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舶用機器 Garmin Cessna Caravan G1000のPDF 飛行機フライトマニュアル補足をオンラインで閲覧またはダウンロードできます。Garmin Cessna Caravan G1000 33 ページ。 Integrated flight deck
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MOONEY
M20R
1. The GARMIN G1000 Integrated Avionics System is a fully integrated
flight, engine, communication, navigation and surveillance instru-
mentation system. The system consists of a Primary Flight Display
(PFD), Multi--Function Display (MFD), audio panel (GMA), Air Data
Computer (ADC), Attitude and Heading Reference System (AHRS),
engine / airframe processing unit (GEA), and integrated avionics
(GIA) containing VHF communications, VHS navigation, and GPS
navigation.
2. The primary function of the PFD is to provide attitude, heading, air
data, navigation, and alerting information to the pilot. The PFD may
also be used for flight planning. The primary function of the MFD is to
provide engine information, mapping terrain information and for
flight planning. The audio panel is used for selection of radios for
transmitting and listening, intercom functions, and marker beacon
functions.
3. The primary function of the VHF Communication portion of the
G1000 is to enable external radio communication. The primary func-
tion of the VOR/ILS Receiver portion of the equipment is to receive
and demodulate VOR, localizer, and Glide Slope signals. The prima-
ry function of the GPS portion of the system is to acquire signals from
the GPS 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.
4. Provided the GARMIN G1000 GPS receivers are receiving ade-
quate and usable GPS and/or VHF navigation signals, it has been
demonstrated capable of and meets the accuracy specifications for
the following types of flight operations:
VFR/IFR en--route, oceanic, and terminal operations as well as 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 AC20--138A.
Navigation in the North Atlantic Minimum Navigation Performance
Specification (MNPS) Airspace in accordance with AC91--49 and AC
120--33.
The GARMIN G1000 system meets RNP5 airspace (BRNAV) re-
quirements of AC 90--96 and in accordance with AC 20--138A, JAA
AMJ 20X2 Leaflet 2 Revision 1, and FAA Order 8110.60 for oceanic
and remote
ISSUED 11 - 2004
REVISION A 06--2005
REVISION B 03--2006
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
SECTION I - - GENERAL
AFM SUPPLEMENT
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FAA APPROVED