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Accidents · NTSB ERA13LA300 · Final report

Sikorsky 269C accident near Lumberton, New Jersey, June 22, 2013

On June 22, 2013 at about 7:00 pm local time, a Sikorsky 269C (helicopter), registered N2091E, was substantially damaged in an accident during approach (VFR pattern final) near Lumberton, New Jersey (Flying W Airport). It was a personal flight under general aviation rules (Part 91). 1 person had minor injuries; 1 other was unhurt. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The pilot's movement of the throttle to the idle detent at the beginning of a practice autorotation, which was contrary to procedures and resulted in the engine hesitating during the power recovery and a subsequent hard landing.

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

What the record shows

Date
June 22, 2013 · about 7:00 pm local time
Place
Lumberton, New Jersey · Flying W Airport · map
Type
Accident
Injuries
1 person had minor injuries; 1 other was unhurt.
Weather
visual conditions (good weather)
Aircraft
Sikorsky 269C
Registration
N2091E · registry record · serial S1837
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

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

The pilot initiated a practice autorotation about 951 feet above ground level (agl), rolled off the throttle to the idle detent, and maintained 60 knots during the descent until 50 feet agl, at which time, he flared the helicopter. At the end of the flare, when the helicopter was about 20 to 30 feet agl, the pilot lowered the nose to level the helicopter, began to increase the collective, and rolled on the throttle for a power recovery. The pilot reported that, subsequently, the engine sounded like it was "bogging down" and that the engine rpm was not increasing enough for the helicopter to continue to come to a hover. The helicopter continued to descend and contacted the runway hard, which resulted in substantial damage to the vertical firewall. A postaccident engine run revealed no evidence of a preimpact failure or malfunction that would have precluded normal operation. According to the pilot's flight manual, when performing practice autorotations, the pilot should lower the collective while maintaining the throttle setting to prevent the engine from "loading up or stalling" during recovery. Therefore, it is likely that the pilot rolling the throttle to the idle detent at the beginning of the maneuver, which was contrary to procedures, resulted in the engine hesitating when power was applied for the recovery.

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 approach (VFR pattern final)
  2. Loss of engine power (partial) during approach (VFR pattern final) defining event
  3. Hard landing during landing (flare/touchdown)

The NTSB's findings

  • cause Personnel issues › Action/decision › Action › Incorrect action performance › Pilot
  • cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Powerplant parameters › Not attained/maintained
  • cause Aircraft › Aircraft power plant › Power plant › (general) › Incorrect use/operation

Pilot

  • Certificate: flight instructor, commercial pilot, private
  • Ratings: single-engine land; instructor: helicopter; instrument: helicopter; rotorcraft: helicopter
  • Flight time: 316 hours in all; 47 in this make and model; 227 as pilot in command; 9 on instruments
  • Last flight review: March 10, 2013
  • Medical certificate: Class 2 (with waivers/limitations)
  • Seat: left
  • Injury: minor injuries

The aircraft

  • Airframe total time: 4,799 hours
  • Last inspection: 100-hour inspection, June 3, 2013
  • Maximum gross weight: 2,050 lb
  • Seats: 3
  • Landing gear: fixed
  • Engine: Lycoming HIO-360-D1A (piston); 0 hours total
  • Operator: Helicopter Flight Services

The flight

  • Departed from: N14 Lumberton NJ at 6:00 pm
  • Destination: N14 Lumberton NJ
  • Flight plan: none
  • Runway 19, 3,496 ft by 75 ft

Weather at the time

  • Light: daylight
  • Wind: at 3 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 82°F (28°C), dew point 61°F (16°C)
  • Altimeter: 30.21 inHg
  • Observation at 6:54 pm from VAY, 2 miles away

Injuries

FatalSeriousMinorNone
Flight 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 N2091E the same tail number, which may have belonged to a different aircraft at the time

1982-09-30FTW82IA401 · incident near Intracoastal Ci, LA · minor damage · no 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.