NTSB CAROL · Event
Event WPR26LA034
Registry · N5107S
FAA Aircraft Registry record.
Make / Model
PIPER PA-28R-200
Year of manufacture
1971 · 54 years old at event
Engine
LYCOMING I0360 SER (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19710416
ADS-B equipped
Yes — Mode-S A664CD
Registrant of record
JDC AVIATION LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
On October 28, 2025, about 1845 Pacific daylight time, a Piper Arrow PA-28R-200, N5107S, sustained substantial damage when it was involved in an accident near Upland, California. The pilot and passenger were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The pilot and the passenger were about 33 miles west of Cable Airport (KCCB), Upland, California, when the pilot observed the oil pressure decrease to the lower limit of the green arc. About 14 miles west of CCB, the oil pressure reduced to zero; however, all other engine indications appeared normal. The pilot then decreased the power to about 16–17 inches of Hg and reviewed his checklist. He obtained approval from air traffic control (ATC) to initiate a descent and then commenced a descent from about 5,000 ft mean sea level (msl). The pilot subsequently adjusted the airplane’s course slightly southward to avoid elevated terrain to the north and to maintain proximity to Brackett Field Airport (POC – La Verne, CA) as a precaution. As the airplane descended through 3,000 ft msl, the pilot observed an ”explosion” within the engine cowling. Initially, he observed that there was significant engine roughness accompanied by a minor reduction in power while the airplane began to shake. The pilot then reduced the throttle further; however, he was unable to regain engine power. After determining the airplane’s position, he completed an engine failure checklist, declared an emergency, and informed ATC of the circumstance, and requested to land at POC. The pilot then observed smoke emanating from the cowling, which prompted him to lean the mixture, deactivate the fuel pump, and execute a power-off emergency landing. ATC advised the pilot of the weather conditions at POC, after which he transferred to POC’s tower frequency and updated the controller. He maintained the flaps in the 0° position and retracted the landing gear during the base to final turn. As the pilot maneuvered the airplane onto runway 26L, the stall warning activated. The pilot stated that the airplane stalled in a level attitude about 15-20 feet above the ground and subsequently landed hard on the runway. The airplane touched down on the northern edge of the displaced threshold, where it slid to a stop oriented sideways at the center of runway 26L. The airplane sustained substantial damage to both wings and the lower fuselage. The airplane was recovered to a secure facility for further examination. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2025_WPR26LA034.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…
Browse the full corpus — academia portal ↗