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CHI06CA044

2005-12-13 · Medina, Ohio, United States · None · 1 aircraft · Status: Completed

Airport 1G5

Current FAA registration · N290DM

Make / Model
LANCAIR LANCAIR
Year of manufacture
0000
Engine
LYCOMING 0-290 SERIES (140 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19951031
ADS-B equipped
Yes — Mode-S A2F5D1

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's failure to maintain directional control during landing due to an icy runway. Factors to the accident were the ice/snow contaminated runway surface, snow bank, and the pilot's lack of familiarity with the accident airplane.

Factual narrative

During landing roll the airplane impacted a snow bank situated alongside the runway and subsequently nosed over. The pilot reported that the runway was contaminated with snow and ice patches. The pilot stated that after touchdown the airplane "immediately began drifting toward the left side of the runway." The pilot reported that he attempted to correct for the drift using right rudder but "lost directional control" and departed off the left side of the runway. The pilot reported that he had 11 hours of flight experience in the airplane and the "runway conditions were much more than I was capable of handling with this aircraft." The accident airplane was equipped with a free-castering nose landing gear and directional control is maintained by differential braking when the rudder becomes ineffective at lower speeds. During the landing roll the airplane impacted a snow bank situated alongside the runway and subsequently nosed over. The pilot reported that the runway was contaminated with snow and ice patches. The pilot stated that after touchdown the airplane "immediately began drifting toward the left side of the runway." The pilot reported that he attempted to correct for the drift using right rudder but "lost directional control" and departed off the left side of the runway. The pilot reported that he had 11 hours of flight experience in the airplane and the "runway conditions were much more than I was capable of handling with this aircraft." The accident airplane was equipped with a free-castering nose landing gear and directional control is maintained by differential braking when the rudder becomes ineffective at lower speeds. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_2005_CHI06CA044.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.