NTSB CAROL · Event
Event CEN16LA029
Registry · N9029Y
FAA Aircraft Registry record.
Make / Model
PIPER PA-18-150
Year of manufacture
1970 · 45 years old at event
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19900702
ADS-B equipped
Yes — Mode-S AC7A44
Registrant of record
JOHNSON SCOTT W
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain directional control during the landing and his subsequent improper decision to attempt an aborted landing after the airplane had departed the runway.
Factual narrative
On November 3, 2015, about 1442 eastern standard time, a Piper model PA-18-150 single-engine airplane, N9029Y, was substantially damaged when it collided with trees during an aborted landing at Meyers-Diver's Airport (3TE), Tecumseh, Michigan. The airline transport pilot and his passenger were not injured. The airplane was registered to and operated by the pilot under the provisions of 14 Code of Federal Regulations Part 91 without a flight plan. Day visual meteorological conditions prevailed for the personal flight that had departed 3TE about 1320.The pilot reported that the accident occurred as he was landing on runway 27 (1,820 feet by 100 feet, grass/turf). He reported that he made a normal wheel (two-point) landing; however, as the airplane traversed over the crossing runway 18/36 (asphalt), the airplane bounced back into the air near midfield. He increased engine power after the bounce and subsequently made a full-stall (three-point) landing on the remaining runway. The pilot reported that the airplane immediately veered to the left after the tailwheel made contact with the runway. The airplane subsequently departed the left side of the runway into a grass field. The pilot reported that he was able to regain directional control and reestablish a ground track that was parallel to the runway before he attempted an aborted landing from the grass field. Although he was able to get the airplane airborne, the pilot was unable to clear trees that were located along an airport perimeter road. The airplane sustained substantial damage to the wings and fuselage during the collision with the trees. The pilot reported that there were no mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. Additionally, the pilot reported that the accident likely could have been prevented had he attempted to stop the airplane while in the grass field instead of trying to abort the landing. A postaccident airplane examination, completed by a Federal Aviation Administration (FAA) Airworthiness Inspector, did not reveal any anomalies with the airplane's flight controls, brake system, or tail wheel assembly that would have prevented normal operation. At 1453, the automated surface observing system at the Lenawee County Airport (ADG), located about 11 miles south-southwest of the accident site, reported: wind 180 degrees at 7 knots, surface visibility 10 statute miles, clear sky, temperature 23 degrees Celsius, dew point 7 degrees Celsius, and an altimeter setting of 30.15 inches of mercury. The airline transport pilot reported that he made a normal wheel (two-point) landing; however, as the airplane traversed the airport's crossing runway, the airplane bounced into the air near midfield. He increased engine power after the bounce and subsequently made a full-stall (three-point) landing on the remaining runway. The airplane immediately veered left after the tailwheel contacted the runway. The airplane subsequently departed the left side of the runway into a grass field. The pilot reported that he was able to regain directional control and reestablish a ground track that was parallel to the runway before he attempted to abort the landing and take off from the grass field. Although he was able to get the airplane airborne, the pilot was unable to clear trees located along an airport perimeter road. The pilot reported that there were no mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. Additionally, a postaccident airplane examination did not reveal any anomalies with the airplane's flight controls, brake system, or tailwheel assembly that would have prevented normal operation. The pilot reported that the accident likely could have been prevented if he had attempted to stop the airplane in the grass field instead of trying to abort the landing. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- C Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Pilot - C
Verbatim from NTSB's published report. Source file
NTSB_2015_CEN16LA029.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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