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
PAGE
1-2
(This page intentionally left blank)