NTSB CAROL · Event
Event SEA95LA050
Registry · N8828M
FAA Aircraft Registry record.
Make / Model
PIPER PA-46-600TP
Year of manufacture
2019
Engine
P&W CANADA PT6A-42 (850 hp)
Seats / Engines
6 seats · 1 engine
Last airworthiness date
20191213
ADS-B equipped
Yes — Mode-S AC28BF
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
THE LOSS OF POWER DUE TO LOST OIL PRESSURE AND A FAILED CONNECTING ROD. FACTORS INCLUDE FENCE POSTS AND DUSK LIGHTING CONDITIONS WHICH LIMITED VISIBILITY.
Factual narrative
On February 10, 1995, approximately 1753 mountain standard time, a Beech S-35, N8828M, sustained substantial damage during a forced landing after a loss of engine power while en route to Wolf Point, Montana. The commercial pilot, who was the sole occupant of the aircraft, was uninjured. The flight, which was a non-scheduled cargo flight operated under 14CFR135, had departed Glasgow, Montana about ten minutes earlier. There was no fire and no report of an ELT actuating. Visual meteorological conditions prevailed at the time of the flight. The pilot noted a loss of oil pressure, but the engine continued to run smoothly. About one to three minutes after the loss of oil pressure, the engine started knocking and the pilot shut it down. An inspection by FAA inspectors noted that the number six connecting rod had failed. The engine had five hours since major overhaul. THE PILOT NOTED A LOSS OF OIL PRESSURE, WHICH HE MONITORED. THE ENGINE BEGAN RUNNING ROUGHLY AFTER ONE TO THREE MINUTES, AND HE ELECTED TO MAKE A FORCED LANDING. THE PILOT STATED THAT HE CHOSE A LEVEL SPOT FOR THE FORCED LANDING, BUT IT WAS GETTING DARK AND HE DIDN'T SEE A BARBED WIRE FENCE ACROSS THE LANDING SITE. HE DID NOT SEE THE FENCE POSTS UNTIL FLARING FOR A LANDING. THE RIGHT WING STRUCK TWO FENCE POSTS, CAUSING SUBSTANTIAL DAMAGE. ENGINE TEARDOWN REVEALED THAT A CONNECTING ROD FAILED. THE ENGINE HAD FIVE HOURS SINCE MAJOR OVERHAUL. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_SEA95LA050.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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