Garmin Cessna Caravan G1000 Configuration guide

190-00492-10 Rev 5 Diamond DA 40 / DA 40F
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190-00492-10 Rev 5 Diamond DA 40 / DA 40F
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Garmin Ltd. Or its subsidiaries
c/o Garmin International
1200 E. 151st Street
Olathe, KS 66062 USA
FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH
GFC 700 AUTOMATIC FLIGHT CONTROL SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
LOG OF REVISIONS
Revision
Number Page Number(s) Description FAA Approved Date of Approval
1 All Initial Release Robert
Murray 7/26/2007
2 All Add Software Levels Robert
Murray 9/6/2007
3 All Add Software Levels Robert
Murray 2/28/2008
4 All Add Software Levels Robert
Murray 4/4/2008
5 All
Update Software Levels
for non-WAAS See Page 1 See Page 1

190-00492-10 Rev 5 Diamond DA 40 / DA 40F
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190-00492-10 Rev 5 Diamond DA 40 / DA 40F
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH
GFC 700 AUTOMATIC FLIGHT CONTROL SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
Table of Contents
SECTION I
GENERAL..........................................................................................................7
(NOT FAA APPROVED)
SECTION II
LIMITATIONS................................................................................................14
(FAA APPROVED)
SECTION III
EMERGENCY PROCEDURES.....................................................................26
(NOT FAA APPROVED)
SECTION IVA
NORMAL PROCEDURES.............................................................................40
(NOT FAA APPROVED)
SECTION IVB
ABNORMAL PROCEDURES.......................................................................58
(NOT FAA APPROVED)
SECTION V
PERFORMANCE............................................................................................58
(NOT FAA APPROVED)
SECTION VI
WEIGHT AND BALANCE............................................................................58
(NOT FAA APPROVED)
SECTION VII
SYSTEM DESCRIPTIONS............................................................................59
(NOT FAA APPROVED)

190-00492-10 Rev 5 Diamond DA 40 / DA 40F
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
190-00492-10 Rev 5 Diamond DA 40 / DA 40F
Page 7 of 65
SECTION I
GENERAL
(Not FAA Approved)
G1000
The G1000 Integrated Avionics System is a fully integrated flight, engine,
communication, navigation and surveillance instrumentation system. The
system consists of a Primary Flight Display (PFD), Multi-Function Display
(MFD), audio panel, Air Data Computer (ADC), Attitude and Heading
Reference System (AHRS), engine sensors and processing unit (GEA), and dual
integrated avionics units (GIA) each containing VHF communications, VHF
navigation, and GPS (Global Positioning System).
GIA 63 units are standard and provide non-WAAS GPS position information in
accordance with TSO-C129a class A1. Optional GIA 63W units provide
WAAS augmented GPS position. If the optional GIA63W units incorporate
GPS software level 3.0 or later, the GPS system meets the requirements of TSO-
C145a.
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 flight planning. The audio panel
is used for selection of radios for transmitting and listening, intercom functions,
and marker beacon functions.
The primary function of the VHF Communication portion of the G1000 is to
enable external radio communication. The primary function of the VOR/ILS
Receiver portion of the equipment is to receive and demodulate VOR, Localizer,
and Glide Slope signals. The primary function of the GPS portion of the system
is to acquire signals from the GPS system satellites (and WAAS satellites if so
equipped), recover orbital data, make range and Doppler measurements, and
process this information in real-time to obtain the user's position, velocity, and
time.
If the optional TAWS function is installed in the G1000, the pilot will receive
appropriate aural warnings and cautions for terrain and obstacles. The pilot
should refer to the DA 40/DA 40F Pilot’s Guide for the terrain warning and
caution messages and system information.

FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
190-00492-10 Rev 5 Diamond DA 40 / DA 40F
Page 8 of 65
Operational Approvals
G1000 GPS NAVIGATION SYSTEM, GIA 63 INSTALLED
GIA 63 units are standard and provide position information in accordance with
TSO-C129a class A1. The Garmin G1000 system has been demonstrated
capable of, and has been shown to meet the accuracy requirements for the
following operations provided it is receiving usable navigation data:
•The G1000 Integrated Avionics system as installed in this aircraft
complies with AC 20-138A for navigation within the U.S. National
Airspace System using GPS for IFR en-route, terminal area, and non-
precision approach operations (including those approaches titled “GPS”,
“or GPS”, and “RNAV (GPS)” approaches).
•The G1000 Integrated Avionics system as installed in this aircraft has
been found to comply with the requirements for GPS as a Primary Means
of Navigation for oceanic and remote navigation – RNP-10, per FAA AC
20-138A, FAA Order 8400-12A, and FAA Order 8700-1. Both GPS
receivers are required to be operating and receiving usable signals except
for routes requiring only one Long Range Navigation sensor. This does
not constitute operational approval.
•North Atlantic (NAT) Minimum Navigational Performance
Specifications (MNPS) Airspace per AC 91-49 and AC 120-33. Both
GPS receivers are required to be operating and receiving usable signals
except for routes requiring only one Long Range Navigation sensor. This
does not constitute operational approval.
NOTE
Each GIA 63 computes an independent navigation solution based on its GPS
sensor. The G1000 will use the GPS sensor with the highest signal quality and
will automatically revert to the other sensor if the active sensor fails or if the
secondary sensor is determined to be more accurate. An “AHRS 1 GPS – “
message means that one of the GPSs has failed. Refer to the MFD AUX-GPS
STATUS page to determine the state of the GPSs.
•Enroute and Terminal including RNP5/BRNAV and PRNAV (RNP-1) -
In accordance with JAA TGL-10 Rev 1, ACJ 20X4, AC 90-96A, and AC
90-100A provided the FMS is receiving usable navigation information
from one or more GPS/SBAS receivers.
•The G1000 Integrated Avionics system as installed in this is aircraft is
eligible for B-RNAV in accordance with AMJ20X2.

FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
190-00492-10 Rev 5 Diamond DA 40 / DA 40F
Page 9 of 65
•The G1000 Integrated Avionics system as installed in this aircraft is
eligible for PRNAV in accordance with PRNAV requirements: JAA
Administrative & Guidance Material Section One: General Part 3:
Temporary Guidance Leaflets, Leaflet No 10: Airworthiness and
Operational Approval for Precession RNAV Operations in Designated
European Airspace 7.1 Required Functions.
•Navigation information is referenced to WGS-84 reference system, and
should only be used where the Aeronautical Information Publication
(including electronic data and aeronautical charts) conform to WGS-84 or
equivalent.

FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
190-00492-10 Rev 5 Diamond DA 40 / DA 40F
Page 10 of 65
G1000 GPS/SBAS NAVIGATION SYSTEM, GIA 63W INSTALLED,
G1000 SYSTEM SW 0321.17OR LATER USING GPS SW 3.0 OR LATER
The Garmin G1000 GPS/SBAS receivers, GIA 63W, incorporating SW version
3.0 or later approved version and GA35 (PN 013-00235-00) antennas are
approved under TSO-C145a/TSO-C146a equipment Class 3 and installed in
accordance with AC 20-138A. The Garmin G1000 system has been
demonstrated capable of, and has been shown to meet the accuracy requirements
for the following operations provided it is receiving usable navigation data:
•The G1000 Integrated Avionics system as installed in this aircraft
complies with AC 20-138A for navigation using GPS and WAAS (within
the coverage of a Space-Based Augmentation System complying with
ICAO Annex 10) for IFR en route, terminal area, and non-precision
approach operations (including those approaches titled “GPS”, “or
GPS”, and “RNAV (GPS)” approaches). The G1000 Integrated Avionics
system installed in this aircraft is approved for approach procedures with
vertical guidance including “LPV”, “LNAV/VNAV”, and “LNAV + V”
within the U.S. National Airspace System.
•The G1000 Integrated Avionics system as installed in this aircraft has
been found to comply with the requirements for GPS as a Primary Means
of Navigation for oceanic and remote navigation – RNP-10, (per FAA
AC 20-138A, FAA Order 8400-12A, and FAA Order 8700-1), when
used in conjunction with Garmin WAAS Fault Detection/Exclusion
(WFDE) Prediction Program, part number 006-A0154-01 or later
approved version with GA35 (PN 013-00235-00) antennas selected. Both
GPS/SBAS receivers are required to be operating and receiving usable
signals except for routes requiring only one Long Range Navigation
(LRN) sensor. This does not constitute an operational approval.
•The G1000 WFDE predication program works in combination with the
Garmin AT, Inc. Route Planning Software, version 1.2, or later approved
version. The route planning and WFDE prediction program can be
downloaded from Garmin G1000 website on the Internet. For
information on using the WFDE Prediction Program, refer to Garmin
WAAS FDE Prediction Program, part number 190-00643-01, ‘WFDE
Prediction Program Instructions’.
•North Atlantic (NAT) Minimum Navigational Performance
Specifications (MNPS) Airspace per AC 91-49 and AC 120-33. Both
GPS/SBAS receivers are required to be operating and receiving usable
signals except for routes requiring only one Long Range Navigation
sensor. This does not constitute operational approval.

FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
190-00492-10 Rev 5 Diamond DA 40 / DA 40F
Page 11 of 65
NOTE
Each GIA 63W computes an independent navigation solution based on its GPS
sensor. The G1000 will use the GPS sensor with the highest signal quality and
will automatically revert to the other sensor if the active sensor fails or if the
secondary sensor is determined to be more accurate. An “AHRS 1 GPS – “
message displayed in the ALERTS window means that one of the GPSs has
failed. Refer to the MFD AUX-GPS STATUS page to determine the state of the
GPSs.
•Enroute and Terminal including RNP5/BRNAV and PRNAV (RNP-1) -
In accordance with JAA TGL-10 Rev 1, ACJ 20X4, AC 90-96A, and AC
90-100A provided the FMS is receiving usable navigation information
from one or more GPS/SBAS receivers.
•The G1000 Integrated Avionics system as installed in this is aircraft is
eligible for B-RNAV in accordance with AMJ20X2.
•The G1000 Integrated Avionics system as installed in this aircraft is
eligible for PRNAV in accordance with PRNAV requirements: JAA
Administrative & Guidance Material Section One: General Part 3:
Temporary Guidance Leaflets, Leaflet No 10: Airworthiness and
Operational Approval for Precession RNAV Operations in Designated
European Airspace 7.1 Required Functions.
•Navigation information is referenced to WGS-84 reference system, and
should only be used where the Aeronautical Information Publication
(including electronic data and aeronautical charts) conform to WGS-84 or
equivalent.
G1000 GPS/SBAS NAVIGATION SYSTEM, GIA 63W INSTALLED,
G1000 SYSTEM SW 0369.13 USING GPS SW 2.40
The Garmin G1000 GPS/SBAS receivers, GIA 63W, incorporating SW version
2.40 do not comply with US 14 CFR Part 91, SFAR 97 requirements for TSO-
C145a/TSO-C146a equipment. See Limitations Section for requirements to the
use GPS for navigation.
The Garmin G1000 system with GPS SW 2.40 has been demonstrated capable
of, and has been shown to meet the accuracy requirements for the following
operations provided it is receiving usable navigation data:
•The G1000 Integrated Avionics system as installed in this aircraft
complies with AC 20-138A for navigation using GPS and WAAS (within
the coverage of a Space-Based Augmentation System complying with
ICAO Annex 10) for IFR en route, terminal area, and non-precision
approach operations (including those approaches titled “GPS”, “or

FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
190-00492-10 Rev 5 Diamond DA 40 / DA 40F
Page 12 of 65
GPS”, and “RNAV (GPS)” approaches) when used in conjunction with
Garmin Prediction Program 006-A0154-01 with the 013-00235-00
antenna selection to confirm the availability of RAIM for the intended en
route, terminal, and approach flight in addition to any NOTAMs issued
for the approach. The G1000 Integrated Avionics system installed in this
aircraft is approved for approach procedures with vertical guidance
including “LPV”, “LNAV/VNAV”, and “LNAV + V” within the U.S.
National Airspace System.
•The G1000 Integrated Avionics system as installed in this aircraft has
been found to comply with the requirements for GPS as a Primary Means
of Navigation for oceanic and remote navigation – RNP-10, (per FAA
AC 20-138A, FAA Order 8400-12A, and FAA Order 8700-1), when
used in conjunction with Garmin Prediction Program 006-A0154-01 with
the 013-00235-00 antenna selection to confirm the availability of RAIM
for the intended en route. Both GPS/SBAS receivers are required to be
operating and receiving usable signals except for routes requiring only
one Long Range Navigation (LRN) sensor. This does not constitute an
operational approval.
•North Atlantic (NAT) Minimum Navigational Performance
Specifications (MNPS) Airspace per AC 91-49 and AC 120-33. Both
GPS/SBAS receivers are required to be operating and receiving usable
signals except for routes requiring only one Long Range Navigation
sensor. This does not constitute operational approval.
NOTE
Each GIA 63W computes an independent navigation solution based on its GPS
sensor. The G1000 will use the GPS sensor with the highest signal quality and
will automatically revert to the other sensor if the active sensor fails or if the
secondary sensor is determined to be more accurate. An “AHRS 1 GPS – “
message displayed in the ALERTS window means that one of the GPSs has
failed. Refer to the MFD AUX-GPS STATUS page to determine the state of the
GPSs.
•Enroute and Terminal including RNP5/BRNAV and PRNAV (RNP-1) -
In accordance with JAA TGL-10 Rev 1, ACJ 20X4, AC 90-96A, and AC
90-100A provided the FMS is receiving usable navigation information
from one or more GPS/SBAS receivers.
•The G1000 Integrated Avionics system as installed in this is aircraft is
eligible for B-RNAV in accordance with AMJ20X2.
•The G1000 Integrated Avionics system as installed in this aircraft is
eligible for PRNAV in accordance with PRNAV requirements: JAA

FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
190-00492-10 Rev 5 Diamond DA 40 / DA 40F
Page 13 of 65
Administrative & Guidance Material Section One: General Part 3:
Temporary Guidance Leaflets, Leaflet No 10: Airworthiness and
Operational Approval for Precession RNAV Operations in Designated
European Airspace 7.1 Required Functions.
•Navigation information is referenced to WGS-84 reference system, and
should only be used where the Aeronautical Information Publication
(including electronic data and aeronautical charts) conform to WGS-84 or
equivalent.
ELECTRONIC FLIGHT BAG
The G1000 Integrated Avionics System as installed in this aircraft has been
approved as a Hardware Class 3, Software Type C Electronic Flight Bag (EFB)
in accordance with AC 120-76A when using current FliteChart or ChartView
data. Additional operational approvals may be required.
For operations under part 91, it is suggested that a secondary or back up source
of aeronautical information necessary for the flight be available to the pilot in
the aircraft. The secondary or backup information may be either traditional
paper-based material or displayed electronically. If the source of aeronautical
information is in electronic format, operators must determine non-interference
with the G1000 system and existing aircraft systems for all flight phases.

FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
190-00492-10 Rev 5 Diamond DA 40 / DA 40F
FAA Approved Page 14 of 65
SECTION II
LIMITATIONS
(FAA Approved)
2.1 INTRODUCTION
General Limitations:
1. The Garmin G1000 Cockpit Reference Guide (CRG) must be immediately
available to the flight crew. The required CRG is referenced to the System
Software Version number. The System Software Version number is
displayed at the top right side of the MFD Power-up page.
System Software
Version Garmin G1000 Cockpit Reference Guide (CRG)
revision
0369.13 P/N 190-00324-07, Revision A, or later appropriate
revision.
0321.17 P/N 190-00324-08, Revision A, or later appropriate
revision.
0321.18
Or
0321.19
P/N 190-00324-09, Revision A, or later appropriate
revision.
2. The G1000 installation in the DA 40 requires the following or later FAA
approved LRU software versions. Approved LRU software versions are
referenced to the System Software Version number. The LRU serial
numbers displayed on the screen are for convenience only and should be
disregarded in determining the LRU software revision. For compliance
activities requiring LRU serial number determination, the unit serial
number used must be that on the physical LRU label, not the one displayed
on the SYSTEM STATUS page.
LRU Software Version
LRU 0369.13
WAAS 0369.13 Non-WAAS 0321.17 WAAS 0321.17 Non-WAAS
GDC 1 2.05 2.05 3.02 3.02
GEA 1 2.07 2.07 2.07 2.07
GIA 1 & 2 5.31 5.31 5.51 5.51
GMA 1 3.03 3.03 3.03 3.03
GMU 1 2.01 2.01 2.01 2.01
GPS 1 & 2 2.40 3.03 3.0 3.03
GRS 1 2.10 2.10 2.11 2.11
GTX 1 4.06 4.06 4.06 4.06
MFD1 8.02 8.02 8.20 8.20
PFD 1 8.02 8.02 8.20 8.20
GDL 3.10 3.10 3.20.00 3.20.00
GSA 2.06 2.06 2.06 2.06

FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
190-00492-10 Rev 5 Diamond DA 40 / DA 40F
FAA Approved Page 15 of 65
LRU Software Version
LRU 0321.18
WAAS 0321.19
WAAS 0321.19 Non-WAAS
GDC 1 3.02 3.02 3.02
GEA 1 2.07 2.07 2.07
GIA 1 & 2 5.61 5.61 5.60
GMA 1 3.03 3.03 3.03
GMU 1 2.01 2.01 2.01
GPS 1 & 2 3.0 3.0 3.03
GRS 1 2.11 2.11 2.11
GTX 1 4.06 4.06 4.06
MFD1 9.01 9.01 9.01
PFD 1 9.01 9.01 9.01
GDL 3.20.00 3.20.00 3.20.00
GSA 2.06 2.06 2.06
The system’s databases and System Software Version number are displayed on
the MFD Power-up page immediately after system power-up and must be
acknowledged. The LRU software versions can be verified on the AUX group
sub-page 5, “AUX - SYSTEM STATUS” along with the system’s databases.
3. Operation is prohibited north of 70°N and south of 70°S latitudes. In
addition, operation is prohibited in the following two regions: 1) north of
65°N between 75°W and 120°W longitude and 2) south of 55°S between
120°E and 165°E longitude.
4. The fuel quantity, fuel required, and fuel remaining functions of the FMS
are supplemental information only and must be verified by the flight crew.
5. Navigation must not be predicated upon the use of the TAWS, Terrain or
Obstacle data displayed by the G1000.
6. TAWS must be inhibited prior to the Final Approach Fix (FAF) when
conducting an instrument approach that terminates in a circling to land or
side step maneuver.
NOTE: The terrain display is intended to serve as a situational awareness
tool only. It may not provide either the accuracy or fidelity, or both, on
which to solely base decisions and plan maneuvers to avoid terrain or
obstacles.
7. Pilots are authorized to deviate from their ATC clearance to the extent
necessary to comply with terrain / obstacle warnings from TAWS.
8. The Terrain/Obstacle/Airport databases have an area of coverage as
detailed below:

FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
190-00492-10 Rev 5 Diamond DA 40 / DA 40F
FAA Approved Page 16 of 65
(a) The Terrain Database has an area of coverage from North 75°
Latitude to South 60° Latitude in all longitudes.
(b) The Airport Terrain Database has an area of coverage that includes
the United States, Canada, Mexico, Latin America, and South
America.
(c) The Obstacle Database has an area of coverage that includes the
United States.
NOTE: The area of coverage may be modified, as additional terrain data
sources become available.
9. To avoid unwanted alerts, TAWS must be inhibited when landing at an
airport that is not included in the airport database.
10. The ADF aural identifier must be monitored any time the ADF is used as
the primary source of navigation.
G1000 GPS NAVIGATION SYSTEM LIMITATIONS
1. GPS/SBAS based IFR enroute, oceanic, and terminal navigation is
prohibited unless the pilot verifies and uses a valid, compatible, and current
Aviation database or verifies each waypoint for accuracy by reference to
current approved data.
2. “GPS”, “or GPS”, and “RNAV (GPS)” instrument approaches using the
G1000 System are prohibited unless the pilot verifies and uses the current
Aviation database. GPS based instrument approaches must be flown in
accordance with an approved instrument approach procedure that is loaded
from the Aviation database.
3. Instrument approaches utilizing the GPS receiver must be conducted in the
approach mode (LNAV, LNAV+V, L/VNAV, or LPV), and GPS/WAAS
integrity monitoring must be available at the Final Approach Fix. If there is
not sufficient GPS/WAAS integrity at any time after crossing the Final
Approach Fix, a Loss Of Integrity (LOI) will be annunciated on the HSI
and the approach mode will be aborted.
4. IFR non-precision approach approval using the GPS/SBAS sensor is
limited to published approaches within the U.S. National Airspace System.
Approaches to airports in other airspace are not approved unless authorized
by the appropriate governing authority.
5. Use of the Garmin G1000 GPS/SBAS receivers to accomplish ILS, LOC,
LOC-BC, LDA, SDF, MLS or any other type of approach not approved for
“or GPS” is not authorized. Use of the G1000 VOR/LOC/GS receivers to
fly approaches not approved for “or GPS” requires that VOR/LOC/GS
navigation data is selected and presented on the CDI of the pilot flying (i.e.
proper CDI source selection).

FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
190-00492-10 Rev 5 Diamond DA 40 / DA 40F
FAA Approved Page 17 of 65
NOTE
Not all published approaches are in the AVIATION database. The flight crew
must ensure that the planned approach is in the database.
6. Use of the G1000 VOR/ILS receiver to fly approaches not approved for
GPS requires VOR/ILS navigation data to be present on the display.
7. When conducting missed approach procedures, autopilot coupled operation
is prohibited until the pilot has established a course and rate of climb that
ensures all altitude and path requirements of the procedure will be met.
8. RNP operations are not authorized except as noted in the Operational
Approvals section.

FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
190-00492-10 Rev 5 Diamond DA 40 / DA 40F
FAA Approved Page 18 of 65
G1000 GPS/SBAS NAVIGATION SYSTEM, GIA 63W INSTALLED,
G1000 SYSTEM SW 0369.13 USING GPS SW 2.40
1. The Garmin G1000 GPS/SBAS receivers, GIA 63W, incorporating SW
version 2.40 do not comply with US 14 CFR Part 91, SFAR 97
requirements for TSO-C145a/TSO-C146a equipment. The following
limitations apply ONLY to the GIA 63W WAAS GPS receivers using GPS
SW version 2.40. The following limitations do not apply to GIA 63W
incorporating SW version 3.00 or later or to the non-WAAS GIA 63 GPS
receivers.
•While flying under IFR, the aircraft must be equipped with an approved
and operational alternate means of navigation appropriate to the flight
with the exception of oceanic and remote operations.
•For flight planning purposes, if an alternate airport is required, the
alternate airport must have an approved instrument approach procedure
other than GPS or RNAV that is anticipated to be operational and
available at the estimated time of arrival. All equipment required for this
procedure must be installed and operational.
•For flight planning purposes, Garmin Prediction Program 006-A0154-01
with the 013-00235-00 antenna selection should be used to confirm the
availability of RAIM for the intended flight in accordance with the local
aviation authority guidelines for TSO-C129a equipment. WAAS
NOTAMs (or their absence) and generic prediction tools do not provide
an acceptable indication of the availability for the GIA 63W equipment.
•When flight planning an LNAV/VNAV or LPV approach, operators
should use the Garmin Prediction Program 006-A0154-01 with the 013-
00235-00 antenna selection in addition to any NOTAMs issued for the
approach.

FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
190-00492-10 Rev 5 Diamond DA 40 / DA 40F
FAA Approved Page 19 of 65
GFC 700 LIMITATIONS
1. The GFC 700 AFCS preflight test must be successfully completed prior to
use of the autopilot, flight director or manual electric trim. Use of the
autopilot or manual electric trim system is prohibited if the preflight test is
not satisfactorily completed.
2. A pilot with the seat belt fastened must occupy the left pilot’s seat during
all autopilot operations.
3. The autopilot must be off during takeoff and landing.
4. Autopilot maximum engagement speed – 165 KIAS
Autopilot minimum engagement speed – 70 KIAS
Electric Trim maximum operating speed – 178 KIAS
5. The autopilot must be disengaged below 200 feet AGL during approach
operations and below 800 feet AGL during all other operations.
6. ILS approaches using the GFC 700 autopilot/flight director are limited to
Category I approaches only.

FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
190-00492-10 Rev 5 Diamond DA 40 / DA 40F
FAA Approved Page 20 of 65
CHARTVIEW LIMITATIONS
If the optional ChartView function is installed with GDU software version 8.02
and ChartView database cycle 0709 and prior, the following limitation applies:
At airport locations outside the United States within ±1.5° either side of zero
degrees latitude or longitude the aircraft symbol will be either missing or
incorrectly positioned on terminal charts to include airport diagrams and
approach procedures. Disregard the presentation of position information on all
terminal charts for airports within ±1.5° either side of zero degrees latitude or
longitude.
The list of affected airports below is subject to change by Jeppesen. This list is
accurate as of 30 MARCH 2007. All airports within ±1.5° either side of zero
degrees latitude or longitude will be affected.
Equatorial Region (zero degrees latitude):
ANYN, FOGR, FOOG, FZEA, FZGN, HKKI, HUEN, SBMD, SBMQ, SBUA,
SECO, SEGS, SEII, SELT, SEMT, SENL, SEQU, SEST, SESV, SETR, SKAC,
VRMG, WIPT, WIOO
Prime Meridian Region (zero degrees longitude):
DAOO, DAOV, DAUA, DAUT, DGAA, DGLE, EGCN, EGDM, EGGW,
EGHI, EGKA, EGKB, EGKK, EGLC, EGLF, EGLK, EGLL, EGNJ, EGNV,
EGNX, EGPB, EGPM, EGSC, EGSS, EGTC, EGTF, EGTK, EGUB, EGUL,
EGVN, EGVO, EGWU, EGXC, EGXE, EGXU, EGXW, EGYD, GAGO,
LEAL, LELC, LEVC, LEZG, LFBC, LFBD, LFBG, LFBH, LFBM, LFBN,
LFBP, LFBT, LFBZ, LFCY, LFDN, LFJR, LFOD, LFOH, LFOT, LFOU,
LFOV, LFRG, LFRI, LFRK, LFRM, LFRN