N4886U

Substantial
Minor

CESSNA 206S/N: U20606144

Accident Details

Date
Sunday, August 31, 2008
NTSB Number
ANC08LA113
Location
Galena, AK
Event ID
20081003X62312
Coordinates
64.738052, -158.940002
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The en route loss of engine power due to a mechanic's failure to tighten a fuel line fitting, which became disconnected in flight.

Aircraft Information

Registration
Make
CESSNA
Serial Number
U20606144
Engine Type
Turbo-shaft
Year Built
1979
Model / ICAO
206C206
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
6
FAA Model
U206G

Registered Owner (Current)

Name
WILLIAMS CASEY D
Address
PO BOX 870275
City
WASILLA
State / Zip Code
AK 99687-0275
Country
United States

Analysis

On August 30, 2008, about 1600 Alaska daylight time, a float-equipped Cessna 206 airplane, N4886U, sustained substantial damage during a forced landing, about 62 miles southeast of Galena, Alaska. The airplane was operated as a personal flight under the provisions of 14 Code of Federal Regulations (CFR) Part 91 when the accident occurred. The solo private pilot received minor injuries. Visual meteorological conditions prevailed, and no flight plan was filed. The flight originated at the Wasilla Lake Sea Plane Base, Wasilla, Alaska, about 1300, and was en route to Kiana, Alaska.

During a telephone conversation with the National Transportation Safety Board (NTSB) investigator-in-charge on August 31, the pilot reported that while in level cruise flight the engine began to run rough and lose power. He said that he saw the engine fuel pressure fluctuating, so he elected to switch fuel tanks in an effort to restore engine power. He noted that the roughness improved momentarily, followed by a strong smell of fuel in the cockpit area, which was followed by a complete loss of engine power. He said that he was unable to restart the engine, and selected a marshy tree-covered site as a forced landing area. During the forced landing, the airplane collided with trees, and sustained substantial damage to the fuselage and wings.

On September 2, a Federal Aviation Administration (FAA) airworthiness inspector from the Anchorage Flight Standards District Office traveled to the Big Lake Airport, Big Lake, Alaska, and examined the airplane after it was recovered. The inspector reported he discovered that the main fuel line between the engine driven fuel pump and the main fuel servo assembly was disconnected, with no apparent impact damage to either the line or its connector.

The FAA inspector said that during his postaccident review of the airplane's maintenance records, he discovered that a maintenance technician had removed the fuel line about 1.9 hours before the accident. During a follow-up interview with the FAA inspector, the maintenance technician that removed and reinstalled the fuel line stated that he could not specifically recall if he had tightened the fuel line fitting after the initial installation, and presumed he had not.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC08LA113