneuvering in, near or around areas of hazardous weather. Information contained within data link weather products may not accurately depict current weather condi- tions. WARNING: Do not use the indicated data link weather product age to determine the age of the weather information shown by the data link weather product. Due to time delays inherent in gathering and processing weather data for data link transmission, the weather information shown by the data link weather product may be significantly older than the indicated weather product age. Displaying SiriusXM Weather on the Navigation Map Page 1) Press the MAP Softkey. 2) Press the NEXRAD or XM LTNG Softkey to display the desired weather. Press the applicable softkey again to remove weather data from the Navigation Map Page. Display METAR and TAF information on the Airport Information Page 1) Turn the large FMS Knob to select the WPT Page Group. 2) Turn the small FMS Knob to select the Airport Information Page. 3) P