ERA22LA186 · Henry L Berrier JR ARION LIGHTNING LS-1
Henry L Berrier JR ARION LIGHTNING LS-1 · Accident: loss of engine power (total) during initial climb
From an unrecorded airport to Raleigh County Memorial Airport (BKW)
Event
- NTSB case
- ERA22LA186
- 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
- Completed
- 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
Henry L Berrier JR ARION LIGHTNING LS-1
- Aircraft type
- Henry L Berrier JR ARION LIGHTNING LS-1
- 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
- N6688S
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From not recordedTo Raleigh County Memorial Airport (BKW), Beckley, WV
- Aircraft age
- About 10 years (built 2012)
- 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 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
- Aircraft › Aircraft systems
- Personnel issues › Action/decision
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
The amateur-built airplane was assembled from a kit about 10 years prior to the accident and had only been flown about 250 hours during those 10 years. After performing a preflight inspection and noting no anomalies, the pilot proceeded to take off from a 4,498-ft-long asphalt runway. During takeoff, the engine experienced a partial loss of power at 70 knots, about midfield. The pilot was not sure that he could land on the remaining runway and immediately turned the right fuel tank to on and the engine rpm increased significantly.
Within seconds, the engine lost total power, and the pilot elected to keep the airplane on the runway heading to clear several obstacles at the end of the runway. The pilot attempted a forced landing in a field but pulled up to clear a fence. The airplane subsequently landed hard in the field and collided with a creek bed. The pilot stated that, in retrospect, he should have rejected the takeoff during the initial partial loss of engine power.
Examination of the wreckage revealed that the diaphragm return spring on the engine side of the diaphragm was corroded. Additionally, the electric boost pump’s electrical wire was disconnected from the cockpit pump switch and the pump switch’s spade connector was loose. When the wire was reconnected, the spade connector had to be wiggled to get the pump to activate. Once activated, it pumped normally. Given this information, it is likely neither fuel pump was able to provide adequate fuel flow to the engine to sustain normal operation during the takeoff.
Probable cause
A total loss of engine power due to intermittent operation of both the engine-driven fuel pump and the electric boost pump. Contributing was the pilot’s delay in rejecting the takeoff, after the initial loss of engine power, which resulted in a collision with terrain.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record ERA22LA186
- Event ID
- 20220411104925
- Case number
- ERA22LA186
- 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, cause areas. 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: c85bcc74366355a362890768b75f94d4641bbd74336b90ab65a3a76195b34886; retrieved 2026-09-16T15:07:17.164Z.