User manual GARMIN G1000 TIGERAG-5B PILOTS GUIDE-PART1OF2

[. . . ] Tel: 913/397. 8200 Fax: 913/397. 8282 Garmin AT, Inc. , 2345 Turner Road SE, Salem, OR 97302, U. S. A. Tel: 503/391. 3411 Fax 503/364. 2138 Garmin (Europe) Ltd, Liberty House, Bulls Copse Road, Hounsdown Business Park, Southampton, SO40 9RB, U. K. Tel: 44/0870. 8501241 Fax: 44/0870. 8501251 Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan Tel: 886/02. 2642. 9199 Fax: 886/02. 2642. 9099 Web Site Address: www. garmin. com Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored in any storage medium, for any purpose without the express written permission of Garmin. [. . . ] A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 7-13 SECTION 7 ­ NAVIGATION h) With `LOAD?' highlighted, again press the ENT Key. The selected approach is added to the flight plan as seen in Figure 7-33. b) Turn the large FMS Knob to place the cursor in the altitude field associated with the IAF at HABUK as in Figure 7-34. Figure 7-34 Designate HABUK Altitude Constraint Figure 7-33 Loaded Approach 13) Note the altitude constraints associated with each of the approach waypoints as seen in Figure 7-33. These altitudes are loaded from the database and are initially displayed as white text, indicating these values are not being used to compute vertical deviation guidance. The altitude values must be designated for use by the pilot if they are to be used in computing vertical guidance. a) Press the FMS Knob to activate the cursor. c) Press the ENT Key. Note the altitude is now displayed as light blue text (Figure 7-35), indicating that the value is now be used to compute vertical guidance. The G1000 uses baro corrected altitude when giving vertical guidance to these waypoints. 7-14 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A SECTION 7 ­ NAVIGATION d) Turn the large FMS Knob to select the altitude constraint associated with FALUR as seen in Figure 7-35. Altitude constraint values associated with the Final Approach Fix (FAF) and waypoints beyond the FAF cannot be designated for vertical guidance. These altitude values are always displayed as white text, as in Figure 7-36. Vertical guidance from the FAF to the Missed Approach Point (MAP) is given using the WAAS GPS altitude source, therefore, the displayed altitude values are for reference only. Figure 7-35 Designate FALUR Altitude Constraint e) Press the ENT Key to designate this altitude constraint value for use in computing vertical guidance. In this example, the aircraft has progressed through the final waypoint of the arrival and the flight plan has automatically sequenced to the IAF as the active leg, activating the approach procedure (see Figure 7-45). c) Press the ENT Key to activate the approach. At the TOD, establish a descent vertical speed as previously discussed in Step 16. The aircraft altitude will be 9, 000 feet upon reaching HABUK. Figure 7-45 Approach is Now Active To manually activate the approach procedure, perform the following steps: a) Press the PROC Key. b) Turn the large FMS Knob to highlight `ACTIVATE APPROACH' as shown in Figure 7-46. Figure 7-47 Descending Turn to the Initial Approach Fix (IAF) Figure 7-46 Manually Activate Approach 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 7-19 SECTION 7 ­ NAVIGATION 23) After crossing FALUR the next waypoint is the FAF. The flight phase changes to LPV on the HSI indicating the current phase of flight is in Approach Mode and the approach type is LPV. CDI scaling changes accordingly and is used much like a localizer when flying an ILS approach. The RVSI is no longer displayed and the VDI changes to the Glidepath Indicator (as shown in Figure 7-48) when the final approach course becomes active. The descent continues through the FAF (CEGIX) using the Glidepath Indicator, as one would use a glideslope indicator, to obtain an altitude "AT" 7, 800 feet at the FAF. Note the altitude restriction lines over and under (At) the altitude in the `ALT' field in Figure 7-48. 24) After crossing CEGIX, the aircraft continues following the glidepath to maintain the descent to "AT or ABOVE" 6, 370 feet at the Missed Approach Point (MAP) (RW35R) as seen in Figure 7-49. Figure 7-48 Descending to the FAF 7-20 Figure 7-49 Descending to the Missed Approach Point 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 SECTION 7 ­ NAVIGATION In this missed approach procedure, the fix immediately following the MAP (in this case `6368FT') is not part of the published procedure. [. . . ] Parallel course A parallel course has been selected, causing the vertical deviation to go invalid. NO WGS84 WPT ­ Non WGS 84 The selected waypoint [xxxx] does not use the WGS 84 datum. Cross-check waypoint for navigation -[xxxx] position with alternate navigation sources. TRAFFIC FAIL ­ Traffic device has The G1000 is no longer receiving data from the traffic system. [. . . ]