N8665Z

Substantial
None

CESSNA P206CS/N: P206-0465

Accident Details

Date
Saturday, October 17, 2009
NTSB Number
ANC10LA005
Location
Palmer, AK
Event ID
20091021X43946
Coordinates
61.592777, -149.242218
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The pilot's decision to land on a short gravel runway, and his failure to initiate a go-around, which resulted in an overrun and on-ground collision with a fence.

Aircraft Information

Registration
N8665Z
Make
CESSNA
Serial Number
P206-0465
Engine Type
Reciprocating
Year Built
1968
Model / ICAO
P206CC206
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
WALLING SUSETTE
Address
1700 BRINK DR
Status
Deregistered
City
ANCH
State / Zip Code
AK 99504
Country
United States

Analysis

On October 17, 2009, about 1330 Alaska daylight time, a Cessna P206C airplane, N8665Z, sustained substantial damage when it collided with a fence and terrain while landing at a private airstrip, about 5 miles west of Palmer, Alaska. The airplane was being operated by the pilot as a visual flight rules (VFR) personal local flight under Title 14, CFR Part 91, when the accident occurred. The solo commercial pilot was not injured. Visual meteorological conditions prevailed, and no flight plan was filed. The flight originated at the Fairview East Airstrip, Palmer, about 1315.

During a telephone conversation with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC) on October 22, the pilot said he overran the end of the runway during landing, and collided with a fence and a ditch. He said the nose landing gear broke off, and the propeller struck the ground. The pilot reported that there were no mechanical problems with the airplane prior to the accident. He indicated there was damage to the nose landing gear and propeller.

During an examination of the airplane by the NTSB IIC on October 21, besides the nose gear and propeller damage, structural damage was discovered on the fuselage, aft of the baggage compartment. The certificated aviation mechanic who helped recover the airplane the day of the accident, said the airstrip was about 1,300 feet long, and the airplane touched down about 400 feet down the runway. He said the fuselage damage was due to a steel fencepost that penetrated the fuselage when the airplane collided with the airport's chain link perimeter fence.

In a written statement to the NTSB, the pilot wrote that he should not have landed at that airstrip.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC10LA005