Garmin Embraer Prodigy 300 NXI User manual

AFMS, G1000 NXi and GFC 700 AFCS in Embraer Model EMB-505 (P300) 190-02545-11 Rev. 1 Page 2 of 40 FAA APPROVED

Garmin Ltd. or its subsidiaries

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 prior written consent 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 and to print one copy of this manual or of any revision hereto, 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 International, Inc.

1200 E. 151st Street

Olathe, KS 66062 USA

Telephone: 913-397-8200

www.garmin.com

190-02545-11 Rev. 1 AFMS, G1000 NXi and GFC 700 AFCS in Embraer Model EMB-505 (P300)

FAA APPROVED Page 3 of 40

Garmin International, Inc.

Log of Revisions

FAA Approved Airplane Flight Manual Supplement for

G1000 NXi Integrated Avionics System and GFC 700 AFCS in Embraer Model

EMB-505 (Phenom 300)

REV

NO.

PAGE NO(S)

DESCRIPTION

DATE OF

APPROVAL

FAA APPROVED

ALL

Original Issue

See Cover

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Table of Contents

Section I – General ...................................................................................................................................... 7

Section II – Operating Limitations ............................................................................................................. 12

Section III – Operating Procedures ........................................................................................................... 25

Section IV – Performance ......................................................................................................................... 33

Section V – Supplements .......................................................................................................................... 35

Section VI – Weight and Balance .............................................................................................................. 37

Section VII – Advisory Information .............................................................................................................. 39

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Section I – GENERAL

The information in this supplement is FAA-approved material and must be attached to the FAA Approved Airplane Flight Manual (AFM) when the airplane has been modified by installation of the Garmin G1000 NXi avionics upgrade in accordance with Garmin International, Inc. approved data, STC SA01933WI.

The information in this supplement supersedes or adds to the basic AFM only as set forth below. Users of the manual are advised to always refer to the supplement for possibly superseding information and placarding applicable to operation of the airplane.

The Garmin G1000 NXi system installed in the Embraer Model EMB-505 (Phenom 300) provides a fully integrated Display, Communications, Navigation and Flight Control system. Functions provided by the G1000 NXi system include: Primary Flight Information, Powerplant Monitoring, Navigation, Communication, Traffic Surveillance, TAWS Class A or B, Weather Avoidance, and a three-axis automatic flight control / flight director system.

Use of this supplement requires the installation of Garmin G1000 NXi hardware and system software version 3643.01 or later in the aircraft. Pilots are advised to carefully review the contents of this revision before operating the airplane.

The following table lists the Pilot’s Guide and Cockpit Reference Guide applicable to the respective system software version.

System Software

Version

Pilot’s Guide Part Number

Cockpit Reference Guide

Part Number

3643.01 or later

190-02548-00 Revision A or later

190-02549-00 Revision A or later

Table 1 - Applicable Pilot's Guide and Cockpit Reference Guide

USE OF THE AFMS

The following definitions apply to WARNINGS, CAUTIONS and NOTES found throughout the AFMS:

OPERATING PROCEDURES, TECHNIQUES AND OTHER RELATED INFORMATION WHICH MAY RESULT IN PERSONAL INJURY OR LOSS OF LIFE IF NOT FOLLOWED.

CAUTION

OPERATING PROCEDURES, TECHNIQUES AND OTHER RELATED INFORMATION WHICH MAY RESULT IN DAMAGE OR DESTRUCTION OF EQUIPMENT, IF NOT FOLLOWED.

NOTE

Operating procedures, techniques and other related information which are considered essential to emphasize.

WARNING

AFMS, G1000 NXi and GFC 700 AFCS in Embraer Model EMB-505 (P300) 190-02545-11 Rev. 1 Page 8 of 40 FAA APPROVED

ELECTRONIC FLIGHT BAG

Electronic aeronautical charts displayed on this system have been shown to meet the guidance in AC 12076D as a Type B Electronic Flight Bag (EFB) for FliteCharts and ChartView. Additional requirements may make a secondary source of aeronautical charts necessary on the aircraft and available to the pilot, such as traditional paper charts or an additional portable electronic device. If the secondary source of aeronautical charts is a Portable Electronic Device (PED), its use must be consistent with the guidance in AC 120-76D.

