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CEN22FA232 · Cessna 182G

6 Jun 2022 · Kenedy, TX, United States

Cessna 182G · Accident: loss of control in flight on approach

From New Braunfels National Airport (BAZ) to Kenedy Regional Airport (2R9)

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Event

NTSB case
CEN22FA232
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
2 · 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

Cessna 182G

Aircraft type
Cessna 182
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
N2118R
Operator
Unknown
Onboard fatalities
Unknown
Route
From New Braunfels National Airport (BAZ), New Braunfels, TXTo Kenedy Regional Airport (2R9), Kenedy, TX
Aircraft age
About 58 years (built 1964)
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
Approach · VFR pattern final
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

  • Not determined › Not determined

Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.

NTSB narrative

The initial portion of the personal flight was conducted in day visual conditions and appeared to proceed uneventfully. Automatic dependent surveillance – broadcast (ADS-B) data revealed that the pilot initiated an enroute descent beginning about 23 miles from the airport. About 10 miles from the airport, the flight became established on an extended final to the runway. About 3 seconds before the final ADS-B data point, the flight track depicted the airplane entering a left turn that gradually increased to 30° bank angle at the end of the available data. A pilot approaching the airport noted that, when he initially observed the accident airplane, it appeared to be straight-and-level and established on an extended final approach. However, when he saw the airplane a short time later, it appeared to be about 30 feet above ground level and descending in a spin. Surveillance video footage depicted the airplane in a steep nose-down, left-wing low attitude immediately before impact, consistent with an in-flight loss of control. The accident site was located about 0.12 miles from the final ADS-B data point.

A postaccident examination provided no evidence of an in-flight structural failure, an anomaly with the primary flight control system, or a loss of engine power. The examination of the wing flap system was unremarkable with exception of the left flap extension cable. Specifically, at the time of the postaccident examination, the swaged cable end of the left flap extension cable was separated with the cable disengaged from the drive pulley. The separated cable end could not be located, which prevented further examination. Although an impression from the flap extension cable along the radius and a witness mark from the cable end washer were observed on the drive pulley, the investigation was not able to determine if those features were formed during normal operation or during the accident sequence.

The pilot's autopsy identified focally severe coronary artery disease, which conveyed an increased risk of a sudden impairing or incapacitating cardiac event such as abnormal heartbeat, heart attack, or chest pain. There was no autopsy evidence that such an event occurred, although such an event does not reliably leave autopsy evidence if it occurs just before death. Despite the risk it conveys, coronary artery disease often does not produce significant symptoms. The circumstances of the accident neither exclude nor clearly indicate a sudden medical event. Thus, whether the pilot's coronary artery disease contributed to the accident cannot be determined.

The pilot had a history of mild depression and anxiety that had been waivered by the Federal Aviation Administration (FAA). Documentation in her FAA records, as of about 5 months before the crash date, indicated that her depression and anxiety were well controlled on a sertraline regimen that had been stable since February 2020, without adverse side effects or neurocognitive deficits. Her postmortem toxicology results were consistent with continued use of sertraline. It is unlikely that the pilot's history of mild anxiety and depression or her use of sertraline contributed to the crash.

Based on the available information, the airplane was under control and above aerodynamic stall airspeed until the end of the available ADS-B data. Whether or not the left wing flap extension cable end separated in-flight or during the impact sequence could not be determined because the cable end was not found. An in-flight separation of the left flap extension cable end would have resulted in a partial retraction of the left flap due to normal aerodynamic forces. The resulting aerodynamic asymmetry caused by a partially retracted left flap and a fully extended right flap would have induced a rolling tendency and could explain the gradual left turn as observed in the ADS-B data; this rolling tendency would have required prompt attention from the pilot to maintain control of the airplane. Ultimately, the cause of the loss of airplane control could not be determined with the available information.

Probable cause

A loss of airplane control on final approach for reasons that could not be determined.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record CEN22FA232
Event ID
20220606105199
Case number
CEN22FA232
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, coordinates, 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: 1a78d4eb2c304e5fb1fe234fa8fa320f5fc3b7209296a23caee2bc47bdd0753d; retrieved 2026-09-15T07:45:41.880Z.