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Sandel ST3400 TAWS/RMI  And now it's under $20,000*.

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ST3400 TAWS/RMI 

What is the Sandel ST3400 TAWS/RMI?

The Sandel ST3400 TAWS/RMI represents a true breakthrough in TAWS technology.  It is the industry’s first self-contained Class A or Class B system that includes an integrated full-color, multi-screen, edge-to-edge display with a built-in RMI function.

Because the ST3400 is a self-contained TAWS system that replaces an existing RMI, the ST3400 does not demand the installation facility associated with other TAWS equipment. This means a substantial cost savings on the installation and less downtime for the aircraft. In many aircraft the ST3400 can be installed in half the time required for other TAWS systems that provide only TAWS capabilities. The ST3400 can be installed in most business aircraft for 50%-70% of the cost to install others TAWS equipment. This includes installation, labor and all necessary interfaces. In addition, the Sandel ST3400 provides higher graphics performance making it the preferred TAWS solution.

Here are just a few of the features that distinguish the ST3400 TAWS/RMI as the higher-performing TAWS system. 

  • Integrated color display. Provides full-time situational awareness that greatly enhances flight safety-not shared with the radar display
  • Real-time graphics. Unlike radar display solutions, the ST3400 displays move with the aircraft heading instantly. It displays a true terrain picture with no latency or delays
  • Standard 3ATI chassis. The ST3400 has minimal or no impact on existing panel layouts
  • Mechanical RMI replacement. Designed as a direct replacement for existing old mechanical RMI’s
  • Smart-interface technology (Patent Pending). Compatible with all vintages of aircraft systems both analog and digital
  • Software configurable. Allows the use of an aircraft resident configuration module
  • Minimal crew training. Intuitive and easy to use, requiring minimal crew orientation
  • Patented rear-projection technology. Use’s Sandel’s patented edge-to-edge display technology providing a large viewing area that is sharp, brilliant and easily readable even in direct sunlight. The Sandel ST3400 TAWS display area is equal in size to a 4” display

The TAWS mandate 

You are probably aware that the FAA has mandated that all U.S.-registered, turbine powered aircraft with six seats or more to install a Terrain Awareness and Warning System (TAWS) by 2005.  TAWS is the new enhanced technology that replaces Ground Proximity Warning Systems (GPWS).

Key Features

  • A self-contained TAWS system with integrated color display and RMI function in a three-inch 3ATI package; no remote processors required
  • The most cost-effective and easy-to-install TAWS solution available
  • Installation time estimated at 30-60 hours
  • Display shows pilot-selectable RMI, terrain, and/or GPS/FMS flight plan
  • Integrated, two-pointer RMI with FMS available as an additional bearing source
  • RMI function defaults to TAWS warning when critical situation arises
  • Requires minimal crew training
  • Standard three-inch RMI-sized package has a minimal or no impact on existing cockpit panel layouts
  • Self contained color display eliminates the need to timeshare with displays such as radar, EFIS or Stormscopeâ
  • Provides predictive warning by comparing the terrain database to altitude data and positioning information from a GPS receiver, INS, FMS or Loran
  • Complies with FAA Class A or Class B TAWS requirements for passenger-carrying turbine aircraft
  • Sharp brilliant color display is readable even in direct sunlight
  • High reliability:  2,000 hour lamp replacement interval, 15,000 hour system MTBF
  • TSO'd to C151a and C113a

Common Applications

  • Use for cost-effective, high performance Class A or Class B FAA compliance
  • Use where ease-of-installation and minimum installation downtime is a primary consideration
  • Use where panel space is at a premium and a 3ATI form factor is desired
  • Use to replace a mechanical RMI and gain TAWS compliance in the process
  • Use when integrated dedicated TAWS display is desired so that radar, MFD or Stormscopeâ displays are not affected
  • Install two independent units cost-effectively to provide redundant (pilot and copilot) TAWS systems

 

ST3400 TAWS/RMI Specifications

Included Interfaces

  • Uses Sandal-pioneered smart interface technology compatible with all vintages of digital and analog aircraft systems
  • Analog and digital interfaces have been proven in thousands of Sandel SN3308 EHSI installations
  • Software configurable (no hardwire jumpers) allows use of airframe resident configuration module
  • External audio output for cautions/warnings
  • Discrete output(s) for master caution and warning
  • Front-mounted USB connector

Installation Components

  • Database uploads through 12 MB/s high-speed Mini-USB from external PC

Specifications
Size: 3ATI x 9.27” rear of ST3400 bezel to ST3400 rear panel, not including Positronics ‘D’ connectors
Mounting: Flush mount or protruding bezel using rear mounted clampshell
TSO: C151a (Class A), C113a
Display: 1 mega-pixel (360,000 color triad)
Environmental: DO-160D
Cooling: Internal Fan, no forced air required
Power: 28VDC nominal, 35 watts maximum
Weight: 3.2 lb.
Software: D0-178-B
Database: Jeppesen Terrain/Obstacle database and Airports/Runways database
Data Loading: Front mounted hi-speed mini-USB using Windows-98 (or later) compatible PC
Config Module: Rear mounted plug-in aircraft configuration module
Interfaces:
GPS/FMS: ARINC 429 or RS-232; includes position, flightplan data, and RMI bearing
Airdata: ARINC 429, RS-232 or Analog  (Not required in Class B installations when used with Garmin 400/500 series receivers)
OAT: ARINC 429 or direct connect to standard probe  (Required if barometric altitude is used)
Heading: ARINC 429 or XYZ
Gear/Flap: Discrete (not required Class B)
RMI:
ADF: ARINC 429 or DC SIN/COS or XYZ
VOR: ARINC 429 or Composite Video
FMS: Part of GPS/FMS input data
Glideslope: ARINC 429 or low-level analog (not required Class B)
Radar Altimiter: 0-2,000 ft. or 0-2,500 ft (not required Class B)
ARINC 565, ALT-50, ALT-55
Audio: 600 ohm unbalanced +14 dbm max
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)
 

 

 

 

 

 

To Contact Us:

Phone: 562.997.7375

Fax: 562.997.7334

sales@longbeachavionics.com

 

We are located on the Southwest corner of Long Beach Airport 

2901 East Spring St. Hanger E

Long Beach, Ca. 90806

Web Site Up-Date 02/03/03