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Accidents · NTSB CEN15LA395 · Final report

Bell Helicopter Textron Canada 429 accident near Port O'Connor, Texas, August 21, 2015

On August 21, 2015 at about 8:30 pm local time, a 2011 Bell Helicopter Textron Canada 429, registered N429AR, was substantially damaged in an accident during enroute (cruise) near Port O'Connor, Texas. It was a personal flight under general aviation rules (Part 91). No one was hurt; 3 people were on board or involved. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The fatigue failure of the tail rotor pitch change link spherical bearing housing as a result of corrosion pitting.

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

What the record shows

Date
August 21, 2015 · about 8:30 pm local time
Place
Port O'Connor, Texas · map
Type
Accident
Injuries
No one was hurt; 3 people were on board or involved.
Weather
visual conditions (good weather)
Aircraft
Bell Helicopter Textron Canada 429, built 2011 · all 429s on the register
Registration
N429AR · registry record · serial 57035
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

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

The commercial pilot reported that, during cruise flight in the helicopter, he felt a "slight vibration" and heard a "very faint bumping sound." A flight control check revealed no anomalies, and the pilot continued the flight to the destination heliport. While in a 4-ft hover, just before touching down, the helicopter began a slow, uncommanded right turn. The pilot applied full left anti-torque pedal, and the turn stopped. He then lowered the collective and landed without incident. A post-flight inspection of the helicopter revealed that one of the tail rotor outboard pitch change links (PCL) was broken. An examination of the failed PCL revealed fatigue fractures due to pitting corrosion between the spherical bearing and the bearing housing. The fatigue fractures propagated during operation until the PCL bearing housing fractured, separating the PCL from the blade pitch horn end spherical bearing, resulting in a loss of pitch control to the affected blade. The PCL was installed on the helicopter 12 days before the manufacturer issued an alert service bulletin (ASB) introducing a 50-hour recurrent inspection of the tail rotor PCLs for axial and radial bearing play. About 6 months later, the Federal Aviation Administration (FAA) subsequently issued an emergency airworthiness directive (EAD) based on the ASB. The tail rotor PCLs on the accident helicopter were inspected in accordance with the ASB and the EAD 9 days after the EAD was issued. The PCL failed 6.6 flight hours after the inspection. The EAD did not require an inspection of the bearing housing portion of the PCL for corrosion, and it could not be determined if the fatigue cracks were present when the inspection was performed. Following the accident, the manufacturer updated the original ASB to include inspections for bearing cracks, corrosion, and anti-corrosion sealant. The FAA also updated the airworthiness directive to reflect the additional inspections.

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. Flight control sys malf/fail during enroute (cruise) defining event

The NTSB's findings

  • cause Aircraft › Aircraft systems › Flight control system › (general) › Failure

Pilot

  • Certificate: flight instructor, commercial pilot, private
  • Ratings: single-engine land; instructor: helicopter; rotorcraft: helicopter
  • Flight time: 9,300 hours in all; 22 in this make and model; 70 in the last 90 days; 23 in the last 30 days; 9,000 as pilot in command; 400 on instruments
  • Last flight review: February 3, 2015
  • Medical certificate: Class 2 (without waivers/limitations)
  • Seat: rgt
  • Injury: no injuries

The aircraft

  • Airframe total time: 1,168.8 hours
  • Last inspection: continuous airworthiness programme, June 19, 2015
  • Maximum gross weight: 7,000 lb
  • Seats: 7
  • Landing gear: fixed
  • Engine 1: Pratt & Whitney 207D1 (turboshaft); 1,242 hours total
  • Engine 2: Pratt & Whitney 207D1 (turboshaft); 1,242 hours total

The flight

  • Departed from: PVT Giddings TX at 7:50 pm
  • Destination: PVT Port O'Connor TX
  • Flight plan: none

Weather at the time

  • Light: daylight
  • Wind: from 070° at 5 knots
  • Visibility: 7 statute miles
  • Sky: clear
  • Temperature: 73°F (23°C), dew point 73°F (23°C)
  • Altimeter: 29.89 inHg
  • Observation at 8:22 pm from PKV, 22 miles away

Injuries

FatalSeriousMinorNone
Flight crew1
Passengers2

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

10 documents, released by the NTSB on March 14, 2017. 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.