Garmin Software Version 0719.00 Betriebsanweisung PDF herunterladen (Seite 72)

Garmin G1000 Cockpit Reference Guide for the Socata TBM 850

190-00708-00 Rev. A

SECTION 6 – AUTOMATIC

FLIGHT CONTROL

6-6

Pitch Hold Mode (PIT)

When the ﬂight director is activated (the

FD Key is

pressed) or switched, Pitch Hold Mode is selected by

default. Pitch Hold Mode is indicated as the active vertical

mode by the ‘PIT’ annunciation. This mode may be used

for climb or descent to the Selected Altitude (shown above

the Altimeter), since Selected Altitude Capture Mode is

automatically armed when the mode is activated.

In Pitch Hold Mode, the ﬂight director maintains a

constant pitch attitude, the pitch reference. The pitch

reference is set to the aircraft pitch attitude at the moment

of mode selection. If the aircraft pitch attitude exceeds

the ﬂight director pitch command limitations, the ﬂight

director commands a pitch angle equal to the nose-up/

down limit.

Figure 6-7 Pitch Hold Mode

Command Bars

Maintain Desired

Pitch Reference

Selected Altitude Capture Mode Armed

Selected

Altitude

Pitch Hold Mode Active

Changing the Pitch Reference

When operating in Pitch Hold Mode, the pitch

reference can be adjusted by

• Using the

NOSE UP/DN Wheel

• Pressing the CWS Button, hand-ﬂying the aircraft

to establish a new pitch reference, then releasing the

CWS Button

Selected Altitude Capture Mode (ALTS)

Selected Altitude Capture Mode is automatically armed

with activation of the following modes:

• Pitch Hold

• Vertical Speed

• Flight Level Change

• Go Around

• Vertical Path Tracking (if the Selected Altitude is to

be captured instead of the VNV Target Altitude)

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