InnaLabs® high performance ITAR-Free inertial sensor solutions InnaLabs® offers a variety of inertial sensors including tactial grade Coriolis Vibratory gyroscopes (CVG) and navigation grade Quartz servo accelerometers offering our customers unparalleled performance

Fast and Intuitive Quality Inspection With precise AR overlay technology, deviations between 3D design data and real-world objects can be identified instantly. This enables fast and accurate quality inspections on the spot. Optimized and Lightweight 3D File Processing Supports the four most popular 3D file formats: FBX, GLTF, OBJ, and STL. Lightweight processing ensures faster matching and smoother inspection workflows. From Inspection to Report — All in One Inspection results can be recorded and documented with image captures, drawings, and notes. Final reports can be exported in PDF, XLS, or CSV formats, making them easy to share and manage.

- A red light mounted on the left side of the aircraft to indicate the aircraft's location - A green light mounted on the right side of the aircraft to indicate the aircraft's location - These lights indicate the aircraft's position, flight direction, and attitude - Visible/IR Mode, Steady/Flash Mode - Light Intensity : FAA FAR 29.1391 ~ 29.1395 - SAE ARP 5825A

Engine Start Begins with ATS. The Air Turbine Starter (ATS) is a key component of an aircraft's secondary power system, driven by Bleed Air supplied from the Auxiliary Power Unit (APU) to accelerate the engine up to approximately 8,900 RPM, enabling engine start. Through the in-house development and localization of the ATS, we have incorporated power generation, optimal design of the shear section with consideration of failure, Containment functionality, as well as lubrication and power transmission systems. In addition, we have secured manufacturing and assembly technologies and continue development aimed at successful operation and the establishment of a mass production system.

Frazier Aviation is part of the Boeing Preferred Supplier Inspection Delegation (PSID) Program and is required to maintain a quality performance level of 98%.

Each SCU can interface with up to eight (8) fuel probes with temperature detection and/or fuel probes with compensators. It will process capacitive and resistive readings to determine the fuel heights for each probe and transmit the calculated fuel volume to the cockpit.

The SCXMC-HDLC card operates through the XMC interface of the SBC and provides real-time communication for control and status data based on synchronization signals. It supports serial communication via the SBCRTM’s Micro D-sub 37-pin connector using a standard D-sub 9-pin interface, allowing long-distance transmission through LVDS signaling. With four transmit/receive channels, it achieves 1–8 Mbps per channel and delivers low-latency performance of less than 40 µs for real-time operations. A device driver program is required for operation, and the Linux driver can be downloaded from Seedcore’s product page. Drivers for other operating systems can be developed upon request. This module is deployed in the L-SAM multi-function radar system, enabling fast and reliable control data communication across mission-critical components.

· Optimized deployment of manned and unmanned aerial assets with separate takeoff and landing runways · Securing aerial/maritime superiority with unmanned combat aerial vehicles (UCAVs) and Drone · Expanded real-time surveillance range through the operation of medium-altitude unmanned reconnaissance aerial vehicles · Enhanced assault capabilities to target and command & control (C2) with manned and unmanned forces