19990611007029A

Accident · Substantial damage

FAA accident report · Robsin R44 · Sevierville, TN · June 11, 1999

Date
June 11, 1999 · 17:00 local
Place
Sevierville, TN
Phase of flight
Normal Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N49669
NTSB investigation
NTSBMIA99LA181
Reported as
Robsin R44
Reported engine
Lycoming O540F1B5
People aboard
3
Fatal injuries
0
Pilot’s flight hours
9,000 total100 in this make and model70 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

199 Robinson R-44 helicopter experienced main rotor and tail rotor failures in flight and sustained substantial damage, other circumstances are unknown. (From .19) on June 11, 1999, about 1715 eastern daylight time, a Robinson R-44, N49669, registered to highway 66 aviation, LLC, dba scenic helicopter tours, operating as a title 14 CFR part 91 sightseeing flight, crashed into a field near Sevierville, Tennessee, after sustaining a main and tail rotor failure while in cruise flight. Visual meteorological conditions prevailed and no flight plan was filed. The aircraft sustained substantial damage and the airline transport-rated pilot and two passengers were uninjured. The flight originated about 20 minutes before the flight. According to the pilot, he was in cruise flight about 400 feet AGL, when he heard a loud "pop" and the helicopter yawed without a control input. Shortly thereafter, he got a low rotor warning horn, both main and tail rotor rpm's went to zero, and he commenced an auto-rotation. He landed in a tobacco field. (.4) the pilot reported that about 10 minutes into his sightseeing flight, at 400 to 500 feet of altitude, in cruise flight, he heard a noise similar to a shotgun blast and experienced vibration, uncommanded yaw, and low rotor and engine RPM. He regained control and conducted a successful autorotation. Postcrash examination of the helicopter revealed drive train, framework, and fuel tank shrapnel damage originating from a failed transmission forward main driveshaft yoke. Examination of the failed yoke by the NTSB materials laboratory revealed a cracked weld that originated during manufacture.

As the FAA filed it

199 ROBINSON R-44 HELICOPTER EXPERIENCED MAIN ROTOR AND TAIL ROTOR FAILURES IN FLIGHT AND SUSTAINED SUBSTANTIAL DAMAGE, OTHER CIRCUMSTANCES ARE UNKNOWN. (FROM .19) ON JUNE 11, 1999, ABOUT 1715 EASTERN DAYLIGHT TIME, A ROBINSON R-44, N49669, REGISTERED TO HIGHWAY 66 AVIATION, LLC, DBA SCENIC HELICOPTER TOURS, OPERATING AS A TITLE 14 CFR PART 91 SIGHTSEEING FLIGHT, CRASHED INTO A FIELD NEAR SEVIERVILLE, TENNESSEE, AFTER SUSTAINING A MAIN AND TAIL ROTOR FAILURE WHILE IN CRUISE FLIGHT. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AND NO FLIGHT PLAN WAS FILED. THE AIRCRAFT SUSTAINED SUBSTANTIAL DAMAGE AND THE AIRLINE TRANSPORT-RATED PILOT AND TWO PASSENGERS WERE UNINJURED. THE FLIGHT ORIGINATED ABOUT 20 MINUTES BEFORE THE FLIGHT. ACCORDING TO THE PILOT, HE WAS IN CRUISE FLIGHT ABOUT 400 FEET AGL, WHEN HE HEARD A LOUD "POP" AND THE HELICOPTER YAWED WITHOUT A CONTROL INPUT. SHORTLY THEREAFTER, HE GOT A LOW ROTOR WARNING HORN, BOTH MAIN AND TAIL ROTOR RPM'S WENT TO ZERO, AND HE COMMENCED AN AUTO-ROTATION. HE LANDED IN A TOBACCO FIELD. (.4) THE PILOT REPORTED THAT ABOUT 10 MINUTES INTO HIS SIGHTSEEING FLIGHT, AT 400 TO 500 FEET OF ALTITUDE, IN CRUISE FLIGHT, HE HEARD A NOISE SIMILAR TO A SHOTGUN BLAST AND EXPERIENCED VIBRATION, UNCOMMANDED YAW, AND LOW ROTOR AND ENGINE RPM. HE REGAINED CONTROL AND CONDUCTED A SUCCESSFUL AUTOROTATION. POSTCRASH EXAMINATION OF THE HELICOPTER REVEALED DRIVE TRAIN, FRAMEWORK, AND FUEL TANK SHRAPNEL DAMAGE ORIGINATING FROM A FAILED TRANSMISSION FORWARD MAIN DRIVESHAFT YOKE. EXAMINATION OF THE FAILED YOKE BY THE NTSB MATERIALS LABORATORY REVEALED A CRACKED WELD THAT ORIGINATED DURING MANUFACTURE.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.