20210618015959A

Accident · Substantial damage

FAA accident report · Mcdonnell Douglas Helicopter 369E · Ferndale, NY · June 18, 2021

Date
June 18, 2021 · 08:15 local
Place
Ferndale, NY
Phase of flight
Hover/Holding
Operating rules
Rotorcraft external load (Part 133)
Operator
HXFL
Damage
Substantial damage
Aircraft
N371EE
NTSB investigation
NTSBERA21LA262
Reported as
Mcdonnell Douglas Helicopter 369E
Reported engine
Allison 250-C20 series
People aboard
1
Fatal injuries
0
Other injuries
2
Pilot’s certificates
Commercial pilot, flight instructor
Pilot’s flight hours
3,852 total1,568 in this make and model104 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 06/18/2021 at approximately 8:15 am EST, a Mcdonnell Douglas Helicopter, model 369E, registration number N371EE, s/n 0371E, certificated in the standard normal category was performing aerial power line work under part 133. The main rotor blade(s) made contact with the life-line catwalk support structure on a high voltage power pole resulting in loss of control of the aircraft. The aircraft crash landed into a wooded area 225 feet north of the power pole and suffered major structural damage to the main rotor system, tail rotor system, fuselage, skids, and tail section. Both the pilot and the lineman suffered serious injuries.

As the FAA filed it

ON 06/18/2021 AT APPROXIMATELY 8:15 AM EST, A MCDONNELL DOUGLAS HELICOPTER, MODEL 369E, REGISTRATION NUMBER N371EE, S/N 0371E, CERTIFICATED IN THE STANDARD NORMAL CATEGORY WAS PERFORMING AERIAL POWER LINE WORK UNDER PART 133. THE MAIN ROTOR BLADE(S) MADE CONTACT WITH THE LIFE-LINE CATWALK SUPPORT STRUCTURE ON A HIGH VOLTAGE POWER POLE RESULTING IN LOSS OF CONTROL OF THE AIRCRAFT. THE AIRCRAFT CRASH LANDED INTO A WOODED AREA 225 FEET NORTH OF THE POWER POLE AND SUFFERED MAJOR STRUCTURAL DAMAGE TO THE MAIN ROTOR SYSTEM, TAIL ROTOR SYSTEM, FUSELAGE, SKIDS, AND TAIL SECTION. BOTH THE PILOT AND THE LINEMAN SUFFERED SERIOUS INJURIES.

NTSB investigation

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