ERA25LA265 · Moyes Liteflite PTY Ltd C DRAGONFLY
Kitty Hawk Flight School Moyes Liteflite PTY Ltd C DRAGONFLY · Accident: loss of engine power (total) en route
From Charleston, NH (private airstrip) to an unrecorded destination
Event
- NTSB case
- ERA25LA265
- Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
- Accident
- InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
- Ongoing
- API-reported fatalities
- 0 · all aircraft and ground
- Ground fatalities
- 0
- OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
- General aviation
- WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
- Visual Meteorological Cond
Moyes Liteflite PTY Ltd C DRAGONFLY
- Aircraft type
- Moyes Liteflite C DRAGONFLY
- Category
- Airplane
- RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
- N4010E
- Operator
- Kitty Hawk Flight School
- Onboard fatalities
- Unknown
- Route
- From Charleston, NH (private airstrip)To not recorded
- Aircraft age
- About 20 years (built 2005)
- Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
- Part 91: General Aviation
- Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
- En route · descent
- Defining eventThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
- Loss of engine power (total)
- DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
- Substantial
Cause areas
No findings designated as a cause are recorded in the NTSB data yet.
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
On July 13, 2025, about 1915 eastern daylight time, a Moyes Liteflite Model C Dragonfly airplane, N4010E, was substantially damaged when it was involved in an accident near Charleston, New Hampshire. The pilot was seriously injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 glider tow flight. The pilot reported that the accident flight was his fifth tow flight of the day. There were no anomalies noted during preflight inspection or before the takeoff engine runup checks. The airplane departed with about 4-gallons of fuel onboard. After reaching an altitude of 3,500 ft, the glider released and the pilot reduced engine power to idle and entered a routine spiraling descent to land. During the descent, the airplane experienced a total loss of engine power which the pilot did not observe until he advanced the throttle, and the engine did not respond. A witness at the departure airport recorded a video of the airplane as it descended. The video showed the airplane in a left turning descent before it entered a shallow right spiraling descent. The airplane remained in the right turn until it impacted the ground. The airplane came to rest in an upright position in a grass field about one-half mile from the departure airport. Postaccident examination of the airplane by an Federal Aviation Administration inspector revealed that the tubular structure of the fuselage exhibited deformation and fractures from impact forces. Flight control continuity was established from the cockpit to all of the flight control surfaces. The engine remained attached to the fuselage and the throttle control cables remained attached and were continuous to the throttle control lever. The fuel tank contained about 2-gallons of fuel and the fuel filter was free of contamination. The airplane was retained for further examination.
Verbatim NTSB factual narrative from the NTSB dataset
Sources
NTSB record ERA25LA265
- Event ID
- 20250714200524
- Case number
- ERA25LA265
- Dataset
- full-current
- Source SHA-256
- 5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
Source notes (4)
- Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
- Filled from the NTSB case API where the bulk record had no value: investigation status. Values present in the bulk record are kept.
- The date is the local date, which is the same as the UTC date the NTSB stores.
- API snapshot SHA-256: e2fd29dddab6352dbf40dd50e9e4d1a8ecfff1865da69fbadd1f82fa74d295cd; retrieved 2026-09-16T20:04:52.393Z.