The Oasis® is a new Electronic Standby Instrument System (ESIS). This system replaces multiple mechanical gauges with one highly reliable, highly accurate 4-inch diagonal display. The modular system architecture allows installation flexibility in an already crowded instrument panels by separation the Display Unit (DU) Aerosonic Sensing Unit (ASU). The display unit's thin design fits in the smallest and most shallow panel spaces while the ASU can be placed in any convenient space in the aircraft, eliminating running pitot / static plumbing through the bulkhead.
In the event that the function of primary flight displays is lost, you can transition seamlessly to the familiar format on the OASIS®. An optional internal battery power provides further protection from primary instrument power loss and will provide the flight critical information for a minimum of one hour.
Functionality:
Altitude
Airspeed
Attitude
Heading (requires remote magnetometer)
Slip / Skid (optional)
Display: 4.0 inch diagonal screen
Chassis: 3.0 inch ATI opening
Dimensions- Chassis depth: 1.35 inches, Bezel: 4.0 inches x 3.0 inches, Sensor Module: 3.0 inches x 3.0 inches x 6.25 inches
Display module includes the following input: Power input supplied from Sensor Module
Sensor module includes the following input / output: Interface to an external magnetometer including power (optional), Power output to Display Module, Pneumatic ports for Pitot / Static source(s), RS232 for AIr data, RS422 for AHRS data
Altitude: -1,500 to +55,000 ft
Airspeed: 20 to 450 kts
Max roll / pitch rate: 200 deg / sec
Operating temperature- Display: -20۫ to +55۫ C, Sensor Module: -40۫ to +70۫ C
Baro setting: 28.00 to 30.99
Reliability: 10,000 hrs MTBF
Unit
EA
Hazardous
No
Oversize
No
This part is included in the following categories: