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 12 of 31
FAA APPROVED DATE: _________________
2.3
Minimum Equipment
If the installation of the GTN is not limited to VFR, the GTN must have the
following system interfaces fully functional in order to be used for IFR
operations:
Interfaced Equipment
Number
installed
Number
Required for
IFR
External HSI/CDI/EHSI
1 or more
1
External GPS Annunciator
See Note 1
1
Table 1 – Required Equipment
Note 1: Certain installations require an external GPS annunciator panel. If installed, this annunciator
must be fully functional to use the GTN for IFR operations.
Single engine piston aircraft under 6,000 lbs maximum takeoff weight:
Required Equipment for IFR operations: Single GTN Navigator
Single engine turbine aircraft or multi-engine piston aircraft under 6,000 lbs
maximum takeoff weight:
Required Equipment for IFR operations: Single GTN Navigator plus a second
source of GPS navigation or a separate source of VHF navigation.
Operation in remote or oceanic operation requires two sources of GPS navigation.
Aircraft over 6,000 lbs maximum takeoff weight:
Required Equipment for IFR operations: Single GTN Navigator plus a second
source of GPS navigation or a separate source of VHF navigation.
Operation in remote or oceanic operation requires two sources of GPS navigation.
