5N-VRG
FlightFinder has no observed route profile for this registration. The documented safety events below are available independently of live flight tracking.
Safety history
- November 14, 1998AccidentHull loss
Laboratory analyses revealed the presence of a fatigue crack on the inner mid spar fitting of the engine n°3. The crack has been present for a reasonable time. The Airworthiness Directive 93-11-02 asks the replacement of the fittings by improved model at least for July 97. The fittings of engine n°3 were from the old design. Full accident record