[. . . ] Integrated Flight Deck Cockpit Reference Guide Socata TBM 850 SYSTEM OVERVIEW FLIGHT INSTRUMENTS ENGINE & AIRFRAME SYSTEMS NAV/COM/TRANSPONDER AUDIO PANEL AUTOMATIC FLIGHT CONTROL NAVIGATION FLIGHT PLANNING PROCEDURES HAZARD AVOIDANCE ADDITIONAL FEATURES ABNORMAL OPERATIONS ANNUNCIATIONS & ALERTS INDEX Copyright © 2007 Garmin Ltd. This manual reflects the operation of System Software version 0719. 00 or later for the Socata TBM 850. Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions. Garmin International, Inc. , 1200 East 151st Street, Olathe, Kansas 66062, U. S. A. [. . . ] 2) Turn the small FMS Knob to the left to display a list of flight plan waypoints as shown in Figure 7-8. Figure 7-8 Flight Plan Waypoint List (PFD) 3) Turn the large FMS Knob to select the desired waypoint. Select a Direct-to Destination to a Nearest Airport 1) Press the Direct-to ( ) Key. The list is only populated when navigating a flight plan. 3) Turn the small FMS Knob to the right to display the `NRST' airports to the aircraft's current position as shown in Figure 7-9. 7-4 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A SECTION 7 ­ NAVIGATION 4) Turn the large FMS Knob to select the desired airport. Select a Direct-to Destination to a Recently Entered Identifier 1) Press the Direct-to ( ) Key. The list is only populated when navigating a flight plan. 7. 3 NAVIGATING AN EXAMPLE FLIGHT PLAN NOTE: The following example flight plan is for instructional purposes only. All database information depicted should be considered not current. Figure 7-10 Recently Entered Waypoints List (PFD) 3) Turn the small FMS Knob to the right to display the `RECENT' waypoints as shown in Figure 7-10. 3) Press the ENT Key to cancel the direct-to. The following discussion is an example of navigating a flight plan with the WAAS capable GPS system while the G1000 provides vertical guidance through descents. A lateral flight plan (LNAV) would be navigated in much the same way, but would not include vertical guidance when the final approach course is active. The example is a flight plan from KMKC to KCOS filed using the TIFTO2 departure, various Victor Airways, and the DBRY1 arrival with the transition at TBE. A missed approach will be executed at the Missed Approach Point (MAP). A few enroute changes are demonstrated. NOTE: If the loaded arrival procedure has published altitudes contained in the navigation database, these are for turbojet aircraft only. Accept or change these values as desired to meet the requirements of the clearance. 1) Prior to departure, the TIFTO2 departure, the airways, and the DBRY1 arrival at KCOS are loaded. Note the magenta arrow in Figure 7-11 indicating the active departure leg. After takeoff, ATC assigns a heading of 240º. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 7-5 SECTION 7 ­ NAVIGATION 2) Figure 7-11 shows the aircraft on the assigned heading of 240º. `TERM' (Terminal) is the current CDI flight phase displayed on the HSI indicating 1. 0 nm CDI scaling. The aircraft turns to heading 290° as seen in Figure 7-12. Figure 7-12 Assigned Heading of 290º Figure 7-11 Assigned Heading of 240º 7-6 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A SECTION 7 ­ NAVIGATION 4) V4 is now be entered into the flight plan. Turn the large FMS Knob to highlight the desired flight plan insertion point as shown in Figure 7-13. The V4 entry point (TOP) will be placed immediately above the highlighted waypoint (SLN). c) Turn the small FMS Knob to display the Waypoint Information Window. Enter the desired entry point for V4, in this case Topeka VOR (TOP) is used as shown in Figure 7-14. Figure 7-14 Entering V4 Entry Point d) Press the ENT Key. [. . . ] SLCT FREQ ­ Select appropriate The system notifies the pilot to load the approach frequency for the appropriate frequency for approach. SLCT NAV ­ Select NAV on CDI for The system notifies the pilot to set the CDI to the correct NAV receiver. PTK FAIL ­ Parallel track unavailable: Bad parallel track geometry. PTK FAIL ­ Parallel track unavailable: Invalid leg type for parallel offset. [. . . ]