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Location:
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Fairfield, California
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Accident Number:
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WPR20LA163
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Date & Time:
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June 2, 2020, 12:50 Local
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Registration:
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N65PJ
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Aircraft:
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Bell 206
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Aircraft Damage:
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Substantial
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Defining Event:
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Collision with terr/obj (non-CFIT)
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Injuries:
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3 Fatal
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Flight Conducted Under:
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Part 133: Rotorcraft ext. load
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Analysis
The pilot of the helicopter was retrieving two linemen after they completed powerline work and transporting them back to the landing zone via longline. A witness stated that, after picking up the linemen, the helicopter ascended into the powerlines, impacting, and severing one line located about 210 ft above ground level. The helicopter subsequently impacted terrain, rolled downhill, and came to rest in a ravine.
Examination of the helicopter revealed no evidence of mechanical malfunctions or anomalies that would have precluded normal operation. The main rotor blades displayed evidence of blade contact, and the engine compressor impeller contained debris consistent with the engine operating at the time of ground impact. The circumstances of the accident are consistent with the pilot’s failure to maintain adequate clearance from powerlines, which resulted in the main rotor impacting a wire and subsequent impact with terrain.
Probable Cause and Findings
The National Transportation Safety Board determines the probable cause(s) of this accident to be: The pilot’s failure to maintain adequate clearance from powerlines while conducting external load operations, which resulted in the main rotor contacting a wire and a subsequent collision with terrain.
Findings
Personnel issues - Monitoring environment - Pilot
Personnel issues - Aircraft control - Pilot
Environmental issues - Wire - Response/compensation
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Factual Information
History of Flight
Maneuvering-low-alt flying - Miscellaneous/other
Maneuvering-low-alt flying - Collision with terr/obj (non-CFIT) (Defining event)
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On June 2, 2020, about 1250 Pacific daylight time, a Bell 206L3 Helicopter, N65PJ, was substantially damaged when it was involved in an accident near Fairfield, California. The pilot and two passengers were fatally injured. The helicopter was operated as a Title 14 Code of Federal Regulations (CFR) Part 133 rotorcraft external load operation.
The helicopter was operated by PJ Helicopters under contract from Pacific Gas and Electric (PG&E) to perform power line repair work. A fuel truck driver associated with the operation stated that he arrived at the landing zone about 0900 on the morning of the accident, where the accident pilot and helicopter were waiting. Flight operations began between 1100 and 1130.
According to the operator around 1250, the two linemen had completed work for the day, and the pilot proceeded to their location to pick them up via longline from the tower on which they had been working. At that time, for unknown reasons, the linemen were lowered to the ground and disconnected from the long line. The helicopter circled for several minutes before it was called back, and the linemen reattached to the longline. A witness stated that he saw the accident helicopter ascend toward the lower line of a set of powerlines. The main rotor contacted the line, followed by the helicopter impacting terrain, where it rolled downhill, and came to rest in a ravine.
According to PG&E, the impacted power line was about 200 ft above ground level (agl), located about mid span between two towers at the bottom of a valley.
Pilot Information
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Certificate:
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Commercial Age:
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38,Male
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Airplane Rating(s):
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None Seat Occupied:
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Left
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Other Aircraft Rating(s):
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Helicopter Restraint Used:
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5-point
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Instrument Rating(s):
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Helicopter Second Pilot Present:
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No
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Instructor Rating(s):
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Helicopter Toxicology Performed:
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Yes
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Medical Certification:
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Class 2 Without waivers/limitations Last FAA Medical Exam:
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December 22, 2019
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Occupational Pilot:
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Yes Last Flight Review or Equivalent:
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Flight Time:
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(Estimated) 3099 hours (Total, all aircraft)
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Passenger Information
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Certificate:
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Age:
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41,Male
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Airplane Rating(s):
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Seat Occupied:
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None
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Other Aircraft Rating(s):
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Restraint Used:
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Unknown
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Instrument Rating(s):
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Second Pilot Present:
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No
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Instructor Rating(s):
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Toxicology Performed:
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No
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Medical Certification:
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Last FAA Medical Exam:
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Occupational Pilot:
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No
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Last Flight Review or Equivalent:
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Flight Time:
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Passenger Information
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Certificate:
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Age:
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29,Male
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Airplane Rating(s):
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Seat Occupied:
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None
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Other Aircraft Rating(s):
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Restraint Used:
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Unknown
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Instrument Rating(s):
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Second Pilot Present:
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No
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Instructor Rating(s):
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Toxicology Performed:
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No
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Medical Certification:
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Last FAA Medical Exam:
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|
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Occupational Pilot:
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No
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Last Flight Review or Equivalent:
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|
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Flight Time:
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The pilot held a commercial pilot certificate with ratings for rotorcraft-helicopter and instrument helicopter. His most recent Federal Aviation Administration second-class medical certificate was issued on December 23, 2019, at which time he reported 3,099 total hours of flight experience, with 422 hours in the previous six months.
