NTSB CAROL · Event
Event WPR25LA221
Registry · N5204C
FAA Aircraft Registry record.
Make / Model
BEECH B35
Year of manufacture
1950 · 75 years old at event
Engine
CONT MOTOR E185 SERIES (205 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19550827
ADS-B equipped
Yes — Mode-S A68BD5
Registrant of record
PEACE SIGN LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot’s failure to properly configure the airplane during a go-around which resulted in the airplane exceeding its critical angle of attack and an aerodynamic stall at a low altitude.
Factual narrative
The pilot was returning to his home airport and approached the airport from the north. He was initially cleared to land runway 27 but requested to land runway 17 because he was conveniently aligned with it. When about five miles from the airport he slowed the airplane, lowered the landing gear, and “pulled the throttle all the way back.” He stated that he did not recall “raising the propeller speed.” He further stated that he was too high, and extended the flaps to full down, which was something he normally did not do. During the landing flare, he waited for the airplane to settle onto the runway. He realized that the airplane had not touched down as it passed the midpoint of the 2,989 ft long runway and initiated a go-around. During the go-around, the pilot initially thought he had pushed the throttle control full forward, but when “nothing happened,” he looked down and realized he had pushed the mixture control forward. He added throttle and felt the airplane pick up speed. The pilot recalled that he pulled the yoke back to clear the airport perimeter fence and felt the airplane climb. The pilot stated that he had a positive rate of climb and thought he was high enough to begin a left turn and considered raising the flaps and contacting the tower when the airplane impacted the ground and slid into a building. A security video captured the airplane in a wings level attitude beyond the departure end of the runway. The airplane appeared to reach a height of about 20 ft above ground level before the left wing dropped and the airplane descended. Subsequently, it impacted a road and slid into a building, which resulted in substantial damage to both wings. Postaccident pictures of the airplane showed that the landing gear was extended and the flaps were retracted. The throttle control was pulled out about ½-inch, and the mixture control was about 1 ½-inch from full forward. The pilot reported that there were no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. 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).
- — Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Pilot
- — Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot
- — Personnel issues-Action/decision-Action-Incorrect action selection-Pilot
- — Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Airspeed-Not attained/maintained
Verbatim from NTSB's published report. Source file
NTSB_2025_WPR25LA221.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, go-around). 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 …
- NASA NTRS 2025 · Conference Paper
A Training Study to Improve Monitoring During A Go-Around
As part of an FAA program to improve go-around (GA) safety, we were asked to determine if we could improve the performance of the Pilot Monitoring (PM) during a GA maneuver.
- Flight Safety Foundation 2024 · FSF / AeroSafety World
Go-Around Safety Forum Findings
Foundation Go-Around Safety Forum technical findings — examines why pilots fail to execute go-arounds when criteria are met (stabilized approach gate not met, energy state out of envelope, traffic con…
- 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…
Browse the full corpus — academia portal ↗