Products

FAU-39 is an electronic device which can be installed in the center of gravity of an aircraft to monitor the vertical acceleration of the aircraft. During the system operation, the FAU-39 unit records into its internal solid-state memory to following parameters: Aircraft basic information (type, reg. makrs, S/N, etc…) Number of flight hours Number of

Speel´s SACC-2440 is a 3-axis accelerometer, which is intended to sense accelerations of the aircraft in the longitudinal, lateral and vertical axes. It shall be placed close to the center of gravity point of the aircraft. The output circuitry of the unit is equipped with low pass filters to avoid distortion of the signal caused

Speel´s Cockpit Area Microphone (CAM) is intended for sensing the background sounds in an aircraft cockpit. The generated audio signal from the CAM is recorded by SPEEL´s crash-protected cockpit voice recorder or by the CVFDR combined flight data/cockpit voice recorder.

STA-21G converter unit is intended for converting analog synchro signals (pitch, roll and heading) into a digital data format and generating GPS parameters (latitude, longitude, altitude, speed and course). STA-21G transmits digitised position angles together with a GPS parameters via the RS-422 serial line and the ARINC-429 serial line (optional). STA-21G converter unit is specifically designed

SPEEL´s SPOS P501 position sensor is intended to sense the position of the primary control surfaces of an aircraft or other controls. The sensor converts a  rotational movement to an electrical signal. The contactless design of the sensor guarantees high reliability and long technical life of the unit in harsh environments.

The data entry panel DEP-25 is designed for: – entering flight information within the system for registration of flight data BUR-1 (Time, Date, Flight Number, Balance, Weight, Aircraft Number) using a keypad with three keys and four-position rocker switch; – writer status signalling (FAIL); – writer off (using FDR ON switch). The device conforms to RTCA/DO-160D, (release July

ELM 601 device has been designed to monitor the operation load of Walter’s M601 turboprop engine. The whole system, designed into a compact instrument, allows for automatic data collection, recording and indication of service load parameters of the M601 engine such as total number of engine starts, total engine service time, total number of take-off