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Atlas / NTSB / SEA98LA067

NTSB CAROL · Event

Event SEA98LA067

1998-04-26 ARLINGTON, Washington, United States Airport · AWO None 1 aircraft Status: Completed

Registry · N7458K

FAA Aircraft Registry record.

Make / Model

PIPER PA-20

Year of manufacture

1950 · 48 years old at event

Engine

LYCOMING 0-290 SERIES (140 hp)

Seats / Engines

4 seats · 1 engine

Last airworthiness date

19550811

ADS-B equipped

Yes — Mode-S AA0897

Registrant of record

MY PIPER PACER LLC

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's failure to maintain directional control during the landing roll, and his delayed remedial action when the aircraft started to drift off the side of the runway.

Factual narrative

On April 26, 1998, approximately 1610 Pacific daylight time, a Piper PA-20 tail wheel aircraft, N7458K, experienced a collapse of one main landing gear leg during the landing roll at Arlington Municipal Airport, Arlington, Washington. The private pilot and his three passengers were not injured, but the aircraft, which was owned and operated by the pilot, sustained substantial damage. The 14 CFR Part 91 flight, which departed Jefferson County Airport, Port Townsend, Washington, about 30 minutes earlier, was being operated in visual meteorological conditions. No flight plan had been filed, and there was no report of an ELT activation. According to the pilot, he had touched down on both main gear and was beginning the rollout when the left wing picked up and the aircraft began rolling on the right tire only. Soon thereafter, the aircraft started to veer toward the left side of the runway, and the pilot attempted remedial action by applying rudder opposite to the direction the aircraft was drifting. But, by the time of the rudder application, the aircraft had drifted to far from the center of the runway to keep it from departing the runway edge. After the aircraft left the runway, the right main gear dug into the soft terrain, whereupon the gear leg tore away from the fuselage. After touching down on both main landing gear, the left main gear of the tailwheel aircraft lifted off the runway. As the aircraft rolled forward with only the right main gear touching the surface, the aircraft began to veer toward the left edge of the runway. As the aircraft continued toward the edge of the runway, the pilot applied remedial rudder inputs, but the remedial action was not taken in time to keep the aircraft from exiting the side of the runway. As the aircraft exited the runway, the right main gear dug into the soft terrain and was torn from the fuselage. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1998_SEA98LA067.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.