N81052 is a 1982 Piper PA-32-301. It is a fixed-wing single-engine aircraft with 7 seats, powered by a Lycoming IO-540 SER rated at 300 horsepower. The registration is active, with the registrant based in Anchorage, AK. Its standard airworthiness certificate was issued in Feb 1982. It has been registered to its current owner since Jun 2018. This page also carries 1 NTSB event.
- 44 years old
- 1 of 176 Piper PA-32-301
2018
1982
That's everything on file so far — TailWiki checks the FAA registry daily and adds new entries as N81052's record changes.
On April 14, 2011, about 1755 Alaska daylight time, a Piper PA-32 airplane, N81052, sustained substantial damage during an encounter with turbulence in cruise flight, about 13 miles west of Cold Bay, Alaska. The airplane was operated by Peninsula Airways, Inc., Anchorage Alaska, as a visual flight rules (VFR) cargo flight under 14 Code of Federal Regulations, Part 135. The solo airline transport pilot was not injured. Visual meteorological conditions prevailed, and company flight following procedures were in effect. The flight departed False Pass, Alaska, about 1745.
In a written statement to the National Transportation Safety Board (NTSB) dated April 29, the pilot wrote that while descending toward his destination, the airplane encountered severe up and down drafts. During the encounter, the pilot hit his head on the sun visor, even though his seatbelt and shoulder harness were snug and secure. Afterward, he continued to his destination, and landed without incident.
The wind at the destination airport at the time of the accident was reported as 300 degrees at 9 knots, the area forecast valid for the time of the accident, forecast no significant turbulence during the reporting period, and there were no pilot reports of turbulence in the area.
The pilot said there were no preaccident mechanical problems with the airplane. A postaccident examination discovered substantial damage to the stabilator.
An examination of the stabilator by the NTSB investigator-in-charge showed that the right half of the stabilator was bent downward 5-10 degrees outboard of the fuselage attachments. The bottom skins adjacent to the bend were wrinkled. The skins were removed, and revealed downward bending of the stabilator main spar. No signs of fatigue or corrosion were found.
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