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82011-PG-E 

SANDEL SG102 PILOT’S GUIDE 

PAGE  

1-1 

CHAPTER 1

 

   WELCOME TO THE SG102  

What is the SG102? 

The Sandel model SG102 is a solid-state Attitude Heading Reference 
System (AHRS) that combines angular rate, linear acceleration and 
magnetic field measurements to provide primary heading information. 

Roll and pitch information is provided for stabilization of other equipment 
such as weather RADAR or FLIR cameras etc.  

Limitations 

1.

 

For SG102/D, and  SG102 (Mod 1 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 or 
backup attitude information to the flight crew in the primary 
field of view. 

 

2.

 

For SG102 Mod 0: The roll and pitch information provided 
by the SG102 may not be used to display aircraft attitude to 
the aircrew. 

 
3.

 

The SG102 is not approved for aerobatic flight. 

 

4.

 

The SG102 may not provide satisfactory heading 
performance above 70° north latitude or below 70° south 
latitude. 

 

 

 

 

82011-PG-E 

SANDEL SG102 PILOT’S GUIDE 

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1-2 

 

 

 

 

 

 

 

 

 

 

 

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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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