N81052

Substantial
None

PIPER PA-32-301S/N: 32-8206023

Accident Details

Date
Friday, April 15, 2011
NTSB Number
ANC11LA027
Location
Cold Bay, AK
Event ID
20110421X15324
Coordinates
55.733333, -162.983337
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

An in-flight encounter with unforecast turbulence, which resulted in structural damage to the stabilator.

Aircraft Information

Registration
Make
PIPER
Serial Number
32-8206023
Engine Type
Reciprocating
Year Built
1982
Model / ICAO
PA-32-301PA32
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
7
FAA Model
PA-32-301

Registered Owner (Current)

Name
TRUE NORTH AIR LLC
Address
7440 BAILEY DR
City
ANCHORAGE
State / Zip Code
AK 99502-1915
Country
United States

Analysis

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.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC11LA027