NTSB CAROL · Event
Event FTW00LA219
Registry · N105LW
FAA Aircraft Registry record.
Make / Model
CIRRUS DESIGN SR22T
Year of manufacture
2024
Engine
CONT MOTOR TSIO-550-K (315 hp)
Seats / Engines
5 seats · 1 engine
Last airworthiness date
20240322
ADS-B equipped
Yes — Mode-S A01856
Registrant of record
CAN YOU SEE ME NOW LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's failure to maintain control of the glider while maneuvering. Contributory factors were the in-flight separation of the tow rope and the pilot's physical impairment from his use of diphenhyrdramine.
Factual narrative
On July 29, 2000, at 1500 central daylight time, a Let L-23 Super Blankit non-powered glider, N105LW, was destroyed when it impacted trees following a separation of the towrope and loss of control during the initial takeoff climb from the Houston Gliderport, Waller, Texas. The glider was registered to and operated by The Soaring Club of Houston, Houston, Texas. The private pilot, who held a glider rating, sustained fatal injuries. Visual meteorological conditions prevailed and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 personal flight. The local flight was originating at the time of the accident. According to the pilot of the towplane, the takeoff from runway 17 was normal and while climbing through 600 feet agl he initiated a left turn to the east. He reported that as the airplane was turning he "felt the glider release from the tow," and he then banked hard left to give way to the glider. Subsequently, the pilot received a radio transmission that the glider had crashed, and he returned to the airport. Upon landing it was evident that the tow rope had separated, and the glider pilot had not released in the normal manner. According to witnesses, the initial climb-out "appeared quite normal" and "as usual, at the end of the airport the tow plane commenced a left turn." However, the glider continued straight ahead and it entered a climb. The glider was 250-300 feet agl when it began a "very uncoordinated turn to the right," and as it turned through 90 degrees, the "nose of the glider dropped and it entered a spin." Subsequently, the glider completed 1-2 turns before impacting trees and the ground. One witness, who was part of the airport crew and a wing runner for the gliders, stated that "it was picture-perfect for soaring," and "all other flights that day were without incident and none of the pilots of the Blankit that day had mentioned any problems." The separated sections of the rope were removed from the glider attach point and from the tow plane by an FAA inspector. The rope was sent to the NTSB Investigator-In-Charge for examination. The rope was separated approximately 25 feet forward of the attach point on the glider, and the rope's fibers, at the separation point, appeared frayed and uneven. The remainder of the rope appeared clean and was free of abrasions, knots, and nicks. According to Soaring Club personnel, the rope was 5/16-inch polypropylene, with a breaking strength of 1,300 pounds. According to FAA records and the pilot's flight logbook, the pilot was issued a private pilot certificate (single-engine land) on September 19, 1970, and a glider rating on April 30, 2000. He had accumulated a total of 118.4 flight hours, of which 26.2 flight hours were in gliders. His last FAA third class medical certificate was issued on June 14, 1992, and there was no record of the pilot having been issued an FAA medical certificate since that time. Additionally, the FAA does not require a pilot to hold a medical certificate to pilot a glider. An autopsy was performed by the Office of the Medical Examiner of Harris County, Houston, Texas. Toxicological tests were performed by the FAA's Civil Aeromedical Institute, Oklahoma City, Oklahoma. The tests were negative for carbon monoxide, cyanide and ethanol. The tests revealed the following; Bupropion present in blood and urine, bupropion metabolite detected in blood and urine, 0.034 (ug/ml, ug/g) diphenhydramine detected in blood, and diphenhydramine detected in urine. Bupropion is a prescription mediation (commonly known by the trade name Wellbutrin) used in the treatment of depression, attention deficit hyperactivity disorder, and smoking cessation. Diphenhydramine is an over-the-counter antihistamine (commonly known by the trade name Benadryl) used in symptomatic management of allergic symptoms and also for its sedative, antitussive and antispasmodic effects. The American College of Physicians-American Society of Internal Medicine conducted a study (Effects of Fexofenadine, Diphenhydramine, and Alcohol on Driving Performance) on the effects of diphenhydramine on driving performance. The results of that study indicated that "Participants had significantly better coherence after taking alcohol or fexofenadine (Allegra) than after taking diphenhydramine...After participants took diphenhydramine, driving performance was poorest, indicating that diphenhydramine had a greater impact on driving than alcohol did." The pilot of the towplane reported that the takeoff was normal, and while climbing through 600 feet agl, he initiated a turn to the east and he felt the glider release as the airplane was turning. Witnesses reported that when the towplane turned left, the glider continued straight ahead and entered a climb. The glider then entered an uncoordinated turn to the right toward the airport. Subsequently, the glider's nose dropped, and it entered a spin and impacted the ground. When the tow plane landed it was evident that the tow rope had separated, and the glider pilot had not released in the normal manner. The 5/16-inch polypropylene rope separated at a point 25 feet forward of the glider attach point. The rope's fibers, at the point of separation, were frayed and uneven. The remainder of the rope was clean and free of abrasions, knots, and nicks. According to toxicology tests, 0.034 (ug/ml,ug/g) diphenhydramine was detected in the pilot's blood, and an unquantified amount was found in the urine. Diphenhydramine is an over-the-counter drug used as an antihistamine. Results of a study on diphenhydramine concluded that it adversely affects a person's ability to maneuver an automobile. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2000_FTW00LA219.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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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.
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Scoping Review of Aviation Loss of Control Inflight Research
Loss of control – inflight (LOC-I) contributes to aircraft accidents at unacceptably high rates. Significant industry efforts and research have aimed to improve LOC-I prevention, detection, and recove…
- SKYbrary (Eurocontrol) 2024 · SKYbrary article
Loss of Control In-Flight (LOC-I) — SKYbrary Knowledge Base
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- NTSB Aircraft Accident Reports 2022 · Accident report
Loss of Control on Takeoff in Icing Conditions — Citation 560XL
Cessna Citation 560XL fatal takeoff icing accident, March 2018. Investigation of a Citation 560XL loss-of-control takeoff accident in icing conditions.
- Semantic Scholar 2021 · Article (Aviation)
ANALYSIS OF GENERAL AVIATION FIXED-WING AIRCRAFT ACCIDENTS INVOLVING INFLIGHT LOSS OF CONTROL USING A STATE-BASED APPROACH
Inflight loss of control (LOC-I) is a significant cause of General Aviation (GA) fixed-wing aircraft accidents. The United States National Transportation Safety Board’s database provides a rich source…
- NASA NTRS 2021 · Presentation
Use of Design of Experiments in Determining Neural Network Architectures for Loss of Control Detection
Abstract—We describe empirical methods for selecting a neural network architecture to implement belief state inference on generic commercial transport aircraft.
- NASA NTRS 2021 · Conference Paper
Use of Design of Experiments in Determining Neural Network Architectures for Loss of Control Detection
We describe empirical methods for selecting a neural network architecture to implement belief state inference on generic commercial transport aircraft.
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