Справочник Пользователя для Garmin gnc 300

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GARMIN International, Inc.
9875 Widmer Road
Lenexa,  KS  66215   U.S.A.
FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN GNC300 VHF COMMUNICATION TRANSCEIVER / GPS RECEIVER
190-00067-03 Rev. A
FAA APPROVED
Page 4 of 16
 DATE: 10/16/95
SECTION I
GENERAL
1.
The GNC300 System is a fully integrated, panel mounted instrument,
which contains a 760 channel VHF Communications Transceiver and a Global
Positioning System (GPS) Navigation computer. The system consists of a GPS
antenna, a GPS Receiver, and a VHF Communications Transceiver.  The primary
function of the VHF Communication portion of the equipment is to facilitate
communication with Air Traffic Control.  The primary function of the GPS portion
of the system is to acquire signals from the GPS system satellites, recover orbital
data, make range and Doppler measurements, and process this information in real-
time to obtain the user’s position, velocity, and time.
2. Provided the GARMIN GNC300 navigation system is receiving adequate usable
signals, it has been demonstrated capable of and has been shown to meet the
accuracy specifications for:
VFR/IFR enroute, terminal, and non-precision instrument
approach (GPS, Loran-C, VOR, VOR-DME, TACAN, NDB,
NDB-DME, RNAV) operation within the U.S. National
Airspace System in accordance with AC 20-138.
North Atlantic Minimum Navigation Performance
Specification (MNPS) Airspace in accordance with AC 91-
49 and AC 120-33.
Navigation is accomplished using the WGS-84 (NAD-83) coordinate reference
datum.  Navigation data is based upon use of only the Global Positioning
System (GPS) operated by the United States of America.