Garmin G1000 Manual
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190-00709-04 Rev. AGarmin G1000 Pilot’s Guide for the Socata TBM 850247 FLIGHT MANAGEMENT Figure 5-88 Expanded/Collapsed AirwaysQ3.FEPOT Airway Collapsed View Expanded View Collapsing/expanding the airways in the active flight plan: 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 ‘Collapse Airways’ or ‘Expand Airways’, and press the ENT Key. The airways are collapsed/expanded. CLOSEST POINT OF FPL ‘Closest Point of FPL’ calculates the bearing and closest distance at which a flight plan passes a reference waypoint, and creates a new user waypoint along the flight plan at the location closes\ t to a chosen reference waypoint. Determining the closest point along the active flight plan to a selected waypoint: 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 ‘Closest Point Of FPL’’, and press the ENT Key. A window appears with the reference waypoint field highlighted. 3) Enter the identifier of the reference waypoint and press the ENT Key. The G1000 displays the bearing (BRG) and distance (DIS) to the closest point along the flight plan to the selected reference waypoint and creates a user waypoint at this location. The name for the new user waypoint is derived from the identifier of the reference waypoint.
Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04 Rev. A248 FLIGHT MANAGEMENT 5.7 VERTICAL NAVIGATION NOTE: The G1000 supports vertical navigation for all lateral leg types except f\ or CA, CI, FA, FM, HA, HM, PI, VA, VD, VI, VR, and VM. Vertical constraints are not retained in stored flight plans. The G1000 system Vertical Navigation (VNV) feature provides vertical profile guidance during the enroute and teminal phases of flight. Guidance based on specified altitudes\ at waypoints in the active flight plan or to a direct-to waypoint is provided. It includes vertical path guidance to a descending path, which is provided as a linear deviation from the desired path. The desired path is defined by a line joining two waypoints with specified altitudes or as a vertical angle from a specified waypoint/altitude. The vertical waypoints are integrated into the active flight plan. Both manual and autopilot-coupled guidance are supported. Figure 5-89 Enabling/Disabling Vertical Navigation Current Vertical Navigation Profile Disabled (fields dashed) ENBL VNV Softkey CNCL VNV Softkey Current Vertical Navigation ProfileEnabled (valid data) Enabling VNV guidance: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Select the ENBL VNV Softkey; or press the MENU Key, highlight ‘Enable VNV’, and press the ENT Key. Vertical navigation is enabled, and vertical guidance begins with the waypoint shown in the CURRENT VNV PROFILE box (defaults first waypoint in the active flight plan with an altitude enabled for vertica\ l navigation (e.g., HABUK)).
190-00709-04 Rev. AGarmin G1000 Pilot’s Guide for the Socata TBM 850249 FLIGHT MANAGEMENT Disabling VNV guidance: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Select the CNCL VNV Softkey; or press the MENU Key, highlight ‘Cancel VNV’, and press the ENT Key. Vertical navigation is disabled. Canceling vertical navigation results in vertical deviation (V DEV), vertical speed required (VS REQ), and time to top of descent/bottom of descent (TIME TO TOD/BOD) going invalid. \ The Vertical Deviation Indicator (VDI) and Vertical Speed Required Indication (VSRI) on the PFD are removed, and the V DEV, VS REQ, and TIME TO TOD items displayed in the CURRENT VNV PROFILE box are dashed. VNV remains disabled until manually enabled. Vertical guidance in reversionary mode can only be enabled for a direct-to waypoint. The G1000 allows a vertical navigation direct-to to any waypoint in the active flight plan with an altitude constraint “designated” for vertical guidance. Selecting the VNV Direct-to Softkey on the Active Flight Plan Page allows the flight plan to be flown, while vertical guidance based on\ the altitude constraint at the VNV direct-to waypoint is provided. The altitude change begins immediately and is spread along the flight plan from current position to the vertical direct-to waypoint, not just along the leg for the direct-to waypoint. A direct-to with altitude constraint activated by pressing the Direct-to Key also provides vertical guidance, but would bypass flight plan waypoints between the current position in the flight plan and the direct-to waypoint. A top of descent (TOD) point is computed based on the default flight path angle; desc\ ent begins once the TOD is reached. Figure 5-90 Vertical Navigation Direct-To Current Vertical Navigation Profile Prior to VNV Direct-to VNV Direct-To Softkey VNV PROF Softkey Current Vertical Navigation ProfileAfter VNV Direct-to
Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04 Rev. A250 FLIGHT MANAGEMENT Activating a vertical navigation direct-to: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight the desired waypoint. NOTE: The selected waypoint must have a designated altitude constraint (light blue number)\ to be used. If not, the first waypoint in the flight plan with a designated altitude constraint is se\ lected. 3) Select the VNV Direct-To Softkey; or press the MENU Key, highlight ‘VNV Direct-To’, and press the ENT Key. An ‘Activate vertical Direct-to to: NNNNNFT at XXXXXX?’ confirmation window is displayed. 4) Press the ENT Key. Vertical guidance begins to the altitude constraint for the selected waypoint. 5) Press the FMS Knob to remove the flashing cursor. The vertical navigation profile can be modified by directly entering a vertical speed target (VS TGT) and/or flight path angle (FPA) in the CURRENT VNV PROFILE box. Modifying the VS TGT and FPA: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Select the VNV PROF Softkey; or press the MENU Key, highlight ‘Select VNV Profile Window’, and press the ENT Key. The cursor is now located in the CURRENT VNV PROFILE box. 3) Turn the FMS Knobs as needed to edit the values. 4) Press the FMS Knob to remove the flashing cursor. ALTITUDE CONSTRAINTS 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, manually entered 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. Large Light Blue Text Small White Text with Altitude Restriction Bar Large White Text Small Light Blue Subdued Text Small Light Blue Text Figure 5-91 Waypoint Altitude Constraints Cross AT or ABOVE 5,000 ft Cross AT or BELOW 3,000 ft Cross AT 2,300 ft Altitude Constraint Examples Displayed Text Examples
