Garmin Cessna Caravan G1000 User manual

G1000®Integrated Avionics System
Cockpit Reference Guide for the Diamond DA62

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

Copyright © 2015, 2016 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 1373.01 or later for the Diamond
DA62. Some differences in operation may be observed when comparing the information in this
manual to earlier or later software versions.
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Garmin G1000 Cockpit Reference Guide for the Diamond DA62
190-01896-01 Rev. A
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“AOPA”) expressly disclaim all warranties, with respect to the AOPA information included in this
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Printed in the U.S.A

Garmin G1000 Cockpit Reference Guide for the Diamond DA62
190-01896-01 Rev. A
Warnings, Cautions & Notes
WARNING: Do not use terrain avoidance displays as the sole source of infor-
mation for maintaining separation from terrain and obstacles. Garmin obtains
terrain and obstacle data from third party sources and cannot independently
verify the accuracy of the information.
WARNING: Always refer to current aeronautical charts and NOTAMs for
verification of displayed aeronautical information. Displayed aeronautical
data may not incorporate the latest NOTAM information.
WARNING: Do not use geometric altitude for compliance with air traffic
control altitude requirements.The primary barometric altimeter must be used
for compliance with all air traffic control altitude regulations, requirements,
instructions, and clearances.
WARNING: Do not use basemap information (land and water data) as the
sole means of navigation. Basemap data is intended only to supplement other
approved navigation data sources and should be considered only an aid to
enhance situational awareness.
WARNING: Do not rely solely upon the display of traffic information to
accurately depict all of the traffic within range of the aircraft. Due to lack
of equipment, poor signal reception, and/or inaccurate information from
aircraft or ground stations, traffic may be present that is not represented on
the display.
WARNING: Do not use data link weather information for maneuvering in,
near, or around areas of hazardous weather. Information contained within
data link weather products may not accurately depict current weather condi-
tions.
WARNING: Do not use the indicated data link weather product age to deter-
mine the age of the weather information shown by the data link weather
product. Due to time delays inherent in gathering and processing weather
data for data link transmission, the weather information shown by the data
link weather product may be older than the indicated weather product age.

Garmin G1000 Cockpit Reference Guide for the Diamond DA62
190-01896-01 Rev. A
Warnings, Cautions & Notes
WARNING: The displayed minimum safe altitude (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: Always obtain qualified instruction prior to operational use of
this equipment.
WARNING: Do not use a QFE altimeter setting with this system. System
functions will not operate properly with a QFE altimeter setting. Use only
a QNH altimeter setting for height above mean sea level, or the standard
pressure setting, as applicable.
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.
WARNING: Because of variation in the earth’s magnetic field, do not rely
on the accuracy of attitude and heading indications (GRS 77 installations
only) in the following geographic areas: 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: When using the autopilot to fly an approach with vertical guid-
ance, the autopilot will not level the aircraft at the MDA/DH even if the MDA/
DH is set in the altitude preselect.

Garmin G1000 Cockpit Reference Guide for the Diamond DA62
190-01896-01 Rev. A
Warnings, Cautions & Notes
WARNING: Do not rely solely upon the display of traffic information for col-
lision avoidance maneuvering. The traffic display does not provide collision
avoidance resolution advisories and does not under any circumstances or
conditions relieve the pilot’s responsibility to see and avoid other aircraft.
WARNING: Do not rely on information from a lightning detection system
display as the sole basis for hazardous weather avoidance. Range limitations
and interference may cause the system to display inaccurate or incomplete
information. Refer to documentation from the lightning detection system
manufacturer for detailed information about the system.
WARNING: Use appropriate primary systems for navigation, and for terrain,
obstacle, and traffic avoidance. Garmin SVT is intended as an aid to situ-
ational awareness only and may not provide either the accuracy or reliability
upon which to solely base decisions and/or plan maneuvers to avoid terrain,
obstacles, or traffic.
WARNING: Intruder aircraft at or below 500 ft. AGL may not appear on the
Garmin SVT display or may appear as a partial symbol.
WARNING: Do not use the Garmin SVT runway depiction as the sole means
for determining the proximity of the aircraft to the runway or for maintaining
the proper approach path angle during landing.
WARNING: Do not operate the weather radar in a transmitting mode when
personnel or objects are within the MPEL boundary.
WARNING: Always position the weather radar gain setting to Calibrated for
viewing the actual intensity of precipitation. Changing the gain in weather
mode causes precipitation intensity to be displayed as a color not representa-
tive of the true intensity.
CAUTION: Do not clean display surfaces with abrasive cloths or cleaners
containing ammonia. They will harm the anti-reflective coating.

Garmin G1000 Cockpit Reference Guide for the Diamond DA62
190-01896-01 Rev. A
Warnings, Cautions & Notes
CAUTION: Repairs should only be made by an authorized Garmin service
center. Unauthorized repairs or modifications could void both the warranty
and affect the airworthiness of the aircraft.
NOTE: Lamp(s) inside this product 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
NOTE: Do not rely solely upon data link services to provide Temporary Flight
Restriction (TFR) information. Always confirmTFR information through official
sources such as Flight Service Stations or Air Traffic Control.
NOTE: All visual depictions contained within this document, including screen
images of the system panel and displays, are subject to change and may not
reflect the most current system and aviation databases. Depictions of equip-
ment may differ slightly from the actual equipment.
NOTE: 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 system utilize GPS as a precision electronic
NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information
presented by the system can be misused or misinterpreted and, therefore,
become unsafe.
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 harm-
ful interference, and (2) this device must accept any interference received,
including interference that may cause undesired operation.
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.