From autopilot to electromechanical actuators and inertial sensors, Safran Electronics & Defense's Automatic Flight Control Systems (AFCS) improve the performance and maneuverability of your helicopters.
Pilot’s workload reduction
Flight safety improvement
Tailored for any type of helicopters, civil or military
More than100,000,000
Autopilot, multifunction avionics platform, electromechanical actuation systems and inertial navigation, Safran Electronics & Defense enhance your helicopters.
Capitalizing on its expertise in APM autopilots and fly-by-wire flight control computers, Safran has designed an innovative multifunction avionics computer. Scalable and modular, UCAP concentrates many avionics functions in an ultra compact package: autopilot, Vehicle Management System (VMS), AHRS, advanced maintenance functions (health monitoring, usage & maintenance monitoring), sense & avoid...
Trim actuators, or parallel actuators, artificially reproduce the piloting forces for helicopters. They provide load compensation functions, offer precise force feedback and can be controlled in autopilot mode.
Compact and lightweight, SEMA series linear actuators allow very fast movements of low amplitude of the flight controls, thus improving helicopter stability.
Safran Electronics & Defense integrates inertial sensors, APIRS heading and attitude unit or SkyNaute GNSS hybrid navigation unit to guarantee a high level of precision and reliability for optimal flight control in complete safety.
Yes, we retrofit legacy systems (e.g., GE Frame 5, Siemens V94.2) with modern digital controllers, typically completing hardware integration within 4-8 weeks. Software migration requires additional validation time.
We recommend annual performance testing under ISO 3977-2 standards. Critical applications (e.g., offshore platforms) may require semi-annual tests with emissions compliance checks.
All rad-hard devices (e.g., FPGA, ADC) are QML Class V certified under MIL-PRF-38535 and tested to MIL-STD-883 Method 1019 for SEU tolerance. Full qualification reports are available upon request.
Our ASICs and power management ICs operate across -55°C to +175°C ambient temperatures, with derating curves provided in military temperature range (MTR) datasheets.
Our PMA parts (e.g., actuators, sensors) hold FAA/EASA Form 1 certification and match OEM form/fit/function. Installation requires SB/MB documentation per FAA AC 23.1529.
All NAS/MS fasteners include full DNA traceability: melt source (AMS 2301), heat/lot numbers, and AS9100-compliant MTRs with ultrasonic test reports.
AOG orders ship within 4 hours for stocked items (FAA-PMA, EASA Part 21G). Non-stock critical parts trigger priority manufacturing with 72-hour max turnaround.