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Garmin G1000 Cockpit Reference Guide for the Socata TBM 850

190-00708-00 Rev. A

SECTION 6 – AUTOMATIC

FLIGHT CONTROL

6-7

The white ‘ALTS’ annunciation indicates Selected

Altitude Capture Mode is armed (see Figure 6-7). The

ALT SEL Knob is used to set the Selected Altitude (shown

above the Altimeter) until Selected Altitude Capture Mode

becomes active.

As the aircraft nears the Selected Altitude, the ﬂight

director automatically transitions to Selected Altitude

Capture Mode with Altitude Hold Mode armed (Figure

6-8). This automatic transition is indicated by the green

‘ALTS’ annunciation ﬂashing for up to 10 seconds and the

appearance of the white ‘ALT’ annunciation. The Selected

Altitude is shown as the Altitude Reference beside the

‘ALTS’ annunciation.

At 50 feet from the Selected Altitude, the ﬂight director

automatically transitions from Selected Altitude Capture

to Altitude Hold Mode and holds the Selected Altitude

(shown as the Altitude Reference). As Altitude Hold Mode

becomes active, the white ‘ALT’ annunciation moves to the

active vertical mode ﬁeld and ﬂashes green for 10 seconds

to indicate the automatic transition.

Figure 6-8 Automatic Mode Transitions During Altitude Capture

Altitude Reference (in this

case, equal to Selected

Altitude)

Flash up to 10 sec, Indicating Automatic Transition

Changing the Selected Altitude

NOTE: Pressing the CWS Button while in Selected

Altitude Capture Mode does not cancel the

mode.

Use of the ALT SEL Knob to change the Selected

Altitude while Selected Altitude Capture Mode is active

causes the ﬂight director to revert to Pitch Hold Mode

with Selected Altitude Capture Mode armed for the new

Selected Altitude.

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 6-7). 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 SEL 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.

If the Selected Altitude is reached during CWS

maneuvering, the Altitude Reference is not changed.

To adjust the Altitude Reference in this case, the CWS

Button must be pressed again after the Selected Altitude

is reached.

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Garmin Software Version 0719.00 Guía de usuario Pagina 73

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