Casualties unknown

1995-02-15: Piper PA-46-310P (N9YP) — Chippewa Falls, WI

Chippewa Falls, WI, US

On February 15, 1995, a Piper PA-46-310P (registration N9YP) was involved in an aviation accident near Chippewa Falls, WI. Investigators recorded the probable cause as: The pilot's improper decision to depart into known adverse weather conditions, and the subsequent encounter with freezing drizzle, resulting in an inadvertent stall and collision with the terrain during an approach to land. 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

A single-engine airplane exceeded maximum gross weight and aft CG limits at takeoff and landing. During an icing-related diversion, it struck the ground during approach, with air induction lever and anti-ice switches not set per procedures.

Flight Details

The single-engine airplane departed with two pilots, two passengers, baggage, and equipment. At takeoff, the airplane was 955 pounds over the maximum allowable gross weight and 2 inches beyond the aft center of gravity (CG) limit.

Diversion and Icing Conditions

After approximately four hours of flying, the pilot elected to divert to another airport due to icing conditions. The airplane had been flying in light freezing rain, which the Pilot's Operating Handbook (POH) stated should be avoided. Severe mixed icing was reported 25 miles northwest of the airport.

Accident Sequence

During the descending left turn from base leg to final approach for Runway 22, the airplane dropped, struck the ground, and slid 250 feet. The wings separated from the airplane during the ground slide after contacting two trees.

Aircraft Configuration and Performance

At the time of the accident, the airplane was calculated to be approximately 600 pounds over the maximum landing weight, and 2 inches beyond the aft CG limit. The air induction lever was found in the primary position, not the required alternate position for icing conditions. Additionally, the propeller and stall warning heat switches were off.

Post-Accident Examination

A satisfactory postaccident engine run was completed. Winds at the airport were from 150 degrees at 10 knots, gusting to 16 knots.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001207X03022. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.