The U.S. aircraft register, updated daily · Carbon Free Flight by 2050
Accidents · NTSB FTW84LA166 · Preliminary: the investigation is not finished

Bell 206L-1 accident near W Camrn Blk 624, March 12, 1984

On March 12, 1984 at about 4:45 pm local time, a Bell 206L-1 (helicopter), registered N1076N, was destroyed in an accident near W Camrn Blk 624. It was a flight of an unrecorded kind under charter and air-taxi rules (Part 135). 4 people were killed and 1 person was seriously injured. The weather was instrument conditions (cloud, fog or low visibility).

Preview. This page is not yet listed for search engines.

The NTSB's probable cause their words, unchanged

The NTSB has not yet published a probable cause for this accident. Investigations usually take one to two years; this page updates when the final report is released.

Source: NTSB aviation accident database, copy made October 4, 2026. Docket and reports at the NTSB.

What the record shows

Date
March 12, 1984 · about 4:45 pm local time
Place
W Camrn Blk 624
Type
Accident
Injuries
4 people were killed and 1 person was seriously injured.
Weather
instrument conditions (cloud, fog or low visibility)
Aircraft
Bell 206L-1 · all 206L-1s on the register
Registration
N1076N · registry record · serial 45369
Damage
Destroyed
Flight
Flight of an unrecorded kind · charter and air-taxi rules (Part 135)

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

THE PILOT AND PASSENGERS BOARDED THE HELICOPTER IN AN ATTEMPT TO FLY OFF THE RIG BEFORE THE PASSAGE OF A SQUALL LINE. THE ACFT ENGINE WAS BEING STARTED WHEN THE ACFT WAS BLOWN OFF THE PLATFORM AND INTO THE WATER BY A GUST OF WIND. THE ACFT IMPACTED THE SEA 100 FT BELOW THE PLATFORM IN A TAIL FIRST ATTITUDE.

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

Pilot

  • Certificate: commercial pilot
  • Ratings: multi-engine land; single-engine land; rotorcraft: helicopter
  • Flight time: 3,045 hours in all; 879 in this make and model; 164 in the last 90 days; 2,288 as pilot in command
  • Medical certificate: Class 2 (valid medical--no waivers/lim.)
  • Seat: rgt

The aircraft

  • Airframe total time: 4,510 hours
  • Last inspection: approved inspection programme, March 4, 1984; 19 hours since
  • Maximum gross weight: 4,150 lb
  • Seats: 6
  • Landing gear: fixed
  • Engine: Allison 250C-28 (turboshaft); 0 hours total

The flight

  • Runway 0

Weather at the time

  • Light: daylight
  • Wind: from 290° at 25 knots
  • Sky: not recorded at 400 ft
  • Temperature: 59°F (15°C), dew point 59°F (15°C)
  • Altimeter: 30.00 inHg
  • Observation at 5:00 pm from VER, 46 miles away

Injuries

FatalSeriousMinorNone
Crew1
Passengers31

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.

About this page

Everything above comes from the NTSB's public accident database: the narrative, probable cause and findings are the NTSB's own words, and the coded tables behind its report (pilot, aircraft, flight, weather, injuries, sequence of events) are written out in plain English. Pilots' ages, home towns and medical details are left out on purpose. The documents and photographs are the NTSB's docket, the folder of records gathered during the investigation, shown as the NTSB released them (the NTSB redacts some personal details first) and listed under the NTSB's own titles. This site's own text never names pilots, passengers or anyone else involved. A preliminary report describes what is known soon after the event and can change; the final report, with the probable cause, usually follows one to two years later and this page is refreshed when it does. Case number FTW84LA166.