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April 9, 1998 · Schleicher ASW-19B · N297B

Hamptonville, NC

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
April 9, 1998
Injury Outcomes
1 injury (1 fatality)
Location
Hamptonville, NC
Aircraft
Schleicher ASW-19B
Tail Number
N297B
Operator
Kenlett
Injuries
Fatal
Aircraft Damage
Substantial
NTSB Number
MIA98LA128

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.

NTSB Probable Cause

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

Full 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.

Flight

Event TypeAccident
Event Time16:08 EDT
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftSchleicher ASW-19B
Tail NumberN297B
Aircraft CategoryGli
DamageSubstantial
OperatorKenlett
Operating RulePart 91
Engine TypeUnknown
Engine DetailsUnknown
Seats1

People & Injuries

Injury Summary1 injury (1 fatality)
Fatal1
Serious0
Minor0
Uninjured0
Total1
Crew 1Age 72 · Third Class

Conditions

ConditionsVMC
LightDaylight
Wind260° @ 15 kt
Visibility20 sm
CeilingBroken clouds 10000 ft
Temperature / Dew Point0 C
Altimeter29.00 inHg
Observation Time20:45
Weather SourceWFAC

Appendix: Source Data