User manual GARMIN G1000 BEECHCRAFTA36 G36 COCKPIT REFERENCE GUIDE A36 G36SYSTEMSOFTWAREVERSION0458.01

[. . . ] G1000 TM Cockpit Reference Guide for the Beechcraft A36/G36 Copyright © 2005 Garmin Ltd. This manual reflects the operation of System Software version 0458. 01 or later for the Beechcraft A36/G36. 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. [. . . ] The aircraft is currently tracking inbound on the 116 degree radial of Panoche VORTAC. Enter Panoche VORTAC (PXN) and Clovis VORTAC (CZQ) into the GPS flight plan, in preparation to intercept this leg. With the flight plan activated, press the CDI softkey to set the CDI to GPS. As a result, the VOR annunciation flashes yellow and the autopilot reverts to default Roll Hold (ROL) mode. Flashes for ten seconds, then transitions to ROL. . 3. Now, press the NAV key to reactivate the autopilot using GPS guidance. At this moment, the autopilot couples to GPS guidance and steers the aircraft toward the active flight plan leg. Once the flight plan leg is intercepted, the autopilot continues to track GPS guidance to the end of the flight plan. 2. 33 30 0 3 VO 1. R M od e 2. 30 27 6 33 0 GP 27 Clovis VORTAC (CZQ) 21 12 24 3 9 SM ode 3. GP n Leg ht Pla S Flig V 230 6 24 21 Figure 6-24 Transition to GPS Flight Plan 6-16 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36 15 18 Panoche VORTAC (PXN) 9 12 15 18 SECTION 6 ­ AUTOMATIC FLIGHT CONTROL Flight Level Change (Descent) 1. In preparation for the approach to KFAT, set Selected Altitude to 3, 000 feet using the ALT knob. `FLC' is annunciated with the airspeed reference, which defaults to the current aircraft airspeed. The Autopilot maintains 142 knots by controlling pitch. 1. Cruise Altitude of 7, 000 MSL 3. As the aircraft reaches the selected altitude, the autopilot changes from Flight Level Change mode to Altitude Hold mode. `ALT' flashes in green, indicating the selected altitude is captured. After the capture is finished, the autopilot holds the aircraft at the selected altitude. 2. 2. FLC Mod e 3. Selected Altitude of 3, 000 MSL ALT Hold Mode Figure 6-25 FLC Descent Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36 6-17 SECTION 6 ­ AUTOMATIC FLIGHT CONTROL ILS Approach 1. Upon being given vectors from ATC, set the Selected Heading to the heading given by ATC. Turn the HDG knob to set the Heading Bug to comply with ATC vectors, as requested. 3. In preparation for the approach and at the pilot's discretion, tune the localizer frequency, then set the CDI to LOC by pressing the CDI softkey. `LOC' and `GS' appear in white in the roll axis and pitch axis modes armed fields, respectively. The autopilot will calculate when to begin the turn to intercept the final approach course. At the Decision Height, press the AP DISC button and land the aircraft, or press the GA button to execute a missed approach. 4. 2. 5. 33 30 0 3 27 Clovis (CZQ) 6 GPS Cour 24 se 9 9 29 12 2 HILAN 2. Figure 6-26 ILS Approach to KFAT 6-18 4. 3. 075 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36 02 5 12 15 18 2 2 21 1. 0 KFAT HD G M e od LO C /G S Mo de 5. 11 0 SECTION 6 ­ AUTOMATIC FLIGHT CONTROL Go-Around / Missed Approach 1. When the decision is made to execute a missed approach, apply full power and press the GA button. The autopilot will disconnect and the flight director command bars will establish a 7 degree nose-up climb. Note when the autopilot disconnects the `AP' annunciation flashes yellow for five seconds. Following the published Missed Approach Procedure, climb to the prescribed altitude. To have the autopilot fly to the hold point, set the CDI to GPS by pressing the CDI softkey, then press the NAV key. The autopilot flies direct to Clovis VORTAC according to the loaded approach while maintaining the current attitude. [. . . ] This can also occur with user waypoints in a flight plan that is deleted. Remove the waypoint from the flight plan if it no longer exists in any database, OR update the waypoint name/identifier to reflect the new information. FPL WPT MOVE ­ Flight plan The system has detected that a waypoint coordinate has changed due to a new waypoint moved. This occurs when a stored flight plan contains procedures that have been manually Verify user modified procedures. [. . . ]