WPR25LA221
2025-07-23 · Helena, Montana, United States · Minor · 1 aircraft · Status: Completed
Airport HLN
Current FAA registration · N5204C
- 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
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
FAA avdata. C = Cause, 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 ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
- Aviation Herald Aviation press ↗
- AVweb Aviation press ↗
- Pilots of America Community ↗
- Reddit /r/flying Community ↗
- FlightAware Aviation press ↗
- AOPA accident database Aviation press ↗
- Google News News ↗
- DuckDuckGo News ↗
Related research
Matched on aircraft type or causal vocabulary (stall, go-around). All research papers
- 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…