Download Garmin Software Version 0370.17 Cockpit Reference Guide
Transcript
SECTION 6 – AUTOMATIC FLIGHT CONTROL Vertical Speed Mode (VS) 1) Press the VS Key. The flight director is now activated (if not already active) and ‘VS’ is displayed in green in the Active Mode field and the Vertical Speed Bug will appear on the Vertical Speed Indicator. Pitch commands are given to manually maintain vertical speed. Press the AP Key to engage the autopilot for maintaining the current vertical speed. Altitude Hold Mode is automatically armed with ‘ALT’ displayed white in the Armed Mode field to the right of the ‘VS’ annunciation. 2) The Vertical Speed Bug can be adjusted in 100 fpm increments by pressing the NOSE UP/NOSE DN Keys to set the desired vertical speed. The vertical speed setting will be displayed in the Selected Vertical Speed box and in the Vertical Speed Reference field in the AFCS Status Bar. Vertical Speed Mode is active. The Vertical Speed box is located above the VSI when the aircraft is climbing and below the VSI when descending. 3) Vertical speed may also be changed by pressing and holding the CWS Button to manually establish the desired vertical speed using the control wheel. When the CWS Button is released, the current vertical speed will be maintained. 4) A desired altitude may be entered in the Selected Altitude Box by turning the ALT Knob. With Altitude Hold Mode armed, as the selected altitude is reached ‘ALT’ will flash in green for 10 seconds in the Acitve Mode field, after which the annunciation stops flashing. This signals the altitude capture is complete and the selected altitude will be maintained. If only the flight director is engaged, pitch and roll commands are given to manually maintain the selected altitude. Vertical Speed Reference Altitude Hold is Armed. Selected Altitude Selected Vertical Speed Vertical Speed Reference Bug Flight Director command bars indicate a climb at the prescribed vertical speed, to the Selected Altitude. Figure 6-13 Vertical Speed Hold Mode 6-6 Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B