Flight management – Garmin G1000 Socata TBM 850 User Manual
Page 291

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