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Accidents · NTSB CEN13FA025 · Final report

Agusta Spa AW139 accident near Houma, Louisiana, October 22, 2012

On October 22, 2012 at about 11:02 am local time, a Agusta Spa AW139 (helicopter), registered N385RH, was substantially damaged in an accident during landing (flare/touchdown) near Houma, Louisiana (Houme-Terrebonne Airport). It was a positioning flight under general aviation rules (Part 91). 1 person was seriously injured; 1 other was unhurt. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The helicopter’s sudden and severe vertical vibrations during landing, which resulted in a collision with terrain. The reason for the helicopter’s sudden and severe vertical vibrations could not be determined during postaccident examinations.

Source: NTSB aviation accident database, copy made November 2, 2026. Docket and reports at the NTSB.

What the record shows

Date
October 22, 2012 · about 11:02 am local time · cases in 2012
Place
Houma, Louisiana · Houme-Terrebonne Airport · cases near this airport · map
Type
Accident
Injuries
1 person was seriously injured; 1 other was unhurt.
Weather
visual conditions (good weather)
Aircraft
Agusta Spa AW139 · all AW139s on the register
Registration
N385RH · no longer on the register · serial 41013
Damage
Substantial damage
Flight
Positioning flight · general aviation rules (Part 91)

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

The flight crew was repositioning the helicopter to another landing pad when the accident occurred. According to the flight crew and flight data recorder (FDR) data, as the helicopter was touching down, it began to experience severe vertical vibrations and to oscillate violently. The pilot reported that he lowered the collective but that the vibrations and oscillations intensified. The pilot then increased the collective to lift the helicopter off the ground. The helicopter became airborne, but the violent oscillations and vibrations continued. The pilot initiated a left pedal turn to avoid another helicopter, at which time, the oscillations and vibrations were so severe that the pilots' headsets came off of their heads. The helicopter entered a spin and impacted the grass hard while moving laterally to the left. The pilots shut down and then exited the helicopter. The blue main rotor blade damper was replaced the night before the accident. A maintenance test flight was performed following the replacement. The flight crewmembers who flew the test flight reported that there was a slight vibration from the main rotor system and that one of the five main rotor blades had a "slight dip" in its track. There was no record of the main rotor blade out-of-track discrepancy nor of a main rotor track and balance inspection being performed subsequent to this flight. Although an out-of-track blade could cause a persistent vertical vibration, an examination of the main rotor blades, elastomeric bearings, main rotor dampers, main rotor rod ends, main gearbox attachment points and antitorque beam, and automatic flight control system did not reveal any anomalies that could account for the vertical vibrations reported by the flight crew and recorded on the FDR.

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. Unknown or undetermined during landing (flare/touchdown) defining event
  2. Loss of control on ground during landing (flare/touchdown)
  3. Collision with terrain or object (not controlled flight into terrain) during landing (flare/touchdown)

The NTSB's findings

  • cause Not determined › Not determined › (general) › (general) › Unknown/Not determined

Pilot

  • Certificate: airline transport pilot
  • Ratings: instrument: helicopter; rotorcraft: helicopter
  • Flight time: 3,153 hours in all; 257 in this make and model; 105 in the last 90 days; 26 in the last 30 days; 1,840 as pilot in command; 1,340 on instruments
  • Last flight review: June 6, 2012
  • Medical certificate: Class 1 (without waivers/limitations)
  • Seat: rgt
  • Injury: serious injuries

Co-pilot

  • Certificate: airline transport pilot, flight instructor, commercial pilot
  • Ratings: multi-engine land; single-engine land; single-engine sea; instructor: airplane multi-engine; instructor: airplane single-engine; instructor: helicopter; instructor: instrument airplane; instrument: airplane; instrument: helicopter
  • Flight time: 7,340 hours in all; 25 in this make and model; 60 in the last 90 days; 15 in the last 30 days; 5,375 as pilot in command
  • Last flight review: March 21, 2012
  • Medical certificate: Class 1 (with waivers/limitations)
  • Seat: left
  • Injury: no injuries

The aircraft

  • Airframe total time: 2,063 hours
  • Last inspection: continuous airworthiness programme, October 14, 2012
  • Maximum gross weight: 14,994 lb
  • Landing gear: retractable
  • Engine 1: P&W Canada PT6C-67C (turboshaft); 1,016 hours total
  • Engine 2: P&W Canada PT6C-67C (turboshaft); 2,063 hours total
  • Operator: Era Helicopters LLC

The flight

  • Departed from: KHUM Houma LA
  • Destination: KHUM Houma LA
  • Flight plan: none
  • A second pilot was aboard

Weather at the time

  • Light: dawn
  • Wind: from 070° at 3 knots
  • Visibility: 10 statute miles
  • Temperature: 55°F (13°C), dew point 55°F (13°C)
  • Altimeter: 30.06 inHg
  • Observation at 10:55 am from KHUM

Injuries

FatalSeriousMinorNone
Flight crew11

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

22 documents, released by the NTSB on May 15, 2015. 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 Helicopter Specialist’s Factual Report PDF, 7 pages View Download
2 Attachment 1 – Dampers Investigation Report PDF, 38 pages View Download
3 Attachment 2 - Elastomeric Bearing Exam Report PDF, 33 pages View Download
4 Attachment 3 - Honeywell Report - Aiop Investigation Report (Rev B) PDF, 23 pages View Download
5 Attachment 4 - Logbook Records PDF, 8 pages View Download
6 Attachment 5 – BEA Memo on Elastomer Bearing Examination PDF, 1 page View Download
7 Cockpit Voice Recorder 12 - Factual Report of Group Chairman (Placeholder) PDF, 1 page View Download
8 Flight Data Recorder Factual Report PDF, 15 pages View Download
9 Flight Data Recorder Factual Report Tabular Data data file Download
10 Sound Spectrum Study PDF, 4 pages View Download
11 Pilot/operator Aircraft Accident Report, NTSB Form 6120.1 PDF, 11 pages View Download
12 Witness Statements PDF, 9 pages View Download
13 On Scene Inspection Results PDF, 4 pages View Download
14 Hums Data PDF, 10 pages View Download
15 Pilot Records PDF, 8 pages View Download
16 Weight and Balance Information PDF, 1 page View Download
17 Statement of Party Representatives to NTSB Investigation PDF, 10 pages View Download
18 Release of Aircraft Wreckage, NTSB Form 6120.15 PDF, 1 page View Download
19 Photo 1 – Left Side View of N385RH PDF, 1 page View Download
20 Photo 2 – Right Side View of N385RH PDF, 1 page View Download
21 Photo 3 – Underside of N385RH PDF, 1 page View Download
22 Photo 4 – Front Right View of N385RH 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.

Connections how this case links to the rest of the register

Aircraft
Place

The whole map of how records connect · these connections as data: /graph/accident/CEN13FA025.json.

The bigger picture in Aviation Analytics: accidents over time since 1982, by model, by phase of flight and conditions, by place and on the map.

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 does not name anyone involved, its policy at this time. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.