Skip to content

Atlas / NTSB / FTW98LA228

NTSB CAROL · Event

Event FTW98LA228

1998-05-17 OZARK, Arkansas, United States Airport · 7MS Minor 1 aircraft Status: Completed

Registry · N23548

FAA Aircraft Registry record.

Make / Model

AERONCA 65-C

Year of manufacture

1939 · 59 years old at event

Engine

CONT MOTOR A&C65 SERIES (65 hp)

Seats / Engines

2 seats · 1 engine

Last airworthiness date

19570605

ADS-B equipped

Yes — Mode-S A21E18

Registrant of record

ROGERS SAMUEL

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's failure to maintain aircraft control.

Factual narrative

On May 17, 1998, at 1800 central daylight time, an Aeronca 65-C airplane, N23548, owned and operated by a private individual under Title 14 CFR Part 91, sustained substantial damage during a loss of control while landing near Ozark, Arkansas. The solo student pilot received minor injuries. Visual meteorological conditions prevailed for the cross country solo instructional flight that departed Huntsville, Arkansas, at 1715. A flight plan was not filed. The student pilot, endorsed for solo flight in the aircraft, had flown 33.3 hours (24.8 solo) in this aircraft. The student pilot reported that during the wheel landing, the airplane nosed over to the inverted position. The FAA inspector, examining the airplane, found structural damage to the wing and spars. The cabin area exhibited buckling. The owner/witness reported that the aircraft landed in the center of the runway with the tailwheel approximately one foot off the runway surface. As the aircraft's speed slowed, the tail became more elevated and the aircraft flipped over and landed on its back. At the time of the accident the wind was calm. Examination of the aircraft revealed that the wheels spun freely and the brakes functioned normally. The right wing was twisted and several ribs on the left wing were damaged. Fabric damage occurred to the right wing and the vertical stabilizer. The propeller, engine, and carburetor were damaged. The student pilot, endorsed for solo flight in the aircraft, reported that during landing the airplane nosed over to the inverted position. A witness observed the aircraft land in the center of the runway with the tailwheel approximately one foot off the runway surface. As the aircraft's speed slowed, the tail became more elevated and the aircraft flipped over and landed on its back. The wind was calm. Examination of the aircraft revealed that the wheels spun freely and the brakes functioned normally. The student had 33.3 hours (24.8 solo) in make and model. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1998_FTW98LA228.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

What the literature says.

Academic papers and agency reports matching this event's aircraft type or causal vocabulary (loss of control). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.

Browse the full corpus — academia portal ↗