Garmin G1000 guide for designated pilot examiners and certified flight instructors

G1000TM

guide for designated pilot examiners and certified flight instructors

Garmin G1000 Guide for Designated Pilot Examiners & Certified Flight Instructors

190-00368-02 Rev.A

COPYRIGHT

© 2004 Garmin Ltd. or its subsidiaries. All rights reserved.

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

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GarminAT, Inc., 2345Turner Road SE, Salem, Oregon 97302, U.S.A.
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Web SiteAddress: 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® is a registered trademark of Garmin Ltd. or its subsidiaries and G1000™ is a trademark of Garmin Ltd. or its subsidiaries. These trademarks may not be used without the express permission of Garmin.

November 2004

Printed in the U.S.A.

190-00368-02 Rev.A

Garmin G1000 Guide for Designated Pilot Examiners & Certified Flight Instructors

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TABLE OF CONTENTS & LIST OF FIGURES

TABLE OF CONTENTS

Copyright

Table of Contents & List of Figures

Introduction

G1000 System Overview

G1000 System Components

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1

2

3

GDU 1040..............................................................................................................................................................................................................................		3
GIA 63....................................................................................................................................................................................................................................		4
GDC 74A................................................................................................................................................................................................................................		4
GRS 77....................................................................................................................................................................................................................................		4
GTX 33/GTX 32.....................................................................................................................................................................................................................		5
GEA 71...................................................................................................................................................................................................................................		5
GMA 1347.............................................................................................................................................................................................................................		5
Sample System Operation/Failure Mode Scenarios for FAA-S-8081-4D		7
Areas of Operation Section IV: Recommendations for Failure Simulation.................................................................................................................		8
Areas of Operation Section IV: Recommendations for Failure Simulation (Cessna Nav III)................................................................................		10
Area of Operation SectionVII, D: Recommendations for Failure Simulation..........................................................................................................		10
Index		11
	LIST OF FIGURES
Figure 1	G1000 System..............................................................................................................................................................................................................	2
Figure 2	GDU 1040 (PFD Shown).............................................................................................................................................................................................	3
Figure 3	Reversionary Mode......................................................................................................................................................................................................	6
Figure 4	G1000 System Failure Indications............................................................................................................................................................................	6

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Garmin G1000 Guide for Designated Pilot Examiners & Certified Flight Instructors

190-00368-02 Rev.A

INTRODUCTION

Technology, such as that found in the G1000 integrated avionics system has the potential to bring a higher level of safety to general aviation (GA). However, this can only occur if pilots operating aircraft with such equipment are properly trained and held accountable to the Practical Test Standards (PTS). The purpose of this document is to provide both an overview of the typical G1000 potential failure modes and sample system operation/failure mode scenarios that correspond to the applicable sections of FAA-S-8081-4D, Instrument Rating Practical Test Standards, so that the Designated Pilot Examiner (DPE) and Certified Flight Instructor – Instrument (CFII) can properly prepare pilots for the instrument rating by simulating realistic failures and teaching appropriate failure response plans.

The system recommendations provided in this document are Garmin’s recommendations only and are superseded by the aircraft manufacturer’s recommendations and FAA-approved documentation for each aircraft model. The basic G1000 system architecture is similar across many aircraft models. However, the location of the actual components of the system, the location and grouping of the circuit breakers, and the engine instrumentation presentations vary between aircraft. Therefore, it is important to review the aircraft manufacturer documentation for each aircraft model.

NOTE:As part of Garmin’s commitment to flight safety,any specific questions or recommendations about both this document and the G1000 system as it is to be used for the instrument check-ride can be sent via e-mail to“[e-mail]”. For general questions, please visit “http://www.garmin.com/support” to correspond with Garmin’s aviation technical support specialists.

190-00368-02 Rev.A

Garmin G1000 Guide for Designated Pilot Examiners & Certified Flight Instructors

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