Casualties unknown

1990-04-20: Beech F33A (N179DD) — Delta Delta Partnership — Milwaukee, WI

Milwaukee, WI, US

On April 20, 1990, a Beech F33A (registration N179DD) operated by Delta Delta Partnership was involved in an aviation accident near Milwaukee, WI. Investigators recorded the probable cause as: THE UTILIZATION OF IMPROPER PROCEDURES ON THE PART OF THE PILOT IN COMMAND BY ATTEMPTING TO EXECUTE A COUPLED APPROACH OUTSIDE THE PARAMETERS OF THE AUTOPILOT. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

During a coupled ILS approach, the pilot engaged the autopilot approach mode while high and fast at a 2000 ft/min descent. Glideslope capture led to pitch excursions that exceeded the aircraft's stress limits, though the pilot landed safely.

Incident Overview

A pilot executed a coupled Instrument Landing System (ILS) approach using the autopilot approach mode. The aircraft was in an unstabilized condition at the time of engagement, being high and fast with a rate of descent of approximately 2000 feet per minute.

Approach Details

The approach parameters were outside those required for a stabilized approach. When the autopilot captured the glide slope, the aircraft responded with a series of abrupt pitch movements. The nose pitched down sharply, causing the aircraft to fly through the glide slope. Subsequently, the aircraft pitched up sharply, again flying through the glide slope, this time above it. This sequence repeated with another nose-down pitch before the pilot was able to disengage the autopilot.

Autopilot Behavior

The pitch excursions during the glide slope capture and subsequent oscillations were rapid and extreme. The autopilot's attempt to correct for the initial high and fast condition resulted in overcontrolling, leading to multiple cycles of pitch changes.

Outcome

The pilot successfully landed the aircraft without any further incident. However, the pitch oscillations experienced during the approach imposed loads on the airframe that exceeded the aircraft's designed stress limits.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X22885. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.