Sandel SG102 Pilot's Manual

Attitude heading reference system (ahrs)
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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:
10-MAY-2016
Pilots Guide 82011-PG-E
Effectivity:
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
Errata:
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
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.
PAGE 1 OF 2
82011-PG-ERR-E4
SANDEL SG102 PG ERRATA
PAGE 2 OF 2

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Summary of Contents for Sandel SG102

  • Page 1 Insert this update ahead of the cover page of the Pilot’s Guide referenced Chapter 2 “Power Interruptions” statement should be updated to read as below. follows: The SG102 can recover from momentary power interruptions in flight Date: 10-MAY-2016 without losing its initialization. If extended power interruptions are...
  • Page 2 SG102 Attitude Heading Reference System (This page intentionally left blank) Pilot’s Guide Revision E 82011-PG-E SANDEL SG102 PILOT’S GUIDE PAGE II...
  • Page 3: Copyright

    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.
  • Page 4: Table Of Contents

      Operational and legal issues   With the exception of the superseding information contained in this Approvals section, operation of the SG102 is as described in the SG102 Pilot’s Guide   Conventions Used in This Manual referenced above.   Table of Contents  ...
  • Page 5: Chapter 1 Welcome To The Sg102

    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...
  • Page 6: Chapter 2 Operation

    Outputs Flagged Flying an aircraft equipped with an SG102 does not require any special If the SG102 is inoperative or detects an internal error, all outputs will be piloting skills; however there are a few key points for the pilot: flagged.
  • Page 7: Chapter 3 Technical Specifications

    (This page intentionally left blank) Technical TSO-C4c “Bank and Pitch Instruments” Standard Order (TSO): TSO-C6d “Direction Instrument, Magnetic (Gyroscopically Stabilized)” Software RTCA/DO-178, Level C Certification: Environmental RTCA DO-160E Category: 82011-PG-E SANDEL SG102 PILOT’S GUIDE PAGE 3-1 82011-PG-E SANDEL SG102 PILOT’S GUIDE PAGE 3-2...
  • Page 8: Chapter 4 Installation Information

    Installer Address: ______________________________________________________ (This page intentionally left blank) ______________________________________________________ ______________________________________________________ Installer Phone: ________________________________________ Work Order #: __________________________________________ Installer: ______________________________________________ Notes: ______________________________________________________ ______________________________________________________ ______________________________________________________ ______________________________________________________ Mod level: ______________________________________________________ 82011-PG-E SANDEL SG102 PILOT’S GUIDE PAGE 4-1 82011-PG-E SANDEL SG102 PILOT’S GUIDE PAGE 4-2...
  • Page 9: Chapter 5 Glossary

    A device that measures the earth’s magnetic field The inability of the equipment or any sub-part of that Failure equipment to perform within specified limits. (This page intentionally left blank) 82011-PG-E SANDEL SG102 PILOT’S GUIDE PAGE 5-1 82011-PG-E SANDEL SG102 PILOT’S GUIDE PAGE 5-2...
  • Page 10: Chapter 6 Avionics Acronyms

    Attitude Heading Reference System Federal Aviation Administration Magnetic Heading Pilot’s Operating Handbook (This page intentionally left blank) RTCA Radio Technical Commission on Aeronautics (rtca.org) Technical Standard Order 82011-PG-E SANDEL SG102 PILOT’S GUIDE PAGE 6-1 82011-PG-E SANDEL SG102 PILOT’S GUIDE PAGE 6-2...

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