Garmin gnc 300 Manuel D’Utilisation
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
FAA APPROVED
190-00067-03 Rev. A
DATE: 10/16/95
Page 5 of 16
SECTION II
LIMITATIONS
1.
The GARMIN GNC300 Pilot’s Guide, P/N 190-00067-00, must be
immediately available to the flight crew whenever navigation is predicated on
the use of the system.
immediately available to the flight crew whenever navigation is predicated on
the use of the system.
2.
The GNC300 must utilize software version 2.02 or later FAA approved
revision. The software version is displayed on the GNC300 self test page
immediately after turn-on for 5 seconds.
revision. The software version is displayed on the GNC300 self test page
immediately after turn-on for 5 seconds.
3.
IFR enroute and terminal navigation is prohibited unless the pilot verifies the
currency of the data base or verifies each selected waypoint for accuracy by
reference to current approved data.
currency of the data base or verifies each selected waypoint for accuracy by
reference to current approved data.
4.
Instrument approaches must be accomplished in accordance with approved
instrument approach procedures that are retrieved from the GPS equipment
data base. The GPS equipment data base must incorporate the current update
cycle.
instrument approach procedures that are retrieved from the GPS equipment
data base. The GPS equipment data base must incorporate the current update
cycle.
(a) Instrument approaches must be conducted in the approach mode and
Receiver Autonomous Integrity Monitoring (RAIM) must be available at
the Final Approach Fix.
the Final Approach Fix.
(b) Accomplishment of ILS, LOC, LOC-BC, LDA, SDF, and MLS
approaches are not authorized.
(c) Coupling of the autopilot/flight director to GPS deviation data on the arc
segment of approaches incorporating an arc transition is not authorized.