Flight management – Garmin G1000 King Air C90GT User Manual

Page 289

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190-00663-01 Rev. A

Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT

275

FLIGHT MANAGEMENT

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

13)

Note the altitude constraints associated with each of the approach waypoints as seen in Figure 5-128. These

altitudes are loaded from the database and are displayed as light blue text, indicating these values are
“designated” for use in computing vertical deviation guidance.

Note: To no longer use the displayed altitude for calculating vertical deviation guidance, perform the
following:

a

) Press the FMS Knob to activate the cursor.

b

) Turn the small FMS Knob to highlight the desired altitude.

c

) Press the CLR Key.

d

) Press the FMS Knob to deactivate the cursor.

After making the altitude “non-designated”, it is displayed as white text.

Altitude constraint values associated with the Final Approach Fix (FAF) and waypoints beyond the FAF cannot be
designated for vertical guidance. These altitude values are always displayed as white text, as in Figure 5-128.
Vertical guidance from the FAF and on to the Missed Approach Point (MAP) is given using the WAAS GPS
altitude source, therefore, the displayed altitude values are for reference only.

Figure 5-128 Vertical Guidance is Active to the FAF

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