Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective by Garmin
190-00820-11 Rev. A
83
FLIGHT INSTRUMENTS
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
Required
Vertical
Speed
Indicator
Vertical
Deviation
Indicator
VNV Target
Altitude
Terminal
Phase of
Flight
GPS is
Selected
Navigation
Source
Figure 2-32 Vertical Navigation Indications (PFD)
Top of Descent Message
Criteria
VNV Indication Removed
Required Vertical
Speed (RVSI)
Vertical
Deviation (VDI)
VNV Target
Altitude*
Aircraft > 1 min before the next TOD due to flight plan change
X
X
X
VNV cancelled (
CNCL VNV
Softkey pressed on MFD)
X
X
X
Distance to active waypoint cannot be computed due to
unsupported flight plan leg type (see Flight Management
Section)
X
X
X
Aircraft > 250 feet below active VNV Target Altitude
X
X
X
Current crosstrack or track angle error has exceeded limit
X
X
X
Active altitude-constrained waypoint can not be reached within
maximum allowed flight path angle and vertical speed
X
X
* If the flight director has been engaged to fly a VNV flight plan, the VNV Target Altitude being held remains displayed
while on level flight plan legs.
Table 2-2 VNV Indication Removal Criteria
Содержание CIRRUS PERSPECTIVE SR2x
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