The cameras: state-of-the-art technology & smart functions Our cameras are equipped with stateof-the-art technology (e.g., newest CMOS sensors) and a range of advanced smart functions. The system is running smoothly and reliably at all flight altitudes, demonstrating resilience to aircraft-specific vibration. With high VIS sensitivity sensors and automatic IR illumination the cameras adapt perfectly to the ever-changing lighting conditions within the cabin and deliver crisp images up to Full-HD @ 30 fps. Integrated video motion detection / threat detection. Intelligent recording: focus on the crucial moments In an ideal scenario, countless hours of streaming are completely uneventful. Our smart video recorder combines loop recording with video detection motion. With motion detection capabilities, the system intelligently identifies the critical moments and automatically removes eventless times from the recording. The focus on significant events (and the pre-event period) saves valuable storage space, while maximizing the potential of the recording system. That’s our formula for efficiency. Subtle elegance: harmonizing cabin designs with unobtrusive cameras Aesthetics matter! We understand that our customers want to preserve the design integrity of their cabins. The true beauty of surveillance cameras lies in their seamless integration and unobtrusive presence., our cameras are designed for perfect blending into aircrafts interiors. To minimize space requirements, a strong emphasis was on low weight and a compact form factor. Cargo Surveillance Thanks to integrated motion detection, all issues such as shifting cargo or blind passengers in the cargo hold are detected. A significant safety improvement for commercial airliners as well as for air freighters.

We have taken the standard housing configuration of the P1 & P3 mounting dimensions while incorporating true differential pair contacts within the P1 & P3 dimensional constraints. P1 connector housing contains 21 position true differential pair blind mate contacts allowing board designers to carry high density differential pair signals from the LRU via motherboard to daughter-card plug in modules with a single connector P1 type housing.

Supports non-destructive inspection of aircraft composite skin structures and is composed of a piezoelectric layer sensor, data acquisition equipment, and damage analysis software. Utilizes piezoelectric sensors to generate Lamb-wave and acquire signals, collecting data to accurately detect and assess composite damage. Visualizes inspection results on display such as damage location, size and index. - POD Accuracy: 1 inch 90% or more - POD Precision : Position error within 30 mm - 64 channels / 230 path reference detection time within 10 minutes - Sensor : Resonance resistance less than 400kΩ - Sensor : MIL-STD-810G - Sensor : RTCA DO-160 Section 23.0 - DAQ : x128 Piezoelectric sensor interface

Depending on the applications of our customers we offer a very wide range of solutions with liquid and / or gaseous fluids in a very wide and varied spectrum of pressure, flow and other characteristics. Liquids: Industrial grade oils (ISO VG type) with more complex oils like SKYDROL ® and other synthetic oils Water whether ...

- Capable of manufacturing various types of cable assemblies, including MIL-DTL-38999, D-Sub, and other military-grade connectors - Expertise in both internal and external cable assembly configurations - In-house testing capabilities for electrical characteristics, including insulation resistance, dielectric withstand voltage, and continuity - Equipped with dedicated facilities and specialized equipment for cable assembly production and testing

To guarantee maximum safety and reliability, our DA 30 features a brushless motor and a contactless wear-free position sensor. This means maximum service life with the greatest‐possible power delivery and its design prevents electromagnetic emissions (EMI) caused by brush sparking. The housing made of saltwater‐resistant aluminum is HART‐coat treated, meets the IP‐67 standard for water and dust sealing and provides an integrated Sub‐D connector (MIL spec. circular connector or cable gland on request). Brackets integrated in the housing for horizontal and vertical assembly. 8‐fold, ball‐bearing supported, steel gear train, drive shaft with ANSI multi‐tooth. The DA 30 series can be equipped with a standard PWM input (Pulse Width Modulation) that has two different interfaces: a differential, galvanic isolated interface (Opto‐Coupler) and a single‐ended interface with CMOS levels that is also used to program the servo parameters. It includes analog position feedback to detect the drive shaft position. A differential RS‐422 PWM interface can be chosen instead of the opto‐coupled interface. The DA 30 with digital serial command interface (RS‐485) receives its commands via a CRC secured protocol. It can return not only the shaft position in digital format, but also several diagnostic data such as the level of the supply voltage, current consumption and the temperature of the motor and electronics in digital form (optionally also the humidity within the actuator case). These kind of diagnostic capabilities help to determine the health state of the actuators before, during and after deployment.

Low Insertion Loss, Good IMD Performance RF Coaxial Switches: SPST to SP8T Switches, Transfer Switches from DC to 200 GHz Power Dividers and Power Combiners Wilkinson Types from 2 to 16 Ways Frequency Range from 400 MHz to 26.5 GHz

The main wheel assembly refers to the complete structural unit that includes the wheel, tire, axle, bearings, and in most cases, the braking system. As the primary load-bearing gear, the assembly is engineered to absorb high-impact forces during landing and provide strong braking performance during deceleration. Its design integrates durability, safety, and serviceability, making it a critical element of aircraft ground operations.