Sandel
Avionics
SN3308 Navigation Display
Installation Manual
90106-IM-G(4) Installation Manual W SIG.doc
Page 8
1
GENERAL
INFORMATION
1.1 Introduction
The information contained within this Installation Manual describes the features,
functions, technical characteristics, components, approval procedures, installation
considerations, setup procedures, checkout procedures, and instructions for
continued airworthiness for the Sandel Avionics SN3308 Navigation Display. The
SN3308 is available in several dash-number configurations depending on installation
on pilot’s side, copilot’s side, or center panel. In the manual any reference to GPS
receivers is generic and can be applied to Loran receivers.
1.2 Equipment
Description
1.2.1 Features
The Sandel SN3308 Navigation Display is an advanced microprocessor controlled
airborne multipurpose electronic display which is FAA approved under technical
standard order TSO-C113. The SN3308 employs a patent-pending active matrix
liquid crystal (AMLCD) projection display. It is designed to combine the functions of:
x
Horizontal Situation Indicator (HSI)
x
DME Readout
x
Marker Beacon Indicator
x
WX-500 Stormscope® Display
x
Long-Range Navigation (GPS or Loran) Map Display
x
GPS Annunciators and External Mode Switches
Outputs of heading and course datum and bootstrap heading output are provided.
The versatile digital and analog interface properties of the unit provide for
compatibility with most VHF navigation receivers, ADF’s, DME’s, GPS’s, remote
gyros and flux gates.
The SN3308 is designed to display the downloaded flightplan data from a connected
GPS receiver or from a Jeppesen database (available on software version 2.00 or
later). The moving map database for the SN3308 as well as the internal operating
system software are field uploadable through the use of a portable computer
equipped with a Windows operating system and an RS-232C Serial Port.
