19711 CAMPUS DRIVE  SANTA ANA, CA 92707
PHONE: 949-757-0290 FAX: 949-757-0293
FAA CERTIFIED REPAIR STATION YH3R997L
                   

 
Sandel
ST3400 TAWS/RMI Display
ST3400 The Sandel ST3400 is an integrated panel-mount system that outperforms cumbersome remote-mount TAWS systems that weigh and cost far more. A 3-ATI-size system that features a TAWS database, processor and oversized, high-resolution color display in a single unit, the ST3400 meets TSO C151b for both Class A and Class B requirements. Also incorporating RMI functionality, the ST3400 serves as a drop-in replacement for conventional RMI units, displaying terrain maps, topographic maps, navigation waypoint maps and TCAS data.

Key Features

  • TSO’d and FAA-approved for Class A and Class B TAWS requirements
  • Self-contained, panel-mounted unit combines terrain, traffic and NAV
  • Full-time, 360-degree-viewable, sunlight-readable display
  • Full-time terrain and topo mapping, with TCAS I overlays and track-based flight plans
  • Patented SandelSmart I/O for analog and digital compatibility
  • Direct aftermarket replacement for standard RMI units
  • Easy and inexpensive to install
 ST3400
ST3400

Operational Benefits

  • Complete FAA TAWS compliance
  • Meets Class A TAWS requirements for airlines and Part 135 operations
  • Meets Class B TAWS requirements for Part 91 operations
  • Full-time terrain display
  • Runway and waypoint overlay
  • Integrated TAWS computer and flat-panel display
  • RMI display
  • Highly reliable
Click here to download the Manufacturers Brochure for the ST3400
Specifications

Weight

  • 3.2 lb. (1.45 kg)

Size

  • 3ATI x 9.27 in. (23.55 cm) rear of ST3400 bezel to ST3400 rear panel
    (excluding Positronics ‘D’ connectors)

Mounting

  • Flush mount or protruding bezel using rear mounted clampshell

TSO

  • C151b TAWS (Class A and Class B versions available)
  • C113a Multi-Function display

Display

  • 1 mega-pixel, 256 color

Environmental

  • l DO-160D
  • [(A2)(F1)]ZBAB[(H)(R)]XXXXXXZBABB[WW]M[XXF2]XXA

Cooling

  • Internal Fan, no forced air required

Power

  • 28VDC 35 watts nominal

Software

  • DO-178B, Level C

Database

  • Jeppesen Terrain/Obstacle and Airports/Runways

Data Loading

  • Front mounted mini-USB port using Windows 2000 (or later) compatible PC

Config. Module

  • Rear mounted plug-in aircraft configuration module Interfaces

GPS/FMS

  • ARINC 429 or RS-232; includes position, flight plan data, and RMI bearing

Air Data

  • ARINC 429, RS-232 or Analog (Not required in Class B installations when used with approved GPS receiver supplying altitude data)

OAT

  • ARINC 429 or direct connect to standard probe (Required if barometric altitude is used)

Heading

  • ARINC 429 or XYZ

Gear/Flap

  • Discrete (Optional in Class B installations)

RMI ADF

  • ARINC 429 DC SIN/COS or XYZ

VOR

  • ARINC 429 or Composite Video

Glideslope

  • ARINC 429 or low-level analog (Optional in Class B installations)

Radar Altimeter

  • 0-2,000 ft. or 0-2,500 ft. (Optional in Class B installations) ARINC 565, ALT-50, ALT-55

Traffic

  • (TAS, TCAD and TCAS I): ARINC 429

Audio

  • 600-ohm low-level and 8-ohm direct speaker outputs

Remote Annunciators

  • ARINC 429 or Discrete, 250ma maximum (optional)

Data Recording

  • 10 hours of TAWS flight data, including recording of alert data, output via USB

Note: Two inputs available for each source for reversionary operation (2nd input optional)