NTSB CAROL · Event
Event FTW99LA053
Aircraft involved
Probable cause & findings
The pilot's loss of control as result of his improper recovery from a bounced landing.
Factual narrative
On December 16, 1998, at 1726 central standard time, a Pointer KR-2 experimental homebuilt airplane, N202DP, was substantially damaged during a hard landing near Denton, Texas. The private pilot sustained serious injuries and his passenger sustained minor injuries. The airplane was registered and operated by the pilot/builder under Title 14 CFR Part 91. Visual meteorological conditions prevailed for the local flight for which a flight plan was not filed. The personal flight originated from the Denton Municipal Airport (DTO) at 1630. According to an eyewitness who was holding short for takeoff from runway 35, he observed the Volkswagen powered low wing homebuilt airplane during the landing flare. The witness stated that the tricycle gear equipped airplane landed hard and bounced about 15 feet up into the air. The witness further stated that "he expected the pilot of the homebuilt airplane to add power and recover, but instead the airplane dropped onto the runway in a nose down attitude in a slight right turn." In a brief statement on the narrative portion of the enclosed NTSB Form 6120.1/2, the pilot states that he "hit the runway too hard and bounced." The pilot did not have any further recollection of the accident until he was loaded into the medical evacuation helicopter. The passenger, who was seated in the right seat, stated in the enclosed passenger statement form that "the aircraft bounced upon contact with the runway." The passenger added that "some seconds later I could no longer see the runway because we were in a high pitch attitude." The passenger concludes that "it was not long before the aircraft rolled over on its back to the right and crashed." The airplane came to rest in the inverted position on the right side of the runway. The FAA inspector that responded to the accident site confirmed that the nose portion of the fuselage, the right wing, and the top of the vertical stabilizer sustained structural damage. The homebuilt airplane, which was not equipped with shoulder harnesses for any of its occupants, had accumulated a total of 58 flight hours since new. A witness stated that the tricycle gear equipped airplane landed hard and bounced about 15 feet up into the air. The witness further stated that 'he expected the pilot of the homebuilt airplane to add power and recover, but instead the airplane dropped onto the runway in a nose down attitude in a slight right turn.' In a brief statement, the pilot stated that he 'hit the runway too hard and bounced.' The pilot did not have any further recollection of the accident. The passenger, who was seated in the right seat, stated in the enclosed passenger statement form that 'the aircraft bounced upon contact with the runway.' The passenger added that 'some seconds later I could no longer see the runway because we were in a high pitch attitude.' The passenger concludes that 'it was not long before the aircraft rolled over on its back to the right and crashed.' The airplane came to rest in the inverted position on the right side of the runway. The homebuilt airplane, which was not equipped with shoulder harnesses, had accumulated a total of 58 flight hours since new. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1998_FTW99LA053.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Beyond the agency record
Search this event elsewhere.
Pre-filled searches into the sources where news + community discussion of aviation events lives. External sources are reported, not agency. Treat them as signal that something happened, not as fact about what happened.
Entity-clustered aviation events in the press — last 24 hr + 30-day archive.
Official agency record + docket.
Investigative docket: factual reports, photos, transcripts.
Long-running aviation incident database (Flight Safety Foundation).
Community NTSB synthesis blog — often has photos and witness reports.
Gold-standard aviation incident blog.
Aviation industry news search.
GA pilot forum — informed but rumor-prone.
GA pilot subreddit search.
Tail-number page — flight history (free tier limited).
AOPA Air Safety Institute search.
Mainstream press coverage. Recent events only.
Privacy-preserving news search.
External links open in a new tab. We don't ingest their content; we deep-link search queries.
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
SKYbrary comprehensive knowledge-base entry on Loss of Control In-Flight — definitions, contributing factors, accident case studies (Air France 447, Colgan 3407), and prevention strategies.
- 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.
Browse the full corpus — academia portal ↗