Garmin GTN 635 Handbuch Ergänzung - Seite 12

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Garmin GTN 635 Handbuch Ergänzung
GARMIN Ltd. or its Subsidiaries, c/o
Garmin International 1200 E. 151
Olathe, KS 66062 USA
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
External HSI/CDI/EHSI
External GPS Annunciator
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.
190-01007-A2 Rev. 1
FAA APPROVED DATE: _________________
AIRPLANE FLIGHT MANUAL SUPPLEMENT or
st
Street
SUPPLEMENTAL AIRPLANE FLIGHT MANUAL
Number
installed
1 or more
See Note 1
Table 1 – Required Equipment
MARCH 18, 2011
for STC SA02019SE-D GARMIN GTN
NAVIGATION SYSTEM
Number
Required for
IFR
1
1
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