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SANDEL SN4500 4/5-ATI High-Definition Primary Navigation Display

Offering modular convenience and flexibility, Sandel’s SN4500 High-Definition Primary Navigation Display is the new standard in NAV displays. Incorporating patented LED backlight technology, the SN4500 is the ideal replacement for aging 4-in. and 5-in. electromechanical HSIs, to give your cockpit unmatched resolution, unbelievable color and a state-of-the-art technology update.

Featuring an ultra-wide viewing angle (180 degrees in both the horizontal and vertical axes), the SN4500 also boasts an MTBF in excess of 10,000 hours. And with Sandel’s patented display engine generating a resolution of 200 pixels per inch — unmatched in the industry for brightness clarity, readability and color fidelity — you’ll find the SN4500 transforms your panel as it gives you a better view of the airspace around you.

Drawing from our experience with thousands of compact integrated displays in service, we designed the SN4500 to do what nothing else can: Replace your electromechanical HSI with a modular electronic display.

This allows you to achieve maximum performance at minimum disruption to your aircraft. And by saving on both acquisition and installation costs, the SN4500 is a cost-effective way to enhance both the operational and the residual value of your aircraft. Reliable, affordable and backed by Sandel’s award-winning product support.

The SN4500 improves situational awareness by presenting Compass, Map, Flight Plan and safety systems data in a bright, high-resolution format. FAA-certified as a primary navigation display, the SN4500 even incorporates overlaid weather, along with traffic information from TCAS, TCAD and TAS receivers, to maximize situational awareness.

It also incorporates our revolutionary Smart I/O, which automatically accepts input from analog and digital aircraft systems, streamlining installation and reducing costs.

Key Features & Functions:

  • Bright, sunlight-readable, high-definition LED-backlit display with 200-pixel-per-inch resolution — twice that of conventional liquid crystal or CRT screens
  • Patented LED backlight technology for high reliability and long life
  • Displays vertical deviation from WAAS-enabled GPS receivers
  • Ultra-wide left-to-right/up-down viewing angle
  • Full-color moving map supporting GPS- or FMS-supplied waypoints, heading, bearing pointers for VOR and ADF, DME display and marker beacons
  • Upgradable system combines navigation with TCAS and datalink weather
  • Internal Jeppesen NavData™ database supplements IFR flight plan data and approach waypoints derived from your GPS receiver’s IFR-approved database
  • One-touch toggle between 360-degree compass and 70-degree ARC view
  • HDG and CRS sync functions automatically set the heading bug directly to your current heading, or the course pointer to a VOR station
  • Graphical bearing pointers and digital bearings supplied for any selected navigation source
  • Auto-slew function simplifies waypoint sequencing
  • Supports remote heading and course knobs
  • One-touch declutter for each display item
  • Approved for use as a primary navigation display
  • Designed for turbine-powered fixed-wing aircraft and helicopters
  • Compatible with 4-in. and 5-in. instrument panels

Specifications:

  • Weight
    • SN4500: 3.5 lb. (1.59 kg)
    • Bracket & Connectors: 0.5 lb (0.23 kg)
  • Dimensions
    • 9.60 in (24.384 cm)
      9.27 in (23.546 cm) from panel to back of unit
    • Body: 3.970 in x 3.970 in (10.084 cm x 10.084 cm)
    • Bezel: 4.060 in x 4.060 in (10.312 cm x 10.312 cm)
  • Power Requirements: 22-33 VDC, 28 VDC @ 1.4A (40W) nominal
  • Cooling Requirements: Internal fan requiring ambient air at fan input
  • Mounting: Standard 4-ATI panel cutout with clamp and Positronic® connectors.
    Bezel adapters available for mounting in 4x5 and 5x5 panel cutouts
  • Operating Environment: -20° C. to +70° C., +55,000 ft. altitude (max.)
  • Certification Basis: TSO C113, Airborne Multipurpose Electronic Displays, and TSO C6d,
    C34e, C35d, C36e, C40c, C41d, C118
    DO-160E Env. Cat. [(A2)(F1)Z]BAB[HR]XXXXXXZBABBC[WW]M[XXE2F2X]XXAX
    DO-178B, Software Level C
    DO-254, Hardware Level C
  • Interfaces
    • Heading: Bi-phase stepper (Mid-Continent 4305 & KG102)
      XYZ synchro (ARINC 407)
      ARINC 429
    • Flux Gate: Standard 400-Hz XYZ 3-wire interface with external excitation (if required)
    • NAV: Analog and ARINC 429
    • DME: 2 King serial or ARINC 568 digital (e.g. KN62/64, KN63)
      1 Analog DME input (40 mV/nm)
    • ADF: SIN/COS, Synchro and ARINC 429
    • GPS: ARINC 429, RS-232 and RS-422
    • Composite NAV: 2 ARINC 0.5V inputs, Internal NAV Converter
    • Marker Beacons: 3 discrete inputs
    • Switch/Annunciators: Discrete and ARINC 429
    • Lightning Detection: WX-500 Stormscope
    • Traffic (option): ARINC 429 (TAS, TCAD, TCAS I and TCAS II)
    • Weather (option): RS-232 datalink weather