190-00709-04 Rev. AGarmin G1000 Pilot’s Guide for the Socata TBM 850251 FLIGHT MANAGEMENT White TextLight Blue TextLight 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 manually. 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 because of an invalid constraint condition. 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 manually and matches a published altitude in the navigation database. The system cannot use this altitude in determining vertical speed and deviation guidance because of an invalid constraint condition. Table 5-8 Altitude Constraint Size and Color Coding Altitudes associated with arrival and approach procedures are not “auto-designated”. This means the system does not automatically use the altitudes loaded with the arrival or appr\ oach for giving vertical speed and deviation guidance. Note that these altitudes are displayed as white text up to, but not including, the FAF. The FAF is always a “reference only” altitude and cannot be designated, unless the selected app\ roach does not provide vertical guidance. In this case, the FAF altitude can be designated. Altitudes that have been designated for use in vertical guidance can be \ “un-designated” using the CLR Key. The altitude is now displayed only as a reference. It is not used to give vertical guidance. Other displayed altitudes may change due to re-calculations or be rendered invalid as a result of manually changing an altitude to a non-designated altitude. Designating a waypoint altitude to be used for vertical guidance: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Press the FMS Knob, and turn to highlight the desired waypoint altitude. 3) Turn the small FMS Knob to enter editing mode. 4) Press the ENT Key. The altitude is now shown in blue, indicating it is usable for vertical guidance. Designating a procedure waypoint altitude to be used for vertical guidance: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Press the FMS Knob, and turn to highlight the desired waypoint altitude. 3) Press the ENT Key. The altitude is now shown in blue, indicating it is usable for vertical guidance. Altitude constraints are displayed and entered in feet mean sea level (MSL) values to the nearest hundred. An altitude constraint in feet above ground level (AGL) format is supported for airports. When a database altitude restriction is displayed, the G1000 allows entry of a different altitude when creating a waypoint, effectively overriding the database restriction (only before the FAF). When a database altitude restriction of type “AT or ABOVE” or “AT or BELOW” is activated, the system uses the “AT” portion of the restriction to define the vertical profile.
Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04 Rev. A252 FLIGHT MANAGEMENT An altitude constraint is invalid if: • Meeting the constraint requires the aircraft to climb • Meeting the constraint requires the maximum flight path angle or maximum vertical speed to be exceeded • The altitude constraint results in a TOD behind the aircraft present position • The constraint is within a leg type for which altitude constraints are not supported • The altitude constraint is added to the FAF of an approach that provides vertical guidance (i.e., ILS or GPS SBAS approach) • The altitude constraint is added to a waypoint past the FAF. Entering/modifying an altitude constraint: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Press the FMS Knob, and turn to highlight the desired waypoint altitude constraint. 3) Enter an altitude constraint value using the FMS Knobs. To enter altitudes as a flight level, turn the small FMS Knob counter-clockwise past zero or clockwise past 9 on the first character, and the system automatically changes to show units of Flight Level. Turn the large FMS Knob clockwise to highlight the first zero and enter the three digit flight level. 4) Press the ENT Key to accept the altitude constraint; if the selected waypoint is an airport, an additional choice is displayed. Turn the small FMS Knob to choose ‘MSL’ or ‘AGL’, and press the ENT Key to accept the altitude. Altitude constraints can be modified or deleted after having been adde\ d to the flight plan. In the event an altitude constraint is deleted and the navigation database contains a\ n altitude restriction for the lateral waypoint, the G1000 displays the altitude restriction from the database provided no predicted altitude can be provided. The G1000 also provides a way to reinstate a published altitude constraint that has been edited. Deleting (un-designating) an altitude constraint provided by the navigation database: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Press the FMS Knob, and turn to highlight the desired waypoint altitude constraint. 3) Press the CLR Key. A ‘Remove VNV altitude constraint?’ confirmation window is displayed. 4) Select ‘OK’ and press the ENT Key. Deleting an altitude constraint that has been manually entered: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Press the FMS Knob, and turn to highlight the desired waypoint altitude constraint. 3) Press the CLR Key. A ‘Remove or Revert to published VNV altitude of nnnnnFT?’ confirmation window is displayed. 4) Select ‘REMOVE’ and press the ENT Key. The manually entered altitude is deleted (it is replaced by a system calculated altitude, if available).
