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Garmin G1000 Cockpit Reference Guide for the Cessna Nav III
190-00384-13 Rev. B
26
GPS Navigation
Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
AlertsAppendixIndex
Large Light
Blue Text
Small White Text
with Altitude
Restriction Bar
Large White
Text
Small Light
Blue Subdued
Text
Small Light
Blue Text
Insertion
Point
Indicator
Altitudes associated with approach procedures are “auto-designated”. This means the
system automatically uses the altitudes loaded with the approach for giving vertical flight
path guidance outside the FAF. Note these altitudes are displayed as small light blue text.
Altitudes associated with arrival procedures are “manually-designated”. This means
the system does not use the altitudes loaded with the arrival for giving vertical flight path
guidance until designated to do so by the pilot. Note that these altitudes are initially
displayed as white text. These altitudes may be “designated” by placing the cursor over
the desired altitude and pressing the ENT Key. After designation, the text changes to light
blue.
Altitudes that have been designated for use in vertical navigation may also be made
“non-designated” by placing the cursor over the desired altitude and pressing the CLR Key.
The altitude is now displayed only as a reference. It will not be used to give vertical flight
path guidance. Other displayed altitudes may change due to re-calculations or rendered
invalid as a result of manually changing an altitude to a non-designated altitude.
The system updates vertical path guidance continuously using ground speed and the
calculated distance to the Bottom of Descent (BOD). Due to turn anticipation guidance
(turn-smoothing), distance to the BOD can be affected by course changes greater than
approximately 5 degrees. Ground speed can be affected by factors such as shifts in wind
direction, aircraft power management, pitch angle, and course changes. Abrupt and/or
substantial changes to either the distance to the BOD, ground speed, or both can cause
similarly abrupt/substantial changes in vertical path guidance.
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