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Accidents · NTSB NYC00FA248 · Final report

Piper PA-32R-301 accident near South Kingstown, Rhode Island, September 3, 2000

On September 3, 2000 at about 5:46 pm local time, a Piper PA-32R-301, registered N8230G, was destroyed in an accident near South Kingstown, Rhode Island. It was a personal flight under general aviation rules (Part 91). 3 people were killed. The weather was instrument conditions (cloud, fog or low visibility).

The NTSB's probable cause their words, unchanged

The pilot's loss of control, and his subsequent overstress of the airplane after a vacuum system failure during flight in instrument meteorological conditions. Factors included the instrument meteorological conditions, a sheared coupling on the vacuum pump, the pilot/owner's failure to ensure the coupling was changed per the manufacturer's recommendations, a lack of regulatory requirement to ensure compliance with the manufacturer's recommendations, and a lack of regulatory requirement to ensure installation of a suitable backup system.

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

What the record shows

Date
September 3, 2000 · about 5:46 pm local time
Place
South Kingstown, Rhode Island · map
Type
Accident
Injuries
3 people were killed.
Weather
instrument conditions (cloud, fog or low visibility)
Aircraft
Piper PA-32R-301 · all PA-32R-301s on the register
Registration
N8230G · no longer on the register · serial 32R-8013102
Damage
Destroyed
Flight
Personal flight · general aviation rules (Part 91)

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

The airplane was headed southwest, level at 8,000 feet, either in, or above instrument meteorological conditions. The pilot was instructed to change radio frequency, and after he checked in with the next sector controller, no further transmissions were heard from him. The airplane descended to 7,400 feet, then climbed to 8,500 feet over a period of 4 minutes. It remained at 8,500 feet for about a minute, then descended to and maintained between 8,100 and 8,200 feet for another minute. The airplane then made a descending turn to the right, with rates of descent up to approximately 16,000 feet per minute. The wreckage path was 1,900 feet in length, and began with parts from the airplane's tail section. About 500 feet from the beginning, was a section of the right wing, and 400 feet beyond that, the entire left wing. The stabilator spar and left wing separations exhibited downwards bending. The airplane was equipped with a vacuum-driven attitude indicator (AI) and directional gyro (DG). It also had a standby vacuum system, which required a reduction of power to properly operate. One low-vacuum annunciator light exhibited filament characteristics consistent with its being lit at the time of the accident. The other light was a diode-type, and could only be/was tested as operational. Post-accident examination found that the vacuum pump flex coupling was sheared, and the vacuum-driven instruments did not exhibit any rotational scoring. The vacuum pump coupling was manufactured in 1979. The manufacturer recommended changing the coupling every 6 years. There was no regulatory requirement to change the coupling, nor was there any regulatory requirement for redundant systems in case of vacuum system failure.

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

Pilot

  • Certificate: private
  • Ratings: single-engine land; instrument: airplane
  • Flight time: 1,291 hours in all
  • Last flight review: April 17, 2000
  • Medical certificate: Class 2 (expired)
  • Seat: left
  • Injury: fatal

The aircraft

  • Airframe total time: 1,458 hours
  • Last inspection: annual inspection, December 7, 1999
  • Maximum gross weight: 3,600 lb
  • Seats: 7
  • Landing gear: retractable
  • Engine: Lycoming IO-540 (piston); 0 hours total

The flight

  • Departed from: CQX Chatham MA at 5:05 pm
  • Destination: PNE Philadelphia PA
  • Flight plan: IFR
  • A second pilot was aboard

Weather at the time

  • Light: daylight
  • Visibility: 2 statute miles
  • Sky: overcast at 500 ft; not recorded
  • Temperature: 73°F (23°C), dew point 0°F (-18°C)
  • Altimeter: 29.95 inHg
  • Observation at 5:45 pm from OQU, 10 miles away

Injuries

FatalSeriousMinorNone
Crew1
Passengers2

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

The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.

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.