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Accidents · NTSB CHI07FA183 · Final report

Piper PA-46-500TP accident near Wellsville, Missouri, June 28, 2007

On June 28, 2007 at about 1:15 pm local time, a Piper PA-46-500TP, registered N477MD, was destroyed in an accident near Wellsville, Missouri. It was a personal flight under general aviation rules (Part 91). 3 people were killed. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The pilot's failure to activate the pitot heat as per the checklist, resulting in erroneous airspeed information due to pitot tube icing, and his subsequent failure to maintain aircraft control. Contributing to the accident was the pilot's continued flight in an area of known adverse weather.

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

What the record shows

Date
June 28, 2007 · about 1:15 pm local time
Place
Wellsville, Missouri · map
Type
Accident
Injuries
3 people were killed.
Weather
visual conditions (good weather)
Aircraft
Piper PA-46-500TP · all PA-46-500TPs on the register
Registration
N477MD · registry record · serial 4697264
Damage
Destroyed
Flight
Personal flight · general aviation rules (Part 91)

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

The pilot, before departure, obtained a weather briefing that indicated there were thunderstorms and areas of heavy precipitation along the route of flight. The pilot told the briefer that the airplane was equipped with onboard radar for weather avoidance. After takeoff, the pilot received two adverse weather advisories from the departure air traffic controller. The pilot acknowledged, requested and was cleared for course deviations to avoid the weather. The pilot was subsequently told to contact an en route traffic control center. The pilot did not request an update on, nor was he advised of, any additional adverse weather after switching over. Avionics data recovered from the wreckage showed the airplane encountered decreasing outside air temperatures (OAT) during the en route climb to a cruise altitude. The OAT decreased below freezing as the airplane climbed through 15,900 feet mean sea level. The primary flight display's (PFD) airspeed data decreased from about 140 knots indicated airspeed (KIAS) to 0 KIAS. During the loss of airspeed, the airplane's recorded climb rate decreased and the airplane entered a left turn. At this point, the en route controller asked the pilot if he had been given a clearance to deviate around weather. The pilot responded, "mike delta we've got problems uh... ." There were no additional communications received from the pilot and radar contact with the airplane was lost shortly thereafter. The recovered PFD data indicated that the airplane exceeded its maximum structural operating speed during a rapid descent. In the descent, the airplane reached a ground speed of 250 knots and vertical loads reaching 5g. The recovered data and witness marks from the right wing indicated the airplane sustained an in-flight breakup after exceeding the airplane's maximum load factor limit. A review of the available weather data indicated that there was an area of extreme precipitation associated with thunderstorms east of the accident site and that the airplane was likely in instrument meteorological conditions at the time of the upset. An on-scene investigation did not reveal any pre-impact anomalies with the airplane and its related systems. Analysis of the recovered PFD and Multi-Function Display (MFD) data indicated that the pilot did not utilize the available pitot tube heat that would have afforded ice protection. Recovered PFD/MFD data, along with a weather analysis, indicated that the airplane was operating in an environment conducive for pitot tube icing. Additionally, recovered data showed airspeeds were recorded during the rapid descent at altitudes lower than the observed freezing level. The before takeoff checklist indicated, "Pitot Heat ... ON."

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: 1,000 hours in all
  • Last flight review: November 1, 2006
  • Medical certificate: Class 3 (without waivers/limitations)
  • Seat: left
  • Injury: fatal

The aircraft

  • Airframe total time: 201.7 hours
  • Last inspection: continuous airworthiness programme, June 1, 2007
  • Maximum gross weight: 5,134 lb
  • Seats: 6
  • Landing gear: retractable
  • Engine: Pratt & Whitney Canada PT6A-42A (turboprop); 0 hours total

The flight

  • Departed from: SUS St Louis MO at 12:50 pm
  • Destination: CFE Buffalo MN
  • Flight plan: IFR

Weather at the time

  • Light: daylight
  • Wind: from 210° at 3 knots
  • Visibility: 10 statute miles
  • Sky: broken clouds at 2,200 ft
  • Temperature: 70°F (21°C), dew point 68°F (20°C)
  • Altimeter: 30.07 inHg
  • Observation at 1:17 pm from COU, 30 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.