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Accidents · NTSB DCA09IA064 · Final report

Airbus A330-323 incident near Kagoshima, Jp, June 23, 2009

On June 23, 2009 at about 3:03 am local time, a Airbus A330-323, registered N805NW, was involved in an incident during enroute (cruise) near Kagoshima (Kagoshima airport). It was flown under non-U.S. commercial rules. No one was hurt; 217 people were on board or involved. The weather was instrument conditions (cloud, fog or low visibility).

The NTSB's probable cause their words, unchanged

Brief and temporary blockage of the pitot probes in cruise flight, most likely due to ice crystals aloft, leading to erroneous airspeed indications and airplane automation degradation as designed. Contributing to the incidents were design features of the Thales AA probes which left them more susceptible to high altitude ice crystal icing than other approved pitot probe designs.

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

What the record shows

Date
June 23, 2009 · about 3:03 am local time
Place
Kagoshima, Japan · Kagoshima
Type
Incident
Injuries
No one was hurt; 217 people were on board or involved.
Weather
instrument conditions (cloud, fog or low visibility)
Aircraft
Airbus A330-323 · all A330-323s on the register
Registration
N805NW · registry record · serial 0552
Damage
Not recorded
Flight
Flight · non-U.S. commercial rules

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

Both aircraft were in normal cruise flight at high altitude, in the vicinity of convective weather conditions, and both flight crews were aware of the weather. Crew statements and recorded data for both flights did not indicate any airplane anomalies prior to the events. Shortly before the unreliable airspeed events, each airplane encountered a visible effect of the weather conditions, the Northwest crew reported seeing moderate rain and hail, and the TAM crew reported an abrupt temperature change and St. Elmo’s Fire. Within seconds both airplane’s autopilot and autothrust disconnected, master warnings and cautions were indicated, primary airspeed display was lost or fluctuated, and the airplanes transitioned into Alternate Flight Law. According to Airbus documentation and analysis, if an airspeed discrepancy of more than 20kts or an altitude discrepancy of more than 400ft is detected between one ADR and the two others, the subject ADR is rejected. Then if a discrepancy occurs between the two remaining ADR, all auto flight functions are lost and autopilot, flight director, and autothrust disconnect. Applicable procedures for both airplanes call for autopilot and autothrust to be OFF, and for the pilot to pitch to 5 degrees and set thrust levers to the CLB detent. Both flight crews turned the airplanes to exit the weather area and the airspeed indications returned to normal within a short time. The behavior of the airplane systems is consistent with, and supports a brief and temporary blockage of two or more pitot probes likely by an accretion of ice crystals aloft. Existing airplane flight manual/QRH procedures were sufficient to prevent a dangerous situation from occuring, however the airplane would, as designed, be operating in a lower level of automation. The autopilot disengaged automatically as intended due to its airspeed monitoring function. The flight crew’s attempt to reengage the autopilot during the unreliable airspeed event, and erroneous altitude reading, followed by pilot side stick inputs, exacerbated the altitude excursion experienced by the TAM flight, however the airplane was not actually in danger of a stall.

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. Flight instrument malf/fail during enroute (cruise) defining event

The NTSB's findings

  • cause Aircraft › Aircraft systems › Ice/rain protection system › Pitot/static anti › ice › Capability exceeded

The aircraft

  • Landing gear: retractable
  • Engine 1: P&W PW4000 SER (turbofan); 0 hours total
  • Engine 2: P&W PW4000 SER (turbofan); 0 hours total
  • Operator: Northwest Airlines INC

The flight

  • Departed from: Hong Kong
  • Destination: Tokyo
  • Flight plan: IFR
  • A second pilot was aboard

Weather at the time

  • Light: daylight
  • Temperature: 0°F (-18°C), dew point 0°F (-18°C)

Injuries

FatalSeriousMinorNone
Cabi7
Flight crew2
Passengers208

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.