Enhanced Flight Data Recorder /Cockpit Voice Recorder Systems for Improved Compliance and Reliability
Several aviation authorities have mandated—or are in the process of mandating—the use of Solid-State Recorders and Underwater Locator Beacons (ULBs) with increased performance requirements.
Key regulatory milestones include:
By 2018: All flight recorder-mounted ULBs must have a minimum 90-day transmission duration.
By 2019: All flight recorders are expected to be solid-state types with a minimum recording duration of 120 minutes.
Post-ED112 requirements: Flight recorders must be capable of storing 20 to 25 hours of data.
In response to both regulatory changes and operational needs, Fokker Services introduces a new generation of Solid-State Flight Data Recorders (FDRs), Cockpit Voice Recorders (CVRs), and ULBs for integration across your fleet. These units offer significant advantages over traditional tape-based systems, including:
Improved technical dispatch reliability
Reduced maintenance costs
Increased system performance and recording integrity
To further enhance survivability and regulatory compliance, Recorder Independent Power Supply (RIPS) units can also be offered, either as add-on modules or integrated solutions.
Installation of an AlliedSignal CAS-67A TCAS II Traffic Alert and Collision Avoidance System.
Installation of an RTA-83A VHF Communication System.
Installation of the aircraft data link system for communication supporting Air Traffic Services (ATS) and an ICG Iridium Satcom, installation of the Universal Avionics UniLink� UL-801 Communications Management Unit, and UNS-1Lw Flight Management Systems f
Installation of a RDR-4B Weather Radar/Windshear System.
Installation of the MK VII Enhanced Ground Proximity Warning System
Installation of a CAS-81 TCAS II and dual TRA-67 Mode S transponders.
Installation of a CAS-81 TCAS II system and dual Bendix/King TRA-67 Mode S transponders.
Installation of Universal flight data recorder.
Remanufacture AiResearch P/N 176840-1 Bleed Air Precooler Assembly by replacing the core assembly