Garmin DA42-L360 Bedienungsanleitung

G1000®Integrated Flight Deck

Cockpit Reference Guide for the Diamond DA42-L360

FLIGHT INSTRUMENTS

ENGINE INDICATION SYSTEM

NAV/COM/TRANSPONDER/AUDIO PANEL

AUTOMATIC FLIGHT CONTROL SYSTEM

GPS NAVIGATION

FLIGHT PLANNING

PROCEDURES

HAZARD AVOIDANCE

ADDITIONAL FEATURES

ABNORMAL OPERATION

ANNUNCIATIONS & ALERTS

APPENDIX

INDEX

This manual reﬂects the operation of System Software version 1054.01 or later for the Diamond

DA42-L360. Some differences in operation may be observed when comparing the information

in this manual to earlier or later software versions.

Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A.

Tel: 913/397.8200 Fax: 913/397.8282

Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.

Tel: 503/391.3411 Fax 503/364.2138

Garmin (Europe) Ltd, Liberty House, Bulls Copse Road, Hounsdown Business Park,

Southampton, SO40 9RB, U.K.

Tel: 44/0870.8501241 Fax: 44/0870.8501251

Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan

Tel: 886/02.2642.9199 Fax: 886/02.2642.9099

For after-hours emergency, aircraft on ground (AOG) technical support for Garmin panel mount

and integrated avionics systems, please contact Garmin’s AOG Hotline at 913.397.0836.

Web Site Address: www.garmin.com

Except as expressly provided herein, no part of this manual may be reproduced, copied,

transmitted, disseminated, downloaded or stored in any storage medium, for any purpose

without the express written permission of Garmin. Garmin hereby grants permission to

download a single copy of this manual and of any revision to this manual onto a hard drive or

other electronic storage medium to be viewed for personal use, provided that such electronic

or printed copy of this manual or revision must contain the complete text of this copyright

notice and provided further that any unauthorized commercial distribution of this manual or any

revision hereto is strictly prohibited.

Garmin® and G1000®are registered trademarks of Garmin Ltd. or its subsidiaries. FliteCharts®,

and SafeTaxi®are trademarks of Garmin Ltd. or its subsidiaries. These trademarks may not be

used without the express permission of Garmin.

NavData®is a registered trademark of Jeppesen, Inc.; Stormscope®is a registered trademark

of L-3 Communications; and XM®is a registered trademark of XM Satellite Radio, Inc.

August, 2010 190-01062-01 Rev. A Printed in the U.S.A.

Garmin G1000 Cockpit Reference Guide for the DA42-L360

190-01062-01 Rev. A

Warnings, Cautions & Notes

WARNING: Navigation and terrain separation must NOT be predicated upon

the use of the terrain function. The G1000 Terrain Proximity feature is NOT

intended to be used as a primary reference for terrain avoidance and does not

relieve the pilot from the responsibility of being aware of surroundings during

ﬂight. The Terrain Proximity feature is only to be used as an aid for terrain

avoidance and is not certiﬁed for use in applications requiring a certiﬁed

terrain awareness system. Terrain data is obtained from third party sources.

Garmin is not able to independently verify the accuracy of the terrain data.

WARNING: The displayed minimum safe altitudes (MSAs) are only advisory

in nature and should not be relied upon as the sole source of obstacle and

terrain avoidance information. Always refer to current aeronautical charts

for appropriate minimum clearance altitudes.

WARNING: The altitude calculated by G1000 GPS receivers is geometric

height above Mean Sea Level and could vary signiﬁcantly from the altitude

displayed by pressure altimeters, such as the GDC 74A Air Data Computer,

or other altimeters in the aircraft. GPS altitude should never be used for

vertical navigation. Always use pressure altitude displayed by the G1000

PFD or other pressure altimeters in aircraft.

WARNING: Do not use outdated database information. Databases used in

the G1000 system must be updated regularly in order to ensure that the

information remains current. Pilots using any outdated database do so

entirely at their own risk.

WARNING: Do not use basemap (land and water data) information for

primary navigation. Basemap data is intended only to supplement other

approved navigation data sources and should be considered as an aid to

enhance situational awareness.

WARNING: Trafﬁc information shown on the G1000 Multi Function Display

is provided as an aid in visually acquiring trafﬁc. Pilots must maneuver

the aircraft based only upon ATC guidance or positive visual acquisition of

conﬂicting trafﬁc.

WARNING: XM Weather should not be used for hazardous weather

penetration. Weather information provided by the GDL 69A is approved only

for weather avoidance, not penetration.

Garmin G1000 Cockpit Reference Guide for the DA42-L360

190-01062-01 Rev. A

Warnings, Cautions & Notes

WARNING: NEXRAD weather data is to be used for long-range planning

purposes only. Due to inherent delays in data transmission and the relative

age of the data, NEXRAD weather data should not be used for short-range

weather avoidance.

WARNING: Use of the Stormscope is not intended for hazardous weather

penetration (thunderstorm penetration). Stormscope information, as

displayed on the G1000 MFD, is to be used only for weather avoidance, not

penetration.

