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Atlas / NTSB / SEA02LA167

NTSB CAROL · Event

Event SEA02LA167

2002-08-28 Big Creek, Idaho, United States Airport · U60 None 1 aircraft Status: Completed

Registry · N5781F

FAA Aircraft Registry record.

Make / Model

PIPER PA-28-140

Year of manufacture

1968 · 34 years old at event

Engine

LYCOMING 0-320 SERIES (180 hp)

Seats / Engines

4 seats · 1 engine

Last airworthiness date

19681021

ADS-B equipped

Yes — Mode-S A76EA2

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's failure to maintain directional control during the aborted takeoff. Factors include high density altitude, variable winds, and a ditch near the point where the aircraft departed the side of the runway.

Factual narrative

On August 28, 2002, approximately 1650 mountain daylight time, a Piper PA-28-140, N5781F, impacted the terrain during an aborted takeoff from Big Creek Airport, Big Creek Lodge, Idaho. The private pilot and his passenger were not injured, but the aircraft, which is owned and operated by the pilot, sustained substantial damage. The 14 CFR Part 91 personal pleasure flight, which was departing for McCall, Idaho, was being operated in visual meteorological conditions. No flight plan had been filed. According to the pilot, during the takeoff roll, just as the main gear were lifting off, the aircraft seemed to lose lift and "dropped" back onto the runway surface. At that point, the pilot looked at the windsock at the far end of the runway and determined that it was indicating a tailwind. He therefore made the decision to abort, but as he tried to bring the aircraft to a stop, he was unable to maintain directional control and the aircraft departed the left side of the runway. After departing the runway, the aircraft's nose gear and right main gear entered a nearby drainage ditch, thus allowing the right wing to impact the terrain and sustain substantial damage. Based on the ambient conditions of 70 degrees Fahrenheit and an altimeter setting of 30.20 inches of mercury, it was determined that the density altitude at the time of the attempted takeoff was approximately 7,550 feet. According to the pilot, the engine seemed to be producing "peak power," and there were no indications that there had been any problem with the engine or the aircraft's systems. During a high density altitude takeoff, just as the aircraft's main gear were lifting off the runway, the aircraft dropped firmly back onto the runway surface. At that point, the pilot looked at the windsock at the far end of the runway and saw that it indicated a tailwind. He therefore elected to abort the takeoff, but failed to maintain adequate directional control of the aircraft during its deceleration. The aircraft therefore departed the left side of the runway, whereupon the nose gear and right main gear entered a nearby drainage ditch, which allowed the right wing to impact the terrain and sustain substantial damage. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_2002_SEA02LA167.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.