NTSB CAROL · Event
Event ERA11LA434
Registry · N51SV
FAA Aircraft Registry record.
Make / Model
AVIAT AIRCRAFT INC A-1C-200
Year of manufacture
2026
Engine
LYCOMING IO-360-A1D6 (200 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20260130
ADS-B equipped
Yes — Mode-S A660BA
Registrant of record
AVIAT AIRCRAFT INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
A total loss of engine power for undetermined reasons.
Factual narrative
On July 31, 2011, about 1545 eastern daylight time, a Nord Stampe SV4C, N51SV, was substantially damaged following a loss of engine power and collision with terrain at Old Rhinebeck Airport (NY94), Rhinebeck, New York. The commercial pilot sustained minor injuries. The airplane was registered to and operated by the Rhinebeck Aerodrome Museum under the provisions of 14 Code of Federal Regulations Part 91 as an air show flight. Visual meteorological conditions prevailed and no flight plan was filed. The local flight originated at NY94 about 1500. The pilot reported the following. He was participating in an air show demonstration, called a "bombing routine." Fuel was added to the fuel tank prior to engine start, and the flight departed with about 12 gallons on board. Aircraft preflight and ground operations were normal. During one of the bombing runs, about 350 feet above the ground, he dropped his bomb and added throttle to pull up and away for the next pass. He heard a "pop" and the engine rpm decreased. He unsuccessfully attempted to recover the engine with throttle movements. He attempted a restart, confirmed the fuel valve positions, and checked the magnetos. Unable to restart the engine, he attempted a forced landing. The airplane clipped trees and came to rest, inverted, at the edge of a stand of trees at the south end of the runway. An inspector with the Federal Aviation Administration responded to the accident site and examined the wreckage. There were approximately five gallons of fuel remaining in the fuel tank. Both upper and lower wings received structural damage. An examination of the engine revealed normal spark plug color and wear and the exhaust was clean. Internal engine continuity was confirmed. The wreckage was recovered to the museum hangar where a detailed examination of the fuel system was performed. After recovery of the wreckage, the engine-driven fuel pump was removed from the engine and examined. The pump was disassembled and found in an "operational condition internally." No reason for the loss of engine power was found. The pilot was participating in an air show display known as a "bombing routine." Preflight and ground operations were normal, and the airplane departed with about 12 gallons of fuel on board. During one of the bombing passes, the engine made a "pop" sound and lost power. The pilot attempted to recover power with throttle movements without success. He checked the fuel valve and magnetos, but was unable to restart the engine. During a forced landing, the airplane clipped trees and came to rest, inverted, at the edge of a stand of trees near the runway. A postaccident examination of the engine revealed no evidence of an engine malfunction or failure. It was noted that, at the time of the accident, the airplane was being operated in conditions conducive to carburetor icing at glide and cruise power. The reason for the loss of engine power could not be determined. 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 Not determined-Not determined-(general)-(general)-Unknown/Not determined - C
- C Aircraft-Aircraft systems-(general)-(general)-Failure - C
Verbatim from NTSB's published report. Source file
NTSB_2011_ERA11LA434.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 ↗