User manual GARMIN G1000 MOONEY COCKPIT REFERENCE GUIDE M20M,M20R,ANDM20TN

[. . . ] Integrated Flight Deck Cockpit Reference Guide Mooney M20M, M20R, & M20TN Copyright © 2004 - 2006 Garmin Ltd. This manual reflects the operation of System Software version 0424. 20 or later for the Mooney M20M, M20R, and M20TN. 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. [. . . ] From this point, the autopilot continues to operate in Altitude Hold Mode. 5) 2) 6) 3) After reaching the minimum engage altitude and activating Vertical Speed Mode, press the AP Key, engaging the autopilot in default Roll Hold and Vertical Speed modes. 3. HDG Mode 070 Selected Altitude of 7, 000 MSL 5. ALT Mode 4. M VS T , AL ode d rme eA Mod 1. 2. Figure 6-20 Departure Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN 6-15 SECTION 6 ­ AUTOMATIC FLIGHT CONTROL Intercepting a VOR Radial After climbout, the autopilot continues to fly the aircraft on a heading of 070 degrees at an altitude of 7, 000 feet. 1) Tune the VOR frequency, then set the CDI to VOR by pressing the CDI Softkey. Note the autopilot is still in Heading Mode and continues to fly a heading of 070 degrees. This arms the Navigation Mode and the white annunciation `VOR' appears to the left of the active Heading Mode. 3) The system calculates the point at which the autopilot changes from Heading Mode to Navigation Mode. When the aircraft reaches this point, `VOR' flashes green in the active mode field. The autopilot continues the turn until the aircraft is established on the selected course. 4) V 10 7 070 R HDG Mode, VO Armed 2. 3. VO R M od e 33 0 1. 29 6 30 3 27 6 Panoche VORTAC (PXN) 24 9 21 12 Figure 6-21 Intercepting a VOR 6-16 Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN 15 18 SECTION 6 ­ AUTOMATIC FLIGHT CONTROL Flying a Flight Plan / GPS Course 1) 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 6-22 Transition to GPS Flight Plan Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN 15 18 Panoche VORTAC (PXN) 9 12 15 18 6-17 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 6-23 FLC Descent 6-18 Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN SECTION 6 ­ AUTOMATIC FLIGHT CONTROL ILS Approach 1) Load the Runway 29R ILS approach for KFAT into the flight plan. 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 6-24 ILS Approach to KFAT 4. 3. 075 Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN 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 6-19 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. [. . . ] 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. Verify that the user-modified procedures in stored flight plans are correct and up to date. FPL TRUNC ­ Flight plan has been This occurs when a newly installed aviation database eliminates an obsolete approach or arrival used by a stored flight plan. [. . . ]