User manual GARMIN G1000 DIAMOND COCKPIT REFERENCE GUIDE DA40 DA40F0369.11ORLATER

[. . . ] Integrated Flight Deck Cockpit Reference Guide Diamond DA40/40F Copyright © 2004-2006 Garmin Ltd. This manual reflects the operation of System Software version 0369. 11 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. [. . . ] 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 DA40/40F 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 DA40/40F 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 DA40/40F 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 annunciation `FLC' appears next to the Airspeed Reference, which defaults to the current aircraft airspeed, 142 knots. Altitude Hold Mode is armed automatically. 2) Reduce power to allow descent in Flight Level Change Mode. 3) Upon capturing the Selected Altitude, the flight director changes from Flight Level Change to Altitude Hold Mode. The annunciation `ALT' flashes in green to indicate the altitude capture. After the capture is complete, the autopilot holds the aircraft level at the Selected Altitude. 1. Cruise Altitude of 7, 000 MSL 2. FLC Mod e 3. Selected Altitude of 3, 000 MSL ALT Hold Mode Figure 6-23 FLC Descent Garmin G1000 Cockpit Reference Guide for the DA40/40F 6-17 SECTION 6 ­ AUTOMATIC FLIGHT CONTROL ILS Approach 1) Transition from GPS Navigation Mode to Heading Select Mode. c) Set the Selected Heading after getting vectors from ATC and press the HDG Key. 2) Use Heading Select Mode to comply with ATC vectors as requested. 33 30 0 3) In preparation for approach, tune the localizer frequency and select LOC mode on the HSI. [. . . ] 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. [. . . ]