CEN25FA296 · Helms Richard LANCAIR IVP
Helms Richard LANCAIR IVP · Accident: loss of control in flight during initial climb
From an unrecorded airport to Quakertown Airport (UKT)
Event
- NTSB case
- CEN25FA296
- 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
- 1 · all aircraft and ground
- Ground fatalities
- Unknown
- 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
Helms Richard LANCAIR IVP
- Aircraft type
- Helms Richard LANCAIR IVP
- 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
- N49BX
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From not recordedTo Quakertown Airport (UKT), Quakertown, PA
- 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
- Initial climb
- 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 control in flight
- DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
- Destroyed
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 30, 2025, at 1046 eastern daylight time, a Lancair IVP airplane, N49BX, was destroyed when it was involved in an accident near Greenwood, Indiana. The pilot was fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. ADS-B data was not available from the FAA as FAA ADS-B data relies on data received by official FAA receivers, and no data was found for the accident flight. However, preliminary ADS-B data from a commercial service that utilizes private receiver data was obtained which depicted the accident flight. The airplane was also equipped with a Garmin G900X avionics suite which had data recording capability that captured the accident flight. The data recorded by the Garmin system ended about 13 seconds before the ADS-B data. The Garmin and ADS-B data showed that the airplane departed from runway 19 at the Indy South Greenwood Airport (HFY), Greenwood, Indiana, at 1045. After takeoff, the airplane began a climbing left turn. The turn continued for about 30 seconds when the turn radius decreased while continuing to the left. The data then showed a rapid descent to the right. The total duration of the flight from the beginning of the takeoff roll was about 1 minute 30 seconds.
Figure 1. A 3-dimensional depiction of recorded data. The red/gray path depicts data from a commercial ADS-B source. The yellow/green path depicts recorded data from the Garmin avionics. The Garmin avionics also recorded engine parameters. The final portion of the data showed that the engine was at 38 inches of manifold pressure, 2,650 rpm, and a fuel flow of about 44.5 gallons per hour. All engine readings were steady from power application during the takeoff until the end of the recorded data.
Verbatim NTSB factual narrative from the NTSB dataset
Sources
NTSB record CEN25FA296
- Event ID
- 20250730200665
- Case number
- CEN25FA296
- 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: 8282f385e16b1cc0a6e8a7959649427a6b5c3f3899628a900c44604247112bdc; retrieved 2026-09-15T09:07:25.471Z.