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Accidents · NTSB WPR17FA120 · Final report

Piper PA 28-180 accident near Santa Rosa Valley, California, June 4, 2017

On June 4, 2017 at about 10:29 pm local time, a 1967 Piper PA 28-180, registered N4871L, was substantially damaged in an accident during maneuvering (low-alt flying) near Santa Rosa Valley, California. It was a personal flight under general aviation rules (Part 91). 2 people were killed. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The pilot's exceedance of the airplane's critical angle of attack while intentionally maneuvering in a steep bank at low altitude, which resulted in an accelerated aerodynamic stall and subsequent loss of control.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
June 4, 2017 · about 10:29 pm local time
Place
Santa Rosa Valley, California · map
Type
Accident
Injuries
2 people were killed.
Weather
visual conditions (good weather)
Aircraft
Piper PA 28-180 180, built 1967 · all PA 28-180s on the register
Registration
N4871L · no longer on the register · serial 28-4226
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

The commercial pilot and his son were conducting a personal flight. About 15 minutes after takeoff, the airplane flew a series of passes over a horse arena where the pilot's daughter was riding. The arena was situated within a geographic bowl depression, surrounded by hilly terrain and adjacent to three sets of power transmission lines. A pilot witness in an airplane flying above the accident airplane described the accident airplane's flight path as low and erratic, and a witness close to the arena described the initial pass as "aggressive." The pilot conducted the final pass over the arena at a much lower altitude than the previous passes. Multiple witnesses described the engine noise as "sputtering" and then going quiet either during the descent for the final pass, or just as the airplane flew over the arena. The engine sound then increased as the airplane climbed and entered a steep right bank, then descended into power lines and impacted the ground about 600 ft south of the arena. Calculations based on witness reports and impact geometry indicated that the radius of the turn before impact would have required a high angle of bank, resulting in an increase in stall speed, which would have led to an accelerated stall at an altitude too low for recovery. Examination revealed no anomalies with the airframe or engine that would have precluded normal operation, and damage signatures and witness accounts indicated that the engine was producing power at the time of the accident. Damage to the airplane's fuel tanks indicated that they contained fuel at the time of impact. The pilot's son, who was not a pilot, was seated in the front left seat. Since the airplane was equipped with dual controls, it could not be determined who was flying the airplane at the time of the accident. The pilot was familiar with the terrain in the area of the accident site. Witnesses stated that he had performed low passes there multiple times in the past and was aware of the power lines at the edge of the arena. The reduction in engine noise as reported by witnesses could have been the result of an actual loss of engine power or a power reduction made by the pilot to descend more rapidly in order to perform the pass at a lower altitude; however, if the pilot had been flying at an appropriate and safe altitude and the airplane had experienced a loss of engine power, it would have been within gliding distance of open terrain adequate for a forced landing. Given the pilot's previous behavior and the circumstances of the accident flight, it is likely that the pilot was performing an intentional, ostentatious display at low altitude when the accident occurred. Toxicology testing of the pilot indicated the presence of multiple impairing medications, as well as tetrahydrocannabinol carboxylic acid, a metabolite of tetrahydrocannabinol (THC), the active compound in marijuana. However, no blood was available for toxicology testing, and there is no known relationship between tissue levels and impairment. As a result, whether the pilot's use of multiple potentially impairing substances contributed to the accident could not be determined.

The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.

The factual record from the NTSB's investigation tables, in plain English

What happened, in order

  1. Low altitude operation/event during maneuvering (low-alt flying)
  2. Abrupt maneuver during maneuvering (low-alt flying) defining event
  3. Loss of control in flight during maneuvering (low-alt flying)
  4. Aerodynamic stall/spin during maneuvering (low-alt flying)
  5. Collision with terrain or object (not controlled flight into terrain) during maneuvering (low-alt flying)

The NTSB's findings

  • cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
  • cause Personnel issues › Action/decision › Info processing/decision › Decision making/judgment › Pilot
  • cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Altitude › Incorrect use/operation
  • cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Angle of attack › Not attained/maintained
  • Personnel issues › Physical › Health/Fitness › Use of medication/drugs › Pilot

Pilot

  • Certificate: commercial pilot
  • Ratings: multi-engine land; single-engine land; single-engine sea; instrument: airplane
  • Flight time: 1,989 hours in all; 500 in this make and model
  • Medical certificate: Class 3 (with waivers/limitations)
  • Seat: rgt
  • Injury: fatal

The aircraft

  • Airframe total time: 5,939.9 hours
  • Last inspection: annual inspection, February 1, 2017; 29 hours since
  • Maximum gross weight: 2,400 lb
  • Seats: 4
  • Landing gear: fixed
  • Engine: Lycoming O-360-A4A (piston); 1,796 hours total
  • Fire on the ground

The flight

  • Departed from: CMA Camarillo CA at 10:13 pm
  • Destination: CMA Camarillo CA
  • Flight plan: none

Weather at the time

  • Light: daylight
  • Wind: from 250° at 5 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 70°F (21°C), dew point 61°F (16°C)
  • Altimeter: 29.86 inHg
  • Observation at 10:55 pm from KCMA, 11 miles away

Injuries

FatalSeriousMinorNone
Flight crew1
Passengers1

Documents from the investigation the NTSB's docket: the evidence folder behind the report

11 documents, released by the NTSB on March 5, 2019. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.

The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.

Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.