What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) At approximately 08:15 the pilot departed gulf platform high island 573 in route for high island 264. Approximately 3 to 4 minutes later the dispatcher at petroleum helicopters, inc (phi) base received a may day distress call. There were no further communications. The pilot received fatal injuries. The aircraft was recovered in the area of high island 560 in approximately 240' of water. Post examination of the aircraft, engine and associated components showed an uncontained failure of the #3 engine turbine disk. Post examination also revealed that there was very little if no inertia left in the main rotor system when the aircraft impacted the water. Continuity was established to all of the flight controls. The main landing gear floats were never activated. The transmission, sevos, free wheeling unit and tail rotor drive system were all inspected and found to be intact or operational in accordance with the manufacturers requirements. The operator will file an mmir report and forward it to their certificate management office in accordance with their general maintenance manual.
As the FAA filed it
(-23) AT APPROXIMATELY 08:15 THE PILOT DEPARTED GULF PLATFORM HIGH ISLAND 573 IN ROUTE FOR HIGH ISLAND 264. APPROXIMATELY 3 TO 4 MINUTES LATER THE DISPATCHER AT PETROLEUM HELICOPTERS, INC (PHI) BASE RECEIVED A MAY DAY DISTRESS CALL. THERE WERE NO FURTHER COMMUNICATIONS. THE PILOT RECEIVED FATAL INJURIES. THE AIRCRAFT WAS RECOVERED IN THE AREA OF HIGH ISLAND 560 IN APPROXIMATELY 240' OF WATER. POST EXAMINATION OF THE AIRCRAFT, ENGINE AND ASSOCIATED COMPONENTS SHOWED AN UNCONTAINED FAILURE OF THE #3 ENGINE TURBINE DISK. POST EXAMINATION ALSO REVEALED THAT THERE WAS VERY LITTLE IF NO INERTIA LEFT IN THE MAIN ROTOR SYSTEM WHEN THE AIRCRAFT IMPACTED THE WATER. CONTINUITY WAS ESTABLISHED TO ALL OF THE FLIGHT CONTROLS. THE MAIN LANDING GEAR FLOATS WERE NEVER ACTIVATED. THE TRANSMISSION, SEVOS, FREE WHEELING UNIT AND TAIL ROTOR DRIVE SYSTEM WERE ALL INSPECTED AND FOUND TO BE INTACT OR OPERATIONAL IN ACCORDANCE WITH THE MANUFACTURERS REQUIREMENTS. THE OPERATOR WILL FILE AN MMIR REPORT AND FORWARD IT TO THEIR CERTIFICATE MANAGEMENT OFFICE IN ACCORDANCE WITH THEIR GENERAL MAINTENANCE MANUAL.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.
Other reports on N457PH · 1
Matched to the same aircraft by N-number and date.