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FTW99LA037

1998-11-27 · STUTTGART, Arkansas, United States · None · 1 aircraft · Status: Completed

Airport SGT

Current FAA registration · N5025C

Make / Model
BELLANCA 7GCBC
Year of manufacture
1978 · 20 years old at event
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19780915
ADS-B equipped
Yes — Mode-S A64468

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The separation of the left main landing gear bolt.

Factual narrative

On November 27, 1998, at 1345 central standard time, a Bellanca 7GCBC tailwheel equipped airplane, N5025C, groundlooped during the landing roll at the Stuttgart Municipal Airport, Stuttgart, Arkansas. The airplane, being flow by a private individual under Title 14 CFR Part 91, was owned by Tool Goose Flying Company, Tunica, Mississippi. The private pilot and the pilot rated passenger were not injured and the airplane sustained substantial damage. Visual meteorological conditions prevailed for the personal cross country flight that departed Tunica, Mississippi, at 1310. During personal telephone interviews, conducted by the investigator-in-charge, the pilot, passenger, and the airport manager reported the following information. The airplane landed in a 3 point attitude on the centerline of runway 18. During the landing roll with approximately 25 knots speed, the airplane veered to the right side of the runway. Application of the left rudder and the left brake by both occupants had no effect. Subsequently, the airplane departed the runway and groundlooped. The pilot and airport manager, who both examined the airplane, found structural damage to the fuselage and the left wing. The left main landing gear and propeller were also damaged. The airport manager reported that the left main wheel "rolled freely." The FAA inspector reported a separation of a left main landing gear bolt. The reason for the bolt separation was not determined. The pilot estimated that the failed bolt had accumulated 1302.2 flight hours since installation. During the landing roll, the airplane veered to the right side of the runway and application of the left rudder and brake by both occupants did not change the ground track. The airplane departed the runway and groundlooped. The FAA inspector, who examined the airplane, reported a separation of a left main landing gear bolt. The reason for the bolt separation was not determined. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1998_FTW99LA037.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

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