NTSB CAROL · Event
Event ERA25LA094
Registry · N458K
FAA Aircraft Registry record.
Make / Model
BEECH 58
Year of manufacture
1974 · 50 years old at event
Engine
CONT MOTOR IO 520 SERIES (285 hp)
Seats / Engines
6 seats · 2 engines
Last airworthiness date
19740312
ADS-B equipped
Yes — Mode-S A590B5
Registrant of record
AUGUST AERO LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot’s failure to follow the emergency procedures and extend the landing gear manually after the landing gear did not initially extend normally.
Factual narrative
The pilot was on a return, cross country flight to his home airport in instrument meteorological conditions. The pilot reported that he first performed a non-precision approach into the airport, where he reported that the landing gear extended normally. After performing a missed approach, the pilot retracted the landing gear and he then performed a precision approach in the opposite direction. The pilot reported that he put the landing gear switch in the down position, but that the landing gear did not extend. The pilot elected to continue the approach without troubleshooting, extending the gear manually, or referring to the emergency checklist. The pilot subsequently landed the airplane on the runway with the landing gear retracted, which resulted in substantial damage to the fuselage. After the accident, the pilot performed an operational check and troubleshooting of the landing gear without authorization. The pilot reported that the landing gear again failed to extend, but would retract during his testing. The pilot also reported that the manual landing gear extension system operated normally. During the testing, the pilot said he found an “open circuit of the gear relay due to moisture or foreign debris.” After troubleshooting, the pilot reported that the landing gear started to operate normally. After the pilot had performed the unauthorized troubleshooting, a Federal Aviation Administration inspector examined the landing gear system, and performed a functional test, during which he found that it operated normally. 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).
- — Personnel issues-Task performance-Use of equip/info-Use of equip/system-Pilot
- — Aircraft-Aircraft systems-Landing gear system-Gear extension and retract sys-Not used/operated
- — Personnel issues-Task performance-Use of equip/info-Use of checklist-Pilot
Verbatim from NTSB's published report. Source file
NTSB_2024_ERA25LA094.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 ↗