Aircraft and Owner/Operator Information
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Aircraft Make:
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Bell
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Registration:
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N65PJ
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Model/Series:
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206 L3
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Aircraft Category:
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Helicopter
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Year of Manufacture:
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1985
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Amateur Built:
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Airworthiness Certificate:
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Normal
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Serial Number:
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51127
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Landing Gear Type:
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Skid
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Seats:
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7
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Date/Type of Last Inspection:
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100 hour
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Certified Max Gross Wt.:
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4150 lbs
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Time Since Last Inspection:
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18.5 Hrs
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Engines:
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1 Turbo shaft
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Airframe Total Time:
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16960.7 Hrs
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Engine Manufacturer:
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Rolls-Royce
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ELT:
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C126 installed, activated, did not aid in locating accident
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Engine Model/Series:
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M250-C30P
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Registered Owner:
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Rated Power:
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650 Horsepower
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Operator:
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Operating Certificate(s) Held:
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Rotorcraft external load (133)
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Meteorological Information and Flight Plan
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Conditions at Accident Site:
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Visual (VMC)
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Condition of Light:
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Day
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Observation Facility, Elevation:
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KVCB,109 ft msl
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Distance from Accident Site:
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5 Nautical Miles
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Observation Time:
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12:53 Local
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Direction from Accident Site:
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41°
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Lowest Cloud Condition:
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Clear
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Visibility
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10 miles
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Lowest Ceiling:
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None
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Visibility (RVR):
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Wind Speed/Gusts:
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/ Turbulence Type
Forecast/Actual:
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None / None
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Wind Direction:
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Turbulence Severity Forecast/Actual:
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N/A / N/A
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Altimeter Setting:
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29.95 inches Hg
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Temperature/Dew Point:
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15°C / 11°C
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Precipitation and Obscuration:
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No Obscuration; No Precipitation
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Departure Point:
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Fairfield, CA
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Type of Flight Plan Filed:
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None
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Destination:
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Fairfield, CA
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Type of Clearance:
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None
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Departure Time:
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Type of Airspace:
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Wreckage and Impact Information
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Crew Injuries:
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1 Fatal
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Aircraft Damage:
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Substantial
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Passenger Injuries:
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2 Fatal
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Aircraft Fire:
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On-ground
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Ground Injuries:
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Aircraft Explosion:
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None
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Total Injuries:
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3 Fatal
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Latitude, Longitude:
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38.309722,-122.03388(est)
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The helicopter was recovered from the site for examination. Flight control continuity was established from the single cockpit control to the control surfaces through breaks in the system consistent with impact damage.
Continuity was confirmed from the main rotor drive shaft to the main rotor. The freewheeling unit operated normally. The transmission-to-engine main drive shaft remained attached at the transmission via the Kaflex. The aft Kaflex was fractured.
One main rotor blade (white blade) was fractured about 73 inches from the blade grip. The trailing edge of the blade was split down its length starting about 13 inches from the grip. The tip of the rotor blade was separated from the blade and displayed evidence of a wire strike.
The white pitch change link was fractured about 6 inches from the lower end of the tube.
The other main rotor blade (red blade) was fractured about 36 inches from the grip. The outer skin separated from the carbon layup of the top surface of the blade. The interior core separated from the lower surface of the blade. The trailing edge of the blade was split down its length in a few locations with the interior core missing. The red pitch change link was fractured at the lower end connection.
Examination of the transmission, pylon, and hydraulics system revealed no anomalies.
Examination of the engine revealed no evidence of preimpact mechanical malfunctions or anomalies. The compressor impeller was undamaged and displayed evidence of dirt ingestion consistent with operation at the time of impact.
Administrative Information
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Investigator In Charge (IIC):
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Cornejo, Tealeye
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Additional Participating Persons:
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Jeffrey Snider; Federal Aviation Administration; Sacramento, CA John McCoy; Pacific Gas and Electric; Sacramento, CA
Seth Gunsauls; PJ Helicopters, Inc.; Red Bluff, CA Jeff Johnson; Wilson Construction; Canby, OR Jon-Adam Michael; Rolls Royce; Indianapolis, IN
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Original Publish Date:
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March 22, 2023 Investigation Class:
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3
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Note:
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The NTSB did not travel to the scene of this accident.
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Investigation Docket:
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https://data.ntsb.gov/Docket?ProjectID=101367
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