Garmin Bell 407 GTN Benutzerhandbuch - Seite 9
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1.6
HTAWS Function (Optional)
HTAWS shall NOT be used for navigation purposes.
HTAWS shall only be inhibited when in visual contact with terrain and when
the pilot can be assured of maintaining clearance from terrain and obstacles.
RP Mode shall only be used when in visual contact with terrain.
External HTAWS annunciators installed in the aircraft shall be fully functional
in order to use the HTAWS system.
The external "HTAWS ALERT ACK" switch shall be used in lieu of the Alert
Acknowledge function under the Terrain page menu to minimize pilot workload
during alert conditions.
Terrain Proximity and HTAWS are separate features and
mutually exclusive. If "HTAWS" is shown on the bottom
right of the dedicated terrain page, then HTAWS is installed.
1.7
Datalinked Weather Display (Optional)
This limitation applies to datalinked weather products from SiriusXM via a
GDL 69/69A and Connext via a GSR 56.
Data link weather information shall not be used for maneuvering in, near, or
around areas of hazardous weather.
The indicated data link weather product age shall not be used to determine the
age of the weather information shown by the data link weather product.
Information provided by data link weather products may not accurately depict
current weather conditions. Due to time delays inherent in gathering and
processing weather data for data link transmission, the weather information
shown by the data link weather product may be significantly older than the
indicated weather product age.
Data link services shall not be the sole means used to obtain Temporary Flight
Restriction (TFR) or Notice to Airmen (NOTAM) information. Not all TFRs
and NOTAMS may be available on the GTN.
1.8
Traffic Display (Optional)
The display of traffic is an aid to visual acquisition and shall not be utilized for
aircraft maneuvering.
1.9
Flight Planner/Calculator Functions
The Fuel Planning page shall not be used as a means to determine actual fuel on
board the aircraft.
RFMS, Bell 407 GTN GPS/SBAS System
FAA APPROVED
NOTE
190-01007-J4 Rev. 1
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