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Accidents · NTSB CHI02LA181 · Final report

Bell 206B accident near Three Rivers, Michigan, July 6, 2002

On July 6, 2002 at about 2:45 pm local time, a Bell 206B (helicopter), registered N60EA, was substantially damaged in an accident near Three Rivers, Michigan. It was a personal flight under general aviation rules (Part 91). No one was hurt; 2 people were on board or involved. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

A loss of tail rotor effectiveness.

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

What the record shows

Date
July 6, 2002 · about 2:45 pm local time
Place
Three Rivers, Michigan · map
Type
Accident
Injuries
No one was hurt; 2 people were on board or involved.
Weather
visual conditions (good weather)
Aircraft
Bell 206B · all 206Bs on the register
Registration
N60EA · registry record · serial 2068
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

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

The helicopter sustained substantial damage during an emergency landing after liftoff. The pilot reported that a normal takeoff was made to the southwest, and upon reaching an altitude of 75 feet, he began a turn to the south and noticed that the aircraft was not responding to the turn. When the helicopter began to accelerate forward it started to spin to the right and the tail rotor lost all effectiveness. The helicopter spun 3 and 1/2 revolutions and the pilot then maneuvered it to an open pasture for the emergency landing. He lowered the collective bringing the aircraft to the ground for a level touchdown with no forward motion. The pilot stated that a local airport reported a wind from the southeast at 4 knots, and prior to the departure the wind was "non existent." No anomalies were found with the helicopter or its flight control systems that were determined to exist prior to impact. According to the FAA, a loss of tail rotor effectiveness (LTE) is "not related to an equipment or maintenance malfunction and may occur in all single-rotor helicopters at airspeeds less than 30 knots. It is the result of the tail rotor not providing adequate thrust to maintain directional control, and is usually caused by either certain wind azimuths (directions) while hovering, or by an insufficient tail rotor thrust for a given power setting at higher altitudes."

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, private
  • Ratings: multi-engine land; single-engine land; instrument: airplane; rotorcraft: helicopter
  • Flight time: 970 hours in all; 369 in this make and model; 50 in the last 90 days; 30 in the last 30 days; 870 as pilot in command
  • Last flight review: February 26, 2002
  • Medical certificate: Class 2 (valid medical--no waivers/lim.)
  • Seat: rgt
  • Injury: no injuries

The aircraft

  • Airframe total time: 7,300 hours
  • Last inspection: 100-hour inspection, July 1, 2002; 20 hours since
  • Maximum gross weight: 3,600 lb
  • Seats: 5
  • Landing gear: fixed
  • Engine: Allison 250-C20 (turboshaft); 0 hours total
  • Operator: Phoenix Precision Air LLC

The flight

  • Departed from: Three Rivers MI at 2:45 pm
  • Destination: GSH Goshen IN
  • Flight plan: none

Weather at the time

  • Light: daylight
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 70°F (21°C), dew point 55°F (13°C)
  • Altimeter: 30.29 inHg
  • Observation at 2:57 pm from IRS, 18 miles away

Injuries

FatalSeriousMinorNone
Crew1
Passengers1

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.

Other NTSB records under N60EA the same tail number, which may have belonged to a different aircraft at the time

2017-10-24CEN18LA020 · accident near Groom, TX · substantial damage · no injuries
2016-04-07CEN16WA147 · accident near Suwalki · substantial damage · serious injuries

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.