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SANDEL SG102 PILOT’S GUIDE
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III
Pilot information
Original Publication Date: 10 APR 2014
This guide provides information on the use and operation of the SG102
Attitude Heading Reference System.
Information in this guide is current as of publication or revision date.
Specifications and operational details are subject to change without notice
at the discretion of Sandel Avionics, Inc.
Copyright
Copyright 2014 Sandel Avionics, Inc.
May be covered by one or more US and foreign patents (pending).
All rights reserved. No part of this manual may be reproduced, stored or
distributed without written permission of Sandel Avionics, Inc. Additional
copies of this manual are available from:
Sandel Avionics, Inc.
2401 Dogwood Way
Vista, CA 92081
USA
Tel: (760) 727-4900
Fax: (760) 727-4899
www.sandel.com
Revision notice
The “Effectivity, Errata, and Revision History” allow the use of this Pilot
Guide with a specific software release. The “Effectivity, Errata, and
Revision History” specifically lists the software to which this Pilot’s Guide
applies and corrects any errors or omissions in this revision of the Pilot’s
Guide. Document number 82011-PG-ERR, Effectivity, Errata, and
Revision History” can be found on page VI of this Pilot’s Guide.
Operational and legal issues
The information provided by the SG102 is displayed by external
equipment. It is the pilot’s responsibility to ensure the correct
configuration and use of the external equipment. Always refer to your
approved Aircraft Flight Manual Supplement for operation and limitations
on the use of installed equipment.
Note: Because aircraft vary in their installed equipment, it is important to
note that what is displayed by the information provided by the SG102 may
vary depending on the presence or absence of equipment.
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SANDEL SG102 PILOT’S GUIDE
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IV
Approvals
The FAA has approved the SG102 under the following TSOs:
TSO-C4c
Bank and Pitch Instruments
TSO -C6d
Direction Instrument, Magnetic (Gyroscopically Stabilized)
The following RTCA Standards apply to this product:
DO-160E:
Environmental (See Installation Manual)
DO-178B
Software Level C
Installation of the SG102 Attitude Heading Reference System in a type-
certificated aircraft must be performed in accordance with the Sandel
SG102/MT102 Installation Manual, document number 82011-IM (latest
revision).
Conventions Used in This Manual
This manual uses terms, which should be familiar to aviation-minded
readers, such as “magnetic heading” and “gyro”. Terms, which are
specific to the SG102, will be placed in the glossary.
