Garmin G1000 Pilot’s Guide for Diamond DA40/40F
190-00592-06 Rev. A
366
AUTOMATIC FLIGHT CONTROL SYSTEM
SY
STEM
O
VER
VIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO P
ANEL
& CNS
FLIGHT
MANA
GEMENT
HAZARD
AV
OID
ANCE
AFCS
ADDITIONAL FEA
TURES
APPENDICES
INDEX
ALTITUDE HOLD MODE (ALT)
Altitude Hold Mode can be activated by pressing the
ALT
Key; the flight director maintains the current aircraft
altitude (to the nearest 10 feet) as the Altitude Reference. The flight director’s Altitude Reference, shown in the
AFCS Status Box, is independent of the Selected Altitude, displayed above the Altimeter. Altitude Hold Mode
active is indicated by a green ‘ALT’ annunciation in the AFCS Status Box.
Altitude Hold Mode is automatically armed when the flight director is in Selected Altitude Capture Mode (see
Figure 7-6). Selected Altitude Capture Mode automatically transitions to Altitude Hold Mode when the altitude
error is less than 50 feet. In this case, the Selected Altitude becomes the flight director’s Altitude Reference.
CHANGING THE ALTITUDE REFERENCE
NOTE:
Turning the
ALT
Knob while in Altitude Hold Mode changes the Selected Altitude, but not the flight
director’s Altitude Reference, and does not cancel the mode.
With the
CWS
Button depressed, the aircraft can be hand-flown to a new Altitude Reference. When the
CWS
Button is released at the desired altitude, the new altitude is established as the Altitude Reference.
Figure 7-7 Altitude Hold Mode
Command Bars Hold Pitch Attitude
to Maintain Altitude Reference
Altitude Hold
Mode Active
Altitude
Reference
Selected
Altitude
Selected
Altitude
Bug
Summary of Contents for Diamond DA40
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