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WPR24FA014 · Piper PA-28-140

17 Oct 2023 · Williams, AZ, United States

Piper PA-28-140 · Accident: aerodynamic stall/spin during initial climb

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Event

NTSB case
WPR24FA014
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
3 · 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

Piper PA-28-140

Aircraft type
Piper PA-28
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
N6192J
Operator
Unknown
Onboard fatalities
Unknown
Route
From not recordedTo not recorded
Aircraft age
About 47 years (built 1976)
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
  • Environmental issues › Conditions/weather/phenomena
  • Personnel issues › Task performance

Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.

NTSB narrative

Two flight instructor-certificated pilots and a passenger on a personal flight departed from an airport in high density-altitude conditions with a slight tailwind. A witness located near the airport reported observing the airplane flying at a low altitude over the trees with its wings wobbling. He stated that the airplane climbed to a maximum altitude of about 100 to 200 ft above ground level (agl) before it began a left turn toward the airport road then fell straight toward the ground. The circumstances of the accident flight, the accident site evidence, and the witness account were consistent with the airplane entering an aerodynamic stall and uncontrolled descent at low altitude. Although the witness reported that he felt certain that he heard the engine shut down about 3 to 5 seconds before impact, propeller damage and propeller strike marks on the ground were evidence of engine power at impact. Further, postaccident examination of the airframe and engine revealed no evidence of mechanical failure or malfunction that would have precluded normal operation. Regardless, based on the witness’s description of the airplane’s wings wobbling in flight, the aerodynamic stall was imminent before the reported change in engine sound, and the pilot flying did not adequately adjust the airplane’s pitch to prevent it. The left-seat pilot’s toxicology results detected isomers of tetrahydrocannabinol (THC) and their metabolites, indicating that he had used one or more cannabis products. Whether the detected delta-9-THC, delta-8-THC, and cannabidiol (CBD) came from the same product or multiple products is unknown. Delta-9-THC and delta-8-THC have potential to cause cognitive and psychomotor impairment. However, the precise timing of the left-seat pilot’s use of these substances and whether the substances were causing significant impairing effects at the time of the accident cannot be determined from the measured levels of the substances and their metabolites. The measured levels of psychoactive substances were relatively low, but this does not exclude associated impairment. The right-seat pilot’s toxicology results indicated that he had used several medications commonly used to treat cold or allergy symptoms. The likelihood of these medications causing significant impairment was low. However, the presence of these medications might indicate a potentially distracting or otherwise impairing condition such as an acute upper respiratory infection or symptomatic seasonal allergies. Whether the right-seat pilot was experiencing such effects from an underlying condition at the time of the accident could not be determined from the available medical evidence. The airplane was equipped with dual flight controls, and both pilots were qualified to fly the airplane. However, based on the available video evidence from previous flights, during which the left-seat pilot was flying the airplane and the right-seat pilot provided comments and suggestions without intervening on the controls, the left-seat pilot was likely flying the airplane during the accident flight. Video evidence from previous flights indicated that the left-seat pilot had allowed the airplane’s airspeed to decay to the point of stall warning horn activation on three occasions during two previous takeoffs without the passenger on board.

Probable cause

The pilot’s failure to maintain sufficient airspeed and exceedance of the airplane’s critical angle of attack during initial climb after takeoff, resulting in an aerodynamic stall. Contributing was the pilot’s inadequate preflight airplane performance planning for the high density-altitude.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record WPR24FA014
Event ID
20231017193255
Case number
WPR24FA014
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: f76bad74d3a7852d630e7c5682ab0fefda2c96bdbc02f7b89c3498b6ef1c61cf; retrieved 2026-09-15T08:07:06.478Z.