For operations under 14 CFR 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 airplane. If the source of aeronautical information is in electronic format, operators must determine non-interference with the G1000 NXi system and existing aircraft systems for all flight phases.

Garmin International holds an FAA Type 2 Letter of Acceptance (LOA) in accordance with RTCA/DO-200A and AC 20-153B for database integrity, quality, and database management processes for many of its aviation databases. LOA status and RTCA/DO-200A List of Applicable Avionics (190-01999-00) can be viewed at FlyGarmin.com.

REDUCED VERTICAL SEPARATION MINIMUMS (RVSM)

This airplane is equipped for operations in Reduced Vertical Separation Minimum (RVSM) airspace when the required equipment is maintained in accordance with the Airplane Maintenance Manual. This does not constitute operational approval. Operational approval must be obtained in accordance with applicable operating rules.

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ABBREVIATIONS AND TERMINOLOGY

The following glossary is applicable within the airplane flight manual supplement

AC Advisory Circular ADS-B Automatic Dependent Surveillance - Broadcast AFCS Automatic Flight Control System AFM Airplane Flight Manual AFMS Airplane Flight Manual Supplement AHRS Attitude and Heading Reference System ALT Altitude, or AFCS altitude hold mode, or ALT button on the GMC 710 AFCS

Mode Controller

AMC Acceptable Means of Compliance AMMD Airport Moving Map Display APCH Approach Aux Auxiliary B-RNAV Basic Area Navigation BARO Barometric Setting CFR Code of Federal Regulations CS-ACNS Certification Specification – Airborne Communications, Navigation, and

Surveillance

DEST Destination EASA European Aviation Safety Agency EFB Electronic Flight Bag ELEV Elevation ESA Enroute Safe Altitude FAA Federal Aviation Administration FDE Fault Detection/Exclusion FIS-B Flight Information Service-Broadcast FMS Flight Management System FPL Flight Plan FPM Feet Per Minute FRT Fixed Radius Transitions GDU Garmin Display Unit GFC Garmin Flight Control GIA Garmin Integrated Avionics Unit GMC Garmin Mode Control Unit GNSS Global Navigation Satellite System GPS Global Positioning System

AFMS, G1000 NXi and GFC 700 AFCS in Embraer Model EMB-505 (P300) 190-02545-11 Rev. 1 Page 10 of 40 FAA APPROVED

ICAO International Civil Aviation Organization IFR Instrument Flight Rules JAA Joint Aviation Authorities LNAV Lateral Navigation LNAV/VNAV Lateral Navigation / Vertical Navigation LOA Letter of Acceptance LP Localizer Performance LPV Localizer Performance with Vertical Guidance MFD Multi-Function Display MPS Meters per Second MSA Minimum Safe Altitude MSL Mean Sea Level MT Meters ODA Organization Designation Authorization PBN Performance Based Navigation PED Portable Electronic Device PFD Primary Flight Display P-RNAV Precision Area Navigation QFE The altimeter setting which will cause the altimeter to read the height above

the airport or runway threshold elevation. RAIM Receiver Autonomous Integrity Monitoring RF Radius-to-Fix RNAV Area Navigation RNP Required Navigation Performance RVSM Reduced Vertical Separation Minimums SAPT Service Availability Prediction Tool SBAS Satellite Based Augmentation System STC Supplemental Type Certificate STD Standard TAWS Terrain Awareness and Warning System TGL Temporary Guidance Leaflet TIS Traffic Information System TOAC Time Of Arrival Control TSO Technical Standard Order VFR Visual Flight Rules VNAV Vertical Navigation VNV Vertical Navigation Button on the AFCS Mode Controller

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VS Vertical Speed VSD Vertical Situation Display WAAS Wide Area Augmentation System WFDE WAAS Fault Detection/Exclusion WGS-84 World Geodetic System – 1984

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Section II – OPERATING LIMITATIONS

TABLE OF CONTENTS

GARMIN G1000 NXi Avionics System ...................................................................................................... 13

G1000 NXi GNSS (GPS/SBAS) Navigation System Operational Approvals ............................................ 14

G1000 NXi GNSS (GPS/SBAS) Navigation System Limitations .............................................................. 22

Traffic Avoidance System Limits ............................................................................................................... 23

Data Link Weather (XM, CONNEXT, or FIS-B Weather) .......................................................................... 23

Kinds of Operations Equipment List .......................................................................................................... 23

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