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Accidents · NTSB ERA25LA327 · Preliminary: the investigation is not finished

Amateur-built ZENAIR ZODIAC 601HDS accident near Connerton, Florida, September 1, 2025

On September 1, 2025 at about 8:05 pm local time, a 2004 amateur-built ZENAIR ZODIAC 601HDS, registered N680LM, was substantially damaged in an accident during enroute near Connerton, Florida (Pilot Country airport). It was a personal flight under general aviation rules (Part 91). 2 people had minor injuries. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The NTSB has not yet published a probable cause for this accident. Investigations usually take one to two years; this page updates when the final report is released.

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

What the record shows

Date
September 1, 2025 · about 8:05 pm local time
Place
Connerton, Florida · Pilot Country · map
Type
Accident
Injuries
2 people had minor injuries.
Weather
visual conditions (good weather)
Aircraft
Amateur-built ZENAIR ZODIAC 601HDS, built 2004
Registration
N680LM · registry record · serial 6-3635
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

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

On September 01, 2025 about 1605 eastern standard time, an experimental amateur-built Zenith Zodiac 601 HDS, N680LM, was substantially damaged when it was involved in an accident near Connerton, Florida. The pilot and the passenger received minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The pilot reported that he planned to provide rides to four relatives, each on a separate 15-minute flight with a departure from and return to Pilot Country Airport (X05), Brooksville, Florida. In preparation for these flights, the pilot purchased 3 gallons of 89 octane automotive fuel. After he added the fuel, he estimated the airplane's total fuel to be 9.8 gallons prior to the first flight. Before the passengers arrived, the pilot performed a preflight inspection of the airplane and did not notice any abnormalities. On the first two flights, the pilot noted normal engine performance, including normal temperature and pressure readings. The first flight’s duration was 16 minutes, while the second was 12 minutes. The pilot estimated that the total fuel onboard for the accident flight was 6 to 7 gallons. The pilot stated that the airplane’s cruise fuel consumption was 3.8 to 4.0 gallons per hour (gph), and that the 4 gallons of fuel was sufficient for the upcoming 15-minute flight. The pilot departed on the third flight at 1601. He did not notice anything abnormal during the ground roll or with the initial climb rate. About 420 ft above ground level (agl), the pilot reported “the engine suddenly stopped without any warning.” He further explained there were “no abnormal noises, vibrations or power deviations” prior to the loss of engine power. He then adjusted the airplane’s pitch attitude for best glide speed, turned into the wind and prepared for an off-field landing. The pilot attempted to restart the engine twice but was unsuccessful, though he did note that the starter was functioning during these attempts. He then performed a forced landing in a nearby field. During the landing sequence, the airplane nosed over and came to rest inverted. The pilot was able to self-extricate, then helped his passenger through the airplane’s shattered canopy. A Federal Aviation Administration Inspector examined the wreckage at the scene of the accident and observed substantial damage to both wings, the fuselage and rudder of the airplane. Fuel was found in both wing tanks and the fuselage-mounted tank. The header tank was not examined. The wreckage was recovered and retained for further examination.

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 engine power (total) during enroute defining event

The aircraft

  • Airframe total time: 261.9 hours
  • Last inspection: condition inspection, November 1, 2024; 62 hours since
  • Maximum gross weight: 1,300 lb
  • Seats: 2
  • Landing gear: fixed

The flight

  • Departed from: X05 Brooksville, Fl FL at 8:01 pm
  • Flight plan: none
  • Runway 36, 3,700 ft by 75 ft

Weather at the time

  • Light: daylight
  • Wind: from 040° at 13 knots, gusting 23
  • Visibility: 10 statute miles
  • Sky: a few clouds at 5,000 ft
  • Temperature: 88°F (31°C), dew point 73°F (23°C)
  • Altimeter: 29.91 inHg
  • Observation at 3:53 pm from KBKV, 8 miles away

Weather report (METAR): METAR KBKV 011953Z 04013G23KT 10SM FEW050 31/23 A2991 RMK AO2 PK WND 05027/1920 SLP128 T03110228=

Injuries

FatalSeriousMinorNone
Flight crew1
Passengers1

Documents from the investigation the NTSB's docket: the evidence folder behind the report

The NTSB has not released the docket for this case yet. The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), is usually released when the investigation is nearly complete, and the list here is refreshed when it appears. Check 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.