N4035G

We’re still collecting data for this aircraft. Routes appear once we’ve seen it fly enough times.

Safety history

  • June 8, 2006Accident

    The inadequate manufacturing of the plates of the tail rotor tension-torsion bar assembly resulting in fatigue failure.

    Fairchild Hiller FH-1100

  • February 18, 1985Accident

    PURPOSE OF THE FLT WAS TO TEST THE HELICOPTER AFTER AN ANNUAL INSPECTION. THE PLT FLEW THE ACFT FOR APRX 1 HOUR FROM THE LEFT SEAT WITH THE ACFT OWNER IN THE RIGHT SEAT BEFORE THE OWNER DEPLANED THE ACFT AND THE PLT MOVED INTO THE RIGHT SEAT. PLT STATED THAT ON TAKEOFF THE HELICOPTER BEGAN MOVING TO THE RIGHT BECAUSE OF THE RIGHT CG. (PLT WEIGHT WAS 251 LBS.) HE WAS UNABLE TO MOVE THE CYCLIC FAR ENOUGH TO THE LEFT TO COUNTERACT THE MOVEMENT BECAUSE HIS LEG WAS RESTRICTING THE TRAVEL. THE RIGHT S

    Hiller FH-1100