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Accidents · NTSB ENG20IA005 · Final report

Agusta A109 incident near Penobscot, Maine, November 16, 2019

On November 16, 2019 at about 11:45 pm local time, a 2004 Agusta A109 (helicopter), registered N901EM, suffered minor damage in an incident during enroute (cruise) near Penobscot, Maine. It was flown under charter and air-taxi rules (Part 135). No one was hurt; 4 people were on board or involved. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

Fatigue fracture of the main rotor blade tip cap leading edge and subsequent partial separation of the tip cap, resulting in increased vibrations in the main rotor.

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

What the record shows

Date
November 16, 2019 · about 11:45 pm local time
Place
Penobscot, Maine · map
Type
Incident
Injuries
No one was hurt; 4 people were on board or involved.
Weather
visual conditions (good weather)
Aircraft
Agusta A109 E, built 2004 · all A109s on the register
Registration
N901EM · registry record · serial 11614
Damage
Minor damage
Flight
Flight · charter and air-taxi rules (Part 135)

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

The main rotor blade tip cap leading edge fractures initiated due to fatigue cracking with multiple initiation sites. At the time of the incident, the possibility of fatigue cracking of the leading edge of the P/N 709-0103-29-109 tip cap was a known issue, and Leonardo technical bulletin (bollettino tecnico, or BT) No. 109EP-85 and Federal Aviation Administration (FAA) airworthiness directive (AD) 2007-26-52 were previously issued to inspect for incipient cracks before they grew large enough to result in an inflight separation of the tip cap. These inspections primarily relied on visual inspection of the tip cap leading edge using magnification, and only required dye penetrant inspection of the leading edge if there are doubts about the presence of cracks or if damage other than a crack was found. It is possible that the fatigue crack on tip cap serial number L206 was present during its last inspection, but the visual inspection did not detect the presence of this crack. The crack on the tip cap leading edge remained undetected and propagated until the incident flight, when aerodynamic forces led to partial separation of the upper skin from the lower skin and core. While a visual inspection method can detect surface cracks, variances in the inspection environment (such as lighting), inspector experience, and operators’ maintenance practices can affect the success in detecting surface damage, such as a crack. After the initial issuance of BT No. 109EP-85 and FAA AD 2007-26-52, there continued to be a recurrence of partial and complete inflight separations of tip caps, with at least six known tip cap failures due to fatigue cracking. This indicates that reliance primarily on a visual inspection was not sufficient to eliminate the issue of detecting fatigue cracks before they resulted in a failure of the tip cap. A revision to BT No. 109EP-85 required dye penetrant inspection of the tip caps, which should provide a more reliable inspection method for identifying surface cracks.

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. Sys/Comp malf/fail (non-power) during enroute (cruise) defining event

The NTSB's findings

  • cause Aircraft › Aircraft propeller/rotor › Main rotor system › Main rotor blade system › Damaged/degraded

Pilot

  • Certificate: commercial pilot
  • Ratings: single-engine land; instructor: helicopter; instrument: helicopter; rotorcraft: helicopter
  • Flight time: 3,541 hours in all; 128 in this make and model; 86 in the last 90 days; 22 in the last 30 days; 2,734 as pilot in command; 1,411 on instruments
  • Last flight review: July 3, 2019
  • Medical certificate: Class 2
  • Seat: rgt
  • Injury: no injuries

Passenger

  • Seat: unk
  • Injury: no injuries

Passenger

  • Seat: unk
  • Injury: no injuries

Passenger

  • Seat: unk
  • Injury: no injuries

The aircraft

  • Airframe total time: 9,987.3 hours
  • Last inspection: continuous airworthiness programme, October 7, 2019
  • Landing gear: fixed
  • Engine 1: Pratt & Whitney P&W 206C (turboshaft); 9,748 hours total
  • Engine 2: Pratt & Whitney P&W 206C (turboshaft); 9,240 hours total
  • Operator: Sevenbar Aviation LLC

The flight

  • Departed from: ME15 Blue Hill ME at 11:37 pm
  • Destination: ME02 Bangor ME
  • Flight plan: none

Weather at the time

  • Light: night
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 23°F (-5°C), dew point 28°F (-2°C)
  • Altimeter: 30.51 inHg
  • Observation at 11:56 pm from KBHB, 10 miles away

Injuries

FatalSeriousMinorNone
Flight crew1
Passengers3

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

7 documents, released by the NTSB on February 4, 2021. 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.

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.