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Accidents · NTSB GAA16CA163 · Final report

Enstrom F280 accident near Sodus, New York, March 26, 2016

On March 26, 2016 at about 2:30 pm local time, a 1981 Enstrom F280 (helicopter), registered N5698Y, was substantially damaged in an accident during landing (flare/touchdown) near Sodus, New York (Williamson-Sodus airport). It was an instructional 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

The pilot's improper collective application at touchdown during a practice run-on landing, which resulted in the main rotor system impacting the tailboom and the forward portion of the fuselage impacting terrain during remedial action by the flight instructor. Contributing to the accident was the flight instructor's delayed remedial action.

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

What the record shows

Date
March 26, 2016 · about 2:30 pm local time
Place
Sodus, New York · Williamson-Sodus · map
Type
Accident
Injuries
No one was hurt; 2 people were on board or involved.
Weather
visual conditions (good weather)
Aircraft
Enstrom F280 F, built 1981
Registration
N5698Y · no longer on the register · serial 1212
Damage
Substantial damage
Flight
Instructional flight · general aviation rules (Part 91)

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

The flight instructor reported that he asked the pilot receiving instruction to demonstrate a run-on landing on the sod between the runway and taxiway. He reported that as the helicopter touched down at about 25 miles per hour (21.72 knots), the pilot lowered the collective to the full down position while the helicopter was still moving forward with considerable momentum. The helicopter began to "lurch forward" and the nose of the helicopter started to lower. The flight instructor then came on the flight controls, but the helicopter had progressed to an "extreme nose low attitude," and he applied aft cyclic to prevent the main rotor blades from impacting terrain. The main rotor blades instead impacted and separated the tailboom. The fuselage continued moving forward and the nose impacted terrain and then settled back on the skids. The helicopter sustained substantial damage to the fuselage, main rotor system, tailboom, and tail rotor system. The flight instructor verified that there were no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. The flight instructor reported that he recommended landing on sod due to potential wear on the bottom of the skids from friction with the paved runway. He also reported that the pilot had successfully performed run-on landings in the past on the sod area. As a safety recommendation, the flight instructor reported that landing the helicopter on the runway instead of the sod may have lessened the effects of improper application of the collective at touchdown. He reported that he should have verbally reviewed the importance of using the collective to control the friction with the landing surface while in the traffic pattern to ensure the pilot's intentions were mutually understood. He further reported that he should have maintained a guarded position on the flight controls regardless of the pilot's abilities to decrease the flight instructor's reaction time for maneuver recovery.  Enstrom Helicopter Corporation has published the Enstrom 280F Training Maneuvers Manual (2014). This manual discusses objectives and descriptions for a shallow approach and run-on landing, and states in part: Caution, Enstrom does not endorse practicing run-on landings. Run-on landings should only be accomplished on a smooth, hard surface; and should always be planned to the center of the runway to preclude sliding off the runway, and overturning. After ground contact, maintain heading with pedals and maintain collective position. Ensure that power is maintained until the helicopter comes to a complete stop to insure directional control. The Federal Aviation Administration has published the Helicopter Instructor's Handbook FAA-H-8083-4 (2012). This handbook provides instructional information for a shallow approach and run-on landing and states in part: In any case, do not rapidly lower the collective after touchdown. Smooth reduction of collective prevents a rapid stop that could result in damage to the aircraft or injury to the crew. For helicopters equipped with skids, it may be better to practice running landings on a hard surface runway instead of on a grassy field because there is less probability of catching a skid, which can lead to dynamic rollover. In addition, check the condition of the skid shoes before and after practicing running takeoffs and landings.

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. Simulated/training event during landing
  2. Abnormal runway contact during landing (flare/touchdown) defining event
  3. Loss of control on ground during landing (landing roll)
  4. Dynamic rollover during landing (landing roll)
  5. Attempted remediation/recovery during landing (landing roll)
  6. Part(s) separation from AC during landing (landing roll)
  7. Collision during takeoff/land during landing (landing roll)

The NTSB's findings

  • cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Student/instructed pilot
  • cause Aircraft › Aircraft propeller/rotor › Rotorcraft flight control › Main rotor control › Incorrect use/operation
  • cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Pitch control › Incorrect use/operation
  • factor Personnel issues › Action/decision › Action › Delayed action › Instructor/check pilot

Flight instructor

  • Certificate: flight instructor, commercial pilot
  • Ratings: single-engine land; instructor: helicopter; instructor: instrument helicopter; instrument: helicopter; rotorcraft: helicopter
  • Flight time: 3,847 hours in all; 151 in this make and model; 44 in the last 90 days; 20 in the last 30 days; 3,657 as pilot in command; 1,267 on instruments
  • Last flight review: April 15, 2015
  • Medical certificate: Class 2 (with waivers/limitations)
  • Seat: rgt
  • Injury: no injuries

Dual student

  • Certificate: flight instructor, commercial pilot
  • Ratings: single-engine land; single-engine sea; instructor: airplane single-engine; instructor: instrument airplane; instrument: airplane
  • Flight time: 1,698 hours in all; 9 in this make and model; 7 in the last 90 days; 5 in the last 30 days; 1,593 as pilot in command; 825 on instruments
  • Last flight review: December 19, 2015
  • Medical certificate: Class 2 (with waivers/limitations)
  • Seat: left
  • Injury: no injuries

The aircraft

  • Airframe total time: 2,070 hours
  • Last inspection: 100-hour inspection, October 27, 2015
  • Maximum gross weight: 2,600 lb
  • Seats: 2
  • Landing gear: fixed
  • Engine: Lycoming HIO-360-F1AD (piston); 1,734 hours total
  • Operator: B.A.C. Services

The flight

  • Departed from: SDC Sodus NY at 2:25 pm
  • Destination: SDC Sodus NY
  • Flight plan: none
  • Runway 10, 3,801 ft by 60 ft
  • A second pilot was aboard

Weather at the time

  • Light: daylight
  • Wind: from 110° at 5 knots
  • Visibility: 10 statute miles
  • Sky: scat at 2,100 ft
  • Temperature: 34°F (1°C), dew point 25°F (-4°C)
  • Altimeter: 30.34 inHg
  • Observation at 1:54 pm from KROC, 25 miles away

Injuries

FatalSeriousMinorNone
Flight crew2

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.