Garmin GNC 300の取扱説明書

デバイスGarmin GNC 300の取扱説明書

デバイス: Garmin GNC 300
カテゴリ: GPS受信機
メーカー: Garmin
サイズ: 0.1 MB
追加した日付: 5/20/2013
ページ数: 16
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Garmin GNC 300 取扱説明書 - Online PDF
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要旨

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内容要旨
ページ1に含まれる内容の要旨

ページ2に含まれる内容の要旨

ページ3に含まれる内容の要旨

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 Table of Contents SECTION PAGE GENERAL..............................................................................................................4 LIMITATIONS ......................................................................................................5 EMERGENCY PROCEDURES....................................

ページ4に含まれる内容の要旨

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 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 o

ページ5に含まれる内容の要旨

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 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. 2. The GNC300 must utilize software version 2.02 or later FAA approved revision. The software version is displayed on the GNC300 self

ページ6に含まれる内容の要旨

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 (d) When an alternate airport is required by the applicable operating rules, it must be served by an approach based on other than GPS or Loran-C navigation, the aircraft must have the operational equipment capable of using that navigation aid, and the required navigation aid must be operational. 5. The aircraft must have

ページ7に含まれる内容の要旨

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 2. If "RAIM POSITION WARN" message is displayed the system will flag and no longer provide navigational guidance. The crew should revert to an alternate means of navigation. 3. If "RAIM NOT AVAILABLE" message is displayed in the enroute, terminal, or initial approach phase of flight, continue to navigate using the GPS eq

ページ8に含まれる内容の要旨

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 SECTION IV NORMAL PROCEDURES 1. DETAILED OPERATING PROCEDURES Normal operating procedures are described in the GARMIN GNC300 Pilot’s Guide, P/N 190-00067-00, Rev. A, dated August, 1995, or later appropriate revision. 2. APPROACH MODE / RAIM PREDICTION General Approach Mode Procedures The information contained in this s

ページ9に含まれる内容の要旨

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 NOTE: It is important to verify/enter the altimeter setting at the destination airport. This setting is used to calibrate pressure altitude when the GNC300 is navigating in the approach mode and will directly affect the unit’s capability to provide accurate navigation guidance. (c) When approach mode is available and t

ページ10に含まれる内容の要旨

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 (f) When flying the final approach leg of an active approach, the pilot may activate the missed approach by pressing the GPS APR switch to deactivate the approach mode. The GNC300 will then continue to provide course guidance along the final approach path to the MAP (Missed Approach Point), change the CDI sensitivity t

ページ11に含まれる内容の要旨

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 Course Reversals (Procedure Turn) If a course reversal is required, the pilot must set the required outbound course on the HSI and select HOLD mode with the GPS SEQ switch prior to crossing the FAF outbound. The GNC300 will then provide the appropriate course guidance outbound from the fix. Upon starting the course rev

ページ12に含まれる内容の要旨

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 Approach with DME arc segments Approach procedures which utilize a DME arc transition may be flown using the GNC300. For course guidance along the DME ARC, the pilot must select the NAV Position Page on the GNC300 and assure that the reference waypoint displayed is the approved reference facility for the DME ARC. The di

ページ13に含まれる内容の要旨

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 RAIM Prediction As indicated in Section 2, GPS approaches are not authorized unless RAIM is available at the FAF. RAIM availability at the destination may be predicted using the GNC300. To display predicted RAIM availability for the current destination, select "RAIM Prd?" from the NAV-TIME menu. When the ENT key is de

ページ14に含まれる内容の要旨

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 (a) NAV / GPS switch and annunciators - By depressing this switch, the GNC300 data and the NAV (VOR/ILS) data will be alternately displayed on the pilot’s HSI and selected for the autopilot / flight director input. The source of data being displayed will be annunciated on the face of the unit with either a white NAV leg

ページ15に含まれる内容の要旨

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 (d) GPS SEQ switch and annunciators (AUTO / HOLD) - When AUTO sequencing mode is enabled, depressing this switch disables automatic GPS waypoint sequencing and enables course entry from the pilot’s HSI course needle. The amber HOLD legend is illuminated. If depressed again, the GPS system re-enables automatic waypoint

ページ16に含まれる内容の要旨

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 5. AUTOPILOT / FLIGHT DIRECTOR OPERATION Coupling of the GNC300 System steering information to the autopilot/flight director can be accomplished by engaging the autopilot/flight director in the NAV or APR mode, with the NAV / GPS switch set to GPS. When the autopilot/flight director system is using course information sup


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