Casualties unknown

2000-05-02: Cessna 172M (N13145) — Cornell Aero Works — Cornell, WI

Cornell, WI, US

On May 2, 2000, a Cessna 172M (registration N13145) operated by Cornell Aero Works was involved in an aviation accident near Cornell, WI. Investigators recorded the probable cause as: the pilot not maintaining aircraft control and the stall/spin he encountered. A factor was the extended flaps. 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

An airplane was destroyed after impacting terrain and catching fire during climbout. The pilot and two passengers sustained fatal injuries. Witnesses reported the flaps remained extended and the airplane struggled to gain altitude.

Accident Overview

The airplane was destroyed by impact with terrain and subsequent fire following a loss of control during climbout. The pilot and two passengers sustained fatal injuries.

Witness Observations

A witness reported observing the airplane taxi and take off with flaps extended, describing it as appearing to be a short field takeoff. The airplane did not seem to gain normal altitude and maintained a climb attitude that was not steep, with flaps remaining deployed. The witness estimated the airplane traveled about 1 mile before making a left turn. During the downwind leg, the airplane still appeared to not gain altitude and was approximately 1½ tree lengths above the trees. The witness's line of vision was then obscured by a tree, and they heard the crash. The witness could not remember if the engine was running at impact and stated that during initial climb, the airplane operator called over Unicom for the pilot to raise the flaps, but no response was received, and the flaps apparently never went up.

Another witness stated that the airplane crashed and looked as if it stalled, then pitched nose down and left. The airplane sounded at full power until the sound of the crash.

On-Scene Findings

The airplane was found impacting terrain at approximately 80 degrees pitch down. An on-scene investigation revealed flight control continuity and engine continuity. The engine exhibited thumb compression at all cylinders. The flap jackscrew was recovered and exhibited 5.9 inches of thread extension, corresponding to 40 degrees of flap extension.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X20948. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.