20180429022289I

Incident · Minor damage

FAA incident report · Hughes 369D · Newark, OH · April 29, 2018

Date
April 29, 2018 · 11:35 local
Place
Newark, OH
Airport
Newark Heath
Phase of flight
Hover/Holding
Operating rules
Rotorcraft external load (Part 133)
Damage
Minor damage
Aircraft
N175JL
NTSB investigation
NTSBGAA18CA249
Reported as
Hughes 369D
Reported engine
Rolls-Royce 250-C20B
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor
Pilot’s flight hours
4,540 total3,760 in this make and model150 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 4/29/2018, at approximately 11 :35 am, pilot in command (PIC} and lineman (seated to the pilot's left on work platform) departed the landing zone, located at coordinates N40.14, W82.31. The crew traveled eastbound on the south side of the power lines for 3/4 mile, crossed over a structure and turned back west to begin work.

The PIC descended to the outside phase and then moved the aircraft laterally toward the line. During the approach, the lineman bonded onto the wire and began installing a new spacer between the 4-bundle conductor. As the lineman was working to compress and lock the upper inboard spacer connector, the pilot maneuvered the helicopter closer to better position the lineman.

During repositioning, the PIC heard a noise and felt a vibration from the tail section. Upon realizing the tail rotor made contact with the conductor, the pilot communicated with the lineman to ready and unbond from the conductor. The PIC then moved away from the wire and felt no abnormality of flight. The pilot flew the aircraft under normal operating condition back to the landing zone with no further event. The helicopter was then shut down according to procedure.

During the inspection of the aircraft, the mechanic found the last 4 inches on both tail rotor blades dented and scuffed. No other discrepancies noted.

The columbus flight standards district office was not notified of the accident until 05/04/2018 which was provided by NTSB personnel.

As the FAA filed it

ON 4/29/2018, AT APPROXIMATELY 11 :35 AM, PILOT IN COMMAND (PIC} AND LINEMAN (SEATED TO THE PILOT'S LEFT ON WORK PLATFORM) DEPARTED THE LANDING ZONE, LOCATED AT COORDINATES N40.14, W82.31. THE CREW TRAVELED EASTBOUND ON THE SOUTH SIDE OF THE POWER LINES FOR 3/4 MILE, CROSSED OVER A STRUCTURE AND TURNED BACK WEST TO BEGIN WORK.

THE PIC DESCENDED TO THE OUTSIDE PHASE AND THEN MOVED THE AIRCRAFT LATERALLY TOWARD THE LINE. DURING THE APPROACH, THE LINEMAN BONDED ONTO THE WIRE AND BEGAN INSTALLING A NEW SPACER BETWEEN THE 4-BUNDLE CONDUCTOR. AS THE LINEMAN WAS WORKING TO COMPRESS AND LOCK THE UPPER INBOARD SPACER CONNECTOR, THE PILOT MANEUVERED THE HELICOPTER CLOSER TO BETTER POSITION THE LINEMAN.

DURING REPOSITIONING, THE PIC HEARD A NOISE AND FELT A VIBRATION FROM THE TAIL SECTION. UPON REALIZING THE TAIL ROTOR MADE CONTACT WITH THE CONDUCTOR, THE PILOT COMMUNICATED WITH THE LINEMAN TO READY AND UNBOND FROM THE CONDUCTOR. THE PIC THEN MOVED AWAY FROM THE WIRE AND FELT NO ABNORMALITY OF FLIGHT. THE PILOT FLEW THE AIRCRAFT UNDER NORMAL OPERATING CONDITION BACK TO THE LANDING ZONE WITH NO FURTHER EVENT. THE HELICOPTER WAS THEN SHUT DOWN ACCORDING TO PROCEDURE.

DURING THE INSPECTION OF THE AIRCRAFT, THE MECHANIC FOUND THE LAST 4 INCHES ON BOTH TAIL ROTOR BLADES DENTED AND SCUFFED. NO OTHER DISCREPANCIES NOTED.

THE COLUMBUS FLIGHT STANDARDS DISTRICT OFFICE WAS NOT NOTIFIED OF THE ACCIDENT UNTIL 05/04/2018 WHICH WAS PROVIDED BY NTSB PERSONNEL.

NTSB investigation

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