NTSB CAROL · Event
Event LAX96LA055
Registry · N56DS
FAA Aircraft Registry record.
Make / Model
CESSNA T337G
Year of manufacture
1973 · 22 years old at event
Engine
CONT MOTOR TSIO-360-CB (225 hp)
Seats / Engines
6 seats · 2 engines
Last airworthiness date
20210302
ADS-B equipped
Yes — Mode-S A724ED
Registrant of record
M E L LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
failure of the nose gear strut, during landing.
Factual narrative
On November 25, 1995, at 1710 hours mountain standard time, the nose gear of a homebuilt Schafer Lancair 360, N56DS, collapsed during the landing roll on runway 30L at Williams-Gateway Airport, Phoenix, Arizona. The pilot was completing a local visual flight rules personal flight. The airplane, registered to and operated by the pilot's wife, sustained substantial damage. The certificated private pilot, the sole occupant, was not injured. Visual meteorological conditions prevailed. The flight originated at Williams-Gateway Airport at 1610 hours. The pilot reported that he was practicing touch-and-go landings and takeoffs. On the last landing, the airplane touched down on the main wheels and the nose lowered onto the runway. About 2 or 3 seconds later, the pilot heard a thump under the tail of the airplane. Thereafter, the nose gear lowered and the propeller struck the runway. The pilot was able to raise the airplane's nose momentarily, and as the air speed depleted, the nose lowered again and the airplane skidded down the runway on the upper section of the nose gear strut. Later, the upper section of the strut lodged in a crack in the runway and broke off. The airplane subsequently came to a stop after it momentarily became airborne. The pilot also said in the report that the front "fork to [the] strut attachment [bolts]" failed. The Safety Board's investigator-in-charge asked the pilot to submit the bolts for metallurgical examination, but he elected not to. The pilot was practicing touch-and-go landings. On the last landing, the (lower) nose gear strut failed. The airplane then skidded on the upper strut until it contacted a crack in the runway, then the upper strut failed. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_LAX96LA055.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 ↗