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Atlas / NTSB / MIA98LA128

NTSB CAROL · Event

Event MIA98LA128

1998-04-09 HAMPTONVILLE, North Carolina, United States Fatal 1 aircraft Status: Completed

Registry · N297B

FAA Aircraft Registry record.

Make / Model

CESSNA 172S

Year of manufacture

2023

Engine

LYCOMING IO-360-L2A (180 hp)

Seats / Engines

4 seats · 1 engine

Last airworthiness date

20230420

ADS-B equipped

Yes — Mode-S A30F94

Registrant of record

BOARD OF TRUSTEES OF SOUTHERN ILLINOIS UNIVERSITY

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's failure to maintain airspeed (VSO) while maneuvering at a low altitude.

Factual narrative

On April 9, 1998, about 1608 eastern daylight time, a Schleicher ASW-19B, N297B, registered to Kenlett Inc., operating as a 14 CFR Part 91 personal flight, crashed while maneuvering in the vicinity of Hamptonville, North Carolina. Visual meteorological conditions prevailed and no flight plan was filed. The glider sustained substantial damage. The private pilot was fatally injured. The flight originated from Swan Creek Airport, Jonesville, North Carolina, about 1 hour 52 minutes before the accident. A witness stated he was standing in his front yard when he heard a whistling noise. He looked up and observed a glider at a low altitude, estimated at about 200 feet. The airspeed was described as extremely slow, and the glider was in a right descending turn. The glider made about three to four right 360-degree turns before the nose of the glider was observed to pitch straight down, and the glider disappeared from view below the tree line. He immediately went inside the house and called 911, informing the operator that a glider had crashed. The wreckage of N297B was located about 5 to 6 miles southeast of Swan Creek Airport, Jonesville, North Carolina, in the vicinity of Interstate 77, between highway 421 and highway 21. Examination of the crashsite revealed the glider collided with the ground in about a 30 degree nose down attitude in a northerly direction. The landing gear and bottom of the fuselage were severely damaged, and the tail section was separated forward of the vertical stabilizer. The glider traveled about 80 feet before coming to rest in a gully. Examination of the airframe and flight control system revealed no evidence of a precrash mechanical failure or malfunction. Continuity of the flight controls was confirmed for pitch, roll, and yaw. Postmortem examination of the pilot was conducted by Dr. Patrick L. Lantz, Director of Autopsy Services, Wake Forrest University, Baptist Medical Center, Winston-Salem, North Carolina, on April 11, 1998. The cause of death was multiple injuries. Postmortem toxicology of specimens from the pilot was performed by the Forensic Toxicology Research Section, Federal Aviation Administration, Oklahoma City, Oklahoma. These studies were negative for ethanol, acidic, and neutral drugs. Lidocane, 0.1 (ug/ml, ug/g), was detected in the blood. Morphine, 0.054 (ug/ml, ug/g), was detected in the blood, and 0.088 (ug/ml, ug/g) was detected in liver fluid. A witness observed the glider at about 200 feet, and the airspeed was described as slow. The glider was observed to make several 360-degree turns before the nose of the glider was observed to pitch straight down, and the glider disappeared from view below the tree line. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1998_MIA98LA128.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.