NTSB CAROL · Event
Event DFW07CA147
Registry · N41585
FAA Aircraft Registry record.
Make / Model
PIPER PA-28R-200
Year of manufacture
1974 · 33 years old at event
Engine
LYCOMING I0360 SER (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19740227
ADS-B equipped
Yes — Mode-S A4EA41
Registrant of record
BAS PART SALES LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The inadvertent stall and subsequent hard landing as result of the pilot's failure to maintain airspeed and his delayed relinquishing of the airplane's controls when requested by the flight instructor.
Factual narrative
The pilot failed to maintain airspeed on short final resulting in a stall and a hard landing. The 253-hour private pilot and the 700-hour certificated flight instructor (CFI) were performing a power-off 180-degree approach to land when they overshot the runway while turning to final. Once realigned with the extended centerline of the runway, the flight instructor observed that the airspeed was indicating 70-75 knots while the single-engine airplane descended through an altitude of 200-feet above ground level (AGL). As the flight continued to descend to approximately 30-feet AGL, the private pilot "applied excessive back pressure" and established a pronounced nose-high attitude. The flight instructor attempted to push the nose of the airplane down; however, he was unable to overpower the student. The flight instructor reported that the pilot "did not immediately relinquish the controls when requested by the CFI." Once the flight instructor regained the airplane's controls, he added power to counteract the descent; however, the airplane stalled approximately 15-feet AGL and landed hard on the runway. An examination of the airplane revealed structural damage to both wings. No pre-impact anomalies with the airplane's controls were reported. The pilot failed to maintain airspeed on short final resulting in a stall and a hard landing. The 253-hour private pilot and the 700-hour certificated flight instructor (CFI) were performing a power-off 180-degree approach to land when they overshot the runway while turning to final. Once realigned with the extended centerline of the runway, the flight instructor observed that the airspeed was indicating 70-75 knots while the single-engine airplane descended through an altitude of 200-feet above ground level (AGL). As the flight continued to descend to approximately 30-feet AGL, the private pilot "applied excessive back pressure" and established a pronounced nose-high attitude. The flight instructor attempted to push the nose of the airplane down; however, he was unable to overpower the student. The flight instructor reported that the pilot "did not immediately relinquish the controls when requested by the CFI." Once the flight instructor regained the airplane's controls, he added power to counteract the descent; however, the airplane stalled approximately 15-feet AGL and landed hard on the runway. An examination of the airplane revealed structural damage to both wings. No pre-impact anomalies with the airplane's controls were reported. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2007_DFW07CA147.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). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- 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 …
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- arXiv 2023 · arXiv preprint
Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2023 · arXiv preprint
Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- arXiv 2022 · arXiv preprint
Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER)
Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…
Browse the full corpus — academia portal ↗