20101030052689A

Accident · Substantial damage

FAA accident report · MD Helicopt 369E · Lead Mine, WV · October 30, 2010

Date
October 30, 2010 · 10:30 local
Place
Lead Mine, WV
Phase of flight
Climb
Operating rules
Rotorcraft external load (Part 133)
Operator
IZWL
Damage
Substantial damage
Aircraft
N765WH
NTSB investigation
NTSBERA11FA042
Reported as
MD Helicopt 369E
Reported engine
Rolls-Royce 250-C20R/2
People aboard
4
Fatal injuries
1
Other injuries
3
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
0 total0 in this make and model0 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.

The pilot had just completed an aerial application called a "clipping operation" of fiber optic wire on a power line tower structure. The 3 linemen had just transferred from atop the tower structure to the aircraft and there were 2 linemen in the rear passenger compartment sitting on the floor, 1 lineman on the left skid, and an external load attached to a 40 foot long line. As the pilot cleared the tower structure in a climbing out maneuver, the external load caught on the tower 16 feet from the top, and the aircraft experienced a severe vibration with a subsequent loss of control. The tail rotor contacted one of the lower high voltage power lines (line was de-energized), resulting in loss of tail rotor authority and impact with the ground. The external load synthetic long line had snapped 14 feet above the external load apparatus. This portion of the line and apparatus were found at the base of the tower structure. The rest of the long line remained attached to the cargo hook mount on the fuselage. The lineman on the left skid received fatal injuries. The weather was sunny, clear, and calm, with a 10 mile visibility and no winds.

As the FAA filed it

THE PILOT HAD JUST COMPLETED AN AERIAL APPLICATION CALLED A "CLIPPING OPERATION" OF FIBER OPTIC WIRE ON A POWER LINE TOWER STRUCTURE. THE 3 LINEMEN HAD JUST TRANSFERRED FROM ATOP THE TOWER STRUCTURE TO THE AIRCRAFT AND THERE WERE 2 LINEMEN IN THE REAR PASSENGER COMPARTMENT SITTING ON THE FLOOR, 1 LINEMAN ON THE LEFT SKID, AND AN EXTERNAL LOAD ATTACHED TO A 40 FOOT LONG LINE. AS THE PILOT CLEARED THE TOWER STRUCTURE IN A CLIMBING OUT MANEUVER, THE EXTERNAL LOAD CAUGHT ON THE TOWER 16 FEET FROM THE TOP, AND THE AIRCRAFT EXPERIENCED A SEVERE VIBRATION WITH A SUBSEQUENT LOSS OF CONTROL. THE TAIL ROTOR CONTACTED ONE OF THE LOWER HIGH VOLTAGE POWER LINES (LINE WAS DE-ENERGIZED), RESULTING IN LOSS OF TAIL ROTOR AUTHORITY AND IMPACT WITH THE GROUND. THE EXTERNAL LOAD SYNTHETIC LONG LINE HAD SNAPPED 14 FEET ABOVE THE EXTERNAL LOAD APPARATUS. THIS PORTION OF THE LINE AND APPARATUS WERE FOUND AT THE BASE OF THE TOWER STRUCTURE. THE REST OF THE LONG LINE REMAINED ATTACHED TO THE CARGO HOOK MOUNT ON THE FUSELAGE. THE LINEMAN ON THE LEFT SKID RECEIVED FATAL INJURIES. THE WEATHER WAS SUNNY, CLEAR, AND CALM, WITH A 10 MILE VISIBILITY AND NO WINDS.

NTSB investigation

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