NTSB CAROL · Event
Event NYC97LA110
Registry · N34SK
FAA Aircraft Registry record.
Make / Model
CLASSIC AIRCRAFT CORP WACO YMF
Year of manufacture
1990 · 7 years old at event
Engine
JACOBS R755B SERIES (275 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19901106
ADS-B equipped
Yes — Mode-S A3BC8F
Registrant of record
BIG Q AVIATION CORP
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain directional control and his improper compensation for the wind conditions. Contributing factors were the lack of recent experience in the airplane, and gusty wind conditions.
Factual narrative
On June 8, 1997, about 1445 eastern daylight time, a Waco YMF, N34SK, was substantially damaged during an aborted landing at the Ocean City Municipal Airport, Ocean City, Maryland. The certificated airline transport pilot was not injured. Visual meteorological conditions prevailed for the local proficiency flight. No flight plan had been filed for the flight which originated from Ocean City at 1345, and was conducted under 14 CFR Part 91. In the NTSB Pilot/Operator Aircraft Accident report, the pilot stated: "...I made one full stop and a series of touch and goes, on the last landing which was to be a full stop, I encountered a wind gust on roll out that made the aircraft uncontrollable, resulting in going off the runway [left side] and into the irrigation ditch which runs adjacent to the runway." The airplane was examined by an inspector from the Federal Aviation Administration (FAA) who reported the ground track of the airplane passed through a drainage ditch. The airplane had come to rest inverted with the right main landing gear collapsed, and both spars of the right wing were broken. In a telephone interview, the pilot reported a gust of wind which lifted the right wing, and the left wing tip touched the ground, after which the airplane departed the runway. When asked if there was a problem with either the flight controls or wheel brakes, the pilot replied, "no." The pilot reported the winds were from 70 to 80 degrees, at 12 to15 knots, with gusts at 20 to 25 knots. The pilot also reported he had about 30,000 hours total flight time, had flown 30-35 hours in the preceding year, and had flown 22 hours in preceding 90 days. He had about 300 hours in Wacos, with 3 hours of recent experience in the last year, all within the preceding 30 days. In a letter dated July 11, 1997, the pilot stated, "...In Retrospect: I believe that a cocked tail wheel, a brake failure, plus a gust of wind were contributing factors in the accident." In a memo dated October 23, 1997, an FAA inspector reported, "...Inspection showed that there was right hydraulic pressure and the brake was operative....", and "...Inspection showed that there was not excessive play in the tail wheel when in the locked position...." Runway 02 was 3,200 feet long, and 75 feet wide. The pilot was practicing takeoffs and landing when the accident occurred. According to the pilot, as the tail was settling from a wheel landing, the airplane encountered a gust of wind, which raised the right wing and the left wing struck the ground. He added power to abort the landing; however, the airplane departed the left side of the runway, and struck a drainage ditch. The right main landing gear collapsed and both spars on the right wing were broken. The airplane nosed over and came to rest inverted. In the preceding year, the pilot had acquired 3 hours of flight time in make/model. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1997_NYC97LA110.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 ↗