Garmin Cessna Caravan G1000 Konfigurationshandbuch

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

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

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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

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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

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•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

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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.

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