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Garmin G1000 Diamond DA42NG User Manual

Garmin G1000 Diamond DA42NG
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190-00962-02 Rev. A
Garmin G1000 Pilot’s Guide for the Diamond DA42NG
449
AUTOMATIC FLIGHT CONTROL SYSTEM
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
ROLL HOLD MODE (ROL)
NOTE: If Roll Hold Mode is activated as a result of a mode reversion, the flight director rolls the wings
level.
Whentheightdirectorisactivated,RollHoldModeisselectedbydefault.Thismodeisannunciatedas
‘ROL’intheAFCSStatusBox.Thecurrentaircraftbankangleisheld,subjecttothebankangleconditionslisted
in Table 7-4.
Figure 7-21 Roll Hold Mode Annunciation
Bank Angle Flight Director Response
< 6° Rolls wings level
6 to 25° Maintains current aircraft roll attitude
> 25° Limits bank to 25°
Table 7-4 Roll Hold Mode Responses
CHANGING THE ROLL REFERENCE
The roll reference can be changed by pressing the
CWS
Button, establishing the desired bank angle, then
releasing the
CWS
Button.

Table of Contents

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Garmin G1000 Diamond DA42NG Specifications

General IconGeneral
Display TypeLCD
Resolution1024 x 768 pixels
ManufacturerGarmin
AircraftDiamond DA42NG
Primary Flight Display (PFD)Yes
Multi-Function Display (MFD)Yes
Audio PanelYes, integrated
Operating SystemProprietary
Weather RadarOptional
Power Supply28 VDC
Screen Size10.4 inches
Number of Displays2
AHRSYes
Air Data Computer (ADC)Yes
GPSYes
TransponderYes
Input Methodknobs
NavigationVOR, ILS, GPS
Traffic AvoidanceTAS/TCAS
Terrain AwarenessYes, TAWS

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