Electronic Standby Instrument Display
OAS S The most trusted name in aircra instrumenta on now offers the OASIS®, a new standby instrument system. This display replaces mul ple mechanical gauges with one highly reliable, highly accurate 3-inch device. A separate sensor module allows for the display instrument to fit in the smallest and most shallow panel spaces while the sensor module can be placed in any convenient space in the aircra , elimina ng running pitot/sta c plumbing through the firewall. The OASIS® is available at less than the cost of tradi onal instruments and eliminates addi onal costs associated with repair and calibra on of older mechanical gauges while reducing system weight compared to conven onal backup instruments. In the event that the func on of primary flight displays is lost, you can transi on seamlessly to the familiar format on the OASIS®. Ba ery power provides further protec on from power loss and allows you to focus on the flight cri cal informa on. Complete your all glass cockpit upgrade with the new OASIS®.
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Instruments Sensors Displays Engineering Test Equipment Repair & Overhaul
OASIS® FUNCTIONALITY • Al tude • Airspeed • A tude • Heading (requires remote magnetometer) • Ver cal speed (op onal) • Slip / Skid (op onal) • Rate of turn (op onal) OPERATING SPECIFICATIONS • Al tude: -1000 to +51,000 • Airspeed: 20 to 450 kts • Max roll rate: 200 deg/sec • Opera ng temperature: • Display: -20 to +55 degrees C • Sensor package: -40 to +71 degrees C • Baro se ng: 28.00 to 30.99 • Reliability: 10,000 hrs MTBF • DO 178B Level B • DO 254 Level B • DO 160F • TSO (expected July 2012) FEATURES • Power supply: 10-33 volts DC • Power consump on: 14 wa s at 28 volts DC • Display: 3.5” with wide VGA; 800 x 480 pixels • NVG compa ble (op onal) • The display module includes the following input/output • One channel of RS422 for ADC interface • One channel of RS422 for AHRS interface • One USB 2.0 port for system maintenance • Power input supplied from ADAHRS Module • The ADAHRS module includes the following input/output • Interface to an external magnetometer including power (op onal) • Two channels of RS422 for Display Module interface • Power output to Display Module • Power input supplied by Ba ery Backup unit (op onal) • Pneuma c ports for Pitot/Sta c source(s)
1212 N Hercules Avenue Clearwater, FL 33765 +727.461.3000 FAX +727.447.5926 www.aerosonic.com