NTSB CAROL · Event
Event CEN10CA378
Registry · N164SA
FAA Aircraft Registry record.
Make / Model
ROBINSON HELICOPTER R44
Year of manufacture
2006 · 4 years old at event
TCDS
H11NM · ROBINSON HELICOPTER CO
Engine
LYCOMING O-540-F1B5 (260 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20160229
ADS-B equipped
Yes — Mode-S A1021B
Registrant of record
OLSON HELICOPTERS LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's improper recovery from a bounced landing.
Factual narrative
The pilot was practicing touch and go and full stop landings. On the third landing attempt the pilot had about 25 degrees flaps selected because he recognized he was higher and closer to the runway than normal. He felt he was stabilized on final at about 85 knots by mid-final. He flared and touched down lightly, but the airplane bounced slightly and floated one to two feet above the runway. The pilot added back pressure and the airplane suddenly touched down. The pilot added power and a porpoise developed. The propeller struck the runway and the nose gear collapsed, bending the firewall. The airplane stopped on the runway. The pilot did not report any airplane malfunctions prior to the accident. The pilot was practicing touch and go and full stop landings. On the third landing attempt the pilot had about 25 degrees flaps selected because he recognized he was higher and closer to the runway than normal. He felt he was stabilized on final at about 85 knots by mid-final. He flared and touched down lightly, but the airplane bounced slightly and floated one to two feet above the runway. The pilot added back pressure and the airplane suddenly touched down. The pilot added power and a porpoise developed. The propeller struck the runway and the nose gear collapsed, bending the firewall. The airplane stopped on the runway. The pilot did not report any airplane malfunctions prior to the accident. 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-Airspeed-Not attained/maintained - C
Verbatim from NTSB's published report. Source file
NTSB_2010_CEN10CA378.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 (icing). 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 · Contractor Report (CR)
Icing Physics Studies Using the 3D SIDRM Test Article: 2023 Icing Tests Analysis
In-flight icing is an important safety issue and is a factor that affects aircraft design and performance. Newer regulations are driving a need for improvements in airframe and engine icing simulation…
- arXiv 2025 · arXiv preprint
Multi-Agent Deep Reinforcement Learning for UAV-Assisted 5G Network Slicing: A Comparative Study of MAPPO, MADDPG, and MADQN
The growing demand for robust, scalable wireless networks in the 5G-and-beyond era has led to the deployment of Unmanned Aerial Vehicles (UAVs) as mobile base stations to enhance coverage in dense urb…
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Mathematical Model on the Temporal Dynamics of Aviation Competitive Pricing
This study investigates the competitive dynamics of airport pricing using U.S. airport data to validate the findings. It employs linear and nonlinear ordinary differential equation models to analyze t…
- NASA NTRS 2025 · Presentation
NASA Icing Update – March 2025
This NASA Icing Update was prepared for presentation to the SAE International AC-9C Inflight Icing Technology Committee. This update includes the following topics: planned Rotational Icing Scaling tes…
- arXiv 2024 · arXiv preprint
An energy-stable phase-field model for droplet icing simulations
A phase-field model for three-phase flows is established by combining the Navier-Stokes (NS) and the energy equations, with the Allen-Cahn (AC) and Cahn-Hilliard (CH) equations and is demonstrated ana…
- NASA NTRS 2024 · Presentation
NASA Icing Update – Oct 2024
This presentation provides a status update on select NASA icing research activities for the SAE AC-9C Icing Technical Committee Meeting on Oct 21, 2024.
Browse the full corpus — academia portal ↗