20170802011129A

Accident · Substantial damage

FAA accident report · Sikorsky S-97A · Jupiter, FL · August 2, 2017

Date
August 2, 2017 · 07:20 local
Place
Jupiter, FL
Airport
Gwinn
Phase of flight
Hover/Holding
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N971SK
NTSB investigation
NTSBERA17LA263
Reported as
Sikorsky S-97A
Reported engine
General Electric YT706-GE-700R
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Airline transport
Pilot’s flight hours
6,679 total19 in this make and model32 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.

On August 2, 2017, at 0720 eastern daylight time, a Sikorsky S-97, N971SK, experienced a flight control

Anomaly while lifting to a hover resulting in excessive roll oscillations leading to intermeshing of the

Counter-rotating rotor system resulting in a hard landing. The two airline transport pilots were not

Injured, and the helicopter sustained substantial damage to the rotor system. The helicopter was

Registered to Sikorsky aircraft company in the experimental category, and was operated under the

Provisions of 14 code of federal regulations, part 91. Visual meteorological conditions prevailed for the

Flight, and a company flight plan was active. The flight originated at the william p Gwinn Airport, Jupiter,

Florida.

As the FAA filed it

ON AUGUST 2, 2017, AT 0720 EASTERN DAYLIGHT TIME, A SIKORSKY S-97, N971SK, EXPERIENCED A FLIGHT CONTROL

ANOMALY WHILE LIFTING TO A HOVER RESULTING IN EXCESSIVE ROLL OSCILLATIONS LEADING TO INTERMESHING OF THE

COUNTER-ROTATING ROTOR SYSTEM RESULTING IN A HARD LANDING. THE TWO AIRLINE TRANSPORT PILOTS WERE NOT

INJURED, AND THE HELICOPTER SUSTAINED SUBSTANTIAL DAMAGE TO THE ROTOR SYSTEM. THE HELICOPTER WAS

REGISTERED TO SIKORSKY AIRCRAFT COMPANY IN THE EXPERIMENTAL CATEGORY, AND WAS OPERATED UNDER THE

PROVISIONS OF 14 CODE OF FEDERAL REGULATIONS, PART 91. VISUAL METEOROLOGICAL CONDITIONS PREVAILED FOR THE

FLIGHT, AND A COMPANY FLIGHT PLAN WAS ACTIVE. THE FLIGHT ORIGINATED AT THE WILLIAM P GWINN AIRPORT, JUPITER,

FLORIDA.

NTSB investigation

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