NTSB CAROL · Event
Event WPR10LA191
Aircraft involved
Probable cause & findings
The landing gear collapsing during the landing roll for undetermined reasons.
Factual narrative
On March 21, 2010, about 1905 Pacific daylight time, a Beech 58P, N580TC, sustained substantial damage following the collapse of all three landing gear during landing rollout at the Santa Barbara Municipal Airport (SBA), Santa Barbara, California. The airline transport pilot and his four passengers were not injured. Visual meteorological conditions prevailed at the time of the accident, and a flight plan was not filed. The cross-country flight, which was being operated in accordance with 14 Code of Federal Regulations Part 91, had departed the San Jose International Airport (SJC), San Jose, California, about 1745, with SBA as its destination. In a telephone interview with the NTSB investigator-in-charge (IIC) shortly after the accident occurred, the pilot reported that on final approach he observed "three green lights," which indicated that all three landing gear were down and locked; he added that he did not hear a landing gear warning horn either. The pilot further reported that upon touching down and after rolling out between 500 and 1,000 feet down the runway, the nose gear collapsed followed by the left and right main landing gear collapsing. The airplane came to rest on the runway and just off to the right of centerline. A Federal Aviation Administration (FAA) airworthiness inspector, who conducted a post accident examination of the airplane, reported that both main landing gear inner doors were damaged, but neither of the outer doors sustained any visible damage. The forward pressure bulkhead was substantially damaged. During a post accident examination and repair of the airplane, a certificated Federal Aviation Administration (FAA) airframe and powerplant mechanic reported that he did not identify a mechanical failure or malfunction that could be attributed to the landing gear collapse. The pilot reported that on final approach he observed three green lights illuminated on the instrument panel, indicating to him that all three landing gear were down and locked. He noted that he did not hear a landing gear warning horn. After touching down and during the landing roll, the nose landing gear collapsed, followed by the right main landing gear and then the left main landing gear. The airplane came to rest slightly to the right of the runway's centerline with substantial damage to the forward bulkhead. A postaccident examination of the airplane by a certified Federal Aviation Administration airframe and powerplant mechanic failed to identify either a mechanical failure or malfunction that could have precipitated the landing gear collapse. The reason for the landing gear collapse was undetermined. 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_WPR10LA191.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.
- NASA NTRS 2011 · Conference Paper
Joint thunderstorm operations using the NASA F-106B and FAATC/AFWAL Convair 580 airplanes
During the 1985 thunderstorm season, three joint thunderstorm research flights were conducted within 100 n.mi. of NASA Langley by the NASA Storm Hazards F-106B and the FAA/USAF CV-580 research airplan…
- NTSB Aircraft Accident Reports 2004 · Accident report
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American Airlines 587 (A300-605R) Belle Harbor, NY, November 12, 2001 — 265 fatalities. Investigation of the post-takeoff in-flight breakup of American 587 over Belle Harbor.
- NASA NTRS 2024 · Presentation
American Airlines Flight 587 Crash Investigation: NASA Langley Research Center Participation and Perspective
- NASA NTRS 2019 · Other
Documentation for Three Wake Vortex Model Data Sets from Simulation of Flight 587 Wake Vortex Encounter Accident Case
This document contains a general description for data sets of a wake vortex system in a turbulent environment. The turbulence and thermal stratification of the environment are representative of the co…
- NASA NTRS 2016 · Conference Paper
An overview of SAE ARP 1587: Aircraft gas turbine engine monitoring system guide
A systematic approach to developing an engine monitoring system (EMS) is outlined. An extensive shopping list of EMS capabilities and benefits are included.
- arXiv 2025 · arXiv preprint
Numerical Investigation of Discontinuous Ice Effects on Swept Wings
This study investigates the aerodynamic performance and flow structures of infinite swept wings with artificially simulated discontinuous ice using an enhanced delayed detached-eddy simulation.
Browse the full corpus — academia portal ↗