NTSB CAROL · Event
Event ANC25LA007
Registry · N307AM
FAA Aircraft Registry record.
Make / Model
AVIAT AIRCRAFT INC A-1B
Seats / Engines
2 seats · 1 engine
ADS-B equipped
Yes — Mode-S A3395F
Registrant of record
COPPER RIVER AIRMOTIVE LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot’s improper landing flare which resulted in a hard landing, loss of directional control, and nose-over.
Factual narrative
The pilot reported that, while conducting stop-and-go landings on a beach in his tailwheel-equipped airplane, he flared early which resulted in a hard landing. The pilot lost directional control of the airplane and subsequently nosed over and came to rest inverted resulting in substantial damage to the wings, lift struts, rudder, and vertical and horizontal stabilizers. The pilot reported that there were no preaccident mechanical failures or malfunctions 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).
- — Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Landing flare-Not attained/maintained
- — Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot
Verbatim from NTSB's published report. Source file
NTSB_2024_ANC25LA007.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. Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- Embry-Riddle Scholarly Commons 2021 · Journal article (IJAAA)
Helicopter Shaft Heating Parameters for Polyamide-11 Coating
In this study, the heating parameters required for polyamide-11 (P11) coating of the helicopter shaft were investigated. The torsion value created by the force applied to the middle of the helicopter'…
- NASA NTRS 2019 · Technical Memorandum (TM)
Investigation of Spiral Bevel Gear Condition Indicator Validation via AC-29-2C Combining Test Rig Damage Progression Data with Fielded Rotorcraft Data
This is the final of three reports published on the results of this project. In the first report, results were presented on nineteen tests performed in the NASA Glenn Spiral Bevel Gear Fatigue Test Ri…
- Embry-Riddle Scholarly Commons 2015 · Journal article (IJAAA)
Bio-Fuel Alternatives in South African Airways (SAA) Operations - Is it an Effective Response to Vulnerability over Carbon Taxes and Penalty?
The paper did a comparative analysis of the carbon emission and European Union Emission Trading Surcharges (EU ETS) of South African Airways (SAA) current fleet that used aviation jet A1 fuel and the …
Browse the full corpus — academia portal ↗