NTSB CAROL · Event
Event ERA24LA376
Registry · N6037M
FAA Aircraft Registry record.
Make / Model
BEECH 58
Year of manufacture
1979 · 45 years old at event
Engine
CONT MOTOR IO 520 SERIES (285 hp)
Seats / Engines
6 seats · 2 engines
Last airworthiness date
19790316
ADS-B equipped
Yes — Mode-S A7D5BD
Registrant of record
RALEIGH FLYING CLUB LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
Damage to the landing gear selector switch wire bundle which resulted in an inadvertent retraction of the landing gear during the takeoff roll.
Factual narrative
During the takeoff roll, the pilot accelerated the airplane to rotation speed. Upon starting to rotate the airplane, the nose landing gear began a retraction sequence, collapsing under the airplane, and the pilot reduced the throttles to idle and applied the brakes. The main landing gear also retracted, and the airplane slid to a stop on the runway, resulting in substantial damage to the lower fuselage. Both the pilot and the pilot rated passenger verified that the landing gear handle was in the down position prior to and after the accident sequence. Postaccident examination of the aircraft revealed damage to several wires leading to the landing gear selector switch on the instrument panel. The wires were found to be actively arcing when moved or touched. 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).
- — Aircraft-Aircraft systems-Landing gear system-Land gear sys wiring-Damaged/degraded
- — Aircraft-Aircraft systems-Landing gear system-Gear extension and retract sys-Malfunction
Verbatim from NTSB's published report. Source file
NTSB_2024_ERA24LA376.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 ↗