Garmin G1000 King Air C90GT - Manual (Page 291)

190-00663-01 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 277
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
15) As seen in Figure 5-130, the aircraft is approaching TOD. Note the target vertical speed required to reach the
selected altitude. The Vertical Deviation Indicator (VDI) and the Required Vertical Speed Indicator (RVSI) are
now displayed on the PFD as shown in Figure 5-131. When the aircraft is within one minute of the TOD, it is
annunciated as shown in Figure 5-131, and an aural alert ‘Vertical track’ will be heard.
Figure 5-130 Approaching Top of Descent (TOD)
Figure 5-131 VDI & RVSI Upon Reaching Top of Descent (TOD)
Required Vertical
Speed Indicator
(RVSI)
Vertical Deviation
Indicator (VDI)
Target Altitude