Casualties unknown

1995-12-08: Boeing 727-232 (N543DA) — Boise, ID

Boise, ID, US

On December 8, 1995, a Boeing 727-232 (registration N543DA) was involved in an aviation accident near Boise, ID. Investigators recorded the probable cause as: the pilot-in-command's misjudgment of the remedial action necessary to correct the aircraft's misalignment with the runway. The dark night conditions, fog, and the pilot-in-command's failure to maintain proper alignment with the runway were factors. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards
Boeing 727-232
Photo: Pete Macklin / CC BY-SA 2.0, via Wikimedia Commons

During a coupled Category I ILS approach in fog and dark night, the aircraft's left outboard slats and flap contacted the runway after the captain continued below minimums and the heading drifted right.

Approach and Descent

The flight was conducting a coupled Category I ILS approach under fog and dark night conditions. After passing the final approach fix, the crew was notified that the runway visibility range (RVR) was below minimums. The captain continued the approach to decision height (DH) in accordance with company operations specifications. He visually acquired the runway prior to DH and continued toward landing.

Autopilot Disengagement and Heading Drift

About 60 feet above the runway, the captain disengaged the autopilot. The flight data recorder (FDR) indicated that the aircraft heading then began to drift right. The cockpit crewmembers stated that upon noticing the drift, the captain countered it with aileron and rudder inputs.

Roll Angle and Ground Contact

The FDR indicated a roll angle of -7.50 degrees at the instant maximum vertical G and minimum altitude readings were recorded, increasing to -14.90 degrees one second later. After the flight, damage was observed to the left outboard slats and flap. A Boeing chart indicated that at a pitch angle of 3.9 degrees and landing sink rate of 10 feet per second, the outboard slat and flap will contact the ground at a roll angle between 7.45 and 8.7 degrees.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001207X05080. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.