Flight management – Garmin G1000 Socata TBM 850 User Manual

Page 291

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190-00709-01 Rev. A

Garmin G1000 Pilot’s Guide for the Socata TBM 850

279

FLIGHT MANAGEMENT

SY

STEM

O

VER
VIEW

FLIGHT

INSTRUMENTS

EAS

AUDIO P

ANEL

& CNS

FLIGHT

MANA

GEMENT

HAZARD

AV

OID
ANCE

AFCS

ADDITIONAL

FEA
TURES

APPENDICES

INDEX

13)

Note the altitude constraints associated with each of the approach waypoints as seen in Figure 5-125. These

altitudes are loaded from the database and are initially displayed as white text, indicating these values are not
used in computing vertical deviation guidance. The altitude values must be designated for use by the pilot if
they are to be used in computing vertical guidance.

a)

Press the FMS Knob to activate the cursor.

b)

Turn the large FMS Knob to place the cursor in the altitude field associated with the IAF at HABUK as in Figure
5-125.

Figure 5-125 Designate HABUK Altitude Constraint

c)

Press the ENT Key. Note the altitude is now displayed as light blue text, indicating that the value is now used
in computing vertical guidance. The G1000 is using baro corrected altitude when giving vertical guidance to
these waypoints.

d)

Turn the large FMS Knob to select the altitude constraint associated with FALUR as seen in Figure 5-126.

Figure 5-126 Designate FALUR Altitude Constraint

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