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Accidents · NTSB IAD05LA122 · Final report

Enstrom 280C accident near Saulsville, West Virginia, August 12, 2005

On August 12, 2005 at about 5:30 pm local time, a Enstrom 280C (helicopter), registered N5691B, was substantially damaged in an accident near Saulsville, West Virginia. It was a business 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 pilot's inadequate remedial action following a loss of control during the landing approach.

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

What the record shows

Date
August 12, 2005 · about 5:30 pm local time
Place
Saulsville, West Virginia · map
Type
Accident
Injuries
1 person was seriously injured; 1 other was unhurt.
Weather
visual conditions (good weather)
Aircraft
Enstrom 280C · all 280Cs on the register
Registration
N5691B · no longer on the register · serial 1180
Damage
Substantial damage
Flight
Business flight · general aviation rules (Part 91)

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

While on approach to the landing area, the pilot could not see a windsock, and based his estimation of the wind by watching leaves on the trees. As he approached the landing area at a "normal to steep angle," and while stabilized at approximately 40 knots indicated airspeed, about 100 feet above the ground, the helicopter began a slow, un-commanded yaw to the right. The pilot responded by applying left anti-torque pedal; however, the helicopter continued to yaw to the right. The pilot observed that the engine and rotor rpm were "out of the green," but felt that he could not enter an autorotation due to a power line that was below. He instead increased the throttle, and the helicopter continued to yaw to the right. About 10 feet above the ground, and after about 270 degrees of yaw, the helicopter descended rapidly and impacted the ground, seriously injuring the passenger. Examination of the helicopter following the accident revealed that the tail rotor had sustained impact damage to both blades, and that the tail rotor drive shaft was fractured at the coupling hub. Examination of the fractured portions of the coupling hub revealed signatures consistent with a torsional event, such as a tail rotor strike, and no evidence that the fracture surfaces were rubbing against each other under power. According to Federal Aviation Administration Advisory Circular 90-95, loss of tail rotor effectiveness (LTE) events typically occur in a low airspeed flight regime while maneuvering, such as on final approach to landing. Any maneuver that requires the pilot to operate at high-power, at low airspeed, and with a left crosswind or tailwind, creates an environment where unanticipated right yaw may occur. Additional factors that can influence the severity of the onset of LTE include increases in gross weight and density altitude, low indicated airspeeds, and power droop. Recovery from an LTE event should include the application of full left pedal, while simultaneously moving the cyclic forward to increase speed, and altitude permitting, a reduction in power.

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: instructor: instrument helicopter; rotorcraft: helicopter
  • Flight time: 297 hours in all; 15 in this make and model; 38 in the last 90 days; 22 in the last 30 days; 218 as pilot in command
  • Last flight review: June 1, 2005
  • Medical certificate: Class 2 (with waivers/limitations)
  • Seat: left
  • Injury: no injuries

The aircraft

  • Last inspection: annual inspection, December 1, 2004; 49 hours since
  • Maximum gross weight: 2,350 lb
  • Landing gear: fixed
  • Engine: Avco Lycoming HIO-360 (piston); 0 hours total

The flight

  • Departed from: 6L4 Logan WV at 5:00 pm
  • Destination: NONE Saulsville WV
  • Flight plan: none

Weather at the time

  • Light: daylight
  • Visibility: 4 statute miles
  • Sky: clear
  • Temperature: 82°F (28°C), dew point 63°F (17°C)
  • Altimeter: 30.10 inHg
  • Observation at 1:51 pm from BKW, 17 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 N5691B the same tail number, which may have belonged to a different aircraft at the time

2006-07-15NYC06LA175 · accident near Danville, WV · substantial damage · minor 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.