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CHI03LA054

2003-01-12 · Charleston, Missouri, United States · None · 1 aircraft · Status: Completed

Airport CHQ

Current FAA registration · N66507

Make / Model
CESSNA 150M
Engine
CONT MOTOR 0-200 SERIES (100 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19770114
ADS-B equipped
Yes — Mode-S A8C944

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

the inadequate flare by the pilot. Factors were the loose trim tab cable for undetermined reasons.

Factual narrative

On January 12, 2003, at 1300 central standard time, a Cessna 150M, N66507, owned and piloted by a recreational pilot, was substantially damaged during a hard landing at Mississippi County Airport (CHQ), Charleston, Missouri. Visual meteorological conditions prevailed at the time of the accident. The 14 CFR Part 91 personal flight was not operating on a flight plan. The pilot received no injuries. The flight originated from Everett-Stewart Airport, Union City, Tennessee, at 1200, en route to CHQ. The pilot reported to the Federal Aviation Administration that there was elevator control stiffness during his first approach for landing. In the pilot's written statement he reported that he executed a go-around which was then followed by the accident landing. The airplane impacted the runway in a nose low attitude. An operational check of the airplane flight controls was preformed by the Federal Aviation Administration. No anomalies were noted when the elevators and ailerons were checked to ensure full unrestricted travel. There was no excessive play in the elevator, rudder, ailerons, and elevator. The elevator trim cable did not possess any tension relative to the 10-20 pound tension cited in the Cessna Maintenance Manual. The lack of elevator trim cable tension did not preclude operation of the elevator trim. The airplane impacted the runway during landing in a nose low attitude. The pilot reported elevator control stiffness during his first approach for landing which was then followed by a go-around and the accident landing. No anomalies were noted when the elevators and ailerons were checked to ensure full unrestricted travel. There was no excessive play in the elevator, rudder, ailerons, and elevator. The elevator trim cable did not possess any tension relative to the 10-20 pound tension cited in the manufacturer’s maintenance manual. The lack of elevator trim cable tension did not preclude operation of the elevator trim. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_2003_CHI03LA054.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

Matched on aircraft type or causal vocabulary (go-around, maintenance). All research papers