190-00820-11 Rev. A
Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective by Garmin
105
ENGINE INDICATION SYSTEM
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
3.3 LEANING ASSIST MODE
NOTE
:
The pilot should follow the engine manufacturer’s recommended leaning procedures in the Pilot’s
Operating Handbook (POH).
A leaning assist function is available on the Engine Page to assist in the leaning process.
Accessing Leaning Assist Mode:
1)
Press the
ENGINE
Softkey to display the Engine Page.
2)
Press the
ASSIST
Softkey to identify peaks.
When the
ASSIST
Softkey is pressed, the system initially highlights the number and places a cyan box around
the EGT display of the cylinder with the hottest EGT. The
∆
Peak temperature is the difference between the
peak temperature and the present temperature for the peaked cylinder. When the first peak is detected, “1st” is
annunciated below that cylinder’s EGT bar and the temperature is enclosed in a cyan box.
The system continues to detect peak EGTs for each cylinder lean of peak as the fuel flow is decreased, and the
peak of each cylinder’s EGT is indicated by a cyan marker on the graph. Once all cylinders are lean of peak, the
last cylinder to peak is denoted by the “Last” annunciation below its bar on the graph.
Figure 3-25 Leaning Assist Mode
Cyan Box
Represents Peak
Temperature
Deviation
from Peak
