MARCH 18, 2011
GARMIN Ltd. or its Subsidiaries, c/o
Garmin International 1200 E. 151
st
Street
Olathe, KS 66062 USA
AIRPLANE FLIGHT MANUAL SUPPLEMENT or
SUPPLEMENTAL AIRPLANE FLIGHT MANUAL
for STC SA02019SE-D GARMIN GTN
NAVIGATION SYSTEM
190-01007-A2 Rev. 1
Page 28 of 31
FAA APPROVED DATE: _________________
Section 5.
PERFORMANCE
No change.
Section 6.
WEIGHT AND BALANCE
See current weight and balance data.
Section 7.
SYSTEM DESCRIPTIONS
7.1
Pilot’s Guide
The Garmin GTN 6XX or GTN 7XX Pilot’s Guide, part number and revision
listed below, contain additional information regarding GTN system description,
control and function. The Pilot’s Guides
do not
need to be immediately available
to the flight crew.
y
GTN 6XX Pilot’s Guide
P/N 190-01004-03 Rev A or later
y
GTN 7XX Pilot’s Guide
P/N 190-01007-03 Rev A or later
7.2
Leg Sequencing
The GTN supports all ARINC 424 leg types. Certain leg types require altitude
input in order to sequence (course to altitude, for example). If a barometric
corrected altitude source is not interfaced to the GTN, a popup will appear
prompting the pilot to manually sequence the leg once the altitude prescribed in
the procedure is reached.
This
installation
has
a barometric corrected altitude source. The GTN will
automatically sequence altitude legs.
This
installation
does not have
a barometric corrected altitude source. The
pilot will be prompted to manually sequence altitude legs.’
7.3
Auto ILS CDI Capture
Auto ILS CDI Capture will not automatically switch from GPS to VLOC for
LOC-BC or VOR approaches.
