No fatalities

15 Apr 2011: PIPER PA-32-301 (N81052) — PenAir — Cold Bay, AK

Cold Bay, AK, United States

On 15 Apr 2011, a PIPER PA-32-301 (registration N81052) operated by PenAir was involved in an aviation accident near Cold Bay, AK. No fatalities were reported. Investigators recorded the probable cause as: An in-flight encounter with unforecast turbulence, which resulted in structural damage to the stabilator. This summary draws on records from NTSB; 15 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

A Peninsula Airways Piper PA-32 cargo flight sustained substantial stabilator damage after encountering severe up and down drafts west of Cold Bay, Alaska. The pilot was not injured.

Incident Overview

On April 14, 2011, at approximately 1755 Alaska daylight time, a Piper PA-32 airplane, registration N81052, was substantially damaged during an encounter with turbulence while in cruise flight. The incident occurred about 13 miles west of Cold Bay, Alaska. The aircraft was operated by Peninsula Airways, Inc., of Anchorage, Alaska, as a visual flight rules (VFR) cargo flight under 14 Code of Federal Regulations Part 135. The solo airline transport pilot was uninjured. Visual meteorological conditions prevailed, and company flight following procedures were in effect. The flight had departed False Pass, Alaska, around 1745.

Pilot Account

In a written statement to the National Transportation Safety Board (NTSB) dated April 29, the pilot reported that while descending toward his destination, the airplane encountered severe up and down drafts. During this encounter, the pilot struck his head on the sun visor, despite his seatbelt and shoulder harness being snug and secure. After the turbulence, he continued to his destination and landed without further incident.

Weather and Mechanical Condition

The wind at the destination airport at the time of the incident was reported as 300 degrees at 9 knots. The area forecast valid for the time of the incident forecast no significant turbulence during the reporting period, and no pilot reports of turbulence in the area were received. The pilot stated that there were no preaccident mechanical problems with the airplane.

Damage Examination

A postaccident examination revealed substantial damage to the stabilator. Inspection by the NTSB investigator-in-charge showed that the right half of the stabilator was bent downward 5 to 10 degrees outboard of the fuselage attachments. The bottom skins adjacent to the bend were wrinkled. Removal of the skins revealed downward bending of the stabilator main spar. No signs of fatigue or corrosion were found.

Contributing factors

Causes

Effect on equipment

Other contributing factors

Damaged/degraded