WPR16FA157 · Arion Aircraft LLC LIGHTNING LS-1
Arion Aircraft LLC LIGHTNING LS-1 · Accident: aerodynamic stall/spin during initial climb
From Santa Monica Municipal Airport (SMO) to Van Nuys Airport (VNY)
Event
- NTSB case
- WPR16FA157
- 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
- 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
Arion Aircraft LLC LIGHTNING LS-1
- Aircraft type
- 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
- N341AL
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Santa Monica Municipal Airport (SMO), Santa Monica, CATo Van Nuys Airport (VNY), Van Nuys, CA
- Aircraft age
- About 2 years (built 2014)
- 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
- Aerodynamic stall/spin
- 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 oper/perf/capability
- Personnel issues › Task performance
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
The pilot of the light sport airplane contacted the tower controller at his destination airport, where he planned to complete several touch-and-go maneuvers. The airplane touched down hard on the runway, and during the subsequent takeoff, the pilot reported to the controller that he heard a "banging" sound. The controller observed the left main landing gear "dangling" from the airplane. The pilot advised the controller that he planned to return to the airport for landing; however, as the airplane reached the airport boundary, it began a left turn that gradually progressed into a 70° bank angle. The airplane's bank angle increased further before the airplane entered a nose-down attitude and impacted a building, consistent with an aerodynamic stall.
A normal standard-rate turn would have allowed the pilot to rejoin the downwind leg of the traffic pattern and provided additional time to configure the airplane for a normal landing. However, the aggressive bank angle increased the airplane's stall speed and likely contributed to the pilot's exceedance of the airplane's critical angle of attack.
Examinations of the airframe and engine did not reveal any mechanical malfunctions or anomalies that would have precluded normal operation, although the engine ran about 200 rpm below its maximum power output during the engine run. Although the source of this power loss could not be confirmed, it may have been the result of a reduction in fuel flow from a torn carburetor diaphragm and bent float. Data obtained from the airplane's engine monitor revealed that the engine achieved rated power throughout the accident flight, which suggested that the damage observed to the carburetor was the result of impact. A witness reported hearing the engine sputtering seconds before the airplane impacted the ground, and recorded engine data showed a corresponding decrease to idle power. It could not be determined why the pilot may have retarded the throttle to idle power.
The pilot allowed his Federal Aviation Administration (FAA) medical certificate to expire about 2 years before the accident, a few months after he sustained traumatic injuries, including a traumatic brain injury, in a car accident. Although his personal medical records did not show any permanent neurocognitive or physiological defects, formal testing was not documented. However, acquaintances and flight instructors who flew with the pilot stated that his ability to control the airplane and his decision-making capacity were affected by his injuries. The pilot continued to fly and was involved in three incidents that resulted in damage to the accident airplane; evidence suggested the pilot's physiological condition remained unchanged until the day of the accident. Thus, it is likely that the pilot's injuries impaired his ability to safely operate the airplane and directly contributed to the accident. Furthermore, the pilot ignored recommendations from other pilots to stop flying and continued to operate the airplane with a known physiological impairment.
Probable cause
The pilot's loss of airplane control due to an exceedance of the airplane's critical angle of attack, which resulted in an accelerated stall and subsequent impact with a building. Contributing to the accident was the pilot's unreported physiological impairment from traumatic brain injury, which impaired his ability to safety operate the airplane.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record WPR16FA157
- Event ID
- 20160802X92043
- Case number
- WPR16FA157
- 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: e684ef6643dc0466aa0fbfbb27bd7991b339ee82b4a0cdc86f6197fd53f34e94; retrieved 2026-09-14T21:57:49.116Z.