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Accidents · NTSB ERA15FA141 · Final report

Amateur-built FREEDOM accident near Boynton Beach, Florida, March 2, 2015

On March 2, 2015 at about 5:52 pm local time, a 2008 amateur-built FREEDOM, registered N787Z, was destroyed in an accident during enroute (cruise) near Boynton Beach, Florida. It was a personal flight under general aviation rules (Part 91). 2 people were killed. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

An in-flight loss of control for reasons that could not be determined based on the available evidence.

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

What the record shows

Date
March 2, 2015 · about 5:52 pm local time
Place
Boynton Beach, Florida · map
Type
Accident
Injuries
2 people were killed.
Weather
visual conditions (good weather)
Aircraft
Amateur-built FREEDOM S100, built 2008
Registration
N787Z · no longer on the register · serial 130-001-027
Damage
Destroyed
Flight
Personal flight · general aviation rules (Part 91)

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

The airline transport pilot departed in his light sport aircraft with a friend, who held a student pilot certificate, on a cross-country flight to another airport for lunch. GPS data showed the airplane maneuvered near the accident site for about 30 minutes, performing multiple climbs, descents, and turns. Several witnesses reported hearing the engine "sputter," which was immediately followed by an advance in engine power. Although the airplane's final movements were not captured by witness reports or radar/GPS data, examination of the accident site showed that the airplane was in a steep descent when it impacted a swamp. The impact geometry was consistent with an in-flight loss of control and subsequent uncontrolled descent to ground impact. A postcrash fire ensued, which consumed most of the airplane. Postaccident examination of the airplane and the engine did not reveal any mechanical anomalies that would have precluded normal operation. Although the environmental conditions were favorable for light icing at glide or cruise power, witnesses reported that the engine regained power after "sputtering"; such a gain in power is not consistent with a carburetor ice condition. The cause of the "sputtering" reported by the witnesses could not be determined because the extensive fire damage precluded testing of the engine-driven fuel pump, carburetors, and ignition system components. The pilot reported a vibration in the control stick to the airplane manufacturer in the days leading up to the accident. The manufacturer responded to the pilot on the morning of the accident and stated that the vibration could be the result of an inadequately balanced engine or propeller. However, the propeller's effect on the airplane's performance could not be determined because two of the blades were not recovered from the accident site and the acetal pitch change slide block within the propeller hub was consumed by postcrash fire. Although sedating medications were found in toxicological specimens from both occupants, and the pilot's autopsy found evidence of severe coronary artery disease, the investigation could not determine if these physiological conditions contributed to the accident.

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. Loss of control in flight during enroute (cruise) defining event
  2. Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent
  3. Fire/smoke (post-impact) during post (impact)

The NTSB's findings

  • cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › (general) › Not attained/maintained
  • cause Not determined › Not determined › (general) › (general) › Unknown/Not determined

Pilot

  • Certificate: airline transport pilot, commercial pilot, flight engineer
  • Ratings: multi-engine land; single-engine land; single-engine sea; instrument: airplane; instrument: helicopter; rotorcraft: glider
  • Flight time: 19,400 hours in all; 132 in this make and model
  • Medical certificate: Class 1 (with waivers/limitations)
  • Seat: left
  • Injury: fatal

Pilot-Rated Passenger

  • Certificate: student
  • Flight time: 35.9 hours in all; 0 in this make and model
  • Medical certificate: Sport Pilot
  • Seat: rgt
  • Injury: fatal

The aircraft

  • Airframe total time: 147 hours
  • Last inspection: condition inspection, February 20, 2015; 1 hours since
  • Maximum gross weight: 1,433 lb
  • Seats: 2
  • Landing gear: retractable
  • Engine: Rotax 912ULS (piston); 146 hours total
  • Fire on the ground

The flight

  • Departed from: LNA West Palm Beach FL at 5:17 pm
  • Destination: OBE Okeechobee FL
  • Flight plan: none
  • A second pilot was aboard

Weather at the time

  • Light: daylight
  • Wind: from 090° at 7 knots, gusting 14
  • Visibility: 10 statute miles
  • Sky: broken clouds at 3,700 ft; scat at 2,200 ft
  • Temperature: 79°F (26°C), dew point 68°F (20°C)
  • Altimeter: 30.22 inHg
  • Observation at 5:53 pm from BCT, 8 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.

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.