NTSB CAROL · Event
Event CEN11CA017
Aircraft involved
Probable cause & findings
The partial loss of engine power for undetermined reasons.
Factual narrative
The pilot was performing proficiency maneuvers near the destination airport when the airplane engine power went to idle. The pilot was unable to restore engine power above idle and elected to perform a forced landing on a field. During the forced landing, the airplane sustained substantial damage which included a buckled fuselage above the main landing gear and a separated right wing. The pilot received serious injuries. The on-scene inspection of the airplane did not identify any anomalies that resulted in the loss of engine power. The pilot was performing proficiency maneuvers near the destination airport when the airplane engine power went to idle. The pilot was unable to restore engine power above idle and elected to perform a forced landing on a field. The on-scene inspection of the airplane did not identify any anomalies that would have resulted in the loss of engine power. 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
Verbatim from NTSB's published report. Source file
NTSB_2010_CEN11CA017.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. Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- arXiv 2026 · arXiv preprint
Wave propagation through periodic arrays of freely floating rectangular floes
The two-dimensional propagation of small-amplitude waves through an infinite periodic array of freely-floating rectangular floes is considered under the assumptions of inviscid linearised wave theory.…
- arXiv 2023 · arXiv preprint
A Miniature Non-Uniform Conformal Antenna Array Using Fast Synthesis for Wide-Scan UAV Application
To overcome the limited payload of lightweight vehicles such as unmanned aerial vehicle (UAV) and the aerodynamic constraints on the onboard radar, a compact nonuniform conformal array is proposed in …
- NASA NTRS 2019 · Abstract
Weather Research and Forecasting Model Sensitivity Comparisons for Warm Season Convective Initiation
Mesoscale weather conditions can significantly affect the space launch and landing operations at Kennedy Space Center (KSC) and Cape Canaveral Air Force Station (CCAFS).
- NASA NTRS 2019 · Conference Paper
The effect of ambient conditions on the emissions of an idling gas turbine
Changes in ambient conditions - pressure, temperature, and humidity - affect the exhaust emissions of a gas turbine engine. Such variations must be compensated for during engine certification.
- arXiv 2017 · arXiv preprint
Dynamic System Identification, and Control for a cost effective open-source VTOL MAV
This paper describes dynamic system identification, and full control of a cost-effective vertical take-off and landing (VTOL) multi-rotor micro-aerial vehicle (MAV) --- DJI Matrice 100.
Browse the full corpus — academia portal ↗