20080525838339A

Accident · Substantial damage

FAA accident report · Hughes 369E · Sunrise Beach, MO · May 25, 2008

Date
May 25, 2008 · 19:21 local
Place
Sunrise Beach, MO
Phase of flight
Hovering
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N686F
NTSB investigation
NTSBDEN08FA092
Reported as
Hughes 369E
People aboard
3
Fatal injuries
1
Pilot’s flight hours
2,360 total350 in this make and model33 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.

(-23) Following a local sightseeing flight, the PIC was returning to his private landiing pad. Gusty winds were present in the cove where his helipad was located. According to pilot-rated witnesses, the helicopter was maneuvering slowly and then hovered approximately 200 feet from the pad at about 75 feet over the water when suddenly the helicopter began a series of uncommanded right turns about its vertical axis and began to lose altitude. The helicopter impacted the water, and the front windscreens shattered. Water entered the cabin area, and the helicopter began to sink. Four of the five occupants managed to egress; however, one passenger remained in the cabin and drowned. Post-accident investigation damage to the tail rotor drive shaft was consistent with torsional overstress indicative of a tail rotor striking a surface with power. A flight controls conformity check showed no pre-crash abnormalities. The aircraft was configured with seats and restraints for four occupants.

As the FAA filed it

(-23) FOLLOWING A LOCAL SIGHTSEEING FLIGHT, THE PIC WAS RETURNING TO HIS PRIVATE LANDIING PAD. GUSTY WINDS WERE PRESENT IN THE COVE WHERE HIS HELIPAD WAS LOCATED. ACCORDING TO PILOT-RATED WITNESSES, THE HELICOPTER WAS MANEUVERING SLOWLY AND THEN HOVERED APPROXIMATELY 200 FEET FROM THE PAD AT ABOUT 75 FEET OVER THE WATER WHEN SUDDENLY THE HELICOPTER BEGAN A SERIES OF UNCOMMANDED RIGHT TURNS ABOUT ITS VERTICAL AXIS AND BEGAN TO LOSE ALTITUDE. THE HELICOPTER IMPACTED THE WATER, AND THE FRONT WINDSCREENS SHATTERED. WATER ENTERED THE CABIN AREA, AND THE HELICOPTER BEGAN TO SINK. FOUR OF THE FIVE OCCUPANTS MANAGED TO EGRESS; HOWEVER, ONE PASSENGER REMAINED IN THE CABIN AND DROWNED. POST-ACCIDENT INVESTIGATION DAMAGE TO THE TAIL ROTOR DRIVE SHAFT WAS CONSISTENT WITH TORSIONAL OVERSTRESS INDICATIVE OF A TAIL ROTOR STRIKING A SURFACE WITH POWER. A FLIGHT CONTROLS CONFORMITY CHECK SHOWED NO PRE-CRASH ABNORMALITIES. THE AIRCRAFT WAS CONFIGURED WITH SEATS AND RESTRAINTS FOR FOUR OCCUPANTS.

NTSB investigation

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