NTSB CAROL · Event
Event CHI96LA202
Registry · N853ND
FAA Aircraft Registry record.
Make / Model
PIPER PA-28-181
Year of manufacture
2020
Engine
LYCOMING IO-360-B4A (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20200709
ADS-B equipped
Yes — Mode-S ABB3AD
Registrant of record
UNIVERSITY OF NORTH DAKOTA
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the instructor pilot used an improper procedure when he demonstrated a rejected takeoff and he misjudged the flare.
Factual narrative
On June 14, 1996, at 1830 central daylight time, a Piper PA-44, N853ND, operated by the University of North Dakota (UND), Grand Forks, North Dakota, was substantially damaged during a hard landing. The flight instructor was demonstrating a rejected takeoff and had initiated the maneuver from 150 feet above the runway. The flight instructor and student were not injured. The 14 CFR Part 91 flight had departed runway 17R at Grand Forks Mark Andrews International Airport on a local instructional flight. Visual meteorological conditions prevailed at the time of the accident and no flight plan was filed. The instructor reported that he was attempting to demonstrate a rejected takeoff. However, instead of initiating the maneuver during the takeoff roll and aborting the takeoff on the runway, the instructor initiated the maneuver while on the final approach to the runway. The instructor reported that he made an approach to runway 17R with the airplane descending to about 150 feet AGL at 75 to 80 KIAS. The airplane was configured with the landing gear down and zero degrees flaps. About 100 yards from the runway threshold, he applied power and raised the nose. He reported that as the airplane crossed the threshold, he reduced power on both engines to idle and applied forward elevator establishing a descent for landing. The instructor pilot reported that he started to "round the airplane out about 30 to 50 feet above the runway." The descent rate was too high, so he continued to increase the pitch. He reported that the stall horn sounded "only milliseconds" before the airplane impacted the runway. The airplane started skidding down the runway and the pilots shut off the engines. The pilots evacuated the airplane after it came to a stop and the airplane had been secured. The instructor reported the demonstration he performed of a rejected takeoff was not a recognized or an approved maneuver. He reported that the he had never had this maneuver demonstrated to him. Additionally, this was the first time that he had attempted to demonstrate the maneuver. The instructor reported that he was attempting to demonstrate a rejected takeoff. Instead of initiating the maneuver during takeoff roll he attempted to initiate the maneuver on final approach to the runway. The instructor entered the maneuver from 150 feet AGL at 70 to 80 KIAS. As the airplane crossed the runway threshold, he reduced power on both engines to idle and applied forward elevator, establishing a descent for landing. He started to 'round the airplane out about 30 to 50 feet above the runway.' The descent rate was too high, so he continued to increase the pitch. He reported the stall horn sounded 'only milliseconds' before the airplane impacted the runway. The instructor reported the demonstration he performed of a rejected takeoff was not a recognized or an approved maneuver. He reported that the he had never had this maneuver demonstrated to him. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1996_CHI96LA202.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…
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