Specifications include, but are not limited to: 1. System camera components shall be self-contained in a compact, lightweight gimbal- mounted package designed specifically for mounting on the body of the Cessna 206H aircraft, see Attachment B, inconformance with the system integrator’s FAA Supplemental Type Certificate. External connection wiring to the aircraft cockpit shall be included with termination in a portable tablet-style computer for camera control, video image viewing and video image storage. Outputs shall be provided for external video display on alternate devices as well as the aircraft’s panel mounted display. 2. Electro Optic Visible Sensor: Full HD 1920x1080p, CMOS visible light sensor. 3. Visible Sensor Lens with continuous optical zoom 4. Thermal Sensor with sensitivity 5. Thermal Sensor Lens 6. Thermal Imager, HD Imager, with continuous zoom optics 7. Electronic Image Stabilization
