ATL95LA002
1994-10-01 · COVINGTON, Tennessee, United States · Serious · 1 aircraft · Status: Completed
Airport M04
N731PS has since been reassigned. It is now registered to a different aircraft (CERES AIR C31), which was not involved in this event.
Aircraft involved
Probable cause & findings
The pilot's failure to maintain directional control during landing.
Factual narrative
On October 1, 1994, about 1700 central daylight time, a Cessna 188, N731PS, groundlooped during the landing roll at Covington, Tennessee. The airplane was operated by Baker Flying Service under the provisions of 14 CFR Part 137, and visual flight rules. Visual meteorological conditions prevailed. A flight plan was not filed for the aerial application flight. There were serious injuries to the commercial pilot, and the airplane was substantially damaged. Origination of the flight was Covington, Tennessee, about 1615. The pilot reported that the airplane veered left during the landing and that the right rudder pedal and brake did not operate to oppose the divergent ground path. An inspector from the Tennessee Flight Standards District Office, Memphis, Tennessee, spoke with the pilot, and examined the accident site and the airplane, after the accident. He reported that the pilot said he was attempting to land on the runway, and overshot it. The airplane landed in the grass beside the runway. Tire tracks showed a normal landing roll, until about the last 700 feet where the tracks showed the airplane veered left, then entered a skid, breaking off the right main landing gear at the attachment point. The right wing then, struck the ground. According to the inspector, the rudder pedal, rudder cable, and rudder functioned. The brake pad did not exhibit excessive wear and the hydraulic line did not exhibit any pre-impact failure. THE PILOT OVERSHOT THE CENTERLINE OF THE PREPARED RUNWAY AND LANDED IN THE GRASS ADJACENT TO THE RUNWAY. DURING THE LANDING ROLL THE AIRPLANE GROUNDLOOPED, BREAKING OFF THE RIGHT MAIN LANDING GEAR, AND DRAGGING THE WING ON THE GROUND. HE REPORTED THAT THE RUDDER HAD NOT RESPONDED TO HIS ATTEMPTS TO CORRECT THE OVERSHOOT. AN INSPECTION OF THE RUDDER SYSTEM SHOWED THAT IT WAS FUNCTIONAL. THE BRAKE PAD WAS NOT EXCESSIVELY WORN, AND THE SEVERED WHEEL BRAKE LINE DID NOT EXHIBIT ANY PRE-IMPACT DAMAGE. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1994_ATL95LA002.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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