NTSB CAROL · Event
Event MIA99LA106
Registry · N6CH
FAA Aircraft Registry record.
Make / Model
BEECH 58
Year of manufacture
1971 · 28 years old at event
Engine
CONT MOTOR IO 520 SERIES (285 hp)
Seats / Engines
6 seats · 2 engines
Last airworthiness date
19710518
ADS-B equipped
Yes — Mode-S A7C2C7
Registrant of record
HODGE CLEOPHAS U
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to extend the landing gear.
Factual narrative
On March 16, 1999, about 0300 eastern standard time, a Beech 58, N6CH, operated by a private individual, landed short of runway 09 at Henry E. Rohlsen Airport, St. Croix, Virgin Islands. Visual meteorological conditions prevailed at the time, and no flight plan was filed for the 14 CFR Part 91 personal flight. The airplane was substantially damaged. The airline transport-rated pilot reported no injuries. The flight originated from St. Thomas, at 0240. The flight landed short of runway 09 in a flat attitude, and the airplane continued in an easterly direction, striking the lights at the arrival end of the runway before coming to rest. There was no radio communications from the airplane before the accident that indicated the pilot was experiencing any problems with the airplane. The pilot said, "...after turning final approach...I completed the before landing check and selected gear down position with a green light. Over the runway, I closed the throttles for touchdown when there was a thump and the aircraft dipped to the left, then skidded on it's belly to a stop on the left side off the runway in grass." The airplane was placed on jacks, and an examination of the landing gear was conducted under the supervision of the FAA. No discrepancies were found during the examination of the landing gear. The FAA inspector wrote in his memorandum to the NTSB, "...it is my firm belief that the pilot did not lower the landing gear at the time of the landing. There was no damage to the main landing gear doors or scratch marks at the doors which indicated the pilot never did lower the gear. All damage was in the structure (airframe)...." The flight landed short of runway 09 in a flat attitude, and the airplane continued in an easterly direction, striking the lights at the arrival end of the runway before coming to rest. There was no radio communications from the airplane before the accident that indicated the pilot was experiencing any problems with the airplane. The pilot said, '...after turning final approach...I completed the before landing check and selected gear down position with a green light. Over the runway, I closed the throttles for touchdown when there was a thump and the aircraft dipped to the left, then skidded on it's belly to a stop on the left side off the runway in grass.' Examination of the landing gear revealed no discrepancies. The FAA inspector wrote in his memorandum to the NTSB, '...it is my firm belief that the pilot did not lower the landing gear at the time of the landing. There was no damage to the main landing gear doors or scratch marks at the doors which indicated the pilot never did lower the gear. All damage was in the structure (airframe)....' Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1999_MIA99LA106.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 ↗