190-00709-04 Rev. AGarmin G1000 Pilot’s Guide for the Socata TBM 850253 FLIGHT MANAGEMENT Reverting a manually entered altitude constraint back to the navigation database value: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Press the FMS Knob, and turn to highlight the desired waypoint altitude constraint. 3) Press the CLR Key. A ‘Remove or Revert to published VNV altitude of nnnnnFT?’ confirmation window is displayed. 4) Select ‘REVERT’ and press the ENT Key. The altitude is changed to the navigation database value. 5) Press the FMS Knob to remove the flashing cursor. Modifying a system calculated altitude constraint: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Press the FMS Knob, and turn to highlight the desired waypoint altitude constraint. 3) Press the CLR Key. An ‘Edit or Revert to published VNV altitude of nnnnnFT?’ confirmation window is displayed. 4) Select ‘EDIT’ and press the ENT Key. 5) Edit the value using the FMS Knobs, and press the ENT Key. 6) Press the FMS Knob to remove the flashing cursor.
Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04 Rev. A254 FLIGHT MANAGEMENT 5.8 PROCEDURES The G1000 can access the whole range of instrument procedures available. Departures (DPs), arrivals (STARs), and non-precision and precision approaches (APPRs) are stored within the database and can be loaded using the Procedures (PROC) Key. The selected procedure for the departure or arrival airport is added to the active flight plan. No waypoints\ are required to be in the active flight plan to load procedures; however, if the departure and arrival airport are already loaded, the procedure loading window defaults to the appropriate airport, saving some time selecting the correct airport on the Procedure Loading Page. Whenever an approach is selected, the choice to either “load” or “activate” \ is given. “Loading” adds the approach to the end of the flight plan without immediately using it for na\ vigation guidance. This allows continued navigation via the intermediate waypoints in the original flight plan, but keeps the procedure available on the Active Flight Plan Page for quick activation when needed. “Activating” also adds the procedure to the end of the flight plan but immediately begins to provide guidance to the first waypoint in the approach. DEPARTURES A Departure Procedure (DP) is loaded at the departure airport in the flight plan. Only one departure can be loaded at a time in a flight plan. If a departure is loaded when another departure is already in the active flight plan, the new departure replaces the previous departure. The route is defined by selection of a departure, the transition waypoints, and a runway. LOADING A DEPARTURE INTO THE ACTIVE FLIGHT PLAN Loading a departure into the active flight plan using the PROC Key: 1) Press the PROC Key. The Procedures Window is displayed. 2) Highlight ‘SELECT DEPARTURE’. 3) Press the ENT Key. The Departure Loading Page is displayed. 4) Use the FMS Knob to select an airport and press the ENT Key. 5) Select a departure from the list and press the ENT Key. 6) Select a runway (if required) and press the ENT Key. 7) Select a transition (if required) and press the ENT Key. ‘LOAD?’ is highlighted. 8) Press the ENT Key to load the departure procedure.
190-00709-04 Rev. AGarmin G1000 Pilot’s Guide for the Socata TBM 850255 FLIGHT MANAGEMENT Figure 5-92 Departure SelectionDeparture Airport Departure Preview Available Procedure Actions Departure Choices Loaded Procedures Procedure Loading Page Selection SoftkeysFigure 5-93 Departure Loading Loaded Departure Selected Departure
Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04 Rev. A256 FLIGHT MANAGEMENT Viewing available departures at an airport: 1) From the Airport Information Page (first page in the WPT group), select the DP Softkey. The Departure Information Page is displayed, defaulting to the airport displayed on the Airport information Page. 2) To select another airport, press the FMS Knob to activate the cursor, enter an identifier/facility name/city, and press the ENT Key. 3) Turn the large FMS Knob to highlight the Departure. The departure is previewed on the map. 4) Turn the small FMS Knob to view the available departures. Press the ENT Key to select the departure. The cursor moves to the Runway box. The departure is previewed on the map. 5) Turn the small FMS Knob to view the available runways. Press the ENT Key to select the runway. The cursor moves to the Transition box (only if there are available transitions). The departure is previewed on the map. 6) Turn the small FMS Knob to view the available transitions. Press the ENT Key to select the transition. The cursor moves to the Sequence box. The departure is previewed on the map. 7) Select the INFO-x Softkey to return to the Airport Information Page. REMOVING A DEPARTURE FROM THE ACTIVE FLIGHT PLAN When plans change while flying IFR, departures can be easily removed from the Active Flight Plan. Removing a departure procedure from the active flight plan: 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, and highlight ‘Remove Departure’. 3) Press the ENT Key. A confirmation window is displayed listing the departure procedure. 4) With ‘OK’ highlighted, press the ENT Key. To cancel the removal request, highlight ‘CANCEL’ and press the ENT Key. Or: 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, and turn to highlight the departure header in the active flight plan.\ 3) Press the CLR Key. A confirmation window is displayed listing the departure procedure. 4) With ‘OK’ highlighted, press the ENT Key. To cancel the removal request, highlight ‘CANCEL’ and press the ENT Key. 5) Press the FMS Knob to remove the flashing cursor.