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FTW98LA148

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

Airport SKX

Current FAA registration · N9239Q

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

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 ↗.

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