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Accidents · NTSB ERA11LA175 · Final report

Bell 206-L4 accident near Birmingham, Alabama, March 2, 2011

On March 2, 2011 at about 11:56 pm local time, a Bell 206-L4 (helicopter), registered N154MW, was substantially damaged in an accident during approach (VFR pattern base) near Birmingham, Alabama (Carraway Medical Ctr Heliport airport). It was a flight test under general aviation rules (Part 91). No one was hurt; 1 person was on board or involved. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

A total loss of engine power for undetermined reasons.

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

What the record shows

Date
March 2, 2011 · about 11:56 pm local time
Place
Birmingham, Alabama · Carraway Medical Ctr Heliport · map
Type
Accident
Injuries
No one was hurt; 1 person was on board or involved.
Weather
visual conditions (good weather)
Aircraft
Bell 206-L4 · all 206-L4s on the register
Registration
N154MW · registry record · serial 52154
Damage
Substantial damage
Flight
Flight test · general aviation rules (Part 91)

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

The helicopter pilot reported that, following a maintenance test flight to verify that a newly installed power turbine governor was accurately set, he flew over the anticipated landing area and entered the downwind leg of the traffic pattern. While turning to the base leg of the traffic pattern, about 500 feet above ground level and at 40 to 50 knots, he reported that he heard a loud bang and that the airframe “lurched.” He entered an autorotation and located a vacant parking garage deck within gliding range. The engine-out audio warning sounded and segment lights illuminated. The pilot landed the helicopter and it skidded about 15 feet. A test run determined that the engine operated below the normal specifications for new engines. The pneumatic line from the power turbine governor was found to be leaking and was removed and sent to the NTSB's Materials Laboratory for further examination. That examination revealed superficial longitudinal tool marks that did not extend to the interior surfaces of the flared ends. The interior surface of the flared ends exhibited some localized fretting damage on one side, consistent with damage that could have been caused by inadequate torque at the connection; however, no other anomalies were noted. According to the engine manufacturer, the leak would not have caused the engine to operate below the normal specification. The postaccident examination revealed no preimpact mechanical malfunctions or failures with the helicopter or engine that would have precluded normal operation.

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. Loss of engine power (total) during approach (VFR pattern base) defining event
  2. Off-field or emergency landing during emergency descent
  3. Autorotation Hard landing

The NTSB's findings

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

Pilot

  • Certificate: airline transport pilot, flight instructor, commercial pilot
  • Ratings: multi-engine land; single-engine land; instructor: helicopter; instructor: instrument helicopter; instrument: airplane; instrument: helicopter; rotorcraft: helicopter
  • Flight time: 10,599 hours in all; 1,884 in this make and model; 51 in the last 90 days; 20 in the last 30 days; 10,484 as pilot in command; 2,962 on instruments
  • Last flight review: August 23, 2010
  • Medical certificate: Class 2 (without waivers/limitations)
  • Seat: rgt
  • Injury: no injuries

The aircraft

  • Airframe total time: 4,613 hours
  • Last inspection: approved inspection programme, February 8, 2011; 138 hours since
  • Maximum gross weight: 4,450 lb
  • Seats: 5
  • Landing gear: fixed
  • Engine: Allison 250-C30-P (turboshaft); 0 hours total
  • Operator: Omniflight Helicopters INC

The flight

  • Departed from: AL49 Birmingham AL at 11:41 pm
  • Destination: AL49 Birmingham AL

Weather at the time

  • Light: daylight
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 66°F (19°C), dew point 39°F (4°C)
  • Altimeter: 30.20 inHg
  • Observation at 11:53 pm from BHM, 4 miles away

Injuries

FatalSeriousMinorNone
Flight crew1

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

The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.

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.