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82011-PG-ERR-E4  SANDEL SG102 PG ERRATA  

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SG102 AHRS 
 
Pilot’s Guide Effectivity and Errata 

 
Insert this update ahead of the cover page of the Pilot’s Guide referenced 
below. 
 

 

Date: 

 

Effectivity: 

 
 
 
 
 
 

Errata: 

 
10-MAY-2016 
 

Pilots Guide 82011-PG-E 
 
SG102 Software Version 1.35 for SG102 (Mod 1) 
SG102 Software Version 1.62 for SG102 (Mod 2)  
SG102 Software Version 1.62 for SG102/D 
MT102 Software Version 1.00 

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

 

 

 

 
 

 

82011-PG-ERR-E4  SANDEL SG102 PG ERRATA  

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Chapter 1 Limitation #3 regarding aerobatic flight should be updated to 
read as follows: 
 
Aerobatics: Permitted, software version 1.25 and later. Aerobatic 
maneuvers must be approximately wings level 50% of the time over any 5 
minute period. 
 
 
 
 
Chapter 2 “Power Interruptions” statement should be updated to read as 
follows: 
 
The SG102 can recover from momentary power interruptions in flight 
without losing its initialization. If extended power interruptions are 
experienced and the gyro flag remains, it will be necessary to use an 
alternate means of primary heading information for the remainder of the 
flight. 
 
 
 
 
 

 

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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