User manual GARMIN G1000 DIAMOND COCKPIT REFERENCE GUIDE DA40 DA40F0369.10ORLATER

[. . . ] G1000 TM Cockpit Reference Guide for the Diamond DA40 Copyright © 2004-2006 Garmin Ltd. This manual reflects the operation of System Software version 0369. 10 or later for the Diamond DA40, DA40F. 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. [. . . ] Figure 6-14 depicts the Go Around mode on the PFD. Approach Mode is active Glideslope is active Flight Director command bars indicating descent on localizer/ glideslope path LOC2 is the active navigation receiver on the HSI Figure 6-18 Approach Mode 6-12 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 6 ­ AUTOMATIC FLIGHT CONTROL 6. 7 EXAMPLE PROCEDURES USING AFCS This section provides a scenario-based set of procedures showing various autopilot modes used during a flight. In this scenario, the aircraft departs Reid-Hillview Airport (KRHV) from runway 13L, enroute to Fresno Yosemite International Airport (KFAT). Climb to an altitude of 7, 000 feet MSL and fly a heading of 070 degrees to intercept airway V107. Fly airway V107 to Panoche VORTAC (PXN) using VOR navigation, then fly airway V230 using a GPS flight plan. Prior to reaching Clovis VORTAC (CZQ), descend to 3, 000 feet and load the ILS approach to R29R at KFAT. Fly the ILS approach and execute a missed approach. KRHV 070 NOTE: The diagrams in the following examples are for instructional purposes only and may not be used for navigation. V 30 10 7 33 30 0 33 0 3 Clovis VORTAC (CZQ) 27 6 24 3 V 230 27 9 21 6 12 21 Figure 6-19 Flight Plan Overview Garmin G1000 Cockpit Reference Guide for the DA40 15 18 Panoche VORTAC (PXN) 12 24 9 15 18 KFAT 6-13 SECTION 6 ­ AUTOMATIC FLIGHT CONTROL Departure To climb to the selected altitude and fly an assigned heading: 1) Upon takeoff, set the Selected Altitude to 7000 feet using the ALT Knob. To have the autopilot capture this altitude, use Pitch Hold, Vertical Speed, or Flight Level Change Mode. 2) Upon reaching the desired vertical speed of 1000 fpm, enable the flight director in Vertical Speed Mode. b) Press the AP Key to engage the autopilot in Roll Hold and Vertical Speed modes. 3) Activate Heading Select Mode while the autopilot is engaged in the climb. The autopilot follows the Heading Bug on the HSI and turns the aircraft to the desired heading. 4) As the aircraft climbs to the Selected Altitude, the flight director changes from Vertical Speed to Altitude Hold Mode. This active mode change is indicated by the green `ALT' annunciation flashing for ten seconds. 5) Upon reaching the Selected Altitude, the autopilot completes the capture process and levels the aircraft. From this point, the flight director continues to operate in Altitude Hold Mode. 3. HDG Mode 070 Selected Altitude of 7, 000 MSL 5. ALT Mode 4. Mod VS o LT M e, A d rme de A 1. 2. Figure 6-20 Departure 6-14 Garmin G1000 Cockpit Reference Guide for the DA40 SECTION 6 ­ AUTOMATIC FLIGHT CONTROL Intercepting a VOR Radial NOTE: Changing the HSI mode cancels Navigation Mode and causes the flight director to revert to Roll Hold Mode. During climb-out, the autopilot continues to fly the aircraft in Heading Select Mode. Note that at this point, the flight director is still in Heading Select Mode and the autopilot continues to fly 070°. c) Press the NAV Key to arm Navigation Mode. The white annunciation `VOR' appears to the left of the active roll mode. 2) When the CDI shows less than one dot, the flight director changes from Heading Select to Navigation Mode, and the green annunciation `VOR' flashes. 3) The autopilot continues the turn until the aircraft is established on the Selected Course. 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 Garmin G1000 Cockpit Reference Guide for the DA40 6-15 15 18 SECTION 6 ­ AUTOMATIC FLIGHT CONTROL Flying a GPS Flight Plan 1) Enter Panoche VORTAC (PXN) and Clovis VORTAC (CZQ) into the GPS flight plan, in preparation to intercept this leg. This cancels VOR mode on the HSI and the flight director loses the VOR signal. As a result, the VOR annunciation flashes yellow. Flashes for ten seconds, then transitions to ROL. . If the NAV Key is not pressed within 10 seconds of the HSI mode change, the flight director will roll the wings level and enter Roll Hold Mode. 3) Once the flight plan leg is intercepted, the autopilot continues to track GPS guidance to the end of the flight plan. b) Press the NAV Key to activate GPS Navigation Mode to cause the autopilot to steer the aircraft toward the active flight plan leg. 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. F GPS Leg Plan light V 230 6 24 21 Figure 6-22 Transition to GPS Flight Plan 6-16 Garmin G1000 Cockpit Reference Guide for the DA40 15 18 Panoche VORTAC (PXN) 9 12 15 18 SECTION 6 ­ AUTOMATIC FLIGHT CONTROL Flight Level Change (Descent) While flying the GPS leg from Panoche VORTAC to Clovis VORTAC, the aircraft is cleared to make a descent to 3000 feet in preparation for the approach to KFAT. [. . . ] The G1000 system should be serviced. GDL 69 Message Advisories Alerts Window Message GDL69 CONFIG ­ GDL 69 configuration error. Comments GDL 69 configuration settings do not match those of backup configuration memory. The G1000 system should be serviced GDC 74A Message Advisories Alerts Window Message GDC1 CONFIG ­ GDC1 configuration error. Comments GDC 74A configuration settings do not match those of backup configuration memory. [. . . ]