NTSB CAROL · Event
Event ERA12CA424
Registry · N827EB
FAA Aircraft Registry record.
Make / Model
BEECH 58
Year of manufacture
1970 · 42 years old at event
Engine
CONT MOTOR IO 520 SERIES (285 hp)
Seats / Engines
6 seats · 2 engines
Last airworthiness date
19730829
ADS-B equipped
Yes — Mode-S AB4B42
Registrant of record
EBOR MANAGEMENT INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's inadvertent retraction of the landing gear during the landing.
Factual narrative
The pilot stated that he was performing a "touch and go" landing. After touchdown, the pilot intended to retract the flaps, but inadvertently selected the landing gear control lever. The landing gear partially retracted, and the airplane settled onto the runway, resulting in substantial damage to a nose section bulkhead. A Federal Aviation Administration inspector, who examined the airplane after the accident, observed no evidence of any pre-existing mechanical malfunctions or anomalies that would have precluded normal operation. The pilot stated that he was performing a touch-and-go landing. After touchdown, the pilot intended to retract the flaps, but inadvertently selected the landing gear control lever. The landing gear partially retracted, and the airplane settled onto the runway, resulting in substantial damage to a nose section bulkhead. A postaccident examination of the airplane revealed no evidence of any preexisting mechanical malfunctions or anomalies that would have precluded normal operation. 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 systems-Landing gear system-Gear extension and retract sys-Unintentional use/operation - C
- C Personnel issues-Action/decision-Info processing/decision-Identification/recognition-Pilot - C
Verbatim from NTSB's published report. Source file
NTSB_2012_ERA12CA424.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
In-Flight Separation of Vertical Stabilizer — American Airlines Flight 587
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 ↗