Innovative Solutions & Support, Inc.

The IS&S 10” Flat Panel Display is a self-contained display unit with a built-in Symbol Generator, offering superior performance with a high resolution XGA multi-color LCD flat panel display. The 6×8 inch viewing area (10.4” diagonal) provides enhanced readability, an 80 degree viewing angle, NVIS compliant display lighting, and a non-glare, anti-reflective display surface. The 10” flat panel display is available in PFD and ND format and is available across all three market segments for a variety of cockpits both OEM and retrofit.

Air Data, Attitude and Heading Reference System (ADAHRS) replaces DGVG’s, AHRS and air data computers in a single, compact, light-weight unit. Coupled with the IS&S Beta-3 GPS Receiver it can provide INS grade performance to 25 foot 3D positional accuracy. The IS&S ADAHRS outputs in Digital and Analog in format aircraft attitude, heading, altitude and air speed to interface with existing autopilot and display systems at a fraction of the cost of comparable AHRS alone. Features and Benefits: Versatile interface capability Highly accuracte air data sensors Directional Gyro Mode Software RTCA DO-178B level B Control interfaces via discretes andor ARINC 429 RVSM support GPS aiding for improved accuracy

Technical Overview The IS&S Model 9B-81103-1 Air Data Sensor (ADS) replaces the Rockwell Collins 590A- 3H3J3K3J13K1 Air Data Sensor as either a formfit function replacement unit, or as part of a more comprehensive Reduced Vertical Separation Minimum (RVSM) compatible air data system upgrade. This upgrade includes the IS&S Model 9D-80130 Air Data Display Unit (ADDU). In both configurations the ADS utilizes the same tray and aircraft mating connectors as the displaced Collins 590 unit. The ADS operates the same in both configurations, relative to the flight control system interface and operation. The ADS supplies an analog error signal to the flight control system (FCS) that is proportional to altitude HOLD error, vertical speed HOLD error, Mach HOLD error, Indicated Airspeed HOLD error, or preselect altitude error that is used by the FCS to ascend or descend to a preselected altitude. True Airspeed, Indicated Airspeed, and Altitude programming voltages are also supplied to the flight control system. Reliability and Maintainability Long-term supportability due to modern design. Two-year warranty. MTBF 20, 000 hours. Features Form, fit and function replacement for obsolete Collins – 590A Air Data Controller models: 622-4393-0XX 622-4394-0XX 622-1001-0XX 792-6672-0XX 622-3204-0XX Approved letter of equivalency from OEM of 590A – no certification effort required. Embedded solid-state transducer. Added functions over and above 590A: PIN programmable with aircraft configuration memory module. Applications All aircraft currently using Collins PN (-590A Air Data Controller – includes 590A-3H, 3J, 3K, 3J1, 3K1 series). Civil, military and business aviation. Qualifications DO-160D Environmental Qualification DO-178B Level B software FAA TSO, C106, 52A, C9C Letter of equivalency from the original 590 OEM HIRF > 100 voltsmeter Benefits Plug and Play Replacement for Collins – 590A Air Data Controller. Integrates easily with IS&S RVSM ADDU architecture, including SSEC data. Outputs required Altitude Hold to Auto Pilot (RVSM). With IS&S ADDU, provides certifiable RVSM solution for many aircraft types. Weight savings. Solid state SMT design.