System Tests; Lean Assist Mode - Garmin CIRRUS PERSPECTIVE TOUCH+ Cockpit Reference Manual

SySTEM TESTS

NOTE: Information on system tests is superseded by the current version of the per-
tinent flight manual.
Pilot initiated systems tests are located on the 'System Test' Screen. These tests are ADS-B
and TAWS.
Accessing the System Tests:
From MFW Home, touch Aircraft Systems > System Tests .
1)
2) Touch the desired system test.
System Test
ADS-B
TAWS

LEAN ASSIST MODE

NOTE: The pilot should follow the engine manufacturer's recommended leaning
procedures in the current version of the pertinent flight manual.
A leaning assist function is available on the 'Engine & Fuel' Page to assist in the leaning
process.
Accessing Lean Assist Mode:
From MFW Home, touch Aircraft Systems .
1)
2) Touch the Engine & Fuel Button. The Lean Assist Button will now appear on the
Aircraft Systems Screen.
3) Touch the Lean Assist Button.
When the Lean Assist Button is touched, 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 EGT' s 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" annuncia-
tion below its bar on the graph.
190-02954-01 Rev. A
Tests the Automatic Dependent Surveillance - Broadcast System (ADS-B).
Tests the Terrain Awareness and Warning System (TAWS).
System Tests
Cockpit Reference Guide for the Cirrus SR2x with Perspective Touch+ by Garmin
Engine & Airframe Systems
Description
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