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WPR21FA210 · Mark Coby EARLY BIRD JENNY

27 May 2021 · Stoneville, NC, United States

Mark Coby EARLY BIRD JENNY · Accident: aerodynamic stall/spin during initial climb

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Event

NTSB case
WPR21FA210
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
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

Mark Coby EARLY BIRD JENNY

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
N831HC
Operator
Unknown
Onboard fatalities
Unknown
Route
From not recordedTo not recorded
Aircraft age
About 4 years (built 2017)
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
Destroyed

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, who was the co-owner/co-builder of the experimental amateur-built airplane, was departing on a local flight. The other co-owner/co-builder of the airplane witnessed the accident takeoff and stated that the airplane’s pitch attitude was “a little steep” and that the airplane looked slow as it approached 150 ft above ground level in the climb. Both the co-owner and another witness stated that the airplane’s wings were rocking before one wing dropped and the airplane entered a nose-down descent. The airplane impacted terrain about halfway down the 5,200-ft-long runway, and a postimpact fire ensued. Postaccident examination of the airframe and engine revealed no evidence of mechanical malfunctions or anomalies that would have precluded normal operation. Review of the pilot’s logbook indicated that the accident flight was his third flight in the accident airplane and that he had recorded a total of 0.8 hours of flight experience. The co-owner stated that he and the accident pilot took turns flying the airplane and that the day of the accident was the warmest day on which they had flown the airplane. The co-owner had flown the airplane earlier on the day of the accident and stated that, although the airplane’s takeoff profile was “flatter than usual,” the airplane otherwise performed well and handled as expected. The co-owner also stated that neither he nor the accident pilot had conducted any aerodynamic stalls in the airplane, which was not equipped with a stall warning system. The extent to which the accident pilot had explored the airplane’s low-speed handling characteristics during flight could not be determined based on the available evidence for this accident. Review of the atmospheric conditions about the time of the accident indicated a density altitude of about 2,400 ft. Weight and balance documents for the airplane were not located, and the airplane’s weight and balance condition at the time of the accident was not determined. Autopsy and toxicology results for the pilot revealed evidence of an enlarged heart, anthracosis of the lungs, a carboxyhemoglobin saturation between 11% and 13%, and medications to treat high blood pressure. Minimal soot deposits were found in the trachea. Given the available evidence for this accident investigation, it is unlikely that the pilot’s cardiac condition was a factor in this accident. His carboxyhemoglobin saturation was not likely associated with impairment and was most likely the result of postcrash exposure to carbon monoxide. The circumstances of the accident are consistent with the pilot’s exceedance of the airplane’s critical angle of attack during takeoff, which resulted in an aerodynamic stall and a loss of control. It is likely that the density altitude conditions at the time of the accident degraded the airplane’s takeoff performance and that the pilot’s unfamiliarity with the airplane’s handling characteristics (especially in higher-density-altitude conditions) and with low speed/aerodynamic stalls contributed to his failure to recognize and correct the airplane’s angle of attack before the stall occurred.

Probable cause

The pilot’s exceedance of the airplane’s critical angle of attack during the takeoff initial climb, which resulted in an aerodynamic stall and a loss of control.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record WPR21FA210
Event ID
20210528103160
Case number
WPR21FA210
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: 7a6d42a426e005cfd7f1c5ca1aeded76170cd564290b2455156ce00c17a120e2; retrieved 2026-09-15T07:29:03.068Z.