NTSB CAROL · Event
Event ATL90IA087
Registry · N1024Z
FAA Aircraft Registry record.
Make / Model
LANCAIR LC41-550FG
Year of manufacture
2005
Engine
CONT MOTOR TSIO-550 SER (280 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20050715
ADS-B equipped
Yes — Mode-S A00F1E
Registrant of record
AQUA MEN SERVICE LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
THE REPORTED PERFORMANCE PROBLEM DURING CLIMBOUT WAS UNDETERMINED. THE PILOT'S DECISION TO LAND WITH THE LANDING GEAR RETRACTED CONTRIBUTED TO THE MINOR DAMAGE SUSTAINED.
Factual narrative
WHILE PRACTICING TOUCH AND GO LANDINGS, THE PILOT REPORTED INSUFFICIENT ENGINE POWER ON THE GO PORTION OF THE PROCEDURE. THE PILOT STATED THAT THE AIRPLANE WOULD NOT DEVELOP SUFFICIENT POWER FOR WHAT HE BELIEVED TO BE A SAFE CLIMBOUT. HE ELECTED TO ABORT THE CLIMB AND LANDED ON THE REMAINING RUNWAY WITH THE LANDING GEAR RETRACTED. THE AIRPLANE CAME TO REST ABOUT 4000 FEET FROM THE DEPARTURE END OF THE RUNWAY. RUNWAY 35 IS 8000 FEET LONG. THE AIRPLANE SUSTAINED MINOR STRUCTURAL DAMAGE. SUBSEQUENT INSPECTIONS AND OPERATIONAL CHECKS OF THE ENGINE AND RELATED SYSTEMS FAILED TO DISCLOSE ANY PERFORMANCE PROBLEM WITH THE ENGINE. THERE WERE NO MECHANICAL OR OPERATIONAL PROBLEMS FOUND WITH THE AIRFRAME OR ITS SUBSYSTEMS. THE REASON FOR THE REPORTED POWER PERFORMANCE PROBLEMS WAS NOT DETERMINED. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1990_ATL90IA087.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 ↗