WARNING: The Garmin G1000, as installed in the Diamond DA42-L360

aircraft, has a very high degree of functional integrity. However, the pilot

must recognize that providing monitoring and/or self-test capability for all

conceivable system failures is not practical. Although unlikely, it may be

possible for erroneous operation to occur without a fault indication shown

by the G1000. It is thus the responsibility of the pilot to detect such an

occurrence by means of cross-checking with all redundant or correlated

information available in the cockpit.

WARNING: For safety reasons,G1000 operational procedures must be learned

on the ground.

WARNING: The United States government operates the Global Positioning

System and is solely responsible for its accuracy and maintenance. The GPS

system is subject to changes which could affect the accuracy and performance

of all GPS equipment. Portions of the Garmin G1000 utilize GPS as a

precision electronic NAVigationAID (NAVAID). Therefore, as with all NAVAIDs,

information presented by the G1000 can be misused or misinterpreted and,

therefore, become unsafe.

WARNING: To reduce the risk of unsafe operation, carefully review and

understand all aspects of the G1000 Pilot’s Guide documentation and the

Diamond DA42-L360 Pilot’s Operating Handbook (POH). Thoroughly practice

basic operation prior to actual use. During ﬂight operations, carefully compare

indications from the G1000 to all available navigation sources, including

the information from other NAVAIDs, visual sightings, charts, etc. For safety

purposes, always resolve any discrepancies before continuing navigation.

Garmin G1000 Cockpit Reference Guide for the DA42-L360

190-01062-01 Rev. A

Warnings, Cautions & Notes

WARNING: The illustrations in this guide are only examples. Never use

the G1000 to attempt to penetrate a thunderstorm. Both the FAA Advisory

Circular, Subject: Thunderstorms, and the Aeronautical Information Manual

(AIM) recommend avoiding “by at least 20 miles any thunderstorm identiﬁed

as severe or giving an intense radar echo.”

WARNING: Lamp(s) inside this product may contain mercury (HG) and must

be recycled or disposed of according to local, state, or federal laws. For

more information, refer to our website at www.garmin.com/aboutGarmin/

environment/disposal.jsp.

WARNING: Because of variation in the earth’s magnetic ﬁeld, operating the

system within the following areas could result in loss of reliable attitude and

heading indications. North of 72° North latitude at all longitudes. South of

70° South latitude at all longitudes. North of 65° North latitude between

longitude 75° W and 120° W.(Northern Canada). North of 70° North latitude

between longitude 70°W and 128°W. (Northern Canada). North of 70° North

latitude between longitude 85° E and 114° E. (Northern Russia). South of

55° South latitude between longitude 120° E and 165° E. (Region south of

Australia and New Zealand).

WARNING: Do not use GPS to navigate to any active waypoint identiﬁed as

a ‘NON WGS84 WPT’ by a system message. ‘NON WGS84 WPT’ waypoints are

derived from an unknown map reference datum that may be incompatible

with the map reference datum used by GPS (known as WGS84) and may be

positioned in error as displayed.

CAUTION: The PFD and MFD displays use a lens coated with a special

anti-reﬂective coating that is very sensitive to skin oils, waxes, and abrasive

cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI-

REFLECTIVE COATING. It is very important to clean the lens using a clean,

lint-free cloth and an eyeglass lens cleaner that is speciﬁed as safe for anti-

reﬂective coatings.

CAUTION: The Garmin G1000 does not contain any user-serviceable parts.

Repairs should only be made by an authorized Garmin service center.

Unauthorized repairs or modiﬁcations could void both the warranty and the

pilot’s authority to operate this device under FAA/FCC regulations.

Garmin G1000 Cockpit Reference Guide for the DA42-L360

190-01062-01 Rev. A

Warnings, Cautions & Notes

NOTE: All visual depictions contained within this document, including screen

images of the G1000 panel and displays, are subject to change and may not

reﬂect the most current G1000 system and aviation databases. Depictions

of equipment may differ slightly from the actual equipment.

NOTE: This device complies with part 15 of the FCC Rules. Operation is

subject to the following two conditions: (1) this device may not cause harmful

interference, and (2) this device must accept any interference received,

including interference that may cause undesired operation.

NOTE: The data contained in the terrain and obstacle databases comes from

government agencies. Garmin accurately processes and cross-validates the

data, but cannot guarantee the accuracy and completeness of the data.

NOTE: This product, its packaging, and its components contain chemicals

known to the State of California to cause cancer, birth defects, or reproductive

harm. This notice is being provided in accordance with California’s Proposition

65. If you have any questions or would like additional information, please

refer to our web site at www.garmin.com/prop65.

NOTE: Interference from GPS repeaters operating inside nearby hangars can

cause an intermittent loss of attitude and heading displays while the aircraft

is on the ground. Moving the aircraft more than 100 yards away from the

source of the interference should alleviate the condition.

NOTE: Use of polarized eyewear may cause the ﬂight displays to appear dim

or blank.

NOTE: The purpose of this Cockpit Reference Guide is to provide the pilot

a resource with which to ﬁnd operating instructions on the major features

of the G1000 system more easily. It is not intended to be a comprehensive

operating guide. Complete operating procedures for the system are found

in the G1000 Pilot’s Guide for this aircraft.

Garmin G1000 Cockpit Reference Guide for the DA42-L360

190-01062-01 Rev. A

Warnings, Cautions & Notes

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