What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
Aircraft was stable in cruise flight when the pilots and crew heard and felt a bang and felt the aircraft shudder. After the initial event there was no further vibration of indication of a problem. The crew discussed the possibility of performing a precautionary landing. While discussing the need for a precautionary landing, the #2 engine fire-light illuminated. The crew declared an emergency, secured the #2 engine, and proceeded to complete an emergency landing at Bucyrus Airport (17G).
The landing and shutdown were uneventful.
The resulting damage to the aircraft includes a 1 inch hole in one of the main rotor blades (red), fiberglass and sheet metal damage to the aft engine cowling.
The aircraft manufacturer's evaluation of the damage indicates that the damage to one of the main rotor blades is beyond the limits for field repair.
Although the damage is repairable without scrapping the main rotor blade, it will require a specialized service for repair. The NTSB initially reviewed this damage along with a review of the manufacturer's recommendations for repair and determined that the damage is substantial indicating that the event should be classified as an accident.
After further review, the NTSB notified the FSDO that they have reversed their evaluation and classified the damage not substantial. This event has been reclassified as an incident 05/21/2014 - jld.
As the FAA filed it
AIRCRAFT WAS STABLE IN CRUISE FLIGHT WHEN THE PILOTS AND CREW HEARD AND FELT A BANG AND FELT THE AIRCRAFT SHUDDER. AFTER THE INITIAL EVENT THERE WAS NO FURTHER VIBRATION OF INDICATION OF A PROBLEM. THE CREW DISCUSSED THE POSSIBILITY OF PERFORMING A PRECAUTIONARY LANDING. WHILE DISCUSSING THE NEED FOR A PRECAUTIONARY LANDING, THE #2 ENGINE FIRE-LIGHT ILLUMINATED. THE CREW DECLARED AN EMERGENCY, SECURED THE #2 ENGINE, AND PROCEEDED TO COMPLETE AN EMERGENCY LANDING AT BUCYRUS AIRPORT (17G).
THE LANDING AND SHUTDOWN WERE UNEVENTFUL.
THE RESULTING DAMAGE TO THE AIRCRAFT INCLUDES A 1 INCH HOLE IN ONE OF THE MAIN ROTOR BLADES (RED), FIBERGLASS AND SHEET METAL DAMAGE TO THE AFT ENGINE COWLING.
THE AIRCRAFT MANUFACTURER'S EVALUATION OF THE DAMAGE INDICATES THAT THE DAMAGE TO ONE OF THE MAIN ROTOR BLADES IS BEYOND THE LIMITS FOR FIELD REPAIR.
ALTHOUGH THE DAMAGE IS REPAIRABLE WITHOUT SCRAPPING THE MAIN ROTOR BLADE, IT WILL REQUIRE A SPECIALIZED SERVICE FOR REPAIR. THE NTSB INITIALLY REVIEWED THIS DAMAGE ALONG WITH A REVIEW OF THE MANUFACTURER'S RECOMMENDATIONS FOR REPAIR AND DETERMINED THAT THE DAMAGE IS SUBSTANTIAL INDICATING THAT THE EVENT SHOULD BE CLASSIFIED AS AN ACCIDENT.
AFTER FURTHER REVIEW, THE NTSB NOTIFIED THE FSDO THAT THEY HAVE REVERSED THEIR EVALUATION AND CLASSIFIED THE DAMAGE NOT SUBSTANTIAL. THIS EVENT HAS BEEN RECLASSIFIED AS AN INCIDENT 05/21/2014 - JLD.