NTSB CAROL · Event
Event ATL94LA153
Registry · N44970
FAA Aircraft Registry record.
Make / Model
NAVAL AIRCRAFT FACTORY N3N-3
Year of manufacture
1940 · 54 years old at event
Engine
P&W R-985 SERIES (450 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20031231
ADS-B equipped
Yes — Mode-S A56F72
Registrant of record
BIBBER EUGENE A
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
THE PILOT'S IMPROPER USE OF THE RUDDER DURING LANDING.
Factual narrative
On August 10, 1994, about 1500 eastern daylight time, a Naval Aircraft Factory N3N-3, N44970, collided with trees following a loss of control during landing, at the Laurel Hill Plantation Airstrip, near Beaufort, South Carolina. The airplane was operated by the pilot under 14 CFR Part 91, and visual flight rules. Visual meteorological conditions prevailed. A flight plan was not filed for the local, personal flight. Neither the commercial pilot nor his passenger were injured, and the airplane was substantially damaged. Origination of the flight was a local, private strip about 15 minutes prior to the accident. The pilot reported that after landing, the tailwheel was lowered to the short-grass runway, about half way down its 2,000 foot length. He applied light braking, and the airplane veered to the right. According to the pilot, the right brake locked and control could not be regained with opposite control input. The airplane departed the right side of runway 21 and collided with trees that bounded the runway's western edge. The pilot stated that the passenger did not interfere with the flight controls and that the wind was calm. The airplane was examined by an airworthiness inspector from the South Carolina Flight Standards District Office on August 11, and 24, 1994. His examination report is attached. The inspector stated that, at the accident site while the airplane was still on its nose, the brake pedals were checked. The pedals were firm with no sponginess noted. He stated that both propeller blades were bent forward and that the propeller had dug a trench. During the second examination of the airplane, the right wheel was removed from the axle and the brake examined. The inspector reported that the lining, drum, springs, and cylinder were all in normal condition. No evidence of brake system malfunction or failure was noted. The aircraft log contained an entry dated 01/10/68 that "...showed the removal of agricultural spray equipment and the reinstallation of a front seat with seat belt and instruments in accordance with FAA letter 1/17/57. Aircraft to be used for agricultural training purposes only." NTSB records indicated that the pilot had an accident in the same airplane on June 14, 1991, at Deming, New Mexico. On landing, the airplane veered right, off of the runway. In his report of that accident, the pilot stated that he landed on runway 4 with the tetrahedron indicating a wind from the north. FAA records indicated that the pilot received a re-examination of his proficiency following the accident. The record stated that it was unusual that the pilot arrived in a GA-690 turbopropeller airplane, since the accident was a loss of control on landing in a tailwheel biplane. The record also stated that during the re- examination, the pilot's performance was satisfactory and that the pilot had "lazy" feet regarding rudder control. THE PILOT REPORTED THAT HE LANDED ON THE SOD RUNWAY WITH LIGHT AND VARIABLE WINDS. DURING THE LANDING ROLL, HE LIGHTLY APPLIED BRAKES, AND THE AIRPLANE VEERED RIGHT OFF THE RUNWAY AND COLLIDED WITH TREES. THE BRAKES WERE EXAMINED WITH NO MALFUNCTIONS NOR FAILURES FOUND. THE PROPELLER EXHIBITED DAMAGE THAT INDICATED THE AIRPLANE COLLIDED WITH THE TREES AT A HIGH POWER SETTING. THE PILOT HAD A PREVIOUS ACCIDENT IN THE SAME AIRPLANE. DURING THAT ACCIDENT, THE AIRPLANE LANDED ON RUNWAY 4, WITH NORTH WINDS, AND THE AIRPLANE VEERED OFF OF THE RUNWAY TO THE RIGHT. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1994_ATL94LA153.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 (stall, loss of control). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- Semantic Scholar 2016 · Article (Interacción)
Trajectory Recovery System: Angle of Attack Guidance for Inflight Loss of Control
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- NTSB Aircraft Accident Reports 2010 · Accident report
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- NASA NTRS 2026 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Scoping Review of Aviation Loss of Control Inflight Research
Loss of control – inflight (LOC-I) contributes to aircraft accidents at unacceptably high rates. Significant industry efforts and research have aimed to improve LOC-I prevention, detection, and recove…
- arXiv 2025 · arXiv preprint
Quadratic Programming Approach to Flight Envelope Protection Using Control Barrier Functions
Ensuring the safe operation of aerospace systems within their prescribed flight envelope is a fundamental requirement for modern flight control systems.
- SKYbrary (Eurocontrol) 2024 · SKYbrary article
Loss of Control In-Flight (LOC-I) — SKYbrary Knowledge Base
SKYbrary comprehensive knowledge-base entry on Loss of Control In-Flight — definitions, contributing factors, accident case studies (Air France 447, Colgan 3407), and prevention strategies.
Browse the full corpus — academia portal ↗