NTSB CAROL · Event
Event DFW05CA224
Aircraft involved
Probable cause & findings
The pilot's improper recovery from a bounced landing. A contributing factor was the dark night conditions.
Factual narrative
On August 28, 2005, about 2118 central daylight time, a single-engine Cessna 152 airplane, N4670B, was substantially damaged following a loss of control during landing at the Richard Lloyd Jones Jr. Airport (RVS), near Tulsa, Oklahoma. The instrument rated private pilot, the sole occupant of the airplane, was not injured. The airplane was owned and operated by Spartan Aviation Industries, Inc., of Tulsa, Oklahoma. Night 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 originated from RVS at approximately 2020. The 264-hour pilot reported that he was on final approach for his eighth night landing of the evening when he observed that he was "high" for runway 1R (a 4,208 foot by 100 foot asphalt runway). The pilot initiated a forward slip to lose altitude and the airplane momentarily touched down on the runway before becoming airborne again. The pilot attempted to hold the airplane in a flare but it "started going into oscillations." He then attempted to "go around", but approximately five feet above the ground (agl) the airplane stalled and impacted the runway. The nose landing gear collapsed and the airplane departed the edge of the runway into soft terrain, nosed over, and came to rest in an inverted position. The pilot further reported that there was no mechanical malfunction or failure with the airplane. A Federal Aviation Administration inspector, who examined the airplane, reported that the fuselage, vertical stabilizer, and wings sustained structural damage. The pilot reported calm winds, visibility 10 statute miles, clear skies, temperature 75 degrees Fahrenheit, dew point 65 degrees Fahrenheit and a barometric pressure setting of 29.91 inches of Mercury. On final approach, for his eighth night landing of the evening, the 264-hour instrument rated private pilot observed that he was "high" for runway 1R (a 4,208 foot by 100 foot asphalt runway). The pilot initiated a forward slip to lose altitude and the airplane momentarily touched down on the runway before becoming airborne again. The pilot attempted to hold the airplane in a flare but it "started going into oscillations." He then attempted to "go around", but approximately five feet above the ground (agl) the airplane stalled and impacted the runway. The nose landing gear collapsed and airplane departed the edge of the runway into soft terrain, nosed over, and came to rest in an inverted position. An examination of the airplane revealed the fuselage, vertical stabilizer, and wings sustained structural damage. The pilot reported that there was no mechanical malfunction or failure with the airplane. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2005_DFW05CA224.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 (stall, 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.
- Semantic Scholar 2016 · Article (Interacción)
Trajectory Recovery System: Angle of Attack Guidance for Inflight Loss of Control
This paper describes the design and development of an ecological display to aid pilots in the recovery of an In-Flight Loss of Control event due to a Stall (ILOC-S).
- NTSB Aircraft Accident Reports 2010 · Accident report
Loss of Control on Approach — Colgan Air Flight 3407
Colgan Air 3407 / Continental Connection (Q400) Buffalo NY, February 12, 2009 — 50 fatalities. Definitive investigation of the Colgan 3407 stall-stick-pusher crash on approach to Buffalo.
- NASA NTRS 2026 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- 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…
- arXiv 2025 · arXiv preprint
Quadratic Programming Approach to Flight Envelope Protection Using Control Barrier Functions
Ensuring the safe operation of aerospace systems within their prescribed flight envelope is a fundamental requirement for modern flight control systems.
- 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.
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