20220719007699A

Accident · Minor damage

FAA accident report · Bell 206L-3 · Templeton, PA · July 19, 2022

Date
July 19, 2022 · 13:30 local
Place
Templeton, PA
Phase of flight
Maneuver
Operating rules
General operating rules (Part 91)
Operator
DEJA
Damage
Minor damage
Aircraft
N203PA
NTSB investigation
NTSBERA22LA347
Reported as
Bell 206L-3
Reported engine
Rolls Royce Allison M250 C-30
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor
Pilot’s flight hours
2,390 total1,467 in this make and model167 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.

Note: (the investigation of the aircraft was completed at jimmy stewart airport (kidi) not at the location of the accident. The pilot flew the aircraft here after the wire strike.)

This helicopter is operated under 14CFR part 135 to gather laser data and pictures of electrical transmission lines (lidar). At the time of the accident it was being transitioned from one area of operation (kfkl) to another area of operation wnw of (kidi) and operated under 14CFR part 91.

The pilot in his written statement, stated: ?he was loosely following the western shore of the allegheny river at an altitude of 400 feet. ? He further stated: he saw no signs of activity or obstructions in area and saw a quick flash of light or something white or reflective pushed the aircraft into a descent. He felt a slight shudder afterwards. He had no master caution light, checked the controls then elected to continue to (kidi) jimmy stewart airport.

Inspection of the aircraft showed wire strike damage to both main rotor blade approximately 70 inches inward from the tips. The vertical stabilizer cap along with the GPS and strobe lights were torn off by the wire strike and missing and later found at the accident site. The wiring and cable tore through the aft portion of the vertical stabilizer. There was scaring on the tail rotor blade from hitting these wires. No other damage was noted.

The company president did state in an email that the low level and high rate of speed combination at which the incident occurred was contrary to the flight in the wire environment training the pilot had.

As the FAA filed it

NOTE: (THE INVESTIGATION OF THE AIRCRAFT WAS COMPLETED AT JIMMY STEWART AIRPORT (KIDI) NOT AT THE LOCATION OF THE ACCIDENT. THE PILOT FLEW THE AIRCRAFT HERE AFTER THE WIRE STRIKE.)

THIS HELICOPTER IS OPERATED UNDER 14CFR PART 135 TO GATHER LASER DATA AND PICTURES OF ELECTRICAL TRANSMISSION LINES (LIDAR). AT THE TIME OF THE ACCIDENT IT WAS BEING TRANSITIONED FROM ONE AREA OF OPERATION (KFKL) TO ANOTHER AREA OF OPERATION WNW OF (KIDI) AND OPERATED UNDER 14CFR PART 91.

THE PILOT IN HIS WRITTEN STATEMENT, STATED: ?HE WAS LOOSELY FOLLOWING THE WESTERN SHORE OF THE ALLEGHENY RIVER AT AN ALTITUDE OF 400 FEET. ? HE FURTHER STATED: HE SAW NO SIGNS OF ACTIVITY OR OBSTRUCTIONS IN AREA AND SAW A QUICK FLASH OF LIGHT OR SOMETHING WHITE OR REFLECTIVE PUSHED THE AIRCRAFT INTO A DESCENT. HE FELT A SLIGHT SHUDDER AFTERWARDS. HE HAD NO MASTER CAUTION LIGHT, CHECKED THE CONTROLS THEN ELECTED TO CONTINUE TO (KIDI) JIMMY STEWART AIRPORT.

INSPECTION OF THE AIRCRAFT SHOWED WIRE STRIKE DAMAGE TO BOTH MAIN ROTOR BLADE APPROXIMATELY 70 INCHES INWARD FROM THE TIPS. THE VERTICAL STABILIZER CAP ALONG WITH THE GPS AND STROBE LIGHTS WERE TORN OFF BY THE WIRE STRIKE AND MISSING AND LATER FOUND AT THE ACCIDENT SITE. THE WIRING AND CABLE TORE THROUGH THE AFT PORTION OF THE VERTICAL STABILIZER. THERE WAS SCARING ON THE TAIL ROTOR BLADE FROM HITTING THESE WIRES. NO OTHER DAMAGE WAS NOTED.

THE COMPANY PRESIDENT DID STATE IN AN EMAIL THAT THE LOW LEVEL AND HIGH RATE OF SPEED COMBINATION AT WHICH THE INCIDENT OCCURRED WAS CONTRARY TO THE FLIGHT IN THE WIRE ENVIRONMENT TRAINING THE PILOT HAD.

NTSB investigation

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