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Accidents · NTSB ERA18FA122 · Final report

MD Helicopter 600 accident near Smethport, Pennsylvania, April 8, 2018

On April 8, 2018 at about 9:11 pm local time, a 1998 MD Helicopter 600, registered N602BP, was destroyed in an accident during maneuvering (hover) near Smethport, Pennsylvania. It was an other work-use flight under external-load helicopter rules (Part 133). 2 people were killed and 1 person was seriously injured. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The helicopter pilot's failure to maintain adequate clearance during power line construction work, which resulted in the helicopter's main rotor striking and becoming entangled with a wire and a subsequent dynamic rollover and collision with terrain. Contributing to the accident was the pilot's and linemen's decision to continue work without a secondary safety device installed, which was contrary to standard operating procedures.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
April 8, 2018 · about 9:11 pm local time
Place
Smethport, Pennsylvania · map
Type
Accident
Injuries
2 people were killed and 1 person was seriously injured.
Weather
visual conditions (good weather)
Aircraft
MD Helicopter 600 N, built 1998
Registration
N602BP · no longer on the register · serial RN025
Damage
Destroyed
Flight
Other work-use flight · external-load helicopter rules (Part 133)

The NTSB's narrative final · quoted from the NTSB record

The pilot of the helicopter was conducting a power line construction flight. The power lines were supported by a series of structures made of either wood (dual-pole, H-frame) or steel (single pole). A static line was affixed to the top of the structures above the power lines. The purpose of the flight was to remove the static line from the wheeled, pulley device (dolly) that temporarily secured the static line and permanently secure the static line to the structures. One lineman completed the task from the skid of the hovering helicopter, and another lineman inside the helicopter passed tools and equipment back and forth to the lineman on the skid. The accident occurred when the crew (the pilot and the two linemen) were working on the second structure, which was constructed of wood. During work on that structure, the helicopter hovered facing westbound adjacent to the wooden structure with the pilot, both linemen, and the structure on the helicopter's left side. The static line sloped upward aft of the helicopter toward the uphill structure and downward and to the right toward the downhill structure. The initial steps taken for the task included wrapping the line with a spiraled wire coating (armor rod) and attaching a safety strap (safety). The lineman on the helicopter skid attached the first half of the armor rod ahead of the dolly and manipulated the line and the dolly to complete the wrap. According to the pilot, the lineman opened the spring-loaded locking gate on the dolly above the static line to wrap the second half of the armor rod, which was "normal" before the attachment of the safety. About that time, the pilot felt the helicopter being "pulled" toward the structure. The pilot stated that he made cyclic and pedal inputs to avoid the structure but reported that "all I remember is rolling over the structure." The pilot stated that he neither felt nor heard anything unusual before the helicopter was pulled toward the structure. Visual examination of the static line, helicopter rotor blades, and visual and metallurgical examination of the dolly revealed that, as the lineman on the skid wrapped the armor rod, and before he attached the safety, the aft portion of the main rotor struck the static line, which broke the locking gate that secured the line inside the dolly. Once free of the dolly, the static line fell between the uphill and downhill structures and over the left front skid of the helicopter, which created the pivot point over which the helicopter rolled inverted. The pilot and the linemen began work without installing a safety. According to the operator's director of safety, the safety strap aboard the helicopter was "not long enough" to install it before work began. The holding company of the subsidiary that hired the operator as an independent contractor had a safety manual for linemen who performed work from helicopters. The manual indicated that "secondary securement systems shall be utilized" when clipping wire (permanently securing a static line to the structures).

The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.

The factual record from the NTSB's investigation tables, in plain English

What happened, in order

  1. Miscellaneous/other during maneuvering (hover)
  2. Collision with terrain or object (not controlled flight into terrain) during maneuvering (hover)
  3. External load event (Rotorcraft) during maneuvering (hover) defining event
  4. Loss of control in flight during maneuvering (hover)
  5. Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent

The NTSB's findings

  • cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › (general) › Not attained/maintained
  • cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
  • cause Environmental issues › Physical environment › Object/animal/substance › Wire › Response/compensation
  • factor Personnel issues › Action/decision › Info processing/decision › Decision making/judgment › Flight crew
  • factor Personnel issues › Action/decision › Action › Incorrect action performance › Flight crew
  • factor Personnel issues › Task performance › Use of equip/info › Use of policy/procedure › Flight crew

Pilot

  • Certificate: commercial pilot
  • Ratings: instrument: helicopter; rotorcraft: helicopter
  • Flight time: 6,200 hours in all; 250 in this make and model; 150 in the last 90 days; 50 in the last 30 days
  • Medical certificate: Class 2 (without waivers/limitations)
  • Seat: left
  • Injury: serious injuries

The aircraft

  • Airframe total time: 5,203.6 hours
  • Last inspection: 100-hour inspection, February 4, 2018; 73 hours since
  • Maximum gross weight: 4,500 lb
  • Landing gear: fixed
  • Engine: Allison 250-C47 (turboshaft); 0 hours total
  • Operator: High Line Helicopters, LLC

The flight

  • Departed from: Smethport PA at 9:00 pm
  • Destination: Smethport PA
  • Flight plan: none

Weather at the time

  • Light: daylight
  • Wind: from 290° at 10 knots
  • Visibility: 10 statute miles
  • Sky: overcast at 4,100 ft
  • Temperature: 27°F (-3°C), dew point 10°F (-12°C)
  • Altimeter: 29.95 inHg
  • Observation at 8:53 pm from BFD, 10 miles away

Injuries

FatalSeriousMinorNone
Flight crew21

Documents from the investigation the NTSB's docket: the evidence folder behind the report

23 documents, released by the NTSB on November 4, 2019. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.

#DocumentWhat it is
1 Pilot/operator Aircraft Accident Report, NTSB Form 6120.1 PDF, 9 pages View Download
2 Pilot's Interview Summary PDF, 2 pages View Download
3 Company Officer Interview Summaries with Pilot PDF, 5 pages View Download
4 Witness Statements PDF, 26 pages View Download
5 Memorandum for Record - Director of Safety Hlh PDF, 1 page View Download
6 Correspondence - Quanta Services Lineman Crew Training Discussion PDF, 3 pages View Download
7 Operations Safety Manual Excerpt PDF, 1 page View Download
8 FAA Inspector's Statement PDF, 3 pages View Download
9 Reports from Parties to the Investigation - Boeing and Mdhi PDF, 2 pages View Download
10 Materials Laboratory Factual Report PDF, 12 pages View Download
11 Reports from Parties to the Investigation - Rolls Royce PDF, 12 pages View Download
12 Aircraft Performance - Weight and Balance (FAA) PDF, 2 pages View Download
13 Structures - Md 600N Dimensions PDF, 3 pages View Download
14 Photos PDF, 10 pages View Download
15 Statement of Party Representatives to NTSB Investigation PDF, 4 pages View Download
16 Release of Aircraft Wreckage, NTSB Form 6120.15 PDF, 1 page View Download
17 Evidence Control Form PDF, 6 pages View Download
18 UAS Aerial Imagery-factual/study Report PDF, 13 pages View Download
19 Attachment 1-IMAGE.PDF PDF, 1 page View Download
20 Attachment 2-IMAGE.PDF PDF, 1 page View Download
21 Attachment 3-IMAGE.PDF PDF, 1 page View Download
22 Attachment 4-IMAGE.PDF PDF, 1 page View Download
23 Attachment 5-ORTHOMOSAIC (Google Earth File) - Shelf Item PDF, 1 page View Download

The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.

Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.