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CHI08CA048

2007-12-11 · Elyria, Ohio, United States · None · 1 aircraft · Status: Completed

Airport LPR

Aircraft involved

Probable cause & findings

The pilot's momentary loss of control after takeoff, which resulted in an in-flight collision with a tree. A contributing factor was the presence of the tree.

Factual narrative

The pilot reported that he departed on an instrument flight rules flight plan into a low overcast cloud ceiling. He commented that he lost visual contact with the ground immediately upon liftoff. During the initial climb, the airplane momentarily entered a nose-down attitude. He subsequently corrected the nose down attitude. However, as the airplane began to climb again the right wing impacted a tree. This occurred approximately 1 mile from the airport and within 1 minute of takeoff. After the in-flight collision, he had "full function" of the airplane and elected to continue the planned 31-minute flight to the intended destination. He added that there were no anomalies related to flight control or engine operation during the flight. A post accident inspection revealed impact damage to the leading edge of the right wing, right engine nacelle, and right propeller spinner. In addition, the inspection revealed a 3-inch crack in the aft wing spar at the right main landing gear wheel well. The pilot reported that he departed on an instrument flight rules flight plan into a low overcast cloud ceiling. He commented that he lost visual contact with the ground immediately upon liftoff. During the initial climb, the airplane momentarily entered a nose-down attitude. He subsequently corrected the nose down attitude. However, as the airplane began to climb again the right wing impacted a tree. This occurred approximately 1 mile from the airport and within 1 minute of takeoff. After the in-flight collision, he had "full function" of the airplane and elected to continue the planned 31-minute flight to the intended destination. He added that there were no anomalies related to flight control or engine operation during the flight. A post accident inspection revealed impact damage to the leading edge of the right wing, right engine nacelle, and right propeller spinner. In addition, the inspection revealed a 3-inch crack in the aft wing spar at the right main landing gear wheel well. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_2007_CHI08CA048.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

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