Amateur-built MERLIN LITE accident near Mulberry, Florida, April 2, 2024
On April 2, 2024 at about 2:38 pm local time, a 2023 amateur-built MERLIN LITE (glider), registered N622PC, was substantially damaged in an accident during initial climb near Mulberry, Florida (South Lakeland airport). It was a personal flight under general aviation rules (Part 91). 1 person was killed. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot/builder’s modifications of the motorglider’s engine, which resulted in an excessively lean fuel air mixture, preignition, piston failure, and a subsequent total loss of engine power during the initial climb. Contributing to the outcome was the pilot’s failure to maintain airspeed and his exceedance of the motorglider’s critical angle of attack following the loss of engine power, which resulted in an aerodynamic stall/spin at an altitude too low to recover.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- April 2, 2024 · about 2:38 pm local time
- Place
- Mulberry, Florida · South Lakeland · map
- Type
- Accident
- Injuries
- 1 person was killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Amateur-built MERLIN LITE, built 2023
- Registration
- N622PC · no longer on the register · serial 002
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The kit manufacturer manager reported that the accident flight was the pilot/builder’s second flight in the motorglider, the first of which was two days before the accident. A witness at the airport reported seeing the pilot taxi for takeoff and that the engine sounded “a bit rough,” but due to the nature of the small two-stroke engine he was not concerned. The witness reported that the motorglider took off and, when it reached about 100 ft to 150 ft above ground level (agl), the engine sputtered then went silent. Video footage showed that when the motorglider was about midfield, it turned right, then left, then pitched up before the left wing dropped and the motorglider began a near-vertical left rotating descent to ground impact consistent with a low-altitude stall and spin. Postaccident examination of the motorglider revealed no evidence of any preimpact mechanical malfunctions or failures of the flight controls or airframe that would have precluded normal operation. Examination of the engine revealed that the original airbox had been replaced with an unrestricted cone-type air filter. The main carburetor jet had also been replaced with a smaller jet, which would have resulted in the engine running slightly lean (the builder had reported that he thought the engine had been running too rich). Additionally, a hole was noted in the center of the engine’s single piston. A metallurgical examination of the piston revealed light gray deposits covering portions of the crown surface around the hole. The piston crown had features consistent with pre-ignition damage. This damage was likely the result of an excessively lean mixture due to the unrestricted air intake and smaller main jet. The hole in the piston would have resulted in a total loss of engine power. The distance from the accident site to the end of the available grass area was about 1,300 ft. The kit manufacturer reported that the motorglider’s typical landing roll was about 200 ft or less. Had the pilot aggressively lowered the nose of the motorglider to maintain airspeed following the loss of engine power, it is likely that he could have avoided the low altitude aerodynamic stall/spin and landed within the remaining available runway.
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
- Loss of engine power (total) during initial climb defining event
- Aerodynamic stall/spin during initial climb
- Collision with terrain or object (not controlled flight into terrain) during initial climb
The NTSB's findings
- Aircraft › Aircraft power plant › Engine (reciprocating) › Recip eng cyl section › Failure
- Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
- Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Angle of attack › Not attained/maintained
- Personnel issues › Action/decision › Info processing/decision › Decision making/judgment › Owner/builder
- Aircraft › Aircraft power plant › Power plant › Air intake › Incorrect service/maintenance
- Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Airspeed › Not attained/maintained
Pilot
- Certificate: private
- Ratings: rotorcraft: glider
- Flight time: 118.6 hours in all; 1 in this make and model; 0 in the last 90 days
- Medical certificate: None
- Seat: sngl
- Injury: fatal
The aircraft
- Maximum gross weight: 645 lb
- Seats: 1
- Landing gear: fixed
- Engine: Polini Thor 303DS (piston); 0 hours total
The flight
- Flight plan: none
- Runway 14, 2,412 ft by 100 ft
Weather at the time
- Light: daylight
- Wind: from 180° at 10 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 73°F (23°C), dew point 66°F (19°C)
- Altimeter: 30.01 inHg
- Observation at 9:50 am from LAL, 4 miles away
Weather report (METAR): KLAL 021350Z 18010KT 10SM SKC 23/19 A3001
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
15 documents, released by the NTSB on June 4, 2025. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.
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.
