N8762T

Substantial
None

Cessna 182CS/N: 52662

Accident Details

Date
Sunday, June 22, 2003
NTSB Number
SEA03LA115
Location
Bandon, OR
Event ID
20030701X00980
Coordinates
43.071666, -124.410003
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

Loss of engine power during descent for undetermined reasons.

Aircraft Information

Registration
Make
CESSNA
Serial Number
52662
Engine Type
Reciprocating
Year Built
1960
Model / ICAO
182CC182
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
182C

Registered Owner (Current)

Name
CROOK BRADY G
Address
240 CHICAGO ST
City
BANDON
State / Zip Code
OR 97411
Country
United States

Analysis

On June 22, 2003, about 1330 Pacific daylight time, a Cessna 182C, N8762T, sustained substantial damage during an off airport forced landing, subsequent to a loss of power, approximately one mile south of the Bandon State Airport (S05), Bandon, Oregon. The airplane is owned by the pilot, and was being operated as a visual flight rules (VFR) personal/pleasure flight under Title 14, CFR Part 91, when the accident occurred. The commercial pilot, the sole occupant of the airplane, was not injured. Visual meteorological conditions prevailed and no flight plan was filed for the local flight. The flight originated from Bandon approximately 30 minutes prior to the accident.

During a telephone interview with the National Transportation Safety Board IIC on June 25, the pilot reported that he was descending to the airport, at a reduced power setting, from an altitude of approximately 5,500 feet MSL. He stated that as the airplane reached a two-mile final, for runway 34, the engine began to lose power and would not respond to throttle inputs. The pilot reported that he was unable to land at his intended destination and elected to land in a cranberry bog approximately one mile south of the airport.

During the landing rollout, the airplane sustained substantial damage to the right wing spar and fuselage.

An FAA airworthiness inspector from the Portland, Oregon, Flight Standards District Office examined the aircraft following the accident and reported that there was no evidence found to indicate a mechanical failure or malfunction.

The operator reported that following the accident; the airplanes engine was successfully started and run at multiple power settings. No operating malfunctions or anomalies were noted during the test run.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA03LA115