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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...
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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...
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.
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 ...
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...
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.
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...
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