Document ID: chunk:federal_register_of_legislation:F2007L00699:body:0:p2
Version: federal_register_of_legislation:F2007L00699
Segment Type: other
Provision Reference: 
Character Range: 2816–3655

were not fully implemented in modules of the Honeywell EPIC avionics, as used in Falcon EASy aircraft.
             Consequently, the continuing integrity of the modules' software cannot be demonstrated, as required by software requirements.  Software corruption may then potentially occur during any upload of the operational software and also as random effects under normal conditions.
             This Directive mandates the use of the FLICK tool on a regular basis pending a software correction.  The software load implementing the terminating actions also includes a software correction for the untimely inhibition of the "flap asymmetry" detection below 200ft.  This is mandated to correct a situation that may not conform to EASA CS 25.671 (c) (1).

David Punshon
Delegate of the Civil Aviation Safety Authority

26 February 2007