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82011-PG-E 

SANDEL SG102 PILOT’S GUIDE 

PAGE  

Table of Contents 

Pilot information 

iii

 

Copyright iii

 

Revision notice 

iii

 

Operational and legal issues 

iii

 

Approvals iv

 

Conventions Used in This Manual 

iv

 

Table of Contents 

v

 

Effectivity, Errata and Revision History 

vi

 

CHAPTER 1 WELCOME TO THE SG102 

1-1

 

What is the SG102? 

1-1

 

Limitations 1-1

 

CHAPTER 2 OPERATION 

2-1

 

NORMAL OPERATION 

2-1

 

ABNORMAL OPERATION 

2-2

 

CHAPTER 3 TECHNICAL SPECIFICATIONS 

3-1

 

CHAPTER 4 INSTALLATION INFORMATION 

4-1

 

CHAPTER 5 GLOSSARY 

5-1

 

CHAPTER 6 AVIONICS ACRONYMS 

6-1

 

82011-PG-E 

SANDEL SG102 PILOT’S GUIDE 

PAGE  

VI 

Effectivity, Errata and Revision History 

 

Applies to:

   

SG102/D 

 

SG102 (Mod 1 & Mod 2) 

 MT102 

 

 
With the exception of the superseding information contained in this 
section, operation of the SG102 is as described in the SG102 Pilot’s Guide 
referenced above. 
 

Revision Date 

Comments 

10-APR-2014 

Effectivity, Errata and Revision History 
updated. 
Previous Errata incorporated. 
Page 1-1: SG102/D and SG102 Mod 2 
information added. 
Page 2-1: Initialization information 
updated. 
Page 2-2: Power Interruptions 
description updated. 
Page 3-1: Operational Specifications 
removed. 
Page 4-1: Line for Mod level added. 

D4 

16-FEB-2011 

Updated for software release 1.31 

D3 

03-NOV-2009 

Updated for software release 1.30 

D2 

22-MAY-2009 

Updated for software release 1.26 

D1 

07-MAY-2009 

Updated for software release 1.25 

11-FEB-2009 

Updated copyright. 
Errata removed. 
Updated limitations. 

06-NOV-2008 

Page 2-1 Preflight Initialization period; 
Errata updated. 

31-OCT-2008 

Page vi:  Updated for software release 
1.10 and SG102 Mod 1; Errata updated. 

18-DEC-2008 

Initial Release 

 

Errata 
 

None

Summary of Contents for SG102 AHRS

Page 1: ...described in the SG102 Pilot s Guide referenced above 82011 PG ERR E4 SANDEL SG102 PG ERRATA PAGE 2 OF 2 Chapter 1 Limitation 3 regarding aerobatic flight should be updated to read as follows Aerobat...

Page 2: ...SG102 Attitude Heading Reference System Pilot s Guide Revision E 82011 PG E SANDEL SG102 PILOT S GUIDE PAGE II This page intentionally left blank...

Page 3: ...d 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...

Page 4: ...tion contained in this section operation of the SG102 is as described in the SG102 Pilot s Guide referenced above Revision Date Comments E 10 APR 2014 Effectivity Errata and Revision History updated P...

Page 5: ...and Mod 2 The roll and pitch information provided by the SG102 may not be used to display primary aircraft attitude to the aircrew The roll and pitch information may be used to display reversionary o...

Page 6: ...nder normal conditions the SG102 should be operated with Slaving ON by moving the Slaving selector switch to the ON position To operate in the Slaving OFF mode move the Slaving selector switch to the...

Page 7: ...nce Technical Standard Order TSO TSO C4c Bank and Pitch Instruments TSO C6d Direction Instrument Magnetic Gyroscopically Stabilized Software Certification RTCA DO 178 Level C Environmental Category RT...

Page 8: ..._________________________________ Installer Phone ________________________________________ Work Order __________________________________________ Installer _____________________________________________...

Page 9: ...OSSARY Magnetometer A device that measures the earth s magnetic field Failure The inability of the equipment or any sub part of that equipment to perform within specified limits 82011 PG E SANDEL SG10...

Page 10: ...light Manual Supplement AHRS Attitude Heading Reference System FAA Federal Aviation Administration HDG Magnetic Heading POH Pilot s Operating Handbook RTCA Radio Technical Commission on Aeronautics rt...

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