ERA22FA391 · Aeronca 7AC
Aeronca 7AC · Accident: aerodynamic stall/spin during initial climb
Event
- NTSB case
- ERA22FA391
- 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
Aeronca 7AC
- Aircraft type
- Aeronca 7
- 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
- N1478E
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From not recordedTo not recorded
- Aircraft age
- About 76 years (built 1946)
- 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
According to a friend, the pilot had not flown for 20 years, and purchased the accident airplane the day before the accident flight. The pilot’s friend witnessed and recorded video of the accident takeoff, which revealed that the airplane became airborne and entered a slow speed, nose-high climb that continued into a left turn. The airplane then pitched nose-down and began descending while the engine could be heard operating smoothly and continuously to ground contact. The airplane was found in a nose-down position in a field near the runway with significant damage to the engine and cockpit area. All primary flight control surfaces remained attached, and the empennage was bent upward and forward but remained partially attached. The wreckage examination did not reveal evidence of any preimpact mechanical malfunctions or failures that would have precluded normal operation. Toxicology testing detected diphenhydramine in the pilot’s cavity blood and urine. The concentration of diphenhydramine in cavity blood was reported qualitatively, indicating a level below the laboratory reporting threshold. Given the potential for postmortem redistribution and contamination in cavity blood, it is unlikely that the pilot’s use of diphenhydramine contributed to the accident. The takeoff described by the witness and video appeared consistent with entry into a low altitude aerodynamic stall. The distribution of the wreckage and relatively low energy signatures exhibited by the wreckage at the accident site were also consistent with an aerodynamic stall. Based on this information, it is likely that the pilot exceeded the airplane’s critical angle of attack during the initial climb, which resulted in an aerodynamic stall, loss of control, and impact with terrain.
Probable cause
The pilot's exceedance of the airplane’s critical angle of attack during takeoff, which resulted in an aerodynamic stall and loss of control.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record ERA22FA391
- Event ID
- 20220829105818
- Case number
- ERA22FA391
- 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: 71a96ccdecf51b6bdcafe0f17ff2c1fb28339d3d6a741db17bcad23ba29a964b; retrieved 2026-09-15T07:49:55.736Z.