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Atlas / NTSB / FTW98LA148

NTSB CAROL · Event

Event FTW98LA148

1998-03-12 TAOS, New Mexico, United States Airport · SKX None 1 aircraft Status: Completed

Registry · N9239Q

FAA Aircraft Registry record.

Make / Model

BEECH 58

Year of manufacture

1971 · 27 years old at event

Engine

CONT MOTOR IO 520 SERIES (285 hp)

Seats / Engines

6 seats · 2 engines

Last airworthiness date

19710926

ADS-B equipped

Yes — Mode-S ACCCF1

Registrant of record

RETTIG & ASSOCIATES LLC

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The total failure of the landing gear retraction/extension assembly for reasons undetermined.

Factual narrative

On March 12, 1998, at 1940 mountain standard time, a Beech 58, N9239Q, sustained substantial damage during a gear up landing at Taos Municipal Airport, Taos, New Mexico. The private pilot and his three passengers were not injured, and there was no damage to other property. The flight was operating under Title 14 CFR Part 91, and an IFR flight plan had been filed. The flight originated at Austin, Texas, at 1540 central standard time. According to the pilot's accident report, he attempted to lower the landing gear in preparation for a normal landing on runway 22. When he lowered the landing gear switch, the "gear lock indicators failed to indicate that the landing gear had been moved to the down-and-locked position. The switch was raised and lowered again but failed to lower the landing gear." He also attempted to lower the landing gear by manual extension, but was unsuccessful. After circling the airport for approximately 20-30 minutes, the pilot notified ground personnel of the situation and executed an emergency gear-up landing. Postaccident examination of the aircraft revealed that the landing gear box had failed, causing the flaps attachment tracks to separate from the spar webbing, and the belly formers to be damaged. The pilot attempted to lower the landing gear in preparation for a normal landing. When he lowered the landing gear switch, the gear lock indicators failed to indicate the landing gear in the down-and-locked position. Manual extension of the landing gear was also unsuccessful. After circling the airport for approximately 20-30 minutes, he executed an emergency gear-up landing. Postaccident examination of the aircraft revealed that the landing gear box had failed, causing the flaps attachment tracks to separate from the spar webbing, and the belly formers to be damaged. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1998_FTW98LA148.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

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.

Browse the full corpus — academia portal ↗