NTSB CAROL · Event
Event NYC02LA133
Registry · N9264
FAA Aircraft Registry record.
Make / Model
PIPER J3C-65
Year of manufacture
1946 · 56 years old at event
Engine
CONT MOTOR A&C65 SERIES (65 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19881025
ADS-B equipped
Yes — Mode-S ACD758
Registrant of record
WILKINS PHILLIP D
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The flight instructor's delayed remedial action, and the private pilot's failure to maintain airspeed, which resulted in an inadvertent stall/spin.
Factual narrative
On July 7, 2002, about 0950 eastern daylight time, a Piper J3-C65, N9264, was substantially damaged when it impacted the ground near Trinca Airport (13N), Andover, New Jersey. The certificated flight instructor was seriously injured, and the certificated private pilot received minor injuries. Visual meteorological conditions prevailed at the time. No flight plan had been filed for the local instructional flight, which was conducted under 14 CFR Part 91. The private pilot was receiving training for a tailwheel endorsement. According to the flight instructor, after completing a landing, the private pilot climbed the airplane to 600 feet above the ground, and turned crosswind. At 700 feet, the flight instructor reduced power to simulate an engine failure. The private pilot "kept pulling the nose up," and the flight instructor told him three times to "keep the nose down." The private pilot turned the airplane 90 degrees, towards the airstrip. He then let the airplane "get too slow and low," and the flight instructor took control of the airplane. As he did so, the airplane stalled and entered a right spin. The flight instructor recovered from the spin about 30 feet above the ground, added power, and saw trees ahead. He turned the airplane steeply to avoid trees. However, during the rollout from the steep turn, the airplane's left wing impacted the ground. The flight instructor further added that the accident occurred near the end of the instructional flight, and that the maneuver was the last one before the final landing. He also noted that the private pilot had successfully completed the maneuver three times during the same flight. The private pilot was receiving training for tailwheel endorsement. Near the end of the flight, and after completing a landing, the private pilot climbed the airplane to 600 feet and turned crosswind. At 700 feet, the flight instructor reduced power to simulate an engine failure. The private pilot "kept pulling the nose up," and the flight instructor told him three times to "keep the nose down." The private pilot turned the airplane 90 degrees, towards the airstrip. He let the airplane "get too slow and low," and the flight instructor took control. As he did so, the airplane stalled and entered a right spin. The flight instructor recovered from the spin about 30 feet above the ground, added power, and saw trees ahead. He turned the airplane steeply to avoid the trees, and during the rollout from the steep turn, the airplane's left wing impacted the ground. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_NYC02LA133.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, engine failure). 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
Multi-level Adaptation for Automatic Landing with Engine Failure under Turbulent Weather
This paper addresses efficient feasibility evaluation of possible emergency landing sites, online navigation, and path following for automatic landing under engine-out failure subject to turbulent wea…
- 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…
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