NTSB CAROL · Event
Event ERA10CA191
Registry · N858PR
FAA Aircraft Registry record.
Make / Model
BEECH 58
Year of manufacture
1981 · 29 years old at event
Engine
CONT MOTOR IO 520 SERIES (285 hp)
Seats / Engines
6 seats · 2 engines
Last airworthiness date
19810109
ADS-B equipped
Yes — Mode-S ABC665
Registrant of record
MELBOURNE AIR PARTNERS LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's improper flare while landing, resulting in a bounced landing.
Factual narrative
The pilot stated he was conducting an instrument flight rules flight from Melbourne, Florida to Naples, Florida. Upon arrival at Naples, the pilot was cleared for a very-high frequency omnidirectional radio range approach to runway 5. The pilot encountered visual conditions at 400 feet. He flared the airplane high and fast and the airplane touched down hard on the runway and bounced. The airplane touched backed down on the runway and began to porpoise. The nose wheel sheared off and the airplane continued down the runway and came to a complete stop. Both wings were wrinkled to their wing root and the cabin area was buckled. The pilot stated there was nothing mechanically wrong with the airplane. He simply rounded out too high, and made a hard landing, resulting in the nose landing gear shearing off the airplane. Upon arrival at his destination after an instrument-flight-rules flight, the pilot was cleared for a very-high frequency omnidirectional radio range approach to runway 5. The pilot encountered visual conditions at 400 feet. He flared the airplane high and fast and the airplane touched down hard on the runway and bounced. The airplane touched back down on the runway and began to porpoise. The nosewheel then sheared off and the airplane continued down the runway until it came to a complete stop. Both wings were wrinkled to their wing root and the cabin area was buckled. The pilot stated that there was nothing mechanically wrong with the airplane and that he simply "rounded out" too high and made a hard landing, resulting in the nose landing gear shearing off the airplane. 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 Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Landing flare-Incorrect use/operation - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
Verbatim from NTSB's published report. Source file
NTSB_2010_ERA10CA191.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
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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…
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- NASA NTRS 2024 · Presentation
American Airlines Flight 587 Crash Investigation: NASA Langley Research Center Participation and Perspective
- NASA NTRS 2019 · Other
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